STANDARD
DNVGL-ST-F101
Edition October 2017
Amended December 2017
Submarine pipeline systems
The electronic pdf version of this document, available free of charge
from http://www.dnvgl.com, is the officially binding version.
DNV GL AS
FOREWORD
DNV GL standards contain requirements, principles and acceptance criteria for objects, personnel,
organisations and/or operations.
©
DNV GL AS October 2017
Any comments may be sent by e-mail to
[email protected]
This service document has been prepared based on available knowledge, technology and/or information at the time of issuance of this
document. The use of this document by others than DNV GL is at the user's sole risk. DNV GL does not accept any liability or responsibility
for loss or damages resulting from any use of this document.
Changes - current
CHANGES – CURRENT
This document supersedes the October 2017 edition of DNVGL-ST-F101.
Changes in this document are highlighted in red colour. However, if the changes involve a whole chapter,
section or sub-section, normally only the title will be in red colour.
Amendments December 2017
• Sec.6 Design - materials engineering
— [6.3.3.2] Reference for gauging requirements has been amended.
Changes October 2017
• Sec.1 Introduction
— Rigid risers have been excluded and will be covered in the next revision of DNVGL-ST-F201. This affects
several places.
— Requirements to technology qualification of new technologies.
— Defect has been defined
• Sec.4 Design – loads
— Minor editorial changes and updates
— Previous section 4G400 and 5C500 have been merged into [4.7.4] and updated.
• Sec.5 Design – limit state criteria
— Minor editorial changes and updates
— [5.2.1] has been re-organised except for mitre bend angle that has been reduced from three to two
degrees.
— [5.2.2] has been modified. More guidance is given in general (see also Table 8-1 and [8.7.1]). Some
specific requirements for replacing the system pressure test (old table 5-1) has been removed.
— [5.3.2] The format has been modified slightly. The resistance safety factor, γsc, has now got an additional
—
—
—
—
—
—
index for the relevant limit state. The reason is that the number of γsc’s are increasing. This also implies
that γε has become γsc,dc.
[5.4] Name of some limit states and headings have been modified to make it consistent with Table 5-7.
[5.4.6.8] The criterion has been re-formulated (but is identical) except for the pressure term modified in
line with Safebuck JIP.
[5.4.8] Requirements to fracture and fatigue have been updated and are stated in [5.4.8]. For
recommended practice on how to perform this, new revision of DNV GL-RP-F108 is pointed to. Appendix A
is removed.
[5.4.8] The term sensitive welds has been introduced.
[5.6.1] References to other standards have been updated.
[5.8.2] New. From installation JIP.
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— Changes and modifications to the following:
— Steel making and plate rolling essential variables [7.1.8]
— Hydrogen content [7.2.3.3]
— Hydrostatic testing [7.5.1]
— Subsection [7.1], [7.2], [7.5], [7.6]. Added clarifications and more requirements to coiled line pipe
— [7.4] Requirements to explosion welded clad plates added
— [7.7] Requirements to dimensions and geometrical measurements have been updated based on a specific
workshop with the industry. Further, a minimum diameter of 60 mm has been specified. Dimensional
requirements to smaller pipes have been modified and harmonized with common coil tubing pipes
— [7.9.2] Supp. F; Guidance note to DWTT added, acknowledging challenges with inverse fracture for high
toughness materials and supporting a similar statement in API RP 5L3.
— [7.9.3] Supp. P; Has been modified.
— [7.9.5] Supp. U; Modified to include both approaches to achieve Suffix U; retrospective documentation
and as part of production testing. Restructuring of content to better clarify requirements.
• Sec.8 Construction - components and pipeline assemblies
— Restructuring of content to better clarify requirements.
— Table 8-1 has been modified.
— DNVGL-RP-0034 is acknowledged as an alternative material specification for forged CMn steel.
• Sec.12 Documentation
— Some requirements to documentation in other sections have been moved to this section. A reference to
DNVGL-RP-O101 is also included.
• Sec. 13 Commentary (informative)
— [13.6] Roadmap for use of this standard with pipe-in-pipe systems based on workshop series JIP-
• App.A Fracture limit state of girth welds
— Empty - moved to new revision of DNVGL-RP-F108.
• App.B Mechanical testing and corrosion testing
Minor changes and modifications, e.g. to the following:
— References to DNVGL-RP-F108 added
— Reference to BS 8571 for SENT added
— Clarifications to all-weld tensile testing.
• App.C Welding
In general only minor updates on reference standards and some changes to clarify paragraphs.
— [C.3.4.5] Batch testing modified to be sampled in same positions as WPQ
— [C.4.8.7] Maximum heat input variation for multiple pieces more clarified
— [D.2.1.5] Added requirement for heat input range to be stated on WPS
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Changes - current
• Sec.7 Construction – linepipe
• App.D Non-destructive testing
— [D.7] Fully revised requirements for pipe body inspection (usually applicable for plate mills for SAWL).
— [D.8.13] Added requirement to use 2 angles in AUT setup for inspection of longitudinal imperfections.
• App.E Automated ultrasonic girth weld testing
—
—
—
—
—
—
—
—
—
[E.2] Added requirement to evaluate impact on sensitivity of long seam weld
[E.2] Added requirement for inspection of CRA welds and materials
[E.2] Added requirement for monitoring wall thickness upon AUT inspection of SMLS pipe girth welds.
[E.2] Accommodate for use of adaptive focal laws
[E.2] Added requirement to include SDH reflector for TOFD in reference block
[E.5] Revised acceptance criteria for porosity, Table E-1
[E.5] Added workmanship acceptance criteria for fatigue sensitive welds
[E.8] Added generalised requirements to number of imperfections within scope of AUT qualification
[E.8] Reduced requirements to CCW scanning of defective welds in AUT qualification, now 1 weld is
required.
— [E.8] Added requirement to demonstrate stability upon repeated inspection in AUT validation.
• App.F Requirements for shore crossing and onshore sections
— Updated on land fall, now referred to as shore crossing based on the Crossway JIP by Atteris
Editorial corrections
In addition to the above stated changes, editorial corrections may have been made.
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Changes - current
— [C.8.1.13] Maximum interpass temperature for welding of solid CRA and in root and hot pass for lined/
clad carbon steel increased to 1500C.
The present revision of DNVGL-ST-F101 is mainly reflecting feed-back from experience by several companies
that are hereby acknowledged. The comments improved the quality and content of this standard significantly
and the effort spent by the commenting companies is impressive and hereby acknowledged.
This revision includes results from the following JIP's sponsored by the listed companies. Their contribution is
hereby acknowledged.
Installation JIP
The following companies, listed in alphabetical order, are acknowledged for their contributions to the JIP
ABB
HHI
NOV
Technip
Allseas
JFE Steel
Petrobras
Tideway Offshore Solutions
Bureau Veritas
KW/Petrofac
Saipem
VBMS
EMAS
McDermott
Statoil
WoodGroup Kenny
Heermea Marine Contractors
Nexans
Subsea7
Woodside
Pipe-in-pipe workshop series JIP
The following companies, listed in alphabetical order, are acknowledged for their contributions to the JIP
Genesis
ITP
Shell
Technip
HMC
Petrobras
Subsea7
Vision oil and gas
Intecsea
Saipem
T.D. Williamson
Wood Group Kenny
Crossway JIP performed by Atteris.
Safebuck JIP peformed by Atkins.
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Changes - current
Acknowledgements
Changes – current.................................................................................................. 3
Acknowledgements................................................................................. 6
Section 1 Introduction.......................................................................................... 12
1.1 General........................................................................................... 12
1.2 Objectives....................................................................................... 12
1.3 Scope.............................................................................................. 12
1.4 Application...................................................................................... 12
1.5 Alternative methods and procedures.............................................. 14
1.6 Structure of standard..................................................................... 14
1.7 References...................................................................................... 16
1.8 Definitions.......................................................................................24
Section 2 Safety philosophy.................................................................................. 45
2.1 General........................................................................................... 45
2.2 Safety philosophy structure............................................................ 45
2.3 Risk basis for design...................................................................... 49
Section 3 Concept and design premise development............................................ 53
3.1 General........................................................................................... 53
3.2 Concept development..................................................................... 54
3.3 Design premise............................................................................... 55
3.4 System design principles................................................................ 60
Section 4 Design - loads....................................................................................... 64
4.1 General........................................................................................... 64
4.2 Functional loads..............................................................................65
4.3 Environmental loads....................................................................... 67
4.4 Construction loads.......................................................................... 73
4.5 Interference loads.......................................................................... 73
4.6 Accidental loads..............................................................................74
4.7 Design load effects......................................................................... 74
Section 5 Design – limit state criteria...................................................................81
5.1 General........................................................................................... 81
5.2 System design requirements.......................................................... 82
5.3 Design format................................................................................. 86
5.4 Limit states..................................................................................... 92
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Contents
CONTENTS
5.6 Pipeline components..................................................................... 116
5.7 Supporting structure.....................................................................123
5.8 Installation and repair.................................................................. 123
Section 6 Design - materials engineering........................................................... 127
6.1 General......................................................................................... 127
6.2 Materials selection for line pipe and pipeline components............ 127
6.3 Materials specification.................................................................. 133
6.4 Corrosion control.......................................................................... 136
Section 7 Construction – linepipe....................................................................... 143
7.1 General......................................................................................... 143
7.2 Carbon Manganese (C-Mn) steel linepipe......................................147
7.3 Corrosion resistant alloy linepipe................................................. 165
7.4 Clad or lined steel linepipe........................................................... 169
7.5 Hydrostatic testing....................................................................... 175
7.6 Non-destructive testing................................................................ 176
7.7 Dimensions, mass and tolerances................................................. 179
7.8 Marking, delivery condition and documentation............................188
7.9 Supplementary requirements........................................................189
Section 8 Construction - components and pipeline assemblies.......................... 199
8.1 General......................................................................................... 199
8.2 Component requirements..............................................................200
8.3 Materials....................................................................................... 211
8.4 Manufacture.................................................................................. 214
8.5 Mechanical and corrosion testing................................................. 217
8.6 Pipeline assemblies.......................................................................220
8.7 Hydrostatic testing....................................................................... 224
8.8 Documentation, records, certification and marking.......................226
Section 9 Construction - corrosion protection and weight coating...................... 228
9.1 General......................................................................................... 228
9.2 External corrosion protective coatings..........................................229
9.3 Concrete weight coating............................................................... 230
9.4 Manufacture of galvanic anodes................................................... 233
9.5 Installation of galvanic anodes..................................................... 233
Section 10 Construction – offshore..................................................................... 235
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Contents
5.5 Special considerations.................................................................. 111
10.2 Pipe assemblies onshore.............................................................236
10.3 Pipeline route, pre-installation survey and preparation.............. 237
10.4 Installation spread......................................................................238
10.5 Welding and non-destructive testing.......................................... 247
10.6 Pipeline installation.................................................................... 248
10.7 As-laid survey............................................................................. 254
10.8 Post-lay intervention (seabed intervention and pipeline
protection).......................................................................................... 255
10.9 Tie-in...........................................................................................257
10.10 Pre-commissioning....................................................................259
10.11 As-built survey..........................................................................263
10.12 Documentation.......................................................................... 264
10.13 Installation manual...................................................................264
Section 11 Operations and abandonment........................................................... 268
11.1 General....................................................................................... 268
11.2 Commissioning............................................................................ 270
11.3 Integrity management system....................................................270
11.4 Integrity management process................................................... 273
11.5 Re-qualification........................................................................... 279
11.6 De-commissioning.......................................................................281
11.7 Abandonment.............................................................................. 282
Section 12 Documentation.................................................................................. 283
12.1 General....................................................................................... 283
12.2 Design......................................................................................... 283
12.3 Construction - manufacturing and fabrication.............................286
12.4 Construction - installation and pre-commissioning..................... 288
12.5 Operation - commissioning......................................................... 288
12.6 Operation.................................................................................... 289
12.7 Abandonment.............................................................................. 290
12.8 DFI-resumé................................................................................. 290
12.9 Filing of documentation.............................................................. 292
Section 13 Commentary (informative)................................................................ 293
13.1 General....................................................................................... 293
13.2 Safety and design philosophy..................................................... 293
13.3 Loads.......................................................................................... 294
13.4 Design criteria............................................................................ 295
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Contents
10.1 General....................................................................................... 235
13.6 Pipe-in-pipe.................................................................................302
13.7 Installation................................................................................. 318
13.8 References.................................................................................. 320
Appendix A Fracture limit state of girth welds....................................................321
Appendix B Mechanical testing and corrosion testing......................................... 322
B.1 General......................................................................................... 322
B.2 Mechanical testing and chemical analysis.....................................322
B.3 Corrosion testing.......................................................................... 333
Appendix C Welding............................................................................................ 343
C.1 General......................................................................................... 343
C.2 Welding equipment, tools and personnel...................................... 344
C.3 Welding consumables................................................................... 346
C.4 Welding procedures...................................................................... 350
C.5 Qualification of welding procedures............................................. 360
C.6 Examination and testing for welding procedure qualification........ 368
C.7 Welding and post weld heath treatment requirements................. 375
C.8 Material and process specific requirements.................................. 382
C.9 Hyperbaric dry welding.................................................................386
Appendix D Non-destructive testing (NDT)......................................................... 392
D.1 General......................................................................................... 392
D.2 Manual non-destructive testing and visual examination of
welds.................................................................................................. 394
D.3 Manual non-destructive testing and visual examination of plate,
pipe and weld overlay........................................................................ 418
D.4 Non-destructive testing and visual examination of forgings......... 423
D.5 Non-destructive testing and visual examination of castings......... 428
D.6 Automated non-destructive testing.............................................. 433
D.7 Non-destructive testing of pipe body of welded pipes.................. 434
D.8 Non-destructive testing of linepipe at pipe mills.......................... 441
Appendix E Automated ultrasonic girth weld testing.......................................... 469
E.1 General......................................................................................... 469
E.2 Basic requirements....................................................................... 469
E.3 Procedure......................................................................................479
E.4 Calibration (sensitivity setting).................................................... 480
E.5 Field inspection.............................................................................483
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Contents
13.5 API material grades....................................................................301
E.7 Evaluation and reporting.............................................................. 489
E.8 Qualification.................................................................................. 491
E.9 Project specific automated ultrasonic testing procedure
validation............................................................................................ 500
E.10 Validity of qualification............................................................... 502
E.11 Determination of wave velocities in pipe steels.......................... 503
Appendix F Requirements for shore crossing and onshore sections.................... 505
F.1 General..........................................................................................505
F.2 Safety philosophy..........................................................................510
F.3 Design premise............................................................................. 513
F.4 Design........................................................................................... 515
F.5 Construction.................................................................................. 517
F.6 Operation...................................................................................... 518
F.7 Documentation.............................................................................. 519
Changes – historic.............................................................................................. 520
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Contents
E.6 Re-examination of welds.............................................................. 489
SECTION 1 INTRODUCTION
1.1 General
This standard gives criteria and recommendations on concept development, design, construction, operation
and abandonment of submarine pipeline systems.
1.2 Objectives
The objectives of this standard are to:
— ensure that the concept development, design, construction, operation and abandonment of pipeline
systems are conducted with due regard to public safety and the protection of the environment
— provide an internationally acceptable standard of safety for submarine pipeline systems by defining
minimum requirements for concept development, design, construction, operation and abandonment
— serve as a technical reference document in contractual matters between purchaser and contractor
— provide requirements for designers, purchaser, and contractors.
1.3 Scope
This standard provides guidance and requirements to concept development, design, construction, operation
and abandonment of pipeline systems.
The standard includes guidance and criteria to:
—
—
—
—
—
—
—
—
—
—
—
design basis (survey, environmental data, soil sampling)
design criteria (layout, LRFD format and functional)
material selection and corrosion control
line pipe
components
coating
offshore construction and pre-commissioning
operation and abandonment
material testing
welding
non-destructive testing (NDT).
The focus is on structural integrity of the pipeline.
1.4 Application
Tha applicability of this standard is given in Table 1-1. The standard shall be applied in its entirety.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Table 1-1 Applicability of standard
General
Application
Pipeline systems in the petroleum and natural gas industries.
For submarine pipeline systems that have extraordinary consequences, the
quantification of consequences by the three safety classes provided in this
1
standard may be insufficient, and higher safety classes may be required.
Phases
Concept development, design, construction, operation and abandonment.
Pipeline types
Single rigid metallic pipeline systems, pipeline bundles of the piggyback type and
2
pipeline bundles within an outer pipe .
Pipe-in-pipe.
Risers and compliant risers are covered by DNVGL-ST-F201Dynamic risers.
Extent/battery limits
Pressure and flow
Pipeline system in such a way that the fluid transportation and pressure in the
3
submarine pipeline system is well defined and controlled .
Concept development, design,
construction, operation and
abandonment
Submarine pipeline system .
4
Geometry and configuration
Dimensions
No limitation except that pipe outside diameters shall be above 60 mm.
(Explicit criteria for local buckling, combined loading are only given for straight
pipes with 15 < D/t2 < 45.)
Configurations
Tee’s, wye’s, PLEM or PLET, spools which are integrated part of the pipeline.
Water depth
No limitation, see [5.1.2.1].
Loads
Pressure
No limitation.
Temperature
No limitation.
Material properties need to be documented for relevant temperatures in line with
[5.3.3].
Global deformations
No limitation.
Line pipe Material
General
See [7.1.2.1].
C-Mn steel line pipe is generally conforming to ISO 3183 Annex J but with
modifications and amendments (245-555). Material grade limited to, including,
X80 (DNVGL 555).
CRA line pipe with specific requirements to 22Cr and 25Cr steel and 13Cr
martensitic steel.
Clad and lined line pipe.
Supplementary requirements for sour service, fracture arrest properties, plastic
deformation, dimensional tolerances and high utilization.
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Components
Bends, fittings, flanges, valves, mechanical connectors, CP insulating joints, anchor
flange, buckle arrestor, pig traps, clamps and couplings.
Design
See [5.6].
Material and manufacture
See Sec.8.
Fluids
Categories
See Table 2-1.
CO2 pipelines are in general covered by this standard in line with ISO 13623. The
following aspects needs special attention for CO2 pipelines:
— material selection
— corrosion and sour service evaluations
— operation.
For these aspects, see DNVGL-RP-F104.
Sour service
Generally conforming to ISO 15156.
Installation
Method
See Sec.10.
S-lay, J-lay, towing and laying methods introducing plastic deformations.
Installation requirements for protective and anchoring structures are also included.
1)
Example of extra ordinary consequences may be pristine environment and exploration in arctic climate.
2)
Umbilicals intended for control of subsea installations are not included in this standard. Individual pipes, within an
umbilical, made of materials applicable to this standard, may be designed according to this standard.
3)
Different parts of the pipeline system may be designed to different standards or recommended practices. It
is important to identify differences between these at an early stage and assess these. Examples of conflicting
requirements are; pressure definitions and system test pressure requirements.
4)
The operator may apply this standard on sub-sets of the limits of this standard. Typical example of excluded items is
smaller diameter piping such as kicker lines and designs these to e.g. ISO 15649.
1.5 Alternative methods and procedures
In case alternative methods and procedures to those specified in this standard are used, it shall be
demonstrated that the obtained safety level is equivalent to the one specified herein, see [2.3.5]. Such
alternative methods shall be formally and rigorously justified and accepted by all relevant contracting parties.
Technologies that are not covered by existing, validated requirements, and where failure poses risk to
life, property or the environment, or presents financial risk, shall be qualified. Recommended practice on
technology qualification are given in DNVGL-RP-A203.
1.6 Structure of standard
This standard is based on limit state design. This implies that the same design criteria apply to both
construction/installation and operation. All structural criteria are therefore given in Sec.5.
The standard is organised as follows:
— This section contains the objectives and scope of the standard. It further introduces essential concepts,
definitions and abbreviations.
— Sec.2 contains the fundamental safety philosophy and design principles. It introduces the safety class
methodology and normal classification of safety classes. It gives overall requirements to systematic
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—
—
—
—
—
—
—
—
—
—
—
review or QRA. How this will affect the different phases is further described in subsections [X.1.3], where
X indicates section, in the different sections.
Sec.3 contains requirements to concept development, establishment of design premises, with system
design principles, pipeline safety and control system, and collection of environmental data.
Sec.4 defines the design loads to be applied in Sec.5. It includes classification of loads into functional
loads (including pressure), environmental loads, interference loads and accidental loads. Finally, it defines
design cases with associated characteristic values and combinations.
Sec.5 contains requirements to pipeline layout, system test and mill test. It contains description of the
design (LRFD) format and characterisation of material strength for straight pipes and supports. Design
criteria for the different limit states for all phases; installation, as-laid, commissioning and operation, are
given.
Sec.6 contains materials engineering and includes material selection, material specification (including
required supplementary requirement to the line pipe specification), welding and corrosion control.
Sec.7 contains requirements to line pipe. The requirements to C-Mn steels are based on ISO 3183. The
section also includes requirements to CRAs and lined/clad pipe.
Sec.8 contains requirements to materials, manufacture and fabrication of components and assemblies.
Structural requirements to these components are given in [5.6].
Sec.9 contains requirements to corrosion protection and weight coating.
Sec.10 contains requirements to offshore construction including installation, pre- and post-intervention
and pre-commissioning.
Sec.11 contains requirements to operation including commissioning, integrity management, repair, requalification, de-commissioning and abandonment of the submarine pipeline system.
Sec.12 contains requirements to documentation for the submarine pipeline system from concept
development to abandonment.
Sec.13 is an informative section which discusses several aspects of the standard.
The appendices are a compulsory part of the standard.
— App.A is empty. The content on ECA from previous revision is now reflected in the updated DNVGL-RPF108.
— App.B details the requirements to materials testing including mechanical and corrosion testing as well as
chemical analysis.
— App.C contains requirements to welding including qualification of welding procedures and construction
welding.
— App.D contains requirements to Non-Destructive Testing (NDT) except Automated Ultrasonic Testing (AUT)
of girth welds.
— App.E contains requirements to AUT of girth welds.
— App.F contains selected requirements to shore crossing and onshore parts of the submarine pipeline
system.
Additional requirements or modified requirements compared to the stated ISO standards are denoted by AR
or MR by the end of the paragraph. This applies to [7.2] and [9.3].
Modified requirements compared to the stated ISO standards are given in this standard by stating the ISO
paragraph number in brackets prior to the modified requirements. This applies to Sec.8.
Guidance notes provide additional information, clarification or examples to the paragraph in order to increase
the understanding of the requirement. Guidance notes do not contain requirements.
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1.7 References
1.7.1 General
The following standards include provisions which, through reference in the text, constitute provisions of this
standard.
References are either defined as normative or informative. Normative references in this document are
indispensable for its application. Informative references provide additional information intended to assist the
understanding or use of the document.
Guidance note:
Normative references are typically referred to as "testing shall be performed in accordance with ISO xxx", while informative
references are typically referred to as "testing may be performed in accordance with ISO xxx or ISO yyyy", or "recommended
practice on xx is given in DNVGL-RP-Fxxx".
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In case of conflict between this standard and referenced DNV GL standards or recommended practices, the
standard or recommended practice with the latest edition date shall prevail.
The latest valid edition of each of the DNV GL reference documents applies.
Guidance note:
Any conflict is intended to be removed in next revision of that document.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
This standard is intended to comply with the ISO standard 13623: Petroleum and natural gas industries Pipeline transportation systems, specifying functional requirements for offshore pipelines and risers.
Guidance note:
The following deviations to ISO 13623 standard are intentional:
—
This standard allows higher utilisation for fluid category A and C pipelines. This standard is in compliance with ISO 16708.
—
For design life less than 33 years, a more severe environmental load is specified in this standard, in agreement with ISO
16708.
—
applying the supplementary requirements U, for increased utilisation, this standard allows 4% higher pressure containment
utilisation than ISO 13623.
—
the equivalent stress criterion in ISO 13623 may, under some conditions allow higher utilisation than this standard.
—
requirements to system pressure test (pressure test) are less stringent.
—
minor differences may appear depending on how the pipeline has been defined in safety classes, ISO 13623 does not use the
concept of safety classes.
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The requirements to C-Mn steel line pipe of this standard are intended to comply with the ISO standard 3183
Annex J limited to, including, X80 (DNVGL 555), but with modifications and amendments.
Guidance note:
The latest revision of the DNV GL publications may be found in the publication list at the DNV GL website www.dnvgl.com.
Amendments and corrections to the DNV GL publications are published on www.dnvgl.com when relevant. These shall be
considered as mandatory part of the above standards and recommended practices.
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1.7.2 DNV GL service specifications
The latest revision of the following documents applies.
Table 1-2 DNV GL service specifications
Document code
Title
DNVGL-SE-0160
Technology qualification management and verification
DNVGL-SE-0475 Sec.1
Certification and verification of pipelines
DNVGL-SE-0476
Offshore riser systems
1.7.3 DNV GL Standards
The following documents contain provisions which, through reference in this text, constitute provisions of this
offshore standard. The latest revision of the following document applies.
Table 1-3 DNV GL standards
Document code
Title
DNVGL-OS-A101
Safety principles and arrangements
DNVGL-OS-C101
Design of offshore steel structures, general - LRFD method
DNVGL-OS-E201
Oil and gas processing systems
DNVGL-OS-E301
Position mooring
DNVGl-ST-C501
Composite components
DNVGL-ST-F201
Dynamic risers
DNVGL-ST-N001
Marine operations and marine warranty
1.7.4 DNV GL recommended practices
The latest revision of the following documents applies.
Table 1-4 DNV GL recommended practices
Document code
Title
DNVGL-RP-A203 Sec.1
Technology qualification
DNVGL-RP-B401
Cathodic protection design
DNVGL-RP-C203
Fatigue design of offshore steel structures
DNVGL-RP-C205
Environmental conditions and environmental loads
DNVGL-RP-C211
Structural reliability analysis
DNVGL-RP-C212
Offshore soil mechanics and geotechnical engineering
DNVGL-RP-F101
Corroded pipelines
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
DNV GL AS
Page 17
Document code
Title
DNVGL-RP-F102
Pipeline field joint coating and field repair of line pipe coating
DNVGL-RP-F103
Cathodic protection of submarine pipelines
DNVGL-RP-F105
Free spanning pipelines
DNVGL-RP-F106
Factory applied pipeline coatings for corrosion control
DNVGL-RP-F107
Risk assessment of pipeline protection
DNVGL-RP-F108
Assessment of flaws in pipeline and riser girth welds
DNVGL-RP-F109
On-bottom stability design of submarine pipelines
DNVGL-RP-F110
Global buckling of submarine pipelines
DNVGL-RP-F111
Interference between trawl gear and pipelines
DNVGL-RP-F112
Design of duplex stainless steel subsea equipment exposed to cathodic protection
DNVGL-RP-F113 Sec.1
Pipeline subsea repair
DNVGL-RP-F114
Pipe-soil interaction for submarine pipelines
DNVGL-RP-F115
Pre-commissioning of pipelines
DNVGL-RP-F116
Integrity management of submarine pipeline systems
DNVGL-RP-F118
Pipe girth weld automated ultrasonic testing system qualification and project specific
procedure validation
DNVGL-RP-F204
Riser fatigue
DNVGL-RP-J202
Design and operation or carbon dioxide pipelines
DNVGL-RP-N101 Sec.1
Risk management in marine and subsea operations
DNVGL-RP-N103
Modelling and analyses of marine operations
DNVGL-RP-O101 Sec.1
Technical documentation for subsea projects
DNVGL-RP-O501
Managing sand production and erosion
DNVGL-RP-0034
Steel forgings for subsea applications
1.7.5 DNV GL other publications
The latest revision of the following documents applies.
Table 1-5 DNV GL other publications
Document code
Title
DNVGL-RU-HSLC
Rules for classification: High speed and light craft
DNVGL-CG-0051
Non-destructive testing
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Page 18
1.7.6 Other references
Table 1-6 Other references
Document code
Title
API RP 5L1
Recommended Practice for Railroad transportation of Line Pipe
API RP 5L2
Recommended Practice for Internal Coating of Line Pipe for Non-corrosive Gas Transmission
Service
API RP 5L3
Recommended Practice for Conducting Drop-Weight Tear Tests on Line Pipe
API RP 5LW
Recommended Practice for Transportation of Line Pipe on Barges and Marine Vessels
API RP 17N
Subsea Production System Reliability and Technical Risk Management
API RP 2201
Safe Hot Tapping Practices in the Petroleum & Petrochemical Industries
API Spec 6A
Specification for Wellhead and Christmas Tree Equipment
API Spec 6FA
Specification for Fire Test for Valves
API 5LD
Specification for CRA Clad or Lined Steel Pipe
ASME B16.9
Factory-Made Wrought Buttwelding Fittings
ASME B31.3
Process Piping
ASME B31.4
Pipeline Transportation Systems for Liquid Hydrocarbons and Other Liquids
ASME B31.8
Gas Transmission and Distribution Systems
ASME BPVC-V
Boiler and Pressure Vessel Code Section V - Non-destructive Examination
ASME BPVC-VIII-1
Boiler and Pressure Vessel Code Section VIII - Div. 1 - Rules for Construction of Pressure Vessels
ASME BPVC-VIII-2
Boiler and Pressure Vessel Code Section VIII - Div. 2 - Rules for Construction of Pressure Vessels Alternative Rules
ASNT
American Society for Nondestructive Testing. Central Certification Program (ACCP).
ASTM A 961
Standard Specification for Common Requirements for Steel Flanges, Forged Fittings, Valves, and
Parts for Piping Applications
ASTM A264
Standard Specification for Stainless Chromium-Nickel Steel-Clad Plate
ASTM A370
Standard Test Methods and Definitions for Mechanical Testing of Steel Products
ASTM A388
Standard Practice for Ultrasonic Examination of Steel Forgings
ASTM A577
Standard specification for Ultrasonic Angle-Beam Examination of Steel Plates
ASTM A578
Standard Specification for Straight-Beam Ultrasonic Examination of Rolled Steel Plates for Special
Applications
ASTM A609
Standard Practice for Castings, Carbon, Low Alloy, and Martensitic Stainless Steel, Ultrasonic
Examination Thereof
ASTM A956
Standard Test Method for Leeb Hardness Testing of Steel Products
ASTM A1038
Standard Test Method for Portable Hardness Testing by the Ultrasonic Contact Impedance Method
ASTM C33
Standards specification for concrete aggregates
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Document code
Title
ASTM D 695
Standard Test Method for Compressive Properties of Rigid Plastics
ASTM E110
Standard Test Method for Indentation Hardness of Metallic Materials by Portable Hardness Testers
ASTM E 165
Standard Practice for Liquid Penetrant Examination for General Industry
ASTM E 280
Standard Reference Radiographs for Heavy-Walled (4 1/2 to 12-in. (114 to 305-mm)) Steel
Castings
ASTM E 309
Standard Practice for Eddy-Current Examination of Steel Tubular products Using Magnetic
Saturation
ASTM E 317
Standard Practice for Evaluating Performance Characteristics of Pulse-Echo Testing Instruments
and Systems Without the Use of Electronic Measurement Instruments
ASTM E 426
Standard Practice for Electromagnetic (Eddy Current) Examination of Seamless and Welded
Tubular Products, Austenitic Stainless Steel and Similar Alloys
ASTM E 709
Standard Guide for Magnetic Particle Examination
ASTM E 797
Standard Practice for Measuring Thickness by Manual Ultrasonic Pulse-Echo Contact Method
ASTM E1212
Standard Practice for Quality Management Systems for Non-destructive Testing Agencies
ASTM E1417
Standard Practice for Liquid Penetrant Examination
ASTM E1444
Standard Practice for Magnetic Particle Examination
ASTM E1820
Standard Test Method for Measurement of Fracture Toughness
ASTM G 48
Standard Test Methods for Pitting and Crevice Corrosion Resistance of Stainless Steels and Related
Alloys by Use of Ferric Chloride Solution
AWS C5.3
Recommended Practices for Air Carbon Arc Gouging and Cutting
BS 7488
Fracture mechanics toughness tests. Method for determination of KIc, critical CTOD and critical J
values of metallic materials
BS 8571
Method of test for determination of fracture toughness in metallic materials using single edge
notched tension (SENT) specimens
BS 7910
Guide to methods for assessing the acceptability of flaws in metallic structures
BSI BS 7910
Guide to methods for assessing the acceptability of flaws in metallic structures
BSI PD 5500
Specification for unfired fusion welded pressure vessels
EN 1591-1
Flanges and their joints - Design rules for gasketed circular flange connections - Part 1:
Calculation
EN 1998
Eurocode 8: Design of structures for earthquake resistance
EN 10204
Metallic products - Types of inspection documents
EN 12668
Non destructive testing - Characterisation and verification of ultrasonic examination equipment- All
parts
EN 13445-3
Unfired pressure vessels - Part 3: Design
EN ISO 9606-1
Qualification testing of welders - Fusion welding - Part 1: Steels
EN ISO 14175
Welding consumables - Gases and gas mixtures for fusion welding and allied processes
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Page 20
Document code
Title
IEC 61511
Functional safety - Safety Instrumented Systems for the Process Industry Sector
IMCA M140
Specification for DP capability plots
IMO Res. A.1047
(27)
Principles of safe manning
IMO MSC/Circ.645
Guidelines for Vessels with Dynamic Positioning Systems
ISO 148-1
Metallic materials – Charpy pendulum impact test - Part 1: Test method
ISO 377
Metallic materials - Charpy pendulum impact test
ISO 2400
Welds in steel – Reference block for the calibration of equipment for ultrasonic examination
ISO 3183
Petroleum and natural gas industries - Steel pipe for pipeline transportation systems
ISO 3452
Non-destructive testing – Penetrant testing – All parts
ISO 3690
Welding and allied processes – Determination of hydrogen content in arc weld metal
ISO 3834-2
Quality requirements for fusion welding of metallic materials – Part 2: Comprehensive quality
requirements
ISO 4063
Welding and allied processes – Nomenclature of processes and reference numbers
ISO 4126
Safety devices for protection against excessive pressure
ISO 4136
Destructive tests on welds in metallic materials – Transverse tensile test
ISO 5173
Destructive tests on welds in metallic materials – Bend tests
ISO 5178
Destructive tests on welds in metallic materials – Longitudinal tensile test on weld metal in fusion
welded joints
ISO 5817
Welding - Fusion-welded joints in steel, nickel, titanium and their alloys (beam welding excluded) Quality levels for imperfections
ISO 6507
Metallic materials – Vickers hardness test
ISO 6847
Welding consumables - Deposition of a weld metal pad for chemical analysis
ISO 6892
Metallic materials – Tensile testing
ISO 6947
Welding and allied processes – Welding positions
ISO 7005-1
Pipe flanges - Part 1: Steel flanges for industrial and general service piping systems
ISO 7539
Corrosion of metals and alloys - Stress corrosion testing
ISO 7963
Non-destructive testing – Ultrasonic testing – Specification for calibration block No. 2
ISO 8501-1
Preparation of steel substrates before application of paints and related products – Visual
assessment of surface cleanliness – Part 1: Rust grades and preparation grades of uncoated steel
substrates and of steel substrates after overall removal of previous coatings
ISO 9000
Quality management systems – Fundamentals and vocabulary
ISO 9001
Quality management systems – Requirements
ISO 9606-1
Qualification testing of welders - Fusion welding - Part 1: Steels
ISO 9712
Non-destructive testing – Qualification and certification of NDT personnel
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Page 21
Document code
Title
ISO/TR 9769
Steel and iron – Review of available methods of analysis
ISO 9934
Non-destructive testing – Magnetic particle testing – All parts
ISO 10375
Non-destructive testing – Ultrasonic inspection – Characterization of search unit and sound field
ISO 10474
Steel and steel products - Inspection documents
ISO 10893
Non-destructive testing of steel tubes – All parts
ISO 11484
Steel products – Employer's qualification system for non-destructive testing (NDT) personnel
ISO 12135
Metallic materials - Unified method of test for determination of quasistatic fracture toughness
ISO 12715
Non-destructive testing -- Ultrasonic testing -- Reference blocks and test procedures for the
characterization of contact probe sound beams
ISO/TS 12747
Petroleum and natural gas industries – Pipeline transportation systems – Recommended practice
for pipeline life extension
ISO 13623
Petroleum and natural gas industries – Pipeline transportation systems
ISO 13847
Petroleum and natural gas industries – Pipeline transportation systems – Welding of pipelines
ISO 14284
Steel and iron – Sampling and preparation of samples for the determination of chemical
composition
ISO 14723
Petroleum and natural gas industries - Pipeline transportation systems - Subsea pipeline valves
ISO 14731
Welding coordination – Tasks and responsibilities
ISO 14732
Welding personnel -- Qualification testing of welding operators and weld setters for mechanized
and automatic welding of metallic materials
ISO 15156
Petroleum and natural gas industries - Materials for use in H2S-containing environments in oil and
gas production - All parts
ISO 15589
Petroleum and natural gas industries – Cathodic protection of pipeline transportation systems – All
parts
ISO 15590
Petroleum and natural gas industries – Induction bends, fittings and flanges for pipeline
transportation systems - All parts
ISO 15614-1
Specification and qualification of welding procedures for metallic materials – Welding procedure
test – Part 1: Arc and gas welding of steels and arc welding of nickel and nickel alloys
ISO 15618-2
Qualification testing of welders for underwater welding – Part 2: Diver-welders and welding
operators for hyperbaric dry welding
ISO 15649
Petroleum and natural gas industries – Piping
ISO 15653
Metallic materials, Method of test for the determination of quasistatic fracture toughness
of welds
ISO 15741
Paints and varnishes - Friction-reducing coatings for the interior of on-and offshore steel pipelines
for non-corrosive gases
ISO 16708
Petroleum and natural gas industries – Pipeline transportation systems – Reliability-based limit
state methods
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
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Page 22
Document code
Title
ISO 16828
Non-destructive testing - Ultrasonic testing - Time-of-flight diffraction technique as a method for
detection and sizing of discontinuities
ISO/IEC 17025
General requirements for the competence of testing and calibration laboratories
ISO 17636
Non-destructive testing of welds – Radiographic testing
ISO 17637
Non-destructive testing of welds – Visual testing of fusion-welded joints
ISO 17638
Non-destructive testing of welds – Magnetic particle testing
ISO 17640
Non-destructive testing of welds – Ultrasonic testing – Techniques, testing levels, and assessment
ISO 17643
Non-destructive testing of welds – Eddy current testing of welds by complex-plane analysis
ISO 19232
Non-destructive testing – Image quality of radiographs
ISO 19901-2
Petroleum and natural gas industries – Specific requirements for offshore structures – Part 2:
Seismic design procedures and criteria
ISO 21457
Petroleum, petrochemical and natural gas industries — Materials selection and corrosion control
for oil and gas production systems
ISO 21809
Petroleum and natural gas industries – External coatings for buried or submerged pipelines used in
pipeline transportation systems – All parts
ISO 22825
Non-destructive testing of welds – Ultrasonic testing – Testing of welds in austenitic steels and
nickel-based alloys
MSS SP-55
Quality standard for steel castings for valves, flanges, and fittings and other piping components Visual method for evaluation of surface irregularities
MSS SP-75
High-Strength, Wrought, Butt-Welding Fittings
NACE TM0177
Laboratory Testing of Metals for Resistance to Sulfide Stress Cracking and Stress Corrosion
Cracking in H2S Environments
NACE TM0284
Standard Test Method - Evaluation of Pipeline and Pressure Vessel Steels for Resistance to
Hydrogen-Induced Cracking
NORDTEST
NT Technical Report 394 (Guidelines for NDE Reliability Determination and Description, Approved
1998-04).
NORSOK L-005
Compact flanged connections
NORSOK N-006
Assessment of structural integrity for existing offshore load-bearing structures
NORSOK U-009
Life extension for subsea systems
NORSOK Y-002
Life extension for transportation systems
NS 477
Welding inspectors - Tasks, education and certification
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Page 23
1.8 Definitions
1.8.1 Verbal forms
Table 1-7 Definitions of verbal forms
Term
Definition
shall
verbal form used to indicate requirements strictly to be followed in order to conform to the document
should
verbal form used to indicate that among several possibilities one is recommended as particularly
suitable, without mentioning or excluding others, or that a certain course of action is preferred but not
necessarily required
may
verbal form used to indicate a course of action permissible within the limits of the document
agreement, by
agreement
unless otherwise indicated, this means agreed in writing between manufacturer/contractor and
purchaser
1.8.2 Terms
Table 1-8 Definitions of terms
Term
Definition
abandonment
the activities associated with taking a pipeline permanently out of operation
An abandoned pipeline cannot be returned to operation. Depending on the
legislation this may require cover or removal.
accidental loads
a load with an annual frequency less than 10 , see [5.4.10]
accumulated plastic strain
the sum of plastic strain increments, irrespective of sign and direction
Strain increments shall be calculated from after the line pipe manufacturing.
additional requirements
requirements that applies to this standard, additional to other referred standards
as-built survey
a survey of the installed and completed pipeline system that is performed to
verify that the completed installation work meets the specified requirements and
documents deviations from the original design, if any
as-laid survey
a survey performed either by continuous touchdown point monitoring or by a
dedicated vessel during installation of the pipeline
assemblies, in-line
pipeline components, see Table 1-1, buckle and fracture arrestors, PLEMs and
PLETs which are integrated part of the pipeline and connected or welded to the
pipeline during installation
assemblies, pipeline
risers, pipe strings (for reeling or towing), spools which are welded onshore, see
[8.6].
annual probability
the probability of an event to occur in the period of one year
atmospheric zone
the part of the pipeline system above the splash zone
buckling, global
buckling mode which involves a substantial length of the pipeline, usually
several pipe joints and not gross deformations of the cross-section; upheaval
buckling is an example thereof, see [5.4.7]
-2
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Page 24
Term
Definition
buckling, local
buckling mode confined to a short length of the pipeline causing gross changes
of the cross-section; collapse, localised wall wrinkling and kinking are examples
thereof, see [5.4.3]
characteristic load (Lc)
the reference value of a load to be used in the determination of load effects
The characteristic load is normally based upon a defined fractile in the upper end
of the distribution function for load, see [4.7].
characteristic resistance (Rc)
the reference value of structural strength to be used in the determination of the
design strength
The characteristic resistance is normally based upon a defined fractile in the
lower end of the distribution function for resistance, see [5.3.2].
clad pipe (C)
pipe with internal (corrosion resistant) liner where the bond between (line pipe)
backing steel and cladding material is metallurgical
clamp
circumferential structural element, split into two or more parts
Examples; connecting two hubs in a mechanical connector or two pipe halfshells for repair purpose.
code break
a point or cross section on the pipeline where one set of specifications apply on
one side and another set on the other side
coiled tubing
continuously-milled tubular product manufactured in lengths that require
spooling onto a take-up reel, during the primary milling or manufacturing
process
commissioning
activities associated with the initial filling of the pipeline system with the fluid to
be transported, part of operational phase
commissioning, De -
activities associated with taking the pipeline temporarily out of service
commissioning, Pre -
activities after tie-in/connection and prior to commissioning including system
pressure testing, de-watering, cleaning and drying
concept development phase
the concept development phase will typically include both business evaluations,
collecting of data and technical early phase considerations
condition load effect factor (γC)
a load effect factor included in the design load effect to account for specific load
conditions, see Table 4-5
connector
mechanical device used to connect adjacent components in the pipeline system
to create a structural joint resisting applied loads and preventing leakage
Examples: threaded types, including (i) one male fitting (pin), one female fitting
(integral box) and seal ring(s), or (ii) two pins, a coupling and seals sea ring(s);
flanged types, including two flanges, bolts and gasket/seal ring; clamped hub
types, including hubs, clamps, bolts and seal ring(s); dog-type connectors.
construction phase
the construction phase will typically include manufacture, fabrication and
installation activities
Manufacture activities will typically include manufacture of line pipe and
corrosion protection and weight coating. Fabrication activities will typically
include fabrication of pipeline components and assemblies. Installation activities
will typical include pre- and post intervention work, transportation, installation,
tie-in and pre-commissioning.
contractor
a party contractually appointed by the purchaser to fulfil all, or any of, the
activities associated with design, construction and operation
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
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Page 25
Term
Definition
corrosion allowance (tcorr)
extra wall thickness added during design to compensate for any reduction in wall
thickness by corrosion (internally/externally) during operation, see [6.4.2]
corrosion control
all relevant measures for corrosion protection, as well as the inspection and
monitoring of corrosion, see [6.4.1]
corrosion protection
use of corrosion resistant materials, corrosion allowance and various techniques
for corrosion mitigation, see [6.4.1]
coupling
mechanical device to connect two bare pipes to create a structural joint resisting
applied loads and preventing leakage
design
all related engineering to design the pipeline including both structural as well as
material and corrosion
design case
characterisation of different load categories, see [4.1.5]
defect
for welds a defect is defined as a flaw which is deemed to be unacceptable, for
instance by virtue of its size exceeding a specified acceptance criteria (which
may be based on workmanship or ECA)
All flaws that exceeds the flaw acceptance criteria shall be defined as defects
and repaired.
design life
the initially planned time period from initial installation or use until abandonment
of the equipment or system. The original design life may be extended after a requalification
design premises
a set of project specific design data and functional requirements which are
not specified or which are left open in the standard to be prepared prior to the
design phase
design phase
the design phase will typically be split into FEED-phase, basic design and detail
design. For each design phase, the same design tasks are repeated but in more
and more specific and detailed level
dynamic riser
production risers tied back to floating structures (ISO 13628-1)
element
a structural element in an assembly, e.g. outer and inner pipe, bulkhead of a
pipe-in-pipe system
engineering critical assessment (ECA)
fracture mechanics assessment of the acceptability of flaws in metallic materials
erosion
material loss due to repeated impact of sand particles or liquid droplets
fabrication
activities related to the assembly of objects with a defined purpose in a pipeline
system
fabrication factor (αfab)
factor on the material strength in order to compensate for material strength
reduction (in hoop direction) from cold forming during manufacturing of line
pipe, see Table 5-5
fabricator
the party performing the fabrication
failure
an event affecting a component or system and causing one or both of the
following effects:
— loss of component or system function; or
— deterioration of functional capability to such an extent that the safety of the
installation, personnel or environment is significantly reduced
fatigue
cyclic loading causing degradation of the material
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Page 26
Term
Definition
fittings
elbows, caps, tees, single or multiple extruded headers, reducers and transition
sections
flange
collar at the end of a pipe usually provided with holes in the pipe axial direction
for bolts to permit other objects to be attached to it
flaw
a feature that has been detected by NDT, often caused by welding such as
porosity, lack of fusion etc.
The size of a flaw may be an input to a fracture mechanics assessment (ECA)
to determine its acceptability. Alternatively, assessments may be carried out to
determine a maximum allowable flaw size for sentencing purposes (basis for UT/
AUT acceptance criteria).
fluid categorisation
categorisation of the transported fluid according to hazard potential as defined in
Table 2-1
fractile
the p-fractile (or percentile) and the corresponding fractile value xp is defined
as:
F is the distribution function for xp
hub
the parts in a mechanical connector joined by a clamp
hydrogen induced cracking (HIC)
internal cracking of rolled materials due to a build-up of hydrogen pressure in
micro-voids (Related terms: stepwise cracking)
hydrogen induced stress cracking
(HISC)
cracking that results from the presence of hydrogen in a metal while subjected
to tensile stresses (residual and/or applied)
The source of hydrogen may be welding, corrosion, cathodic protection,
electroplating or some other electrochemical process. Crack growth proceeds
by a hydrogen embrittlement mechanism at the crack tip, i.e. the bulk material
is not necessarily embrittled by hydrogen. HISC by corrosion in presence of
hydrogen sulphide is referred to as Sulphide Stress Cracking (SSC).
hydrostatic test
in some standards or recommended practices used for the mill pressure test. In
this standard referred to as hydrostatic (i.e. with water) pressure test in general
inner pipe
the inner pipe in a pipe-in-pipe system
The purpose of this pipe is to convey the product.
inspection
activities such as measuring, examination, weighing testing, gauging one or
more characteristics of a product or service and comparing the results with
specified requirements to determine conformity
installation (activity)
the operations related to installing the equipment, pipeline or structure, e.g.
pipeline laying, tie-in, piling of structure etc.
installation (object)
see offshore installation
installation manual (IM)
a document prepared by the contractor to describe and demonstrate that the
installation method and equipment used by the contractor will meet the specified
requirements and that the results can be verified
integrity
see pipeline integrity
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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DNV GL AS
Page 27
Term
Definition
jointer
two lengths of pipe welded together by the manufacturer to build up one
complete (≈40’) pipe joint
limit state
a state beyond which the structure no longer satisfies the requirements
The following limit states categories are of relevance for pipeline systems:
— serviceability limit state (SLS): A condition which, if exceeded, renders the
pipeline unsuitable for normal operations. Exceedance of a serviceability limit
state category shall be evaluated as an accidental limit state.
— ultimate limit state (ULS): A condition which, if exceeded, compromises the
integrity of the pipeline.
— fatigue limit state (FLS): An ULS condition accounting for accumulated cyclic
load effects.
— accidental limit state (ALS): An ULS due to accidental (in-frequent) loads.
line pipe
a welded or seamless pipe, available with ends plain, bevelled, grooved, cold
expanded, flanged, or threaded; principally used to convey gas, oil or water
lined pipe (L)
pipe with internal (corrosion resistant) liner where the bond between (line pipe)
backing steel and liner material is mechanical
load
any action causing stress, strain, deformation, displacement, motion, etc. to the
equipment or system
load categories
functional load, environmental load, interference load or accidental load, see
[4.1]
load effect
effect of a single load or combination of loads on the equipment or system, such
as stress, strain, deformation, displacement, motion, etc.
load effect combinations
see [4.7.3]
load effect factor (γF, γE, γA)
the partial safety factor by which the characteristic load effect is multiplied to
obtain the design load effect, see [4.7.3]
load scenarios
scenarios which shall be evaluated, see [4.1]
location class
a geographic area of pipeline system, see Table 2-2
lot
components of the same size and from the same heat, the same heat treatment
batch
manufacture
making of articles or materials, often in large volumes
In relation to pipelines, refers to activities for the production of line pipe, anodes
and other components and application of coating, performed under contracts
from one or more contractors.
manufacturer
the party who is contracted to be responsible for planning, execution and
documentation of manufacturing
manufacturing procedure specification
(MPS)
a manual prepared by the manufacturer to demonstrate how the specified
properties may be achieved and verified through the proposed manufacturing
route
material resistance factor (γm)
partial safety factor transforming a characteristic resistance to a lower fractile
resistance, see Table 5-1
material strength factor (αu)
factor for determination of the characteristic material strength reflecting the
confidence in the yield stress see Table 5-3
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Page 28
Term
Definition
mill pressure test
the hydrostatic strength test performed at the mill, see [5.2.2] and [D.2.1.5]
minimum wall thickness
the specified non-corroded pipe wall thickness of a pipe minus the
manufacturing tolerance
nominal failure probability
a probability of structural failure due to natural uncertainties as reflected in
structural reliability analyses
Gross errors are not included, see [2.3.5]
nominal outside diameter
the specified outside diameter
nominal pipe wall thickness
the specified non-corroded pipe wall thickness of a pipe
nominal strain
the total engineering strain not accounting for local strain concentration factors
nominal plastic strain
the nominal strain minus the linear strain derived from the stress-strain curve,
see Table 1-8
notch
used in connection with fracture toughness testing and consists of the machined
notched plus the fatigue pre-crack
offshore installation (object)
general term for mobile and fixed structures, including facilities, which
are intended for exploration, drilling, production, processing or storage of
hydrocarbons or other related activities/fluids
The term includes installations intended for accommodation of personnel
engaged in these activities. Offshore installation covers subsea installations and
pipelines. The term does not cover traditional shuttle tankers, supply boats and
other support vessels which are not directly engaged in the activities described
above.
operation, incidental
conditions which that are not part of normal operation of the equipment or
system
In relation to pipeline systems, incidental conditions may lead to incidental
pressures, e.g. pressure surges due to sudden closing of valves, or failure of the
pipeline control system and activation of the pipeline safety system.
operation, normal
conditions that arise from the intended use and application of equipment or
system, including associated condition and integrity monitoring, maintenance,
repairs etc.
In relation to pipelines, this should include steady flow conditions over the full
range of flow rates, as well as possible packing and shut-in conditions where
these occur as part of routine operation
operation phase
the operation phase starts with the commissioning, filling the pipeline with the
intended fluid. The operation phase will include inspection and maintenance
activities
In addition, the operation phase may also include modifications, re-qualifications
and de-commissioning.
operator (pipeline)
the party ultimately responsible for concept development, design, construction
and operation of the pipeline system
The operator may change between phases
ovality
the deviation of the line pipe perimeter from a circle
This can be stated as ovalisation (%), or as local out of roundness, e.g.
flattening, (mm).
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Term
Definition
outer pipe
the outer pipe in a pipe-in-pipe system
The main purpose of this pipe is to protect the annulus, keep it dry and not
expose it to excessive pressure
ovalisation
the deviation of the perimeter from a circle. This has the form of an elliptic
cross-section
parameter operating envelop
limitations of the operating parameters in the pipeline control system that will
ensure that the parameter control envelope is not exceeded with an acceptable
reliability
This includes all relevant parameters and links between these including
minimum values if relevant. This will first be established in the concept phase
(mainly based on hydraulic analyses), extended in the design phase and reassessed in the operation phase.
parameter safety envelop
limitations of the operating parameters in the pipeline safety system that will
ensure that the parameter safety envelope is not exceeded with an acceptable
reliability
This will first be established in the concept phase (mainly based on hydraulic
analyses), extended in the design phase and re-assessed in the operation phase.
partial safety factor
a factor by which the characteristic value of a variable is modified to give the
design value (i.e. a load effect, condition load effect, material resistance or
safety class resistance factor), see [5.3]
pipe, high frequency welded (HFW)
pipe manufactured by forming from strip and with one longitudinal seam formed
by welding without the addition of filler metal
The longitudinal seam is generated by high frequency current applied by
induction or conduction.
pipe, seamless (SMLS)
pipe manufactured in a hot forming process resulting in a tubular product
without a welded seam
The hot forming may be followed by sizing or cold finishing to obtain the
required dimensions.
pipe, submerged arc-welded
longitudinal or helical (SAWL or SAWH): Pipe manufactured by forming from
strip or plate, and with one longitudinal (SAWL) or helical (SAWH) seam formed
by the submerged arc process with at least one pass made on the inside and
one pass from the outside of the pipe
pipeline components
any items which are integral parts of the submarine pipeline system such as
bends, fittings, flanges, valves, mechanical connectors, CP isolation joints,
anchor flanges, buckle and fracture arrestors, pig traps, repair clamps and repair
couplings (see Sec.8)
pipeline control system
the basic process control system that ensures that the operating parameters are
within the operating parameter envelop
pipeline integrity
pipeline integrity is the ability of the submarine pipeline system to operate safely
and withstand the loads imposed during the pipeline lifecycle
pipeline integrity management
the pipeline integrity management process is the combined process of threat
identification, risk assessments, planning, monitoring, inspection, maintenance
etc. to maintain pipeline integrity
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Term
Definition
pipeline safety system
the system as per in IEC 61511 that ensures that the operating parameters are
within the safety parameter envelop
The safety parameters can be, but are not limited to, flow, internal pressure,
temperature or composition
pipeline system
pipeline with compressor or pump stations, pipeline control stations, metering,
tankage, supervisory control and data acquisition system (SCADA), safety
systems, corrosion protection systems, and any other equipment, facility or
building used in the transportation of fluids
See also submarine pipeline system.
pipeline walking
accumulation of incremental axial displacement of pipeline due to start-up and
shut-down
positioning/heading keeping
maintaining a desired position/heading within the normal execution of the
control system and environmental conditions
position/heading reference system
all hardware, software and sensors that supply information and or corrections
necessary to give positioning/heading reference
pressure test
see system pressure test
pressure, collapse (pc)
characteristic resistance against external over-pressure, see [5.4.4]
pressure, design (pd)
in relation to pipelines, this is the maximum internal pressure during normal
operation, referred to the same reference elevation as the incidental pressure,
see Table 1-8 and [3.4.2]
pressure, hydro- or hydrostatic test
see pressure, mill test
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Term
Definition
pressure, incidental (pinc)
in relation to pipelines, this is the maximum internal pressure the pipeline
or pipeline section is designed to withstand during any incidental operating
situation, referred to a specified reference elevation, see Table 1-8 and [3.4.2]
Figure 1-1 Pressure definitions
pressure, initiation
the external over-pressure required to initiate a propagating buckle from an
existing local buckle or dent (100-year value), see [5.4.5]
pressure, local; local design, local
incidental or local test
in relation to pipelines, this is the internal pressure at any point in the pipeline
system or pipeline section for the corresponding design pressure, incidental
pressure or test pressure adjusted for the column weight, see [4.2.2]
pressure, maximum allowable
incidental (MAIP)
in relation to pipelines, this is the maximum pressure at which the pipeline
system shall be operated during incidental (i.e. transient) operation
The maximum allowable incidental pressure is defined as the maximum
incidental pressure less the positive tolerance of the pipeline safety system, see
Table 1-8 and [3.4.2].
pressure, maximum allowable
operating (MAOP)
in relation to pipelines, this is the maximum pressure at which the pipeline
system shall be operated during normal operation
The maximum allowable operating pressure is defined as the design pressure
less the positive tolerance of the pipeline control system (PCS), see Table 1-8
and [3.4.2].
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Term
Definition
pressure, mill test (ph)
the test pressure applied to pipe joints and pipe components upon completion of
manufacture and fabrication, see [5.2.2]
pressure, propagating (ppr)
the lowest pressure required for a propagating buckle to continue to propagate,
see [5.4.5]
pressure, shut-in
the maximum pressure that can be attained at the wellhead during closure of
valves closest to the wellhead (wellhead isolation)
This implies that pressure transients due to valve closing shall be included.
pressure, system test (ptest)
in relation to pipelines, this is the internal pressure applied to the pipeline or
pipeline section during testing on completion of installation work to test the
pipeline system for tightness (normally performed as hydrostatic testing), see
[5.2.2]
pressure, test
see pressure, system test
progressive failure
some pipeline concepts may have some structural redundancy, e.g. failure of
one barrier may lead to functional consequences but not to consequences of the
environment
For such concepts, the first failure may lead to a second failure that then may
lead to severe consequences, i.e. progressive failures. This will be typical for
pipe-in-pipe systems.
pup piece
an extra line pipe piece added to a component in order to build up a certain
overall length, typically for construction and/or fabrication purpose
purchaser
the owner or another party acting on his behalf, who is responsible for procuring
materials, components or services intended for the design, construction or
modification of an installation or a pipeline
quality assurance (QA)
planned and systematic actions necessary to provide adequate confidence that a
product or service will satisfy given requirements for quality
(The quality assurance actions of an organisation is described in a quality
manual stating the quality policy and containing the necessary procedures and
instructions for planning and performing the required actions).
quality control (QC)
the internal systems and practices (including direct inspection and materials
testing), used by manufacturers to ensure that their products meet the required
standards and specifications
quality plan (QP)
the document setting out the specific quality practices, resources and sequence
of activities relevant to a particular product, project or contract
A quality plan usually makes reference to the part of the quality manual (e.g.
procedures and work instructions) applicable to the specific case.
ratcheting
accumulated deformation during cyclic loading, especially for diameter increase,
see [5.4.13]
Does not include so called pipeline walking.
reliability
the probability that a component or system will perform its required function
without failure, under stated conditions of operation and maintenance and
during a specified time interval
re-qualification
the re-assessment of a design due to modified design premises and/or sustained
damage
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Term
Definition
resistance
the capability of a structure, or part of a structure, to resist load effects, see
[5.3.2]
riser
a riser is defined as the connecting piping or flexible pipe between a submarine
pipeline on the seabed and installations above water
The riser extends to the above sea emergency isolation point between the
import/export line and the installation facilities, i.e. riser ESD valve.
riser support/clamp
a structure which is intended to keep the riser in place
riser system
a riser system is considered to comprise riser, its supports, all integrated
pipeline components, and corrosion protection system
risk
the qualitative or quantitative likelihood of an accidental or unplanned event
occurring, considered in conjunction with the potential consequences of such a
failure
In quantitative terms, risk is the quantified probability of a defined failure mode
times its quantified consequence.
safety class (SC)
in relation to pipelines; a concept adopted to classify the significance of the
pipeline system with respect to the consequences of failure, see [2.3.4]
safety class resistance factor (γSC)
partial safety factor which transforms the lower fractile resistance to a design
resistance reflecting the safety class, see Table 5-2
single event
straining in one direction.
specified minimum tensile strength
(SMTS)
the minimum tensile strength specified by this standard
For supplementary requirement U, this corresponds to a statistical value equal to
or lower than the mean minus three standard deviations.
specified minimum yield stress (SMYS) the minimum yield stress specified by this standard
For supplementary requirement U, this corresponds to a statistical value equal to
or lower than the mean minus two standard deviations.
splash zone
external surfaces of a structure or pipeline that are periodically in and out of the
water by the influence of waves and tides
spool
a pipe section which is used to connect a pipeline to another subsea structure
(e.g. manifold, PLET, tee) or riser
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Term
Definition
stress-strain curve
a uni-axial material characterisation, see Table 1-8
This may be given based on engineering stress-strain or true stress-strain
dependent on if the reduction in cross sectional area is included in the force-tostress conversion.
Figure 1-2 Stress-strain curve and definitions
submarine pipeline
a submarine pipeline is defined as the part of a submarine pipeline system
which, except for pipeline risers is located below the water surface at maximum
tid
The pipeline may, be resting wholly or intermittently on, or buried below, the
seabed.
submarine pipeline system
a submarine pipeline system extends to the first weld beyond:
— the first valve, flange or connection above water on platform or floater
— the connection point to the subsea installation (i.e. piping manifolds are not
included)
— the first onshore valve, flange, connection or insulation joint, unless
otherwise specified by the on-shore legislation
The component above (valve, flange, connection, insulation joint) includes any
pup pieces, i.e. the submarine pipeline system extends to the weld beyond the
pup piece.
submerged zone
the part of the pipeline system or installation below the splash zone, including
buried parts
supplementary requirements
requirements for material properties of line pipe that are extra to the additional
requirements to ISO and that are intended to apply to pipe used for specific
applications
system effects
system effects are relevant in cases where many pipe sections are subjected
to an invariant loading condition, and potential structural failure may occur in
connection with the lowest structural resistance among the pipe sections, see
[4.7.3]
system pressure test
final test of the complete pipeline system, see [5.2.2]
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Term
Definition
target nominal failure probability
a nominal acceptable probability of structural failure
Gross errors are not included, see [2.3.5]
technology qualification
the process of providing the evidence that technology will function within
specified limits with an acceptable level of confidence
temperature, design, minimum
the lowest possible temperature profile to which the component or system may
be exposed to during installation and operation (100-year value)
This may be applied locally, see [4.2.1.6].
temperature, design, maximum
the highest possible temperature profile to which the equipment or system may
be exposed to during installation and operation (100-year value)
temperature, operation
representative temperature profile(s) during operation
test unit
a prescribed quantity of pipe that is made to the specified outer diameter and
specified wall thickness, by the same pipe-manufacturing process, from the
same heat, and under the same pipe-manufacturing conditions
threats
an indication of impending danger or harm to the pipeline system
tide
see [3.3.4]
ultimate tensile strength (UTS)
the measured ultimate tensile strength
verification
an examination to confirm that an activity, a product or a service is in
accordance with specified requirements
weld, strip/plate end
weld that joins strip or plate joins together
work
all activities to be performed within relevant contract(s) issued by owner,
operator, contractor or manufacturer
yield stress (YS)
the measured yield tensile stress
100-year load effect
the load effect that has a probability of being exceeded within one year equal to
-2
10
1.8.3 Abbreviations
Table 1-9 Abbreviations
Abbreviation
Description
ALS
accidental limit state
AR
additional requirement to the stated ISO standard
API
American Petroleum Institute
APS
application procedure specification
ASD
allowable stress design
ASME
American Society of Mechanical Engineers
ASTM
American Society for Testing and Materials
AUT
automated ultrasonic testing
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Abbreviation
Description
BM
base material
BS
british standard
CE
carbon equivalent
C-Mn
carbon manganese
CMOD
crack mouth opening displacement
CP
cathodic protection
CRA
corrosion resistant alloy
CTOD
crack tip opening displacement
CVN
charpy v-notch
DAC
distance amplitude correction
DC
displacement controlled
DFI
design, fabrication and installation
DGS
distance gain-size
DP
dynamic positioning
DWTT
drop weight tear testing
EBW
electron beam welded
EC
eddy current testing
ECA
engineering critical assessment
EDI
electronic data interchange
EMS
electro magnetic stirring
ERW
electric resistance welding
ESD
emergency shut down
FBH
flat bottom hole
FEED
front end engineering design
FJC
field joint coating
FLS
fatigue limit state
FMEA
failure mode effect analysis
FTA
flowline termination assembly
G-FCAW
gas-flux core arc welding
GMAW
gas metal arc welding
HAT
highest astronomical tide
HAZ
heat affected zone
HAZOP
hazard and operability study
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Abbreviation
Description
HFW
high frequency welding
HIPPS
high integrity pressure protection system
HIC
hydrogen induced cracking
HISC
hydrogen induced stress cracking
ID
internal diameter
ILTA
in-line tea assembly
IM
installation manual
IMCA
international marine contractor’s association
ISO
international organization for standardization
ITP
inspection and testing plan
JCO
pipe fabrication process for welded pipes
JCOE
pipe fabrication process for welded pipes, expanded
J-R curve
plot of resistance to stable crack growth for establishing crack extension
KV
charpy value
KVL
charpy value in pipe longitudinal direction
KVT
charpy value in pipe transversal direction
L
load effect
LAT
lowest astronomic tide
LC
load controlled
LBW
laser beam welded
LBZ
local brittle zones
LRFD
load and resistance factor design
M/A
martensitic/austenite
MAIP
maximum allowable incidental pressure
MAOP
maximum allowable operating pressure
MDS
material data sheet
MPQT
manufacturing procedure qualification test
MPS
manufacturing procedure specification
MR
modified requirement to the stated ISO standard
MSA
manufacturing survey arrangement
MT
magnetic particle testing
MWP
multiple welding process
N
normalised
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Abbreviation
Description
NACE
national association of corrosion engineers
NDT
non-destructive testing
OHTC
overall heat transfer coefficient
P
production
PCS
pipeline control system
PFD
probability of failure on demand
PIM
pipeline integrity management
PiP
pipe-in-pipe
PPT
pre-production trial
PRE
pitting resistance equivalent
PRL
primary reference level
PSS
pipeline safety system
PT
penetrant testing
PTFE
poly tetra flour ethylene
PVC
pressure vessel codes
PWHT
post weld heat treatment
pWPS
preliminary welding procedure specification
PQT
procedure qualification trial
Q
qualification
QA
quality assurance
QC
quality control
QP
quality plan
QRA
quantitative risk assessment
QT
quenched and tempered
ROV
remotely operated vehicle
RT
radiographic testing
SAWH
submerged arc-welding helical
SAWL
submerged arc-welding longitudinal
SC
safety class
SCF
stress concentration factor
SCR
steel catenary riser
SENB
single edge notched bend fracture mechanics specimen
SENT
single edge notched tension fracture mechanics specimen
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Abbreviation
Description
SFC
steel forging class
SLS
serviceability limit state
SMAW
shielded metal arc welding
SMLS
seamless pipe
SMTS
specified minimum tensile strength
SMYS
specified minimum yield stress
SN
stress versus number of cycles to failure
SNCF
strain concentration factor
SRA
structural reliability analysis
SSC
sulphide stress cracking
ST
surface testing
TCM
two curve method
TMCP
thermo-mechanical controlled process
TOFD
time of flight diffraction
TRB
three roll bending
UEL
uniform elongation length, see Table 6-1
ULS
ultimate limit state
UO
pipe fabrication process for welded pipes
UOE
pipe fabrication process for welded pipes, expanded
UT
ultrasonic testing
UTS
ultimate tensile strength
VT
visual testing
WM
weld metal
WAT
wax appearance temperature
WPQT
welding procedure qualification test
WPS
welding procedure specification
YS
yield stress
1.8.4 Symbols – latin characters
a
crack depth
A
cross-sectional area
Ae
pipe external cross-sectional area
Ai
pipe internal cross-sectional area
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As
pipe steel cross-sectional area
B
specimen width
D
nominal outside diameter
Dfat
Miner’s sum
DFF
design fatigue factor, see Equation (5.36)
Di
D–2tnom nominal internal diameter
Dmax
greatest measured inside or outside diameter
Dmin
smallest measured inside or outside diameter
E
Young's modulus
fcb
minimum of fy and fu/1.15, see Equation (5.9)
fu
tensile strength to be used in design, see Equation (5.5)
fu,temp
derating on tensile stress to be used in design, see Equation (5.5)
fy
yield stress to be used in design, see Equation (5.4)
fy,temp
derating on yield stress to be used in design, see Equation (5.4)
g
gravity acceleration
H
residual lay tension, see Equation (4.10)
hbead
height of weld bead including misalignment, see e.g. Table D-4
hl
elevation at pressure point, see Equation (4.1)
Hp
permanent plastic dent depth
href
elevation at pressure reference level, see Equation (4.1)
Hs
significant wave height
ID
nominal inside diameter
k
number of stress blocks
L
characteristic load effect
M
moment
N
axial force in pipe wall (true force) (tension is positive) or Number of load effect cycles
ni
number of stress blocks
Ni
number of stress cycles to failure at constant amplitude
O
ovality,
pb
pressure containment resistance, see Equation (5.8)
pc
characteristic collapse pressure, see Equation (5.11)
pd
design pressure
PDi
(i’th) damaging event, see Equation (5.38)
pe
external pressure
pel
elastic collapse pressure, see Equation (5.12)
pf
failure probability
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pf,T
target nominal failure probability, see Table 2-5
pi
characteristic internal pressure
pinc
incidental pressure
pinit
initiation pressure
pld
local design pressure
pli
local incidental pressure, see Equation (4.1)
plt
local test pressure (system test), see Equation (4.2)
pmpt
mill test pressure, see [7.5.1]
pp
plastic collapse pressure, see Equation (5.13)
ppr
propagating pressure, see Equation (5.16)
ppr,A
propagating buckle capacity of infinite buckle arrestor
pt
system test pressure, see Equation (4.2) and Equation (5.1)
px
crossover pressure, see Equation (5.18)
R
global bending radius of pipe, Reaction force or Resistance
Rm
tensile strength
Rpx
strength equivalent to a permanent elongation of x% (actual stress)
Rtx
strength equivalent to a total elongation of x% (actual stress)
S
effective axial force (tension is positive)
tc
characteristic thickness to be replaced by t1 or t2 as relevant, see Table 5-5
T
temperature
t, tnom
nominal wall thickness of pipe (un-corroded)
T0
testing temperature
t1, t2
pipe wall thickness, see Table 5-5
tcorr
corrosion allowance, see Table 5-5
Tc/Tc’
contingency time for operation/ceasing operation, see [4.3.6] and Figure 4-1
tfab
fabrication thickness tolerance, see Table 7-18
tm,min
measured minimum thickness
Tmax
maximum design temperature, see [4.2.1]
Tmin
minimum design temperature, see [4.2.1]
Tpop
planned operational period, see [4.3.6]
TR/TR’
reference period for operation/ceasing operation, see [4.3.6] and Figure 4-1
TSafe
planned time to cease operation, see [4.3.6] and Figure 4-1
TWF
time between generated weather forecasts, see [4.3.6] and Figure 4-1
W
section modulus or specimen thickness
Wsub
submerged weight
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1.8.5 Symbols – greek characters
α
thermal expansion coefficient
αc
characteristic flow stress ratio, see Equation (5.22)
αfab
fabrication factor, see Table 5-4
αgw
girth weld factor (strain resistance), see Equation (5.31)
αh
strain hardening
αmpt
mill pressure test factor, see Table 5-8
αp
pressure factor used in combined loading criteria, see Equation (5.19)
αpm
plastic moment reduction factor for point loads, see Equation (5.25)
αspt
system pressure test factor, see Table 5-8
αU
material strength factor, see Table 5-3
β
factor used in combined loading criteria, see Equation (5.24)
ε
strain
εc
characteristic bending strain resistance, see Equation (5.30)
εf
accumulated plastic strain resistance
εl.nom
total nominal longitudinal strain
εp
plastic strain
εr
residual strain range
γA
load effect factor for accidental load, see Table 4-4
γc
condition load effect factor, see Table 4-5
γE
load effect factor for environmental load, see Table 4-4
γF
load effect factor for functional load, see Table 4-4
γinc
incidental to design pressure ratio, see Table 3-1
γm
material resistance factor, see Table 5-1
γrot
safety factor for residual strain
γSC,i
safety class resistance factor for limit state i (PB, LB, DC), see Table 5-2
η
usage factor
κ
curvature
ν
Poisson’s ratio
μ
friction coefficient
ρcont
density pipeline content
ρt
density pipeline content during system pressure test
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σ
standard deviation of a variable (e.g. thickness)
σe
equivalent stress, Von Mises, see Equation (5.45)
σh
hoop stress, see Equation (5.46)
σl
longitudinal/axial stress, see Equation (5.47)
τ
lh
tangential shear stress
1.8.6 Subscripts
A
accidental load
BA
buckle arrestor
c
characteristic resistance
d
design value
E
environmental load
e
external
el
elastic
F
functional load
h
circumferential direction (hoop direction)
H
circumferential direction (hoop direction)
i
internal
L
axial (longitudinal) direction
M
moment
mpt
mill pressure test
p
plastic
R
radial direction
Rd
design resistance (i.e. including partial resistance factors)
s
steel
S
SLS
Sd
design load (i.e. including load effect factors)
spt
system pressure test
U
ULS
X
crossover (buckle arrestors)
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SECTION 2 SAFETY PHILOSOPHY
2.1 General
2.1.1 Objective
2.1.1.1 This section presents the overall safety philosophy that shall be applied in the concept development,
design, construction, operation and abandonment of pipelines.
2.1.2 Application
2.1.2.1 This section applies to all submarine pipeline systems which shall be built and operated in
accordance with this standard.
2.1.2.2 The integrity of a submarine pipeline system shall be ensured through all phases, from initial concept
through to final de-commissioning, see Figure 2-1. Two integrity stages are defined:
— establish integrity in the concept development, design and construction phases; and
— maintain integrity in the operations phase.
2.1.2.3 This section also provides guidance for extension of this standard in terms of new criteria, etc.
2.2 Safety philosophy structure
2.2.1 General
2.2.1.1 The integrity of the submarine pipeline system is ensured through a safety philosophy integrating
different parts as illustrated in Figure 2-2.
2.2.1.2 The overall safety principles and the arrangement of safety systems shall be in accordance with
DNVGL-OS-A101 and DNVGL-OS-E201. See also [3.4].
2.2.2 Safety objective
2.2.2.1 An overall safety objective shall be established, planned and implemented, covering all phases from
conceptual development until abandonment.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Guidance note:
Most companies have a policy regarding human aspects, environment and financial issues. These are typically on an overall level,
but may be followed by more detailed objectives and requirements in specific areas. These policies should be used as a basis for
defining the safety objective for a specific pipeline system. Typical statements may be:
—
The impact on the environment shall be reduced to as far as reasonably possible.
—
No releases will be accepted during operation of the pipeline system.
—
There shall be no serious accidents or loss of life during the construction period.
—
The pipeline installation shall not, under any circumstances impose any threat to fishing gear.
—
Diverless installation and maintenance.
Statements such as those above may have implications for all or individual phases only. They are typically more relevant for the
work execution (i.e. how the contractor executes his job) and specific design solutions (e.g. burial or no burial). Having defined
the safety objective, it can be a point of discussion as to whether this is being accomplished in the actual project. It is therefore
recommended that the overall safety objective be followed up by more specific, measurable requirements.
If no policy is available, or if it is difficult to define the safety objective, one could also start with a risk assessment. The risk
assessment could identify all hazards and their consequences, and then enable back-extrapolation to define acceptance criteria and
areas that need to be followed up more closely.
The structural failure probability is reflected in the choice of three safety classes (see [2.2.4]). The choice of safety class should
also include consideration of the expressed safety objective.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
Numbers in the figure refers to section number in this standard.
Figure 2-1 Integrity assurance activities during the pipeline system phases
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Figure 2-2 Safety philosophy structure
2.2.3 Systematic review of risks
2.2.3.1 A systematic review shall be carried out at all phases to identify and evaluate threats, the
consequences of single failures and series of failures in the pipeline system, such that necessary remedial
measures can be taken. The extent of the review or analysis shall reflect the criticality of the pipeline system,
the criticality of a planned operation, and previous experience with similar systems or operations. The
uncertainty in the applied risk review model itself shall also be qualified.
Guidance note:
A methodology for such a systematic review is quantitative risk analysis (QRA). This may provide an estimation of the overall risk
to human health and safety, environment and assets and comprises:
—
hazard identification
—
assessment of probabilities of failure events
—
accident developments
—
consequence and risk assessment.
The scope of the systematic review should comprise the entire pipeline system, and not just the submarine pipeline system.
It should be noted that legislation in some countries requires risk analysis to be performed, at least at an overall level to identify
critical scenarios that might jeopardise the safety and reliability of a pipeline system. Other methodologies for identification of
potential hazards are failure mode and effect analysis (FMEA) and hazard and operability studies (HAZOP). Concrete guidance on
critical aspects are given in the individual sections, typically in [X.1.3] where X indicates section.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
2.2.3.2 Special attention shall be given to sections close to installations or shore approaches where there is
frequent human activity and thus a greater likelihood and consequence of damage to the pipeline. This also
includes areas where pipelines are installed parallel to existing pipelines and pipeline crossings.
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2.2.4 Design criteria principles
2.2.4.1 Safety of the pipeline system is ensured by use of a safety class methodology. The pipeline system is
classified into one or more safety classes based on failure consequences, normally given by the content and
location. For each safety class, a set of partial safety factors is assigned to each limit state.
2.2.5 Quality assurance
2.2.5.1 The safety format requires that gross errors (human errors) shall be controlled by requirements for
organisation of the work, competence of persons performing the work, verification of the design, and quality
assurance during all relevant phases.
2.2.5.2 It is assumed that the operator of a pipeline system has established a quality objective. The operator
shall, in both internal and external quality related aspects, seek to achieve the quality level of products and
services intended in the quality objective. Further, the operator shall provide assurance that intended quality
is being, or will be, achieved.
2.2.5.3 Documented quality systems shall be applied by operators and other parties (e.g. design contractors,
manufactures, fabricators and installation contractors) to ensure that products, processes and services will be
in compliance with the requirements. Effective implementation of quality systems shall be documented.
2.2.5.4 Repeated occurrence of non-conformities reflecting systematic deviations from procedures and/or
inadequate workmanship shall initiate:
—
—
—
—
investigation into the causes of the non-conformities
reassessment of the quality system
corrective action to establish possible acceptability of products
preventative action to prevent re-occurrence of similar non-conformities.
Guidance note:
ISO 9000 gives guidance on the selection and use of quality systems.
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2.2.5.5 Quality surveillance in the construction phase shall be performed by the operator or an inspectorate
nominated by the operator. The extent of quality surveillance shall be sufficient to establish that specified
requirements are fulfilled and that the intended quality level is maintained.
2.2.5.6 To ensure safety during operations phase, an integrity management system in accordance with
[11.3] shall be established and maintained.
2.2.6 Health, safety and environment
2.2.6.1 The concept development, design, construction, operation and abandonment of the pipeline system
shall be conducted in compliance with national legislation and company policy with respect to health, safety
and environmental aspects.
2.2.6.2 The selection of materials and processes shall be conducted with due regard to the safety of the
public and employees and to the protection of the environment.
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2.3 Risk basis for design
2.3.1 General
2.3.1.1 The design format is based upon a limit state and partial safety factor methodology, also called load
and resistance factor design format (LRFD). The load and resistance factors depend on the safety class,
which characterizes the consequences of failure.
2.3.2 Categorisation of fluids
2.3.2.1 Fluids to be transported by the pipeline system shall be categorised according to their hazard
potential as given by Table 2-1.
Guidance note:
It is recommended to categorize CO2 pipelines as more severe by category E unless long operational experience exist by the
operator of CO2 pipeline of similar composition and operated in similar manner. Recommended practice for pipelines conveying CO2
is given in DNVGL-RP-F104.
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Table 2-1 Categorisation of fluids
Category
Description
A
Typical non-flammable water-based fluids.
B
Flammable and/or toxic fluids which are liquids at ambient temperature and atmospheric pressure
conditions. Typical examples are oil and petroleum products. Methanol is an example of a flammable and
toxic fluid.
C
Non-flammable fluids which are non-toxic gases at ambient temperature and atmospheric pressure
conditions. Typical examples are nitrogen, carbon dioxide, argon and air.
D
Non-toxic, single-phase natural gas.
E
Flammable and/or toxic fluids which are gases at ambient temperature and atmospheric pressure conditions
and which are conveyed as gases and/or liquids. Typical examples would be hydrogen, natural gas (not
otherwise covered under category D), ethane, ethylene, liquefied petroleum gas (such as propane and
butane), natural gas liquids, ammonia, and chlorine.
2.3.2.2 Gases or liquids not specifically identified in Table 2-1 should be classified in the category containing
fluids most similar in hazard potential to those quoted. If the fluid category is not clear, the most hazardous
category shall be assumed.
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2.3.3 Location classes
2.3.3.1 The pipeline system shall be classified into location classes as defined in Table 2-2.
Table 2-2 Classification of location
Location
Definition
1
The area where no frequent human activity is anticipated along the pipeline route.
2
The part of the pipeline/riser in the near platform (manned) area or in areas with frequent human activity.
The extent of location class 2 should be based on appropriate risk analyses. If no such analyses are
performed a minimum horizontal distance of 500 m shall be adopted.
2.3.4 Safety classes
2.3.4.1 Pipeline design shall be based on potential failure consequence. This is implicit by the concept of
safety class. The safety class may vary for different phases and locations. The safety classes are defined in
Table 2-3.
Table 2-3 Classification of safety classes
Safety class
Definition
Low
Where failure implies insignificant risk of human injury and minor environmental and economic
consequences.
Medium
Where failure implies low risk of human injury, minor environmental pollution or high economic or political
consequences.
High
Classification for operating conditions where failure implies risk of human injury, significant environmental
pollution or very high economic or political consequences.
2.3.4.2 The partial safety factors related to the safety class are given in [5.3.2].
2.3.4.3 For normal use, the safety classes in Table 2-4 apply:
Table 2-4 Normal classification of safety classes
Phase
1)
Fluid category A, C
Fluid category B, D and E
Location class
Location class
1
2
1
2
Temporary
Low
Low
-
-
Operational
Low
Medium
Medium
High
2,3
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1)
Other classifications may exist depending on the conditions and criticality of failure the pipeline. For pipelines where
some consequences are more severe than normal, i.e. when the table above does not apply, the selection of a
higher safety class shall also consider the implication, on the total gained safety. If the total safety increase is
marginal, the selection of a higher safety class may not be justified.
2)
Installation until pre-commissioning (temporary phase) should be classified as safety class Low.
3)
For safety classification of temporary phases after commissioning, special consideration shall be made to the
consequences of failure, i.e. giving a higher safety class than Low.
2.3.5 Reliability analysis
2.3.5.1 As an alternative to the specific LRFD (and ASD) format, a recognised structural reliability analysis
(SRA) based design method may be applied provided that:
— the method complies with DNVGL-RP-C211
— the approach is demonstrated to provide adequate safety for familiar cases, as indicated by this standard.
Reliability based limit state design shall not be used to replace the safety factors for pressure containment
criterion in Sec.5 with the exception of accidental pressure. Accidental limit states shall be designed based
on SRA in line with [5.4.10] ensuring that the overall nominal failure probability complies with the nominal
failure probability target values in this sub-section.
2.3.5.2 Suitably competent and qualified personnel shall perform the structural reliability analysis, and
extension into new areas of application shall be supported by technical verification.
2.3.5.3 As far as possible, nominal target failure probability levels shall be calibrated against identical or
similar pipeline designs that are known to have adequate safety on the basis of this standard. If this is not
feasible, the nominal target failure probability level shall be based on the failure type and safety class as
given in Table 2-5.
Guidance note:
It can be seen as a contradiction that this standard requires a target failure probability one to two orders of magnitude lower for
pressure containment compared to the other limit states/failure modes. The question is really - How to determine acceptable
target failure probabilities for offshore pipelines?
In order to calibrate proper partial safety factors for all limit states, some backward-engineering on target failure probabilities were
performed, see [13.4]. By applying structural reliability analysis on known pipeline designs using known statistical distribution
for the most important stochastic variables, the implicit target probabilities were established for the different limit states. In this
way the target values were established based on an experienced failure rate that was perceived as acceptable to all stakeholders
including the society at large. The work revealed failure probabilities for pressure containment (hoop stress) one to two orders
of magnitude lower than for the other failure modes. This is the main reason for the differences seen in the recent version of the
standard.
The target failure probabilities may also be seen from a practical point of view. The experienced failures for any structures could
be categorised into gross errors also including the unexpected and unknown and failures due to natural variance (structural
reliability). Looking into historical failure rates for offshore pipelines the gross errors dominate. Then one may argue that the target
probability of failure used in structural reliability analyses do not matter that much. However, the target failure of probability with
respect to pressure containment is in some sense in a special position as it is determining the pipe wall thickness. Being stricter
on the target failure probability increases the wall thickness and thus indirectly the robustness towards other failure modes and at
least some gross errors. Relaxing the target failure probability would reduce the robustness and, thus, the expected failure rate
with respect to several failure rates would most likely increase.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e--Guidance note:
Local factors and associated consequences may be e.g. shipping lanes.
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Table 2-5 Nominal annual target failure probabilities per pipeline vs. safety classes
Limit state
category
Limit state
SLS
All
ULS
Safety classes
Low
10
1)
Pressure containment
ALS
5)
-4
10
Medium
-2
to 10
10
-5
-5
10
-3
to 10
4)
High
Very high
-3
-4
10
-6
10
-6
10
-7
to 10
-7
10
-8
to 10
ULS
2)
FLS
All other
10
-3
10
-4
-5
10
-6
10
3)
ALS
1)
The failure probability for the pressure containment (wall thickness design) is one to two order of magnitudes lower
than the general ULS criterion given in this table, in accordance with industry practice and reflected by the ISO
requirements.
2)
The failure probability will effectively be governed by the last year in operation or prior to inspection depending on
the adopted inspection philosophy.
3)
Nominal target failure probabilities can alternatively be one order of magnitude less (e.g. 10
per km) for any running km if the consequences are local and caused by local factors.
4)
See Table F-2.
5)
The target shall be interpret as probability that a failure occurs in the period of one year.
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per pipeline to 10
-5
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SECTION 3 CONCEPT AND DESIGN PREMISE DEVELOPMENT
3.1 General
3.1.1 Objective
3.1.1.1 This section identifies and provides a basis for definition of relevant field development
characteristics. Further, key issues required for design, construction, operation, and abandonment of the
submarine pipeline system are identified.
3.1.2 Application
3.1.2.1 This section applies to submarine pipeline systems which shall be built according to this standard.
3.1.2.2 The design premises outlined in this section should be developed during the conceptual phase and
reviewed and updated when found necessary.
3.1.3 Systematic review
3.1.3.1 The overall requirement to systematic review in Sec.2 shall be reflected in the concept evaluation.
3.1.3.2 Threats identified may typically have impacts on cost, schedule and performance, and may include:
—
—
—
—
—
—
—
scope changes (flow characteristics, throughputs, maturity of technical solutions)
market factors and prices (material, equipment, contractors)
severe weather conditions (delays to marine operations due to limiting weather conditions)
contractor availability and performance (cost, construction delays, quality)
supply and quality of material (delays, performance)
availability and cost of financing (delays, commercial feasibility)
constructability (limited access for installation vessels, simultaneous operations with other installation
activities, vessel capacity and deck space)
— novel technology.
3.1.3.3 Threat identification for the society/safety report
— environmental impact
— impact on other industries
— safety of life.
3.1.3.4 Threats identification on the pipeline may include:
—
—
—
—
environment
third party activities
geo-hazards
flow constraints.
3.1.3.5 Impacts of the identified threats on operation of the submarine pipeline system shall be evaluated.
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3.2 Concept development
3.2.1 Concept development
3.2.1.1 When selecting the submarine pipeline system concept all aspects related to design, construction,
operation and abandonment shall be considered. Due account should be given to identification of potential
aspects which can stop the concept from being realised:
— long lead effects of early stage decisions (e.g. choice of material grade may affect manufacturing aspects
of line pipe, choice of diameter may give restrictions to installation methods etc.)
— life cycle evaluations (e.g. maintenance activities etc.)
— installation aspects for remote areas (e.g. non-availability of major installation equipment or services and
weather issues).
3.2.1.2 Data and description of field development and general arrangement of the pipeline system shall be
established.
3.2.1.3 The data and description should include the following, as applicable:
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
safety objective
environmental objective
location, inlet and outlet conditions
pipeline system description with general arrangement and battery limits
functional requirements including field development restrictions, e.g., safety barriers and subsea valves
installation, repair and replacement of pipeline elements, valves, actuators and fittings
project plans and schedule, including planned period of the year for installation
design life including specification for start of design life, e.g. final commissioning, installation etc.
data of product to be transported including possible changes during the pipeline system's design life
transport capacity and flow assurance
pipeline safety system requirements including process system layout and incidental to design pressure
ratio evaluations
pipeline sizing data
attention to possible code breaks in the pipeline system
geometrical restrictions such as specifications of constant internal diameter, requirement for fittings,
valves, flanges and the use of flexible pipe or risers
relevant pigging scenarios (inspection and cleaning)
pigging fluids to be used and handling of pigging fluids in both ends of pipeline including impact on
process systems
pigging requirements such as bend radius, pipe ovality and distances between various fittings affecting
design for pigging applications
sand production
second and third party activities
restricted access for installation or other activities due to presence of ice.
3.2.1.4 An execution plan should be developed, including the following topics:
— general information, including project organisation, scope of work, interfaces and project development
phases
— contacts with purchaser, authorities, third party, engineering, verification and construction contractors
— legal aspects, e.g. insurance, contracts, area planning, requirements to vessels.
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3.2.1.5 The design and planning for the submarine pipeline system should cover all development phases
including construction, operation and abandonment.
3.3 Design premise
3.3.1 Hydraulic analyses and flow assurance
3.3.1.1 Hydraulic analyses of the pipeline systems should be performed to determine the required diameter
and pressure to meet the transport capacity requirement.
3.3.1.2 A parameter safety envelope (e.g. pressure, temperature, content composition) shall be determined.
The hydraulics of the pipeline system should be analysed to demonstrate that the pipeline system can safely
transport the fluids within this parameter safety envelope. This shall include identification of constraints and
requirements for its operation. This analysis should cover steady-state and transient operating conditions.
The parameter safety envelope shall also include minimum values if applicable.
Guidance note:
Examples of constraints and operational requirements are allowances for pressure surges, prevention of blockage such as caused
by the formation of hydrates and wax deposition, measures to prevent unacceptable pressure losses from higher viscosities
at lower operation temperatures, measures for the control of liquid slug volumes in multi-phase fluid transport, flow regime
for internal corrosion control erosional velocities and avoidance of slack line operations. It includes requirements to insulation,
maximum shut-down times, requirements for heating etc. as well as description of pressure designing cases (e.g. preservation
cases with methanol) with associated temperatures.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e--Guidance note:
Examples of this may be minimum required pressures for pipeline systems that not are designed for the fully external over
pressure.
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3.3.1.3 The hydraulics of the pipeline system shall be analysed to demonstrate that the pipeline control
system and pipeline safety system meet its requirement during start-up, normal operation, shut-down (e.g.
closing of valves) and all foreseen non-intended scenarios. This shall also include determination of required
incidental to design pressure ratio.
3.3.1.4 The hydraulic analyses shall be used to determine the characteristic high design temperature profile
based on conservative insulation values reflecting the variation in insulation properties of coatings and
surrounding seawater, soil and gravel.
3.3.1.5 The hydraulic analyses shall be used to determine the characteristic low design temperature. Benefit
of specifying low temperatures locally due to e.g. opening of valves is allowed and shall be documented e.g.
by hydraulic analyses.
3.3.2 Environmental condition
3.3.2.1 Environmental phenomena that might impair proper functioning of the system or cause a reduction
of the reliability and safety of the system shall be considered, including:
—
—
—
—
—
wind
tide
waves
internal waves and other effects due to differences in water density
current
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—
—
—
—
—
—
ice
earthquake
geotechnical conditions
geomorphology processes
temperature
marine growth (fouling).
3.3.2.2 Recommended practice for principles and methodologies for establishing environmental conditions
and loads is given in DNVGL-RP-C205.
3.3.3 Collection of environmental data
3.3.3.1 The environmental data shall be representative for the geographical areas in which the pipeline
system shall be installed. If sufficient data are not available for the geographical location in question,
conservative estimates based on data from other relevant locations may be used.
3.3.3.2 Statistical data shall be utilised to describe environmental parameters of a random nature (e.g. wind,
waves). The parameters shall be derived in a statistically valid manner using recognised methods.
3.3.3.3 For the assessment of environmental conditions along the pipeline route, the pipeline may be divided
into a number of sections, each of which is characterised by a given water depth, bottom topography and
other factors affecting the environmental conditions.
3.3.3.4 The environmental data to be used in the design of the submarine pipeline system which is
connected to an offshore structure or routed near an offshore structure are in principle the same as the
environmental data used in the design of the offshore structure.
3.3.4 Environmental data
3.3.4.1 The estimated maximum tide shall include both highest astronomic tide and positive storm surge.
Minimum tide estimates should be based upon the lowest astronomic tide and possible negative storm surge.
3.3.4.2 All relevant sources to current shall be considered. This may include tidal current, wind induced
current, storm surge current, density induced current or other possible phenomena. For near-shore regions,
long-shore current due to wave breaking shall be considered. Variations in magnitude with respect to
direction and water depth shall be considered when relevant.
3.3.4.3 In areas where ice may develop or where ice bergs may pass or where the soil may freeze sufficient
statistics shall be established in order to enable calculations of relevant loads.
3.3.4.4 Air and sea temperature statistics shall be provided giving representative high and low design
values.
3.3.4.5 Marine growth on pipeline systems shall be considered, taking into account both biological and other
environmental phenomena relevant for the location.
3.3.5 Pipeline route
3.3.5.1 The pipeline route shall be selected with due regard to safety of the public and personnel, protection
of the environment, and the probability of damage to the pipeline or other facilities. Agreement with relevant
parties should be sought as early as possible. Factors to take into consideration shall, at minimum, include
the following:
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— Environment
—
—
—
—
—
archaeological sites
exposure to environmental loads
areas of natural conservation interest such as oyster beds and coral reefs
marine parks
turbidity flows.
— Seabed characteristics
—
—
—
—
—
uneven seabed
unstable seabed
seabed geotechnical properties (hard spots, soft sediment and sediment transport)
subsidence
seismic activity.
— Facilities
—
—
—
—
—
offshore installations
subsea structures and well heads
existing pipelines and cables
obstructions
coastal protection works.
— Third party activities
—
—
—
—
—
ship traffic
fishing activity
dumping areas for waste, ammunition, etc.
mining activities
military exercise areas.
— Shore crossing
—
—
—
—
—
local constraints
3rd party requirements
environmentally sensitive areas
vicinity to people
limited construction period.
3.3.5.2 Expected future marine operations and anticipated developments in the vicinity of the pipeline shall
be considered when selecting the pipeline route.
3.3.5.3 In-line assemblies should not be located on the curved route sections of the pipeline.
Guidance note:
It is preferred to have a sagbend length of straight section after a curve before the in-line assembly because of potential rotation.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
3.3.5.4 Pipeline ends should be designed with a reasonable straight length ahead of the target boxes.
Curvatures near pipeline ends should be designed with due regard to end terminations, lay method, lay
direction and existing/planned infrastructure.
3.3.6 Route survey
3.3.6.1 Surveys shall be carried out along the total length of the planned pipeline route to provide sufficient
data for design and construction related activities.
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3.3.6.2 The survey corridor shall have sufficient width to define an installation and pipeline corridor which
will ensure safe installation and operation of the pipeline.
3.3.6.3 The required survey accuracy may vary along the proposed route. Obstructions, highly varied seabed
topography, or unusually or hazardous sub-surface conditions may dictate more detailed investigations. The
survey accuracy shall be sufficient for performing the design, construction and operation activities in a safe
manner.
3.3.6.4 Investigations to identify possible conflicts with existing and planned installations and possible
wrecks and obstructions shall be performed. Examples of such installations include other submarine
pipelines, and power and communication cables.
3.3.6.5 The results of surveys shall be presented on accurate route maps and alignments, scale
commensurate with required use. The location of the pipeline and related facilities, together with seabed
properties, anomalies and all relevant pipeline attributes shall be shown. Reference seawater elevation shall
be defined.
3.3.6.6 Additional route surveys may be required at shore crossings to determine:
— nearshore and onshore geology, bathymetry and topography specific to the coastal environment
— environmental conditions caused by adjacent coastal features
— pipeline route alignment and vertical profile to achieve pipeline stability and protection, and minimise
impact on environmental, archaeological sites, people and existing facilities and operations
— the shore crossings construction method, by open-cut trench and cover, horizontal directional drilling,
tunnelling or jetty structure, or a combination of these
3.3.6.7 All topographical features which may influence the stability and installation or influence seabed
intervention of the pipeline shall be covered by the route survey, including:
— obstructions in the form of rock outcrops, large boulders, pock marks, etc., that could necessitate
remedial, levelling or removal operations to be carried out prior to pipeline installation
— topographical features that contain potentially unstable slopes, sand waves, pock marks or significant
depressions, valley or channelling and erosion in the form of scour patterns or material deposits.
3.3.6.8 Areas where there is evidence of increased geological activity or significant historic events that if
re-occurring may impact the pipeline, additional geohazard studies should be performed. Such studies may
include:
—
—
—
—
—
—
—
extended geophysical survey
mud volcanoes or pockmark activity
seismic hazard
seismic fault displacements
possibility of soil slope failure
mudflow characteristics
mudflow impact on pipelines.
3.3.7 Seabed properties
3.3.7.1 Geotechnical characteristics necessary for evaluating the effects of relevant loading conditions shall
be determined for the seabed deposits, including possible unstable deposits in the vicinity of the pipeline. For
guidance on geotechnical investigation for pipelines, see DNVGL-RP-C212.
3.3.7.2 Geotechnical properties may be obtained from generally available geological information, results
from seismic surveys, seabed bathymetry surveys, and geotechnical in-situ tests and laboratory tests on
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sampled soil. Supplementary information may be obtained from visual surveys or special tests, as e.g. pipe
penetration tests.
3.3.7.3 Soil parameters of main importance for the pipeline response are:
— particle size distribution
— strength parameters (intact and remoulded undrained shear strength for cohesive soils, and angle of
internal friction for non-cohesive soils); and
— relevant deformation characteristics.
These parameters should preferably be determined from adequate laboratory tests or from interpretation of
in-situ tests. In addition, classification and index tests should be considered, such as:
—
—
—
—
—
unit weight
water content
liquid and plastic limit
soil mineralogy and chemistry
other relevant tests.
3.3.7.4 Rock parameters of main importance for pipeline response are:
—
—
—
—
rock type and minerology
rock strength and variability in rock strength with depth below seabed
rock erodibility (e.g. potential for catastrophic cliff erosion)
karst features.
3.3.7.5 It is primarily the characteristics of the upper layer of the seabed that determine the response of
the pipeline resting on the seabed. For situations where the top layer comprises a soil, the determination
of soil parameters for these very shallow soils may be relatively more uncertain than for deeper soils. Also
the variations of the top soil between soil testing locations and between tested locations and non-tested
locations add to the uncertainty. Soil parameters used in the design may therefore need to be defined with
upper bound, best estimate and lower bound limits valid within defined areas or sections of the route. The
characteristic value(s) of the soil parameter(s) used in the design shall be in line with the selected design
philosophy accounting for these uncertainties.
Guidance note:
The upper layer may be slurry with a very low strength. In these cases emphasis should also be made to the soil layer underneath.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
3.3.7.6 Since the distance between geotechnical testing locations is often much longer than the length of
the pipeline involved in a particular design situation, one will in such circumstances have to assume that the
geotechnical characteristics for the designs situation is the worst of high and low estimates obtained from
relevant available geotechnical investigation data related to the entire route or to a defined section of the
route.
3.3.7.7 In areas where the seabed material may be subjected to erosion, special studies of the current and
wave conditions near the bottom including boundary layer effects may be required for the on-bottom stability
calculations of pipelines and the assessment of pipeline spans.
3.3.7.8 Additional investigation of the seabed material may be required to evaluate specific scenarios, as for
example:
—
—
—
—
challenges with respect to excavation and burial operations
the probability of the forming of frees-pans caused by scouring during the operational phase
the probability of pipeline self-burial occurring during the operational phase
challenges with respect to pipeline crossings
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— challenges with the settlement of the pipeline system and/or the protection structure at the valve/tee
locations
— possibilities of mud slides or liquefaction as the result of repeated loading
— implications for external corrosion.
3.3.7.9 Recommended practice on pipe-soil interaction and geotechnical surveys is given in DNVGL-RP-F114.
3.4 System design principles
3.4.1 System integrity
3.4.1.1 The pipeline system shall be designed, constructed and operated in such a manner that:
— the specified transport capacity is fulfilled and the flow assured.
— the defined safety objective is fulfilled and the resistance against loads during planned operational
conditions is sufficient.
— the safety margin against accidental loads or unplanned operational conditions is sufficient.
— system layout, including needs for different valves etc., meets the requirements imposed by the
systematic review of the process control.
3.4.1.2 Pipelines in C-Mn steel for potentially corrosive fluids of categories B, D and E (see [2.3]) should
be designed for inspection pigging. In cases where the pipeline design does not allow inspection pigging, an
analysis shall be carried out in accordance with recognised procedures to document that the risk of failure
leading to a leak is acceptable. For corrosive fluids of other categories the benefit of inspection pigging on
operational reliability shall be evaluated.
3.4.1.3 The need for in-line cleaning and/or inspection, involving the presence of appropriate pig launcher/
receiver should be determined in the design phase.
3.4.1.4 The possibility of changes in the type or composition of fluid to be transported during the lifetime of
the pipeline system shall be assessed in the design phase.
3.4.1.5 Any re-qualification deemed necessary due to changes in the design conditions shall take place in
accordance with provisions set out in Sec.11.
3.4.2 Pipeline control and safety system
-2
3.4.2.1 The incidental pressure is defined as having an annual probability of exceedance less than 10 (a
probability of being exceeded within a year). If the pressure probability density function does not have a
-2
monotonic decay beyond 10 the pressure exceeding the incidental pressure shall be checked as accidental
loads in compliance with [5.4.10].
Guidance note:
Examples of pressure probability density distributions are given in Figure 3-1. An example of a pipeline system with a two peak
distribution may be a pipeline system protected by a HIPP system.
The 100-year value, the incidental pressure (see mark in Figure 3-1), will be used for normal design for both two peak distributions
and single peak distributions. For two peak distributions the second peak pressure shall also be checked for accidental limit state in
accordance with [5.4.10] (see pressure of 1200 in Figure 3-1).
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Guidance note:
When the submarine pipeline system is connected to another system with different pressure definition the pressure values may be
different in order to comply with the requirements of this sub-section, i.e. the design pressure may be different in two connected
systems. The conversion between the two system definitions will often then be based on that the incidental pressures are equal.
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Figure 3-1 Pressure distribution function with two peak distribution
3.4.2.2 The submarine pipeline system shall have a specified incidental pressure or be split into different
sections with different specified incidental pressures. These should all be defined at a defined reference
elevation.
3.4.2.3 To fulfil the requirements in [3.4.2.1] and [3.4.2.2] a pipeline protection system may be required.
This comprises the pipeline control system (PCS) and pipeline safety system (PSS).
Guidance note:
An example of situations where a pipeline control and safety system may not be required is if full shut-in pressure including
dynamic effects, is used as incidental pressure.
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3.4.2.4 The purpose of the PCS is to maintain the operating parameters within the operating envelope during
normal operation e.g. to ensure that the local design pressure is not exceeded at any point in the submarine
pipeline system. The PCS should operate automatically. Due account shall be given to the tolerances of the
PCS and its associated instrumentation, see Table 1-8. Hence, the maximum allowable operating pressure
(MAOP) is equal to the design pressure minus the PCS operating tolerance.
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3.4.2.5 The PCS could be included as a risk reducing measure provided that this system is independent of
PSS and further complies with the following:
— The PCS is not included as a part of the demand rate defined for the PSS
— Failure of an automatic PCS shall not affect the alarm system needed for human intervention.
— The risk reduction factor taken shall be smaller than 10 unless the PCS is built in accordance with safety
system standards, e.g., IEC61511. The assessment of risk reduction factor and evidence to support the
assessment shall be made according to the requirements in IEC61511.
— Risk reduction from human intervention, in addition to PCS, assumes that actions are based upon
information from systems independent of PCS and PSS. The total risk reduction factor resulting from
Human Intervention and the PCS shall be less than 100.
3.4.2.6 The purpose of the PSS is to protect the submarine pipeline system by limiting the operating
parameters within the parameter safety envelope during incidental operation, e.g. to ensure that the local
incidental pressure is not exceeded at any point in the pipeline system in the event of failure of the PCS.
The PSS shall operate automatically. Due account shall be given to the tolerances of the PSS. Hence, the
maximum allowable incidental pressure is equal to the incidental pressure minus the PSS operating tolerance.
3.4.2.7 The PCS is a basic process control system as defined by IEC 61511. The Pipeline Safety shall comply
-3
with the requirements of IEC 61511. PSSs required with a probability of failure on demand of less than 10
shall consist of two independent systems.
The requirements for the level of risk reduction to be provided by the PSS, the SIL Level shall be derived
according to the requirements of [5.4.10] and not from a risk assessment. Figure B-6 provides further
guidance.
3.4.2.8 The PSS may consist of pressure relief devices (ISO 4126) and/or safety instrumented systems, see
IEC 61511. Pressure relief valves are considered fulfilling requirements to the PSS if these are designed and
maintained to relieve the required discharge capacity at a pressure not exceeding the maximum allowable
incidental pressure.
3.4.2.9 A design pressure may be defined for each incidental pressure. The incidental to design pressure
ratio shall be selected such that the pipeline control and safety system meet the requirements in [3.4.2.1]
and [3.4.2.2]. Typical and minimum incidental to design ratios are given in Table 3-1. When design pressure
is used for structural design purpose, this shall be minimum 91% of the incidental pressure.
Guidance note:
This standard use incidental pressure in all limit states. Other referenced standards or recommended practices (e.g. for
components) may use design pressure instead. For such applications, the design pressure shall be the higher of pli/γinc and 0.91·
pli.
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Table 3-1 Incidental to design pressure ratios, γinc
Condition or pipeline system
γinc
Typical pipeline system
1.10
Minimum, except for below
1.05
When design pressure is equal to full shut-in pressure including dynamic effects
1.00
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3.4.3 External corrosion control
3.4.3.1 For the selection and detailed design of external corrosion control, the following conditions relating to
the environment shall be defined, in addition to those mentioned in [3.3.2.1]:
— exposure conditions, e.g. burial, rock dumping, etc.
— sea water and soil resistivity.
3.4.3.2 Other conditions affecting external corrosion which shall be defined are:
— temperature profiles (e.g. average, characteristic high design) along the pipeline and through the pipe
wall thickness
— pipeline fabrication and installation procedures
— requirements for mechanical protection, submerged weight and thermal insulation during operation
— design life
— selected coating and cathodic protection system.
3.4.3.3 Special attention should be given to the shore crossing zone and interaction with relevant cathodic
protection system for onshore vs. offshore pipeline sections.
3.4.3.4 The impact from third party activities on the external pipeline condition, as mentioned in [3.3.5.1]
should be considered.
3.4.4 Internal construction conditions
3.4.4.1 A description of the internal pipeline conditions during the construction phase shall be prepared (this
includes storage, construction, installation, pressure testing and commissioning). The duration of exposure
to sea water or humid air, and the need for using inhibitors or other measures to control corrosion shall be
considered.
3.4.5 Internal corrosion control
3.4.5.1 In order to assess the need for internal corrosion control, including corrosion allowance and provision
for inspection and monitoring, the following conditions shall be defined:
— operating temperature/pressure profiles along the pipeline including expected variations during the design
life
— flow velocity and flow regime
— fluid composition (initial and anticipated variations during the design life) with emphasis on potentially
corrosive components (e.g. hydrogen sulphide, carbon dioxide, water content and expected content of
dissolved salts in produced fluids, residual oxygen and active chlorine in sea water)
— chemical additions and provisions for periodic cleaning
— provision for inspection of corrosion damage and expected capabilities of inspection tools (i.e. detection
limits and sizing capabilities for relevant forms of corrosion damage)
— the possibility of erosion by any solid particles in the fluid shall be considered. Recommended practice for
erosive wear in piping systems is given in DNVGL-RP-O501 Sec.3.
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SECTION 4 DESIGN - LOADS
4.1 General
4.1.1 Objective
4.1.1.1 This section defines the loads to be checked by the limit states in Sec.5. This includes:
—
—
—
—
—
—
load scenarios
categorisation of loads
design load effects
characteristic load
load effect factor combinations
load effect calculations.
4.1.2 Application
4.1.2.1 This section applies to all parts of the submarine pipeline system.
4.1.3 Systematic review
4.1.3.1 The overall requirement to systematic review in Sec.2 implies for this section that a review of loads
based on their uncertainty and importance for the different limit states shall be performed.
4.1.4 Load scenarios
4.1.4.1 All loads and forced displacements which may influence the pipeline shall be taken into account.
For each cross section or part of the system to be considered and for each possible mode of failure to be
analysed, all relevant combinations of loads which may act simultaneously shall be considered.
4.1.4.2 The most unfavourable load scenario for all relevant phases and conditions shall be considered.
Typical scenarios to be covered in the design are:
—
—
—
—
—
—
—
transportation
installation
as laid
water filled
system pressure test
operation
shut-down.
4.1.5 Categorisation of loads
4.1.5.1 The objective of the categorisation of loads into the different load categories is to relate the load
effect to the associated uncertainties.
4.1.5.2 Unless the load is categorised as accidental it shall be categorised as:
— functional load,
— environmental load or
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— interference load.
The load categories are described in [4.2], [4.3] and [4.5] below. Construction loads shall be categorised into
the above loads and are described in [4.4]. Accidental loads are described in [4.6].
4.2 Functional loads
4.2.1 General
4.2.1.1 Loads arising from the physical existence of the pipeline system and its intended use shall be
classified as functional loads.
4.2.1.2 Effects from the following phenomena are the minimum to be considered when establishing
functional loads:
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
weight
reactions from installation vessel (tensioners, straightener, stinger/rollers)
external hydrostatic pressure
static hydrodynamic forces during installation
reactions from soil in sag bend
internal pressure
temperature of contents
pre-stressing
reactions from components (flanges, clamps etc.)
permanent deformation of supporting structure
cover (e.g. soil, rock, mattresses, culverts)
reaction from seabed (friction and rotational stiffness)
permanent deformations due to subsidence of ground, both vertical and horizontal
permanent deformations due to frost heave
changed axial friction due to freezing
possible loads due to ice interference, e.g. bulb growth around buried pipelines near fixed points (in-line
valves/tees, fixed plants etc.), drifting ice etc.
— loads induced by pigging operations.
4.2.1.3 The weight shall include weight of pipe, buoyancy, contents, coating, anodes, marine growth and all
attachments to the pipe.
4.2.1.4 End cap forces due to pressure shall be considered, as well as any transient pressure effects during
normal operation (e.g. due to closure of valves).
4.2.1.5 Temperature due to internal fluid and external environmental shall be determined and corresponding
temperature profiles for the following scenarios:
— the maximum and minimum design (100-year return values) temperature during operation
— representative temperatures during operation
— representative temperatures during installation, as-laid, water filled and system pressure test.
Guidance note:
The temperature is normally determined for the pipe steel (to be used for structural purpose) but may also be required for anodes,
coating etc.
The selection of design or operational temperature is given by Table 4-3.
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4.2.1.6 Local minimum temperature profiles, which may be caused by e.g. sudden shut-downs, may be
applied. This will typically be relevant to defined components and sections of the pipeline (e.g. spots around
valves).
4.2.1.7 Fluctuations in temperature shall be taken into account when checking fatigue strength.
4.2.1.8 For expansion analyses, the temperature difference relative to laying shall be considered. The
temperature profile shall be applied.
4.2.1.9 Pre-stressing, such as permanent curvature or a permanent elongation introduced during
installation, shall be taken into account if the capacity to carry other loads is affected by the pre-stressing.
Pretension forces induced by bolts in flanges, connectors and riser supports and other permanent
attachments, shall be classified as functional loads.
4.2.1.10 The soil pressure acting on buried pipelines shall be taken into account if significant.
4.2.2 Pressure loads
4.2.2.1 The following internal pressures shall be defined at a certain defined reference level; system test
pressure, operating pressure (if relevant), design pressure (if applicable), and incidental pressure, see
[3.4.2] for definitions and Table 1-8. These pressures are summarised in Table 4-1.
Guidance note:
The incidental pressure is defined in terms of exceedance probability within a year. The ratio between the incidental pressure and
the design pressure, see Table 3-1, is determined by the accuracy and speed of the pipeline safety system. When the pressure
source is given (e.g. well head shut-in pressure) this may constitute the selection of the incidental pressure. The design pressure
can then be established based on the pipeline safety system. When transport capacity requirement constitutes the design premise
this may give the design pressure and the incidental pressure can then be established based on the pipeline safety system.
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Table 4-1 Pressure terms
Pressure
Abbreviations
Symbol
Description
Mill test
-
Ph
Hydrostatic test pressure at the mill, see [7.5].
System test
-
Pt
The pressure to which the complete submarine pipeline system is
tested to prior to commissioning, see [5.2.2].
Incidental
-
Pinc
MAIP
-
-
PD
MAOP
-
Maximum allowable
incidental
Design
Maximum allowable
operating
Maximum pressure (100-year value) the submarine pipeline system
is designed to withstand, see [3.4.2].
Maximum allowable incidental pressure is equal to the incidental
pressure minus the pipeline safety system (PSS) operating tolerance.
The maximum pressure during normal operation that the pipeline
control system (PCS) allows.
Maximum allowable operating pressure is equal to the design
pressure minus the pipeline control system (PCS) operating
tolerance, and is hence the upper limit of the pipeline control system.
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4.2.2.2 The local pressure is the internal pressure at a specific point based on the reference pressure
adjusted for the fluid column weight due to the difference in elevation. It can be expressed as:
(4.1)
(4.2)
(4.3)
where:
p li
p inc
ρcont
g
h ref
hl
p lt
pt
ρt
pd
γinc
= the local incidental pressure
= the incidental reference pressure at the reference elevation
= the density of the relevant content of the pipeline
= the gravity
= the elevation of the reference point (positive upwards)
= the elevation of the local pressure point (positive upwards)
= the local system test pressure
= the system test reference pressure at the reference elevation
= the density of the relevant test medium of the pipeline
= the design pressure at the pressure reference elevation
= the incidental to design pressure ratio.
4.2.2.3 In cases where external pressure increases the capacity, the external pressure shall not be taken
as higher than the water pressure at the considered location corresponding to low astronomic tide including
possible negative storm surge.
4.2.2.4 In cases where the external pressure decreases the capacity, the external pressure shall not be
taken as less than the water pressure at the considered location corresponding to high astronomic tide
including storm surge.
4.3 Environmental loads
4.3.1 General
4.3.1.1 Environmental loads are defined as those loads on the pipeline system which are caused by the
surrounding environment, and that are not otherwise classified as functional or accidental loads.
4.3.1.2 Recommended practice for calculation of characteristic environmental loads is given in DNVGL-RPC205.
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4.3.2 Wind loads
4.3.2.1 Wind loads shall be determined using recognised theoretical principles. Alternatively, direct
application of data from adequate tests may be used.
4.3.2.2 The possibility of vibrations and instability due to wind induced cyclic loads shall be considered (e.g.
vortex shedding).
4.3.3 Hydrodynamic loads
4.3.3.1 Hydrodynamic loads are defined as flow-induced loads caused by the relative motion between the
pipe and the surrounding water.
4.3.3.2 All relevant sources for hydrodynamic loads shall be considered. This may include waves, current,
and relative pipe motions and indirect forces e.g. caused by vessel motions.
4.3.3.3 The following hydrodynamic loads shall be considered:
—
—
—
—
drag and lift forces which are in phase with the absolute or relative water particle velocity
inertia forces which are in phase with the absolute or relative water particle acceleration
flow-induced cyclic loads due to vortex shedding, galloping and other instability phenomena
buoyancy variations due to wave action.
Guidance note:
Research into the hydrodynamic coefficients for open bundles and piggy-back lines indicates that the equivalent diameter approach
may be nonconservative, and a system specific computational fluid dynamics (CFD) analysis may be required to have a robust
design.
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4.3.3.4 The applied wave theory shall be capable of describing the wave kinematics at the particular water
depth in question including surf zones hydrodynamics where applicable. The suitability of the selected theory
shall be demonstrated and documented.
4.3.3.5 The current-induced drag and lift forces on the submarine pipeline system shall be determined and
combined with the wave-induced forces using recognised theories for wave- current interaction. A vector
combination of the current and wave-induced water particle velocities may be used, however, calculation of
the total particle velocities and accelerations based upon more exact theories on wave-current interaction is
preferable.
4.3.3.6 Data from model testing or acknowledged industry practice may be used in the determination of the
relevant hydrodynamic coefficients.
4.3.3.7 Consideration shall be given to wave direction, short crested waves, wave refraction and shoaling,
shielding and reflecting effects.
4.3.3.8 Variations in current velocity magnitude and direction as a function of water depth shall be
considered.
4.3.3.9 Where parts of the pipeline system are positioned adjacent to other structural parts, possible effects
due to disturbance of the flow field shall be considered when determining the wave and/or current actions.
Such effects may cause an increased or reduced velocity, or dynamic excitation by vortices being shed from
the adjacent structural parts.
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4.3.3.10 If parts of the submarine pipeline system are built up of a number of closely spaced pipes, then
interaction and solidification effects shall be taken into account when determining the mass and drag
coefficients for each individual pipe or for the whole bundle of pipes. If sufficient data is not available, largescale model tests may be required.
4.3.3.11 For pipelines on or close to a fixed boundary (e.g. pipeline spans), lift forces perpendicular to the
axis of the pipe and perpendicular to the velocity vector shall be taken into account (possible vortex induced
vibrations).
4.3.3.12 In connection with vortex shedding-induced transverse vibrations, potential increase in drag
coefficient shall be taken into account.
4.3.3.13 Possible increased waves and current loads due to presence of Tee’s, Y’s or other attachments shall
be considered.
4.3.3.14 The increased loads from marine growth shall be considered as follows:
— Increased drag/lift area due to the marine growth
— Increased pipe surface roughness and resulting increase in drag coefficient and reduced lift coefficient
— Any beneficial effect of the marine growth should be ignored in stability analyses
4.3.3.15 Tide loads shall be considered when the water depth is a significant parameter, e.g. for the
establishment of wave actions, pipe lay operation particularly near shore approaches/landfalls, etc.
4.3.4 Ice loads
4.3.4.1 In areas where ice may develop or drift, the possibility of ice loads on the pipeline system shall be
considered.
Guidance note:
Ice loads may be due to ice frozen on the pipeline system itself, or partly due to floating ice, or combination of these two.
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4.3.4.2 The possibility of ice scouring and impacts from drifting ice shall be considered for shore approaches
and areas where ice may interfere with the seabed and the submarine pipeline system.
4.3.4.3 Increased hydrodynamic loading due to presence of ice shall be considered.
4.3.4.4 In case of ice frozen to parts of the submarine pipeline system or vessels, (e.g. due to sea spray) the
following forces shall be considered:
—
—
—
—
weight of the ice
impact forces due to thaw of the ice
forces due to expansion of the ice
increased wind, waves and current forces due to increased exposed area.
4.3.4.5 Forces from floating ice shall be calculated according to recognised theory. Due attention shall be
paid to the mechanical properties of the ice, contact area, shape of structure, direction of ice movements,
etc. The oscillating nature of the ice forces (built-up of lateral force and fracture of moving ice) shall be taken
into account. When forces due to lateral ice motion will govern structural dimensions, model testing of the
ice-structure interaction may be required.
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4.3.5 Earthquake
4.3.5.1 Load imposed by earthquake, either directly or indirectly (e.g. due to failure of pipeline gravel
supports), shall be classified as accidental or environmental loads, depending on the probability of
earthquake occurrence in line with accidental loads in [4.6].
4.3.6 Characteristic environmental load effects
4.3.6.1 The characteristic environmental load and the corresponding load effect depend on if the scenario
can be classified as:
— a weather restricted condition, or
— an unrestricted condition (temporary condition or permanent condition).
Figure 4-1outlines the procedure for assessing environmental loads.
For a weather restricted operation, the environmental load is the minimum of the determined Operation limit
(OPLIM) The operation limit may be defined by maximum allowed structural response (e.g. local buckling
in the sag bend), anchor handling capability, safe working conditions on deck, assistance system or any
limitations identified in HAZOP. In case operation limits are stricter for ceasing the operation than for normal
laying this should be evaluated in detail. The operation limit is then dependent on vessels and equipment
used.
For a non-weather restricted operations the environmental load is based on environmental statistics and
therefore independent on vessel and equipment.
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Figure 4-1 Determination of characteristic environmental load
4.3.6.2 Weather restricted operations may start-up based upon reliable weather forecast less than the
operation limit. Uncertainty in the weather forecast for the operational period shall be considered.
Guidance note:
For weather restricted operations and example of how to account for the uncertainty in weather forecast reference is made to
DNVGL-ST-N001.
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4.3.6.3 Operations with a reference period (TR) less than 96 hours and a planned operation period (TPOP)
less than 72 hours can be defined as weather restricted. The operation reference period (TR) is the planned
operation period (TPOP) including contingency time, (TC).
4.3.6.4 An operation can be defined as weather restricted operation even if the planned operation time
exceeds 72 hours provided that the operation can be interrupted and put into a safe condition within the
maximum allowable period for a weather restricted operation. The reference period for such operations is
defined as the planned operation period for ceasing the operation, (T’POP), including the contingency time for
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ceasing the operation (T’C). The planned operation period for ceasing the operations is defined as the time to
safely cease the operation (TSafe) and the weather forecast intervals (TWF).
4.3.6.5 An operation can be defined as a temporary condition if the duration is less than 6 months unless
defined as weather restricted conditions. The environmental load effect for temporary conditions shall be
taken as the 10-year return period for the actual season.
Guidance note:
Conditions exceeding 6 months but no longer than 12 months may occasionally be defined as temporary conditions.
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4.3.6.6 Conditions not defined as weather restricted conditions or temporary conditions shall be defined as
permanent conditions. The environmental load effect for permanent conditions shall be taken as the 100-year
return period.
4.3.6.7 When considering the environmental design load the most unfavourable relevant combination,
position and direction of simultaneously acting environmental loads shall be used in documenting the
integrity of the submarine pipeline system. Functional loads (see [4.2]), interference loads (see [4.5]) and
accidental loads (see [4.6]) shall be combined with the environmental loads as appropriate, see Table 4-3.
4.3.6.8 The characteristic environmental load effect for installation, LE, is defined as the most probable
largest load effect for a given seastate and appropriate current and wind conditions given by:
(4.4)
where:
F(LE)
is the cumulative distribution function of LE, and N is the number of load effect cycles in a sea-state
of a duration not less than 3 hours.
4.3.6.9 The most critical load effect combination for the relevant return period shall be used. When the
correlations among the different environmental load components (i.e. wind, wave, current or ice) are
unknown the characteristic combined environmental loads in Table 4-2 may be used.
Table 4-2 Combinations of characteristic environmental loads in terms of return period
Wind
Waves
Current
Ice
1)
Earthquake
Permanent condition
100-year
100-year
10-year
10-year
10-year
100-year
10-year
10-year
10-year
10-year
10-year
10-year
100-year
100-year
2)
Temporary condition
10-year
10-year
1-year
1-year
1-year
10-year
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1-year
1-year
1-year
1-year
1-year
1-year
10-year
2)
10-year
1)
This is in compliance with ISO 16708, but in conflict with ISO 13623 in case the design life is less than 33 years.
2)
Special attention shall be given to potential waves or current induces by earthquakes.
4.4 Construction loads
4.4.1 General
4.4.1.1 Loads which arise as a result of the construction and operation of the submarine pipeline system
shall be classified into functional and environmental loads.
4.4.1.2 Construction loads include:
— stacking of pipes
— pipe transportation loads
— handling of pipe and pipe sections, e.g. lifting of pipe, pipe joints, pipe strings and pipe spools, and reeling
of pipe strings
— static and dynamic installation loads
— pull-in at landfalls, tie-ins, trenching etc.
— pressure testing
— commissioning activities, e.g. increase in pressure differential due to vacuum drying
— dynamic loads from pre-commissioning activities, e.g. flooding and de-watering with pigs.
4.4.1.3 Inertia loads due to sudden water filling, excessive deformation in overbend and sagbend, and forces
due to operation errors or failures in equipment that could cause or aggravate critical conditions shall be
considered, see [10.1.3].
Guidance note:
The design criteria for such considerations will depend on the likelihood of the scenario. In case the likelihood is less than once in
hundred years, it can be considered as an accidental limit state and be checked in accordance with [5.4.10], else a normal ULS
check apply.
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4.4.1.4 For construction loads imposed by geometrical tolerances, extreme tolerances may be taken as
mean ± 3 standard deviations of the combined tolerances.
4.5 Interference loads
4.5.1 General
4.5.1.1 Loads which are imposed on the pipeline system from 3rd party activities shall be classified as
interference loads. Typical interference loads include trawl interference, anchoring, vessel impacts and
dropped objects.
4.5.1.2 The requirement for designing the submarine pipeline system for interference loads shall be
determined based upon interference frequency studies and assessment of the potential damage. If the
-2
probability of occurrence is less than 10 within a year the load shall be classified as accidental load, see
[4.6].
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4.5.1.3 The trawling loads can be divided in accordance with the three crossing phases:
— Trawl impact, i.e. the initial impact from the trawl board or beam which may cause local dents on the pipe
or damage to the coating.
— Over-trawling, often referred to as pull-over, i.e. the second phase caused by the wire and trawl board or
beam sliding over the pipe. This will usually give a more global response of the pipeline.
— Hooking, i.e. the trawl board is stuck under the pipe and in extreme cases, forces as large as the breaking
strength of the trawl wire are applied to the pipeline.
Each of the three types of trawling loads shall be classified as an ULS or an ALS dependent on their
frequency. Hooking becomes then often an accidental load.
4.5.1.4 Recommended practice for calculations of trawl interference loads is given in DNVGL-RP-F111 Sec.4.
4.5.1.5 The trawl impact energy shall be determined considering, as a minimum:
— the trawl gear mass and velocity
— the effective added mass and velocity.
The impact energy shall be used to determine the required testing energy for testing for the coating and
possible denting of the pipeline wall thickness. In case piggy-back lines these shall also have adequate safety
against trawl impacts.
4.5.1.6 Other 3rd party interference loads shall be calculated using recognised methods.
4.6 Accidental loads
4.6.1 General
4.6.1.1 Loads which are imposed on a pipeline system under abnormal and unplanned conditions and with a
-2
probability of occurrence less than 10 within a year shall be classified as accidental loads.
4.6.1.2 Typical accidental loads can be caused by:
—
—
—
—
—
—
—
—
—
—
extreme wave and current loads
vessel impact or other drifting items (collision, grounding, sinking, iceberg)
dropped objects
infrequent internal over pressure (e.g. in case of malfunction of HIPPS)
seabed movement and/or mud slides
explosion
fire and heat flux
accidental water filling due to wet buckle
operational malfunction
dragging anchors.
4.6.1.3 Recommended practice for size and frequency of accidental loads is given in DNVGL-RP-F107.
4.7 Design load effects
4.7.1 General
4.7.1.1 A load effect is the resulting cross-sectional loads arising as response to applied loads (e.g. weight,
pressure, drag).
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4.7.1.2 The magnitude of a time variant load effect to be used in a limit state criterion is defined by its
probability of being exceeded, the characteristic load effect.
4.7.2 Characteristic load
4.7.2.1 The characteristic load effect is a quantified load effect to be used in the design load effect
calculation. The characteristic load for time invariant loads is the nominal (average) load. The characteristic
load for time variant loads is given in [4.3.6].
4.7.2.2 The characteristic load effect is composed of contributions of functional, environmental and
interference load effects.
4.7.2.3 For non-weather restricted operations, the characteristic load shall be the most critical 100-year load
effect
Guidance note:
The 100-year load effect implies a probability of exceedance less than 10
-2
within a year.
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4.7.2.4 The most critical 100-year load effect is normally governed by extreme functional, extreme
environmental, extreme interference or accidental load effect. Unless special evaluation is carried out to
identify the most critical 100-year load effect, the characteristic load effects in Table 4-3 shall be used.
4.7.2.5 In addition to the characteristic loads defined above, the fatigue load case shall also be checked, see
Table 4-3.
Table 4-3 Characteristic loads
Load effect factor
1)
combination
Extreme Load
Functional load effect
Environmental load
effect
Interference load
effect
Fatigue load effect
5)
Accidental load effect
a, b
Functional
load
100-year
Environmental load
Interference
load
Accidental load
1-year
Associated
NA
Associated
NA
2)
3)
100-year
3)
Associated
UB
NA
a, b
Associated
b
Associated
4)
c
Associated
Associated
Associated
NA
d
Associated
Associated
Associated
BE
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Characteristic load definition:
— n-year: most probable maximum in n years
— UB: upper bound
— BE: best estimate.
1)
The referred load effect factor combinations are given in Table 4-4.
2)
This will normally be equivalent to an internal pressure equal to the local incidental pressure combined with
expected associated values of other functional loads.
3)
This will normally be equivalent to an internal pressure and temperature not less than the operating pressure and
the operating temperature profiles.
4)
As defined in Table 4-2.
5)
The fatigue load cases are;
a)
cyclic functional loading (start-up and shut-down, pressure and temperature cycles shall be represented),
b)
random environmental load (e.g. wave and current spectra, conservative pressure and temperature for the
fatigue damage shall be used) and
c)
repeated interference loading (conservative pressure and temperature for the fatigue damage shall be used)
4.7.3 Design load effect
4.7.3.1 Each limit state, see [5.4], shall be checked for the design load effect.
4.7.3.2 The design load effect can generally be expressed in the following format:
(4.5)
In specific forms, this corresponds to:
(4.6)
(4.7)
(4.8)
Guidance note:
The load combinations to the left are referred to explicitly in the limit state criteria, e.g. Equation (5.19).
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4.7.3.3 The design load effect shall be calculated for the characteristic load (see [4.7.2]) for all relevant load
effect combinations and corresponding load effect factors in Table 4-4.
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Guidance note:
The partial safety factors in this standard have been determined by structural reliability methods to a pre-defined failure
probability. Structural reliability calculations differentiate between single joint failures (local checks) and series system failures
(system effects).
These two kinds of scenarios are expressed as two different load effect combinations:
a)
shall only be considered for scenarios where system effects are present
b)
for local scenarios and shall always be considered.
When system effects are present, the pipeline will fail at its weakest point. Hence, the likely load shall be combined with the
extreme low resistance. Applied to pipelines system effect can be expressed as the weakest link principle (where the chain gets
weaker the longer the chain is). This is characterised by that the whole pipeline is exposed to the same load over time.
Applied to pipelines, system effects are present for:
—
pressure containment
—
collapse, in as installed configuration
—
installation.
The first two are handled by the use of thickness t1. This is also why thickness t2 and not t1 is used for the burst capacity in the
local buckling for pressurised pipes, since it is a local check.
Regarding installation, an extreme environmental load is not likely to occur when the weakest pipe section is at the most exposed
location indicating that system effects not are present. However, combined with a more representative environmental load (in the
extreme case, flat sea), the whole pipeline will undergo the same deformation over time, hence, having a system effect present.
In Table 4-4, load effect factor combination a has a load effect factor of 1.2 for the functional load to cover the system effect
combined with a 0.7 load effect factor for the extreme environmental load giving a more representative environmental load,
applicable for the above.
Another example of where system effects are present is for reeling where the whole pipe is exposed to the same deformation
(neglecting the variation in drum diameter increase). For this application, a condition load factor of 0.82 applies, giving the total
load effect factor of 1.2 × 0.82 close to unity.
Hence, load combination b shall always be checked while load combination a normally is checked for installation only.
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Table 4-4 Load effect factor combinations
Limit state/load
combination
ULS
Load effect combination
Functional
1)
loads
γ
a
System check
b
Local check
2)
Environmental load
F
γ
E
Interference
loads
γ
F
1.2
0.7
1.1
1.3
1.1
FLS
c
1.0
1.0
1.0
ALS
d
1.0
1.0
1.0
Accidental loads
γ
A
1.0
1)
If the functional load effect reduces the combined load effects, γF shall be taken as 1/1.1.
2)
This load effect factor combination shall only be checked when system effects are present, i.e. when the major part
of the pipeline is exposed to the same functional load. This will typically only apply to pipeline installation.
4.7.3.4 The condition load effect factor applies to the conditions in Table 4-5. Condition load effect factors
are in addition to the load effect factors and are referred to explicitly in Equation (4.5) - Equation (4.8).
Guidance note:
Uneven seabed refers to pipeline resting on the seabed and not to installation on un-even seabed. Several condition factors may be
required simultaneously, e.g. for pressure testing of pipelines on seabed, the resulting condition factor will be 1.07 · 0.93 = 1.00.
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Table 4-5 Condition load effect factors, γC
Condition
γc
Pipeline resting on uneven seabed
J-tube pull-in
1.07
1
0.82
System pressure test
0.93
S-lay installation; Local buckling load control check on stinger
2
0.80
2
Reeling installation; Displacement controlled check, seamless pipes
0.77
Reeling installation; Displacement controlled check, welded pipes
2,3
0.82
Otherwise
1.00
1)
Load combination a needs not to be analysed
2)
For installation both load combination a and b shall always be analysed, see also [5.8.2]
3)
This factor has not been re-assessed but reflects the less uniform material properties around the circumference
4.7.4 Load effect calculations
4.7.4.1 The load effect calculations shall be based on accepted principles of statics, dynamics, strength of
materials and soil mechanics.
4.7.4.2 Industry recognised calculations tools, or tools documented to provide corresponding results, should
be used for design and construction analyses of the submarine pipeline system.
4.7.4.3 Model tests may be used in combination with, or instead of, theoretical calculations. In cases where
theoretical methods are inadequate, model or full-scale tests may be required.
4.7.4.4 The dynamic effect shall be taken into account when determining responses to dynamic loads.
4.7.4.5 Load effects shall be split into functional, environmental, interference and accidental load effects.
4.7.4.6 The effect of statistical uncertainty due to the amount and accuracy of data shall be assessed and, if
significant, shall be included in the evaluation of the characteristic load effect.
4.7.4.7 Load effect calculation should be performed applying nominal (non-corroded) cross-section values
unless otherwise required by the standard or recommended practice. For displacement controlled conditions
this may be non-conservative and should be evaluated. For pipelines with internal clad or liner the bending
stiffness contribution should be included in the load effect calculations.
4.7.4.8 Special attention shall be given to ensure that conservative load effect calculations are performed,
implying that the applied cross-section values are conservative. In case larger positive wall thickness
tolerances are agreed (see Table 7-20 and Table 7-21) it should be noted that larger steel cross-sectional
area will generate larger expansion forces.
4.7.4.9 The effective axial force that determines the global response of a pipeline is denoted S. Counting
tensile force as positive:
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(4.9)
4.7.4.10 The effective axial force of a totally restrained pipe in the linear elastic stress range based on thick
wall stress formulation is:
(4.10)
where:
H
= effective (residual) lay tension. The effective axial force in the as-laid condition when the pipe
temperature and pressure is equal to as during laying.
Δ pi
ΔΤ
= internal pressure difference relative to as laid
= temperature difference relative to as laid
4.7.4.11 When non-linear material is required in the analyses for load controlled limit states the stressstrain curve shall be based on specified minimum values accounting for temperature de-rating (fy and fu)
considered being engineering stress values. For displacement controlled or partially displacement controlled
limit states additional analyses based on mean or upper bound stress-strain curves may be required to
ensure an acceptable safety level. Illustration of different stress-strain properties is given in Table 1-8.
Guidance note:
The strain at fu is normally considerably less than the fracture strain and is normally in the order of 6 to 10%. This may be
determined from tests of similar material.
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4.7.4.12 Stress concentration factors (SCF) and strain concentration factors (SNCF) may be applied to the
calculated load effects to reflect different aspects (local geometries, coating, variations in properties) not
captured directly in the load effect calculation.
4.7.4.13 SCF's are mainly used in the linear material range and SNCF's in the non-linear material range.
These may reflect local or global effects.
4.7.4.14 SNCF shall be adjusted for the non-linear stress-strain relationship for the relevant load level.
Plastic strain shall be calculated from the point where the material stress-strain curve deviates from a linear
relationship, see Table 1-8
4.7.4.15 Local SCF's and SNCF's may be applied to reflect:
— variations in actual material yield stress and strain hardenability between pipeline joints and in the weld
metal
— local discontinuities in the weld
— welded attachments
4.7.4.16 Global SCF's and SNCF's may be applied to reflect:
— stiffening effects of coating and variations in coating thickness
— variations in cross-sectional area between pipe joints not included in the load effect calculations.
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Most of these effects should be captured by the load effect calculations (like nominal diameter or nominal
wall thickness difference between pipe joints e.g. buckle arrestor or wall thickness change due to safety
zone).
4.7.4.17 Application of SCF and SNCF depend on the limit state and shall be applied according to Table 4-6.
Table 4-6 Application of stress concentration factors and strain concentration factors
Stress concentration factors (SCF)
Strain concentration factors (SNCF)
Limit state
Local
Global
Local
Global
Load controlled local
buckling
-
-
-
-
Displacement
controlled local
buckling
-
Yes
-
-
Fatigue
Yes
Fracture
Yes
1)
1
Yes
1
Yes
Yes
Yes
1
Yes
1
Yes
The use of SCF/SNCF shall be consistent with the SN-curve used
4.7.4.18 Recommended practice for calculation of the SNCF/SCF for fracture assessment is given in DNVGLRP-F108.
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SECTION 5 DESIGN – LIMIT STATE CRITERIA
5.1 General
5.1.1 Objective
5.1.1.1 This section provides limit state criteria and general requirements for the submarine pipeline
systems.
5.1.2 Application
5.1.2.1 This standard includes no limitations on water depth. However, when this standard is applied in deep
water where experience is limited, special consideration shall be given to:
— other failure mechanisms than those given in this section
— validity of parameter range (environmental/design/operational parameters)
— dynamic effects.
5.1.2.2 This standard does not specify any explicit limitations with respect to elastic displacements or
vibrations, provided that the effects of large displacements and dynamic behaviour, including fatigue effect of
vibrations, operational constraints and ratcheting, are taken into account in the strength analyses and found
acceptable.
5.1.2.3 This standard does not specify any limitations on pipe geometries but some limit states were
developed for a limited geometry and load range that is stated with the criterion. For geometries and loads
outside these limits, criteria need to be developed in accordance with the safety philosophy in Sec.2.
5.1.2.4 The local buckling limit states, see [5.4.3] to [5.4.6], are only applicable to pipelines that are
straight in stress-free condition and are not applicable to e.g. bends.
5.1.2.5 For parts of the submarine pipeline system which extend onshore complementary requirements are
given in App.F.
5.1.2.6 For spiral welded pipes, the following additional limitations apply:
— when supplementary requirement F (fracture arrest properties) is specified, see Sec.7, the possibility for
a running fracture to continue from a weld in one pipe joint to the weld of the next pipe joint shall be
assessed
— external pressure resistance should be documented
— the design shall be based on the load controlled condition, see [5.4.6], unless the feasibility for use of
displacement controlled condition can be documented.
Guidance note:
The limitations to fracture arrest and load controlled condition are due to limited experience with spiral welded pipes subjected to
running fracture or large strains.
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5.1.3 Systematic review
5.1.3.1 The overall requirement to systematic review in Sec.2 implies for this section:
— A clear definition of code break between components and pipeline system.
— Clear definition of the codes’ pressure definitions correspondence.
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— A clear description of the overall system including interfaces and responsibilities, covering both temporary
and permanent phases.
— An overall review of all potential failure modes shall be conducted.
— The structural integrity and functionality of pipeline components shall comply with the safety requirements
for the connected pipeline system see Sec.2.
— Pre-commissioning activities.
Guidance note:
The above will include a HAZID of the installation activity to identify potential impact on design such as selection of safety class
during installation (see [10.6.7]).
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5.2 System design requirements
5.2.1 Submarine pipeline system layout
5.2.1.1 Pipelines shall be protected against impact loads from mechanical interaction.
5.2.1.2 Crossing between pipelines and pipelines or cables should be kept separated by a minimum vertical
distance of 0.3 m. Potential electrical interference and associated consequences between pipelines and cables
shall be considered.
5.2.1.3 The submarine pipeline system shall be protected against unacceptable damage caused by e.g.
dropped objects, fishing gear, ships, anchoring etc. Protection may be achieved by one or a combination of
the following means:
—
—
—
—
concrete coating
burial
cover (e.g. sand, gravel, mattress)
other mechanical protection.
5.2.1.4 Relative settlement between the protective structure and the submarine pipeline system shall be
properly assessed in the design of protective structures, and shall cover the full design life of the submarine
pipeline system. Adequate clearance between the pipeline components and the members of the protective
structure shall be provided to avoid fouling.
5.2.1.5 Attachment to pipeline and other pressure containing parts should be welded via doubler plate and
not directly to the pipe/pressure containing parts. Doubler plate should be fully encircling sleeves, if not,
it shall be circular. The objective of the doubler plate is to distribute stresses in order to reduce the risk of
initiating cracks into the pipe.
5.2.1.6 For structural items welded directly to pressure containing parts and doubler plates the following
apply:
— Design shall be performed for all relevant failure modes, e.g. yielding, fatigue and fracture.
— For duplex stainless steels and 13Cr martensitic stainless steels a stress analysis shall be performed in
each case to determine that local stresses will not initiate HISC. Recommended practice for design of
duplex stainless steels is given in DNVGL-RP-F112.
— Welding directly to the pressure containing parts shall be performed in accordance with qualified welding
procedures according to App.C.
— NDT shall be performed to ensure structural integrity of the pressure containing parts.
— The toe-to-toe distance from other welds shall be minimum 2 · t or 50 mm, whichever is larger.
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5.2.1.7 For doubler plates the following apply:
— The longitudinal welds of fully encircling sleeves shall be made with backing strips avoiding penetration
into the main pipe material unless pre-fabricated and slid onto the pipe.
— Welds between doubler plates and pressure containing parts shall be continuous, and made in a manner
minimising the risk of root cracking and lamellar tearing.
5.2.1.8 Girth welds should not be covered under doubler plates, clamps, or other items.
The requirement to not cover the girth weld is to allow for required NDT, corrosion protection (coating,
anodes or premises for other corrosion evaluations) and leakage detection during FAT testing. For FAT testing
based on pressure drop, see [8.7.4], the encircling sleeve is not allowed to constitute a pressure barrier, i.e.
pressure built up in the void shall be monitored or avoided.
5.2.1.9 The use of mitre welds to correct angular misalignment of more than 2 degrees between the axis
of two adjoining pipes is not permitted and a series of purpose made misalignments are not allowed to
constitute a bend. Moments caused by the axial misalignment and axial force shall be evaluated. For loads
causing yielding, detailed calculations shall be made.
5.2.1.10 For requirements to transitions, see [5.6.1.13] through [5.6.1.16].
5.2.1.11 For piggable components the internal diameter of the component shall meet the requirements
imposed by the pig-train.
Guidance note:
It is recommended that bends radius are designed with a radius not less than 5 × nominal internal pipe diameter (5D bend).
3D bends may be acceptable if PIG is designed for it, typically taking into account:
—
length of the pig
—
pig-body diameter
—
position of the seal- and guide-discs
—
material and size of the discs
—
position of the gauge-plate.
In addition, a trial fit to be performed.
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5.2.2 Pressure test philosophy and criteria
5.2.2.1 The pressure containment structural integrity of the pipeline system is ensured by:
— design criteria and safety factors
— manufacturing requirements
— pressure testing all pressure containing parts by
— strength test prior to being installed in the pipeline system; by strength pressure test (mill pressure
test for pipe joints [7.5.1] and FAT/hydrostatic test for components [8.7]), or through qualification
programs and
— gross error leak test; system pressure test ([5.2.2.2] and [10.10.3]) and hydrostatic test for pipeline
assemblies [7.5.1]. For single connections, making up parts of the pipelines after system pressure test,
the following apply:
— girth welds shall have additional NDT (Golden Weld), see [10.5.3]
— mechanical components shall be back seal tested after installation.
Unless waived by [5.2.2.3] or [7.5.1.6].
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Guidance note:
The above requirements imply that each element of the pipeline system shall be both strength tested and gross error leak tested.
A typical pressure test regime may look like indicated in the following figure:
The following comments apply:
—
Tie-in flanges and couplings may be back-seal tested in order to reveal any leakage as early as possible. If these are not part
of the system pressure test, back seal test shall be performed.
—
Pipeline assemblies (risers, spools etc.) may be hydrostatically leak tested as a risk reducing measure in order to reveal any
leakage as early as possible. If these pipeline assembles are not part of the system pressure test, hydrostatic leak test shall be
performed.
The expressions related to the system pressure test have been altered over a few revisions but are now referred to as leakage
test. The reason why it is now considered being a leakage test is that the girth weld, which is the only part not previously tested,
has a very low utilisation during the system pressure test, less than 48% of SMYS and is therefore very unlikely to fail structurally.
The reason why this term has changed of the revisions is that ISO 13623 operates with two pressure levels for the system
pressure test (pressure test). The strength test is 1.25 times the design pressure and shall be kept for a minimum of 1 hour. The
leak test is 1.1 times the design pressure and shall be kept for a minimum of 8 hours.
DNVGL-ST-F101 only operates with one pressure level 1.05 times the incidental pressure (1.15 times the design pressure) which
shall be kept for minimum 24 hours.
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5.2.2.2 The pipeline system shall be system pressure tested after installation in accordance with [10.10.3]
unless this is waived by agreement in accordance with [5.2.2.3] below. The local test pressure (plt) during
the system pressure test should fulfil the following requirement for the safety class during normal operation:
plt ≥ αspt pli
(5.1)
αspt see Table 5-8.
Note that a system test pressure less than the above may reduce the allowable incidental pressure as given
by Equation (5.6) and Equation (5.7).
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Guidance note:
With an incidental pressure of 10% above design pressure, the above gives a system test pressure of approximately 1.15 times
the local design pressure (for safety class medium and high) at the highest point (given that the test medium density is higher
than
αspt * density of the medium in operation of the pipeline system part tested), see Table 1-8.
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Figure 5-1 Illustration of local pressures and requirements to system pressure test
5.2.2.3 For pipelines where the disadvantages with the system pressure test are extraordinary, alternative
means to ensure the same level of integrity as with the system pressure test are allowed by agreement.
Alternative means to the system pressure test may be considered when all the following criteria have been
met:
— The pipeline section does not contain non-welded connections unless these have been separately tested
after installation in the pipeline system.
— The mill pressure test requirement of [7.5.1] has been met and not waived in accordance with [7.5.1.6].
— Extensive experience with similar pipelines documenting a good track record with respect to defects and
leakages during system pressure test. This implies that:
—
—
—
—
Only C-Mn steel pipelines with a steel grade less than - or equal to X70 may be considered.
Only pipelines consisting of seamless or SAW pipe joints may be considered.
Welding, including repair, by cellulosic electrodes is not allowed.
The pipeline shall not be exposed to nominal tensile longitudinal strains above 0.4% from mill testing
to commissioning.
5.2.2.4 The alternative means shall be established by use of a systematic approach, e.g. FMECA. It shall be
demonstrated that the identified failure modes, i.e. the gross errors and defects which may be revealed by
the system pressure test, will be mitigated or revealed by the alternative means.
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5.2.2.5 A risk assessment shall be carried out addressing not only the risk related to the elements of the
above systematic approach, but also other aspects that are affected by replacing the system pressure test.
Typical other aspects include consequences of accidental water ingress during construction, cleaning of pipe,
interfaces and contractual issues. The systematic approach and the risk assessment shall lead to a technical
assurance program that is implemented and followed up in all relevant phases.
5.2.2.6 During system pressure test, all limit states for safety class low shall be satisfied, see [5.4].
5.2.2.7 Recommended practice for system pressure test including all pre-commissioning activities is given in
DNVGL-RP-F115.
5.2.3 Monitoring/inspection during operation
5.2.3.1 The parameter safety envelope established in the conceptual phase, see [3.3.1] and [5.4.2], shall
be extended/modified in the design phase by the parameters which could violate limit states of a pipeline
system. These shall be monitored, inspected and evaluated with a frequency which enables remedial actions
to be carried out before the system is damaged, see Sec.11.
Guidance note:
As a minimum the monitoring/inspection frequency should be such that the pipeline system will not be endangered due to any
realistic degradation/deterioration that may occur between two consecutive inspection intervals.
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5.2.3.2 Special focus shall be on monitoring and inspection strategies for live pipeline systems i.e. pipeline
systems that are designed to change the configuration during its design life.
Guidance note:
Example of such systems may be pipelines that are designed to experience global buckling or possible free-span developments or
potential pipeline walking.
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5.2.3.3 Instrumentation of the pipeline system may be required when visual inspection or simple
measurements are not considered practical or reliable, and available design methods and previous experience
are not sufficient for a reliable prediction of the performance of the system.
5.2.3.4 Operating requirements affecting safety and reliability of the pipeline system shall be identified
during the design phase, and shall be documented in the DFI Resumé and reflected in the PIM system.
5.3 Design format
5.3.1 General
5.3.1.1 The design format in this standard is based on a load and resistance factor design (LRFD) format.
5.3.1.2 The fundamental principle of the LRFD format is to verify that design load effects, LSd, do not exceed
design resistances, RRd, for any of the considered failure modes in any load scenario:
(5.2)
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Where the fractions i denotes the different loading types that enters the limit state.
5.3.1.3 A design load effect is obtained by combining the characteristic load effects from the different load
categories and certain load effect factors, see [4.7].
5.3.1.4 A design resistance is obtained by dividing the characteristic resistance by resistance factors that
depends on the safety class, reflecting the consequences of failures, see [5.3.2].
5.3.1.5 Design criteria in this standard are based on pipe statistical properties resulting from construction
based on this standard.
Guidance note:
Use of e.g. other line pipe specifications need therefor to be assessed
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5.3.2 Design resistance
5.3.2.1 The design resistance, RRd, can generally be expressed in the following format:
(5.3)
where:
Rc
fc
tc
O0
γm
γSC,i
= the characteristic resistance
= the characteristic material strength, see Equation (5.4) and Equation (5.5)
= the characteristic thickness, see Table 5-5 and Table 5-6
= the out of roundness of the pipe, prior to loading
= the material factor (not used for displacement controlled criteria), see Table 5-1
= the partial resistance factor, see Table 5-2
5.3.2.2 Ovality of the pipeline is defined in Equation (5.14). This will affect the structural capacity of the
pipeline and shall be taken as the maximum ovality prior to loading. Advantage of an ovality less than 0.5%
is not allowed. Ovality in excess of 3% shall be assessed in line with [5.4.12].
5.3.2.3 The material resistance factor, γm, is dependent on the limit state category and is defined in Table
5-1.
Table 5-1 Material resistance factor, γm
1)
Limit state category
γ
SLS/ULS/ALS
FLS
1.15
1.00
m
1)
The limit states (SLS, ULS, ALS and FLS) are defined in [5.4].
5.3.2.4 Based on potential failure consequences the pipeline shall be classified into a safety class see
[2.3.4]. This will be reflected in the safety level by the safety class resistance factor γSC,i given in Table 5-2.
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Guidance note:
The safety class may vary for different phases and different locations.
The safety class resistance factors for pressure containment as listed in Table 5-2 are based on the corresponding hoop stress
design factors for offshore pipelines as given in the referenced ISO 13623 standard for pipeline transport systems. As such the
bursting utilisation using this document will be in line with what has been the industry practice for decades and represents a failure
rate for such pipeline systems that has been perceived as acceptable for all stakeholders including the society at large. When it
comes to other failure modes/limit states calibration of safety factors using structural reliability analyses has concluded with the
same safety class resistance factors as for pressure containment for safety classes Low and Medium while a slightly different value
for safety class High.
DNVGL-ST-F201 utilises the same safety class resistance factor for all failure modes/limit states within the same safety class,
i.e. it does not make any difference between pressure containment and the other limit states. The main reason for this difference
towards this standard is that DNVGL-ST-F201 refers to another ISO standard than this standard, namely the ISO 13628-7 for WO/
C risers which has a somewhat different burst criterion than ISO 13623 and is allowing a somewhat higher utilisation with respect
to bursting.
As such the different safety class resistance factors for pressure containment and safety class high in this standard and DNVGL-STF201 are explained by the different utilisation in the underlying ISO standards. Another more practical explanation is that it can be
claimed that the system effect is more significant for a pipeline in location class 2 than for a riser. For a riser it is typically just a
few joints in the splash zone that is most heavily utilised, while for a pipeline it is normally the whole length in the location class 2.
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Table 5-2 Safety class resistance factors, γ
Limit state
Safety class
resistance factor
SC
Safety class
Low
2),3)
Pressure containment
γ
SC,PC
Local buckling,
collapse and load
controlled
γ
SC,LB
1.04
1.14
Local buckling,
displacement
controlled
γ
SC,DC
2.0
2.5
1)
1.046
Medium
1.138
High
1.308
4)
1.26
3.3
1)
The number of significant digits is given in order to comply with the ISO usage factors.
2)
Safety class low will be governed by the system pressure test which is required to be 3% above the incidental
pressure. Hence, for operation in safety class low, the resistance factor will effectively be minimum 3% higher.
3)
For system pressure test, αU shall be equal to 1.00, which gives an allowable hoop stress of 96% of SMYS both for
materials fulfilling supplementary requirement U and those not.
4)
For parts of pipelines in location class 1, resistance safety class medium may be applied (1.138).
5.3.2.5 Possible beneficial strengthening effect of weight coating on a steel pipe shall not be taken into
account in the characteristic resistance, unless the strengthening effect is documented. Coating which adds
significant bending stiffness to the pipe may increase the stresses/strains in the pipe at any discontinuity in
the coating (e.g. at field joints). When appropriate, this effect shall be taken into account.
5.3.2.6 Possible beneficial strengthening effect of cladding or liner on a steel pipe shall not be taken into
account in the characteristic resistance, unless the strengthening effect is documented.
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5.3.3 Characteristic material properties
5.3.3.1 Characteristic material properties shall be used in the resistance calculations. The yield stress and
tensile strength in the limit state formulations shall be based on the engineering stress-strain curve.
5.3.3.2 The characteristic material strength fy and fu, values to be used in the limit state criteria are:
(5.4)
(5.5)
Where:
f y,temp and fu,temp = the de-rating values due to the temperature of the yield stress and the tensile strength
respectively, see [5.3.3.4].
αU
= the material strength factor, see Table 5-3.
5.3.3.3 The different mechanical properties refer to room temperature unless otherwise stated.
5.3.3.4 The material properties shall be selected with due regard to material type and potential temperature
and/or ageing effects and shall include:
—
—
—
—
yield stress
tensile strength
Young's modulus
temperature expansion coefficient.
For C-Mn steel and 13Cr this shall be considered for temperatures above 50°C, and for 22Cr and 25Cr for
temperatures above 20°C.
Guidance note:
Field joint coating application during installation may also impose temperatures in excess of the above.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e--Guidance note:
If no other information of de-rating effects on the yield stress exist the recommendations for C-Mn steel, 22Cr and 25Cr Figure 5-2
may be used. For 13Cr testing is normally required.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e--Guidance note:
If no other information on de-rating effect of the ultimate stress exists, the de-rating of the yield stress can be conservatively
applied.
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Figure 5-2 Proposed de-rating values for yield stress of C-Mn, 13Cr, 22Cr and 25Cr
5.3.3.5 Any difference in the de-rating effect of temperature for tension and compression shall be accounted
for.
Guidance note:
Difference in de-rating effect for tension and compression has been experienced on 13Cr steel material.
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5.3.3.6 The material strength factor,
upgrade of material, see [7.9.5]
αU, depend on supplementary requirement U as shown in Table 5-3. For
Table 5-3 Material strength factor,
αU
αU
Loading scenario
Normal
Supplementary requirement U
System pressure test
1.00
1.00
Other
0.96
1.00
5.3.3.7 For manufacturing processes which introduce cold deformations giving different strength in tension
and compression, a fabrication factor, αfab, shall be determined. If no other information exists, maximum
fabrication factors for pipes manufactured by specific processes are given in Table 5-4.
The fabrication factor may be increased through heat treatment or external cold sizing (compression), if
documented.
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Table 5-4 Maximum fabrication factor,
α fab
Pipe
Seamless
UO, TRB, ERW and HFW
UOE
α fab
1.00
0.93
0.85
5.3.4 Characteristic wall thickness
5.3.4.1 Two different characterisations of the wall thickness are used; t1 and t2 and are referred to explicitly
in the design criteria. Thickness t1 is used where failure is likely to occur in connection with a low capacity
(i.e. system effects are present) while thickness t2 is used where failure is likely to occur in connection with
an extreme load effect at a location with average thickness. These are defined in Table 5-5.
Table 5-5 Characteristic wall thickness
Characteristic
thickness
Prior to operation
1)
2)
Operation
t1
t-tfab
t-tfab-tcorr
t2
t
t-tcorr
1)
Is intended when there is negligible corrosion (mill pressure test, construction (installation) and system pressure
test condition). If corrosion exist, this shall be subtracted similar to as for operation.
2)
Is intended when there is corrosion.
5.3.4.2 If relevant, erosion allowance shall be compensated for in the similar way as the corrosion allowance.
5.3.4.3 Minimum wall thickness independent on limit state requirements are given in Table 5-6.
The minimum wall thickness requirement is based on failure statistics, which clearly indicate that impact
loads and corrosion are the most likely causes of failure and have the decisive effect on thickness design (not
D/t2).
Table 5-6 Minimum wall thickness requirements
Safety class
High
Location class
2
Nominal thickness
Minimum 12 mm unless equivalent protection against
accidental loads, other external loads and excessive corrosion
is provided by other means. For diameters less than 219
mm (8”) minimum wall thickness can be less but shall be
determined including the above considerations.
5.3.4.4 Wall thickness for on bottom stability calculations is given in [5.5.5.2].
5.3.4.5 The wall thickness should be sufficient to ensure no damage during handling.
Guidance note:
For pipelines with D/t<45 this is normally not a problem with exception for very small diameter pipelines.
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5.4 Limit states
5.4.1 General
5.4.1.1 All relevant limit states (failure modes) shall be considered in design for all relevant phases and
scenarios listed in Sec.4.
Guidance note:
Limit state design implies that the pipeline is checked for all relevant failure modes. The failure modes vary in criticality and are
split into the following limit state categories:
—
serviceability limit state category
—
ultimate limit state category
—
fatigue limit states
—
accidental limit state.
Fatigue and accidental limit states are sub-categories of ultimate limit states accounting for accumulated cyclic load effects and
accidental (in-frequent) loads respectively.
Pipeline limit state checks are typically split into different scenarios. A scenario is not identical with a limit state, and may include
different limit states. A typical link between scenarios and limit states is given in Table 5-7.
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Table 5-7 Typical link between scenarios and limit states
Ultimate limit states
Fracture
Serviceability limit states
Instability
Installation
Free-span
(X)
Trawling/3rd party
(X)
On bottom stability
(X)
X
X
X
X
(X)
1)
Displacement
X
X
(X)
X
X
(X)
Pipeline Walking
Global Buckling
X
Accumulated deformation
X
Ovalisation
X
Dent
X
Global buckling
X
Combined loading
Propagating buckling
Fracture
X
System collapse
Wall thickness design
Fatigue
Scenario
Pressure containment
Local buckling
X
X
(X)
(X)
1
X
(X)
X
X
X
X
Typically applied as a simplified way to avoid checking each relevant limit state
5.4.1.2 In case no specific design criterion is given for a specific limit state this shall be developed in
compliance with the safety philosophy in Sec.2.
5.4.2 Pressure containment (bursting)
5.4.2.1 The pressure containment shall fulfil the following criteria:
(5.6)
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(5.7)
unless:
— the mill test has been waived in accordance with [7.5.1.6],
— the mill test pressure has been reduced in accordance with [7.5.1.4], or
— the system pressure test has been replaced by alternative means in accordance with [5.2.2.3].
αmpt and αspt are given in Table 5-8.
Table 5-8 Pressure test factors
Safety class during operation
1
αmpt
αspt
1)
Low
Medium
High
1.000
1.088
1.251
1.03
1.05
1.05
This factor is given by:
5.4.2.2 The pressure containment resistance pb(t) is given by:
(5.8)
where:
(5.9)
Guidance note:
In the above formulae, t shall be replaced by t1 when used in Equation (5.7) and t2 when used in Equation (5.19).
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5.4.2.3 Reduction in pressure containment resistance due to true compressive forces (load controlled),
N, shall be considered. Recommended practice for reduction in pressure containment capacity due to
compressive axial stresses is given in DNVGL-RP-F101.
5.4.3 Local buckling - general
5.4.3.1 Local buckling (pipe wall buckling) implies gross deformation of the cross-section. The following
criteria shall be fulfilled:
— system collapse (external over pressure only)
— propagation buckling (external over pressure only)
— combined loading criteria, i.e. interaction between external or internal pressure, axial force and bending
moment.
These will be given in the following sub-sections.
5.4.3.2 Large accumulated plastic strain may aggravate local buckling and shall be considered.
5.4.4 Local buckling – system collapse (external over pressure only)
5.4.4.1 The external pressure at any point along the pipeline shall fulfil the following criterion (system
collapse check):
(5.10)
where:
p min = the minimum internal pressure that can be sustained. This is normally taken as zero for as-laid
pipeline.
Guidance note:
The system collapse will occur at the weakest point in the pipeline. This will normally be represented by fy and the minimum wall
thickness, t1.
A seamless produced line pipe’s weakest section may not be well represented by the minimum wall thickness since it is not likely
to be present around the whole circumference. A larger thickness, between t1 and t2, may be used for such pipes if this can be
documented representing the lowest collapse capacity of the pipeline.
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5.4.4.2 The characteristic collapse pressure (pc) (resistance for external over pressure) shall be calculated
as:
(5.11)
where:
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(5.12)
(5.13)
(5.14)
not to be taken less than 0.5%.
Ovalisation caused during the construction phase shall be included in the total ovality to be used
in design. Ovalisation due to external water pressure or bending moment shall not be included.
αfab
= the fabrication factor, see Table 5-4.
Guidance note:
In the above formulas, t shall be replaced by t1 or t2 as given in the design criteria.
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5.4.5 Local buckling - propagation buckling
5.4.5.1 Propagation buckling cannot be initiated unless local buckling has occurred. In case the external
pressure exceeds the criterion given below, buckle arrestors should be installed and spacing determined
based on cost and spare pipe philosophy. The propagating buckle criterion reads:
(5.15)
where:
p min
is the minimum internal pressure that can be sustained. This is normally taken as zero for as-laid
pipeline.
(5.16)
Applies for
15 < D/t2 < 45
α fab is the fabrication factor, see Table 5-4.
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Guidance note:
Collapse pressure, pc, is the pressure required to buckle a pipeline.
Initiation pressure, pinit, is the pressure required to start a propagating buckle from a given buckle. This pressure will depend on
the size of the initial buckle.
Propagating pressure, ppr, is the pressure required to continue a propagating buckle. A propagating buckle will stop when the
pressure is less than the propagating pressure.
The relationship between the different pressures are: pc > pinit > ppr
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5.4.5.2 A buckle arrestor capacity depends on
— propagating buckle resistance of adjacent pipe
— propagating buckle resistance of an infinite buckle arrestor
— length of arrestor.
An integral buckle arrestor may be designed by:
(5.17)
where the crossover pressure px is:
(5.18)
where:
p pr,BA = the propagating buckle capacity of an infinite arrestor. This is calculated by Equation (5.16) with the
buckle arrestor properties
LBA
= buckle arrestor length
(Other parameters refers to line pipe properties, see [13.4.8]).
Guidance note:
The propagating buckle criterion, Equation (5.15), corresponds to a nominal failure probability that is one order of magnitude
higher than the target nominal failure probability. This is because it is dependent on an initiating even. However, for a
buckle arrestor, it is recommended to have a larger confidence and a safety class higher than for the propagating pressure is
recommended.
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5.4.6 Local buckling - combined loading criteria
5.4.6.1 Differentiation is made between:
— load controlled condition (LC condition)
— displacement controlled condition (DC condition).
Different limit states apply to these two conditions.
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Guidance note:
What is required to document the local buckling capacity for pipelines outside the D/t range of 15-45, is partly discussed in
[13.4.9] but is further outlined below. The current formulation has been developed from experiments and a set of FE-analyses
of straight pipes with 15<D/t<60. The main failure mode for this formulation is maximum moment capacity based on gross
ovalisation of the pipe. In this range wrinkling, i.e. local wave-shaped deformation on the compressive side, may also be
experienced but will normally occur beyond the point of maximum moment capacity and, hence, not affecting the above defined
capacity. For higher D/t this wrinkling failure mode may be triggered earlier by imperfections like misalignment over the girth weld.
This was not modelled in the FE analyses referred to above, and it is considered being likely to happen above D/t=45, hence the
limitation. For D/t>45 it is therefore required to check the possibility that the established high-low criterion will not trigger this
failure mode and give a lower capacity. Alternatively it is needed to determine the capacity accounting for this type of imperfection
and failure mode. To do this, a FE-model capable of modelling this failure mode should be established and; • Reproducing the
capacity for D/t=45 • Determine the capacity for the actual D/t • Apply this reduction (i.e. b/a) to the local buckling capacity for
D/t=45 By applying the reduction, any offset in models is avoided. If the difference between this standard's capacity at D/t=45
deviates significantly from the FE results at this D/t value, this needs to be assessed and the difference identified. For D/t<15 a
similar exercise is required, but it is not required to analyse any high-low trigger mechanism.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
5.4.6.2 A load-controlled condition is one in which the structural response is primarily governed by the
imposed loads.
5.4.6.3 A displacement-controlled condition is one in which the structural response is primarily governed by
imposed geometric displacements.
Guidance note:
A pipeline checked for displacement controlled criteria will typically have tensile strains in excess of 0.4% and fracture assessment
is then required, see [5.4.8].
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
5.4.6.4 A load controlled design criterion can always be applied in place of a displacement controlled design
criterion.
Guidance note:
An example of a purely displacement-controlled condition is a pipeline bent into conformity with a continuous curved structure,
such as a J-tube. In that case, the curvature of the pipe axis is imposed but the circumferential bending that leads to ovalisation is
determined by the interaction between the curvature of the axis and the internal forces induced by the curvature.
A less clear-cut example is a pipeline in contact with the rollers of a lay barge stinger. On a large scale, the configuration of the
pipeline has to conform to the rollers, and in that sense is displacement controlled. On a local scale however, bending of the pipe
between the rollers is determined by the interaction between weight and tension and is load-controlled. Contact with the rollers will
further reduce the capacity. The stinger tip will, however, always be load controlled.
Another intermediate case is an expansion spool in contact with the seabed. Pipeline expansion induced by temperature and
pressure imposes a displacement at the end of the spool. The structural response of the spool itself has little effect on the imposed
expansion displacement, and the response is primarily displacement-controlled. However, the lateral resistance to movement of the
spool across the seabed also plays a significant part and induces a degree of load control.
System effect has also a slightly different effect in local buckling – combined loading than for bursting and collapse. A uniform
moment/curvature cannot be applied to the whole pipeline at once but will typically occur as a peak moment moving along the
pipeline. This applies to sag bend, stinger and reeling. Local buckling – combined loading will then be governed by the maximum
moment capacity variation along the pipe. This will occur a small distance (typically in the order of a diameter) into the weak part,
when the peak moment moves from strong to weak section. For such applications, more detailed assessment can be based on a
weak link evaluation, where this weak link is the extreme variation from one joint to another.
The answer to the question on if a condition is load controlled or displacement controlled is impossible since the questions in
wrong, the question should be; how can one take partial benefit of that a condition is partially displacement controlled element?
On a general basis this needs sensitivity analyses. A load controlled criterion can, however, always be applied
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Guidance note:
If the design is based on extreme variation from one joint to the other, benefit may be taken from selection of matching, as closely
as possible, wall thickness/diameter of the pipes and the actual yield stress on both sides of the weld.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
5.4.6.5 Pipe members subjected to bending moment, effective axial force and internal over pressure shall be
designed to satisfy the following criterion at all cross-sections:
(5.19)
Applies for:
15 ≤ D/t2 ≤45
P i > Pe
|SSd|/Sp<0.4
where:
MSd
SSd
pi
pe
pb
Sp and Mp
= the design moment load effect, see Equation (4.6)
= the design effective axial force load effect, see Equation (4.8)
= the internal pressure, see Table 4-3
= the external pressure, see [4.2.2]
= the burst pressure, Equation (5.8)
= denote the plastic capacities for a pipe defined by:
(5.20)
(5.21)
(5.22)
(5.23)
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(5.24)
α c is a flow stress parameter and γp account for effect of D/t2 ratio.
Guidance note:
For applications outside the axial load limitations, see DNVGL-ST-F201.
The left hand side of the combined loading criterion is referred to as interaction ratio in order not to mix it with unity check. In a
unity check, the loads are normally directly proportional to the utilisation while the axial load and internal pressure are squared in
this criterion.
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5.4.6.6 If the pipeline in addition to the axial load, pressure and moment also has a lateral point load, this
should be included by a modification of the plastic moment capacity as follows:
(5.25)
where:
αpm
= plastic moment reduction factor accounting for point load.
(5.26)
R
= reaction force from point load
(5.27)
Applies for R/Ry<0.5
5.4.6.7 Pipe members subjected to bending moment, effective axial force and external overpressure shall be
designed to satisfy the following criterion at all cross-sections:
(5.28)
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Applies for
15 ≤ D/t2 ≤ 45
P
min
< Pe
|SSd|/Sp< 0.4
where:
pmin = the minimum internal pressure that can be sustained. This is normally taken as zero for installation
except for cases where the pipeline is installed water filled
pc
= the characteristic collapse pressure, Equation (5.10). This shall be based on thickness t2.
Guidance note:
For applications outside the axial load limitations, see DNVGL-ST-F201
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
5.4.6.8 Pipe members subjected to longitudinal compressive strain due to applied displacements and internal
over pressure shall be designed to satisfy the following criterion at all cross-sections:
(5.29)
Applies for
15 ≤ D/t2 ≤ 45
p
min
≤ pe
where:
εSd
= design compressive strain Equation (4.7)
(5.30)
(5.31)
(5.32)
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for material having a Lüder plateau:
(5.33)
For other materials:
where:
p min = minimum internal pressure that can be continuously sustained with the associated strain
γSC,DC = strain resistance factor, Table 5-2
αh
=
Table 7-5 and Table 7-11
αgw
= see Sec.13.
5.4.6.9 If the pipeline in addition to the axial load, pressure and curvature also has a lateral point load, this
should be included by a modification of the curvature capacity as follows:
(5.34)
5.4.6.10 Pipe members subjected to longitudinal compressive strain (bending moment and axial force) and
external over pressure shall be designed to satisfy the following criterion at all cross-sections:
(5.35)
Applies for:
15 ≤ D/t2 < 45
p
min
< pe
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Guidance note:
For D/t2 < 23, the utilisation may be increased provided that full scale testing, observation, or former experience indicate sufficient
safety margin in compliance with this standard.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e--Guidance note:
System effects are normally not present for local buckling considerations and, hence, t2 should be used. However, for reeling,
a large portion of the pipeline will be exposed to similar curvature and load combination “a” shall be used combined with the
condition factor and the nominal thickness can be used also for this criteria. The thickness and yield stress variation along the pipe,
in particular between two pipe joints should be evaluated in addition to this system effect.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
5.4.6.11 A higher probability of failure corresponding to a serviceability limit state may be allowed during
the installation phase provided that:
— aids to detect buckle are provided
— repair of potential damage is feasible and may be performed during laying
— buckle arrestors are installed if the external pressure exceeds the initiation propagating pressure.
Relevant resistance factors may then be calibrated according to the SLS requirements in Sec.2.
5.4.7 Global buckling
5.4.7.1 Global buckling implies buckling of the pipe as a bar in compression.
5.4.7.2 The effect of internal and external pressures should be taken into account using the concept of an
effective axial force, see [4.7.4]. The procedure is as for ordinary compression members in air.
5.4.7.3 Distinction shall be made between load-controlled and displacement-controlled global buckling.
Load controlled global buckling condition is characterised by that the applied load is independent on the
deflection of the pipeline
Displacement controlled, or partially displacement controlled global buckling condition is characterised by
that the major part of the applied load is dependent on the deflection of the pipeline. Expansion force due to
pressure and temperature are examples of such.
5.4.7.4 Load-controlled global buckling may be designed in accordance with DNVGL-OS-C101.
5.4.7.5 For displacement controlled global buckling, see [5.5.3].
5.4.8 Fatigue and fracture limit state
5.4.8.1 The submarine pipeline system shall have adequate safety against fracture failures within the
design life of the system. This is in general achieved by selecting materials with adequate fracture toughness
properties, tensile properties and weld quality combined with sound design principles.
5.4.8.2 The fatigue and fracture limit state is in general applicable to all types of materials specified in Table
1-1 as long as the representative materials properties needed to perform the assessments are known or
established. Welds are in general most critical considering the fatigue and fracture limit state because welds
typically have higher stresses due to stress concentrations and weld residual stresses and may include flaws.
This may result in shorter initiation time for fatigue crack growth, tearing or unstable fracture in case of high
stresses/strains combined with low fracture toughness properties.
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5.4.8.3 Special consideration shall be given to the fatigue assessment of construction details likely to cause
stress concentrations, and to the possibility of having low-cycle high strain fatigue. The specific design
criterion to be used depends upon the analysis method, which may be categorized into:
— methods based upon fatigue tests (typically dedicated S-N curves) (see [5.4.8.7]- [5.4.8.14])
— methods based upon fracture mechanics (see [5.4.8.5], [5.4.8.6] and [5.4.8.15]-[5.4.8.18]).
Guidance note:
S-N based and fracture mechanics based fatigue crack growth assessments are different approaches with somewhat different
objectives. Fatigue analyses based on S-N curves are most applicable for evaluating fatigue initiation from weld toes or other
geometrical stress concentrations that are included in the actual S-N curve. Fatigue assessments based on fracture mechanics
is based on the assumption that there is a flaw in the material and that this flaw will grow as a fatigue crack until a defined
length is reached, unstable fracture occurs or the crack is through the wall thickness. This means that these two approaches
may predict different fatigue lives. Currently there are some inconsistencies in the industry when the two approaches are to be
applied and it is recommended that expert advices are sought when in doubt. Recommended practice for how to conclude the
fatigue and fracture limit state based on fracture mechanics are specified in DNVGL-RP-F108.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
Some guidance on low-cycle fatigue assessments may be found in DNVGL-RP-C203, DNVGL-RP-F108 and
Norsok N-006.
5.4.8.4 The different failure modes considered in this limit state are:
— unacceptable fatigue damage according to S-N fatigue assessment approach
— unstable fracture based on fracture mechanics analyses (may be tearing instability or plastic collapse)
— fatigue crack growth until unstable fracture or a defined crack size.
5.4.8.5 Fracture assessment should be based on:
— recognized fracture assessment procedure and local longitudinal stress across the girth weld determined
as follows;
— εl,nom from global FE analyses and relevant stress or strain concentration factors reflecting details not
covered by the global FE analyses, or
— local FE analyses were all relevant geometrical (thickness variation, misalignment, coating) and
material variations are modelled explicitly
— detailed FE-based fracture assessment where the safety margin is ensured by recognised procedure.
Recommended practice on fracture assessment is given in DNVGL-RP-F108.
5.4.8.6 The fatigue and fracture limit state is considered satisfactory if the requirements in Table 5-9 are
met.
Table 5-9 Requirements to fatigue and fracture limit state
Total nominal longitudinal strain
ε l,nom ≤ 0.4%
1),2)
Requirements
The welds shall have acceptable fatigue damage (S-N
approach). The linear damage hypothesis (Miner’s sum)
may be used, see [5.4.8.10] and [5.4.8.11].
Weld flaw acceptance criteria differing from App.D and
App.E may be determined based on fracture mechanics
analyses. Recommended procedure is given in DNVGL-RPF108.
ε l,nom > 0.4%
The welds shall have acceptable fatigue damage (S-N
approach). The linear damage hypothesis (Miner’s sum)
may be used, see [5.4.8.10] and [5.4.8.11].
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The fatigue and fracture integrity shall also be proven
by determining maximum allowable size of weld flaws
based on fracture mechanics assessments. Recommended
practice for pipeline girth welds is given in DNVGL-RP-F108
(procedure may also be applied to other types of welds).
1)
The strain levels refer to strains aroused after pipe manufacturing process.
2)
For pipelines subjected to longitudinal strain exceeding 1.0% or accumulated plastic strain exceeding 2.0% the
supplementary requirement P applies to the line pipes (parent material)
3)
The S-N curves and material properties used in analyses shall represent the actual environment and temperature
conditions.
5.4.8.7 All stress fluctuations imposed on the pipeline system during the entire design life, including the
construction phase, which have magnitude and corresponding number of cycles large enough to cause
fatigue effects shall be taken into account when determining the long-term distribution of stress ranges. The
fatigue check shall include both low-cycle fatigue and high-cycle fatigue.
Guidance note:
Typical causes of stress fluctuations in a pipeline system are:
—
direct wave action
—
vibrations of the pipeline system, e.g. due to vortex shedding (current, waves, wind, towing) or fluid flow
—
supporting structure movements, e.g. installation vessel
—
fluctuations in operating pressure and temperature.
Locations to be checked are the girth welds, seam welds and construction details. Seam welds will be more vulnerable to fatigue
for higher steel grades.
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5.4.8.8 As most of the loads which contribute to fatigue are of a random nature, statistical consideration is
normally required in determining the long-term distribution of fatigue loading effects. Where appropriate,
deterministic or spectral analysis may be used.
5.4.8.9 When using calculation methods based upon fatigue tests, the following shall be considered:
— determination of long-term distribution of stress range, see [5.4.8.7]
— selection of appropriate S-N curve (characteristic resistance) considering geometry and NDT
requirements, see [5.4.8.10]
— determination of stress concentration factor (SCF) not included in the S-N curve
— the environmental condition
— determination of accumulated damage, see [5.4.8.11].
5.4.8.10 The characteristic resistance is normally given as S-N curves, i.e. stress ranges versus number of
cycles to failure, N. The S-N curve shall be applicable for the material, construction detail, NDT acceptance
criteria (weld quality) and stress component (longitudinal vs. hoop etc.), as well as to the surrounding
environment. The S-N curve shall be based on the mean curve of log (N) with the subtraction of two standard
deviations in log (N).
Quality requirements for welds not classified as fatigue sensitive are given in Table D-4, Table D-5 and Table
D-6 for manual NDT and Table E-1 for AUT.
Welds classified as fatigue sensitive shall satisfy Table E-2.
It is acceptable to determine less strict AUT acceptance criteria based on maximum allowable flaw sizes
assessed using fracture mechanics assessments. Recommended approaches for assessing maximum
allowable flaw sizes are given in DNVGL-RP-F108. However, it is not recommended to use fracture mechanics
assessments to allow for lower weld quality than specified in Table E-1. If AUT acceptance criteria are
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determined based on fracture mechanics analyses, it is not necessary to re-calculate the fatigue life and
satisfy Miner's sum using S-N curves representing the lower weld quality.
5.4.8.11 In the general case where stress fluctuations occur with varying amplitude of random order, the
linear damage hypothesis (Miner's rule) may be used. The application of Miner's rule implies that the longterm distribution of stress range is replaced by a stress histogram, consisting of a number of constant
amplitude stress or strain range blocks, (σr)i or (εr)i, and the corresponding number of repetitions, ni. Thus,
the fatigue criterion is given by:
(5.36)
(5.37)
Where:
Dfat
k
ni
Ni
= Miner's sum
DFF
= design fatigue factor, see Table 5-10.
= number of stress blocks
= number of stress cycles in stress block i
= number of cycles to failure at constant stress range of magnitude (σr)i or strain range (εr)i.
5.4.8.12 Allowable design fatigue factors are given in Table 5-10.
Table 5-10 Allowable design fatigue factor
Safety class
Low
Medium
High
DFF
3
6
10
5.4.8.13 Recommend practice for S-N fatigue strength analysis is given in DNVGL-RP-C203 Sec.5.
5.4.8.14 The split between different phases of the design fatigue life shall be agreed in the initiation phase
of the project and be based on the highest safety class during the lifetime.
Guidance note:
For a pipeline where e.g. 50% of the design lifetime can be utilized during the installation and which is classified as safety class
medium (DFFS-N=6) during the operational phase, this will correspond to a damage ratio of 50/6=8.3% of the operational lifetime.
A common split between installation, as laid and operation is 10%, 10% and 80% but depend on the need for fatigue capacity in
the different phases. Other split than the normal 10/10/80 may be defined in agreement with the pipeline operator.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e--Guidance note:
DNVGL-RP-F105 Sec.5 has a partial safety factor format on allowable fatigue damage. Other standards will generally have other
safety factor formats, or most often an allowable utilization without partial safety factors. If DNVGL-RP-F105 Sec.5 is applied to
calculate partial damage contributions, and these are added to damage from other sources to adhere to a criterion in a different
standard, the damage in DNVGL-RP-F105 shall be normalized in an appropriate manner.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
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5.4.8.15 Recommended practice for combined fatigue and fracture assessments of pipelines with focus on
girth welds is given in DNVGL-RP-F108 (the approach may also be applicable to other types of welds and
pipeline details).
Guidance note:
Assessment of crack growth due to cyclic loading applying fracture mechanics does typically not included the initiation time of the
fatigue crack. This may be accounted for in the total fatigue life estimate if properly documented by test data.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
5.4.8.16 If the required girth weld quality is determined based on fracture mechanics assessments, both
maximum longitudinal stress/strain (static loads used to perform fracture check) and dynamic loads (used
to perform fatigue crack growth assessments) shall be considered. Recommended procedures are given in
DNVGL-RP-F108.
Guidance note:
The likelihood that the same girth weld will be subjected to fatigue and maximum longitudinal strain/stress during installation
and later in the as-laid stage may be quite small and it may be acceptable not to combine all load cases in the fracture mechanics
assessments, see DNVGL-RP-F108 for some guidance.
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5.4.8.17 The tensile stress-strain curves and fracture toughness/tearing resistance are important input
to the fracture mechanics analyses. Hence, these parameters shall reflect the relevant material condition
(as-welded, strained, strained and aged), temperature and environment representative for the loading
assessed, see DNVGL-RP-F108 for further guidance. Supplementary requirements for line pipes (parent pipe
requirements) in H2S services are provided in [7.9.2].
5.4.8.18 If it is uncertain whether the environment may reduce the fracture toughness compared to in air
environment or it is uncertain if the fatigue crack growth parameters specified in BS 7910 are representative
the fatigue and fracture limit state is considered fulfilled if all the following requirements are satisfied:
ε l,nom ≤ 0.4% and
— acceptable fatigue damage according to [5.4.8.10] and [5.4.8.11] using S-N curve applicable to the
environment and
— single value fracture toughness testing as described in DNVGL-RP-F108 Sec.7 is performed in the
representative environment with CTODmat ≥ 0.15mm. If Jmat is tested the Jmat requirement may be
derived from CTODmat =0.15mm in accordance with BS 7910, i.e.:
—
(5.1)
(5.38)
where Rp0.2 and Rm represents the actual material at the test temperature and relevant environment.
Or:
Maximum allowable flaw sizes are determined in accordance with DNVGL-RP-F108 where all required testing
is performed in the actual environment.
5.4.8.19 For duplex stainless steels and 13Cr martensitic stainless steels or other materials susceptible to
HISC local stresses shall be sufficient low to avoid initiation of HISC. Recommended practice for design of
duplex stainless steels is given in DNVGL-RP-F112.
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5.4.9 Running ductile failure (fracture arrest properties, supplementary
requirement F)
5.4.9.1 Pipeline systems transporting gas or mixed gas and liquids under high pressure shall have adequate
resistance to running ductile fractures. This may be achieved by using:
—
—
—
—
—
material with low transition temperature and adequate Charpy V-notch toughness
adequate DWTT shear fracture area
lowering the stress level
use of mechanical crack arrestors
by a combination of these methods.
Design solutions shall be validated by calculations based upon relevant experience and/or suitable tests.
Requirements to fracture arrest properties need not be applied when the pipeline design tensile hoop stress is
below 40% of fy.
Guidance note:
CO2 is normally in the liquid dense phase during normal operation of a pipeline. When decompressed, CO2 will change phase from
liquid to gas, and this decompression behavior is significantly different compared to natural gas, and needs to be accounted for in
running ductile fracture assessments for pipelines conveying CO2.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
5.4.9.2 Material meeting the supplementary requirement for fracture arrest properties (F), [7.9.2] is
considered to have adequate resistance to running ductile fracture for applications carrying essentially pure
methane up to 80% usage factor, 15 MPa internal pressure and 30 mm wall thickness. For depths down to 10
meters and onshore, the required Charpy V-notch impact energy shall be specially considered.
5.4.10 Ultimate limit state – accidental loads
5.4.10.1 The design against accidental loads may be performed by direct calculation of the effects imposed
by the loads on the structure, or indirectly, by design of the structure as tolerable to accidents.
5.4.10.2 The acceptance criterion for ALS relate to the overall allowable probability of severe consequences.
5.4.10.3 Design with respect to accidental load shall ensure that the overall nominal failure probability
complies with the nominal failure probability target values in Sec.2. The overall nominal failure probability
from accidental loads can be expressed as:
(5.39)
where:
Pfi|Di
PDi
Pf,target
= the probability of failure for the damaging event i
= the probability of the damaging event i within a year
= the relevant nominal target probability of failure within a year, see [2.3]. The number of
discretisation levels shall be large enough to ensure that the resulting probability is evaluated
with sufficient accuracy.
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Guidance note:
The above criterion implies that analyses of a 1000 year event becomes similar to normal ULS design (analysing for a 100 year
event) with one safety class lower, given that the uncertainties are similar
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5.4.10.4 The inherent uncertainty of the frequency and magnitude of the accidental loads, as well as the
approximate nature of the methods for determination of accidental load effects, shall be recognised. Sound
engineering judgement and pragmatic evaluations are hence required.
5.4.10.5 If non-linear, dynamic finite element analysis is applied, it shall be ensured that system
performance and local failure modes (e.g. strain rate, local buckling, joint overloading and joint fracture) are
adequately accounted for by the models and procedures applied.
5.4.10.6 A simplified design check with respect to accidental load may be performed as shown in Table 5-11
using appropriate partial safety factors. The adequacy of simplified design check shall be assessed on the
basis of the summation above in order to verify that the overall failure probability complies with the target
values in Sec.2.
Table 5-11 Simplified design check versus accidental loads
Prob. of occurrence
1)
-2
≥ 10
-3
-3
>PF≥ 10
-4
>PF≥ 10
-5
>PF≥ 10
-6
10
-4
10
-5
10
Safety class medium
Safety class high
Accidental loads may be regarded similar to environmental
loads and may be evaluated similar to ULS design check
-2
10 >PF≥ 10
Safety class low
To be evaluated on a case by case basis
γC = 1.0
γC = 1.0
γC = 1.0
γC = 0.9
γC = 0.9
Accidental loads or events may be disregarded
γC = 0.8
-6
< 10
1)
When failure mode is bursting the probability of occurrence should be 1-2 order of magnitudes lower, see Table 2-5.
Note to table: Standard industry practice assumes safety factors equal to 1.0 for an accidental event with a probability
-2
of occurrence less than 10 within a year and survival of the pipeline is merely related to a conservative definition of
characteristic resistance. In this standard, accidental loads and events are introduced in a more general context with
a link between probability of occurrence and actual failure consequence. For combined loading the simplified design
check proposes a total factor in the range 1.1-1.2, which is consistent with standard industry practice interpreted as
-4
corresponding to safety class medium for accidental loads with a probability of occurrence equal to 10 .
5.4.11 Dent
5.4.11.1 The acceptance criterion for impact refer to an acceptable dent size. The maximum accepted ratio
of permanent dent depth to the pipe diameter is given in the following criterion:
(5.40)
where:
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Hp
η
= permanent plastic dent depth
= usage factor given in Table 5-12. Load effect factors equal to unity.
Table 5-12 Usage factor (η) for impact
Impact frequency
Usage factor
(per year per km)
η
> 100
0
1-100
0.3
-4
0.7
10 -1
5.4.11.2 When allowing for permanent dents, additional failure modes such as fatigue and collapse shall be
taken into account. Any beneficial effect of internal over-pressure, i.e. pop-out should not be included. The
beneficial effects of protective coating may be taken into account. The impact effectiveness of coating shall
be documented.
5.4.12 Ovalisation
5.4.12.1 The submarine pipeline system shall not be subject to excessive ovalisation. The residual flattening
due to bending and point loads, together with the out-of-roundness tolerance from fabrication of the pipe, is
not to exceed 3%, defined as:
(5.41)
The requirement may be relaxed if:
—
—
—
—
a corresponding reduction in moment resistance has been included
geometrical restrictions are met, such as pigging requirements
additional cyclic stresses caused by the ovalisation have been considered
tolerances in the relevant repair system are met.
5.4.12.2 Ovalisation shall be checked for point loads at any point along the submarine pipeline system. Such
point loads may arise at free-span shoulders, artificial supports and support settlements.
5.4.13 Accumulated deformation
5.4.13.1 Accumulated plastic deformation of pipe caused by cyclic loads leading to increased diameter or
ovality (ratcheting) shall be considered. If the ratcheting causes increased ovality, special consideration shall
also be made of the effect on buckling resistance.
5.4.14 Displacement
5.4.14.1 Accumulated longitudinal displacement of the pipeline (pipeline walking) shall be considered. This
may occur during start-up/shut-down for:
— pipeline shorter than two anchor lengths, or
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— pipeline parts with virtual anchor, and
— pipeline laying on seabed slope, or
— pipeline connected to pulling force (e.g. connected to SCR).
5.4.14.2 Design of pipeline shall ensure that the displacement is acceptable. This may be limited by:
— interference with other structures or (seabed) features
— exposures to other loads or threats
— change in configuration causing un-acceptable loading conditions, e.g. excessive free-spans.
5.5 Special considerations
5.5.1 General
5.5.1.1 This subsection gives guidance on scenarios that shall be evaluated separately. Both the load effects
and acceptance criteria are affected.
5.5.2 Pipe soil interaction
5.5.2.1 For limit states influenced by the interaction between the pipeline and the soil, this interaction shall
be determined taking due account for all relevant parameters and the uncertainties related to these.
In general pipeline soil interaction depends on the characteristics of the soil and the pipeline, on the entire
interaction history since and including laying and on the failure mode in question, which shall all be properly
accounted for in the simulation of the pipeline soil interaction.
5.5.2.2 The main soil characteristics governing the interaction are the shear strength and deformation
properties.
5.5.2.3 Pipeline characteristics of importance are submerged weight in all phases, diameter, stiffness,
roughness of the pipeline surface, and initial embedment from installation which shall all be accounted for as
relevant for the limit state in question.
5.5.2.4 All relevant load effects shall be considered. This includes:
— load duration and history effects (e.g. varying vertical reactions from installation laying pressures in
possible combination with horizontal motions)
— variations in the unit weight of the pipe (e.g. empty, water filled and operation conditions)
— cyclic loading effects (both directly from pipe as well as hydrodynamic loads).
5.5.2.5 Calculation of soil resistance for a design situation shall be based on the worst case of high and low
estimates of shear strength affecting the end result for the design situation, as described in [3.3.7.5]. Where
best estimate and upper and lower bounds of the soil resistance shall be defined these shall all relate to the
worst case shear strength definition, but reflect for all other uncertainties, such as assumptions of laying
effects and uncertainties related to selection of calculation method.
5.5.2.6 Some soils have different resistance values for long term loading and for short term loading, related
to the difference in drained and undrained behaviour and to creep effects in drained and undrained condition.
This shall be taken into account.
5.5.2.7 For limit states involving or allowing for large displacements (e.g. lateral pull-in, pipeline expansion
of expansion loops, global buckling or when displacements are allowed for on-bottom condition) the soil will
be loaded far beyond failure, involving large non-linearities, remoulding of soil, ploughing of soil etc. Such
non-linear effects and the uncertainties related to these shall be considered.
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5.5.2.8 For pipelines that are buried (trenched and/or covered by gravel) and susceptible to global buckling
the uplift resistance and possible increased axial resistance shall be considered. The possible effect of backfill
material from trenching shall be considered.
5.5.2.9 Due to the uncertainties in governing soil parameters, load effects, idealization of calculation models
etc., it is difficult to define universally valid methods for simulation of pipe soil interaction effects. The
limitations of the methods used, whether theoretically or empirically based, shall be thoroughly considered in
relation to the problem at hand. Extrapolation beyond documented validity of a method shall be performed
with care, as shall simplifications from the problem at hand to the calculation model used. When large
uncertainties exist, the use of more than one calculation approach shall be considered.
5.5.2.10 Recommended practice on pipe-soil interaction and geotechnical surveys is given in DNVGL-RPF114.
5.5.3 Global buckling
5.5.3.1 For load controlled global buckling, see [5.4.7].
5.5.3.2 Displacement or partially displacement controlled global buckling may be allowed. This implies that
global buckling may be allowed provided that:
— pipeline integrity is maintained in post-buckling configurations (e.g. local buckling, fracture, fatigue etc.)
— displacement of the pipeline is acceptable.
Guidance note:
It is not sufficient to design HP/HT pipelines for global buckling based on worst case axial and lateral soil resistance combined
with displacement controlled local buckling criteria only. These upper and lower bound soil resistance values will typically have a
probability of exceedance in the order of a couple of per cent and will not alone prove a sufficient nominal failure probability. A
more total evaluation of the failure probability is, hence, required.
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5.5.3.3 The pipeline may buckle globally, either downwards (in a free span), laterally (snaking on the
seabed), or vertically (as upheaval buckling of a buried pipeline or on a free-span shoulder of an exposed
pipeline).
5.5.3.4 The following global buckling initiators shall be considered:
— trawl board impact, pullover and hooking
— out of straightness.
5.5.3.5 Recommended practice for structural assessment of high pressure/high temperature pipelines is
given in DNVGL-RP-F110.
5.5.4 Free spanning pipelines
5.5.4.1 Spanning pipelines shall have adequate safety against local buckling, fatigue, fracture and ovality
and these shall be documented.
5.5.4.2 Recommended practice for free spanning pipelines is given in DNVGL-RP-F105.
5.5.5 On bottom stability
5.5.5.1 The pipeline shall not move from its as-installed position. This does not include permissible lateral
or vertical movements, thermal expansion, and a limited amount of settlement after installation. This applies
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for the entire lifetime of the pipeline (including metal loss due to corrosion or erosion). The stability of the
pipeline shall be documented.
Guidance note:
The acceptance criterion on permissible movements may vary along the pipeline route. Examples of possible limitations to pipeline
movements include:
—
local buckling, fatigue and fracture of pipe
—
deterioration/wear of coating
—
geometrical limitations of supports
—
distance from other pipelines, structures or obstacles.
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5.5.5.2 For weight calculations of the pipe, the nominal wall thickness shall be reduced to compensate for
the expected average weight reduction due to metal loss. For pipelines with minor corrosion allowance this
reduction may be omitted and the nominal thickness used.
5.5.5.3 The submarine pipeline system shall have a specific gravity sufficient to avoid floatation. If a
sufficient low probability of negative buoyancy is not documented, the following criterion applies:
(5.42)
Where:
γw
b
Wsub
= safety factor on weight, 1.1
= buoyancy
= submerged weight.
5.5.5.4 Pipelines shall have adequate safety against sinking. Special considerations shall here be made
to mechanical components such as valves and Tee's. If the soil is, or is likely to be, liquefied, it shall be
documented that the depth of sinking will be satisfactorily limited (either by the depth of liquefaction or by
the build-up of vertical resistance during sinking).
Guidance note:
If the specific submerged weight of the water-filled pipe is less than that of the soil, then no further analyses are required to
document safety against sinking.
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5.5.5.5 Buried pipelines shall have adequate safety against floatation in soil.
5.5.5.6 When the pipeline is routed in areas that may be influenced by unstable slopes that could lead
to slope failure and flow of soil that will impact the pipeline, the probability of such slope failures shall be
evaluated. Any relevant slope failure triggering effect, such as wave loading, earthquake loading or man
made activities (e.g. the pipe-laying itself), shall be considered. Possible flow rates and densities at the
pipeline shall be evaluated for stability. If stability cannot be guaranteed by sufficient weight of the pipeline,
by burial of the pipeline or by other means, re-routing of the pipeline shall be required.
5.5.5.7 The most unfavourable combination of simultaneously acting vertical and horizontal forces on the
pipeline shall be considered. When determining this unfavourable combination, the variation in forces along
the line, including directionality effects of waves and current, should be addressed.
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5.5.5.8 Axial (longitudinal) stability shall be checked. The anode structural connection (when exposed to
friction, e.g., pipelines without weight coating) shall be sufficient to sustain the anticipated friction force.
5.5.5.9 Pipeline movements due to thermal axial expansion, shall be allowed for near platforms/structures
(e.g. at riser tie-in point) and where the pipeline changes direction (e.g. at offset spools). The expansion
calculations shall be based upon conservative values for the axial frictional resistance.
5.5.5.10 In shallow water, the repeated loading effects due to wave action may lead to a reduction of the
shear strength of the soil. This shall be considered in the analysis, particularly if the back fill consists of loose
sand, and in general if the soil consists of silt or sand with high silt content. Both cases may be susceptible to
liquefaction.
5.5.5.11 If the stability of the pipeline depends on the stability of the seabed, the latter should be checked.
5.5.5.12 Recommended practice for stability of pipelines exposed to wave and current loads is given in
DNVGL-RP-F109.
5.5.6 Trawling interference
5.5.6.1 The submarine pipeline system shall be checked for all three loading phases due to trawl gear
interaction, as outlined in [4.5].
5.5.6.2 The acceptance criteria are dependent on the trawling frequency (impact) and the safety class.
5.5.6.3 Trawl pullover loads shall be checked in combination with other relevant load effects. Trawl pullover
shall be combined with global buckling. Accumulation of damage due to subsequent trawling is not normally
allowed.
5.5.6.4 Hooking loads shall be checked in combination with other relevant load effects. All relevant failures
modes shall be checked.
5.5.6.5 Recommended practice for trawl and pipeline interference is given in DNVGL-RP-F111.
5.5.7 Third party loads, dropped objects
5.5.7.1 The submarine pipeline system shall be designed for impact forces caused by, e.g. dropped objects,
fishing gear or collisions. The design may be achieved either by design of pipe, protection or means to avoid
impacts.
5.5.7.2 The design criteria shall be based upon the frequency/likelihood of the impact force and classified as
accidental, environmental or functional correspondingly, see [5.4.10].
5.5.7.3 Recommended practice for risk assessment of pipeline protection is given in DNVGL-RP-F107 Sec.5.
5.5.8 Earthquakes
5.5.8.1 The submarine pipeline system shall have adequate resistance against earthquakes.
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Guidance note:
The following scenarios will typically be considered:
—
Local buckling, collapse etc. of the pipeline due to seabed motions and movements
—
Indirect effects (e.g. caused by movements of secondary structures)
—
Failure of gravel supports
—
Potential damage from mud-slides.
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5.5.8.2 For design against earthquakes, see ISO 19901-2.
5.5.9 Thermal insulation
5.5.9.1 If the submarine pipeline system is thermally insulated,
— it shall be documented that the insulation is resistant to the combination of water, temperature and
hydrostatic pressure.
— It should be documented that the insulation is resistant to oil and oil-based products, if relevant.
— It shall be documented that the required mechanical resistance to external loads is sufficient, as
applicable.
— Degradation of the insulation during construction and operation shall be considered.
5.5.10 Settings from plugs
5.5.10.1 Recommended practice for loads from plugs is given in DNVGL-RP-F113 Sec.5.
5.5.11 Pipe-in-pipe and bundles
5.5.11.1 This standard is based on limit state design methodology and may therefore in general be applied
to pipe-in-pipe and bundles if the load effect calculations are performed adequately.
5.5.11.2 Safety class shall be specified for each element in the pipe-in-pipe system and for each phase. The
classification shall be based on the requirements in Sec.2.
5.5.11.3 No specific limit states are given for pipe-in-pipe and bundle configurations. Relevant failure modes
shall be identified for each element in the pipe-in-pipe system and corresponding limit state as appropriate.
In case the consequences are different for the different failure modes, different safety class may be selected
correspondingly.
5.5.11.4 Progressive failure shall be considered when selecting the safety class, i.e. the impact from failure
of one element on another element. This shall include both structural failures as well as functional failures.
5.5.11.5 In case the combined capacity is utilised, the potential for progressive failure should be considered
in selection of the relevant safety class.
5.5.11.6 Inspection possibilities are more limited for pipe-in-pipe and bundles, and hence detection of
corrosion in annulus and external corrosion is challenging. Further, detection of leaks into annulus (from
internal or external fluids) may not be easily identified and the associated environment in the annulus cannot
be fully controlled or reversed. Documentation of the integrity in the operation phase may be limited for a
pipe-in-pipe compared to a single pipe. This will again affect the life-time extension and re-assessment of the
pipeline.
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5.6 Pipeline components
5.6.1 General
5.6.1.1 This subsection is applicable to pressure containing components (e.g. bends, flanges and connectors,
tees, valves, pipe-in-pipe bulkheads) used in the submarine pipeline system. Supporting structure
requirements are given in [5.7].
5.6.1.2 Design of pipeline components shall be according to a recognized standards or recommended
practices combined with the additional requirements listed in Table 5-13.
5.6.1.3 Design of pipeline components shall also comply with the material, manufacturing and test
requirements for components in Sec.8.
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Table 5-13 Referenced standards for structural design of components
Component
All Components listed below
Example of design standards or recommended practices
2)
1)
Additional design
requirements
ASME VIII Division 2/EN 13445/PD 5500
[5.6.1]
Induction Bends
ISO 15590-1
[5.6.2]
Fittings
Tees: ASME B31.4, B31.8
[5.6.3]
Flanges
ISO 15590-3/ISO 7005-1 or NORSOK L005/EN 1591-1/API
6A/ISO 13628-7
Valves
ISO 14723
Mechanical connectors
ASME VIII Division 2/EN 13445/PD 5500/ISO 13628-7
CP Insulating joints
ASME VIII Division 2/EN 13445/PD 5500
[5.6.4]
[5.6.5]
2)
Anchor flanges
N.A. see note
Bolting
ASME VIII Division 2/EN 13445/PD 5500
Pig traps
ASME VIII Division 2/EN 13445/PD 5500
Repair clamps, repair couplings
and hot taps
DNVGL-RP-F113
Bulkheads
ASME VIII Division 2/EN 13445/PD 5500; see note
[5.6.6]
Hot tap’s:
API RP 2201
3)
See [13.6.5]
1)
Other recognised equivalent standards or recommended practices may be used. The listed standards or
recommended practices shall not be used outside its applicability
2)
Required in case the standards or recommended practices used in the design of a component does not take into
account forces other than the internal pressure, see [5.6.1.6].
3)
Allowable stresses may be based on API 6A (see guidance note)
Guidance note:
An alternative method of calculating the limit stress for the elastic or elastic-perfectly plastic analysis methods of ASME VIII
Division 2 is provided in section 5.2.3.5 of API 6A.
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5.6.1.4 All pressure containing components used in the submarine pipeline system should represent at least
the same safety level as the connecting riser/pipeline section.
5.6.1.5 The design pressure for the pipeline component shall be harmonised with the design pressure of the
submarine pipeline systems.
Guidance note:
This implies that the design pressure for the component shall be selected such that it is consistent with the design and incidental
pressure in the submarine pipeline system. Different design standards or recommended practices have different definitions of
design pressure, and a thorough evaluation is required to ensure the consistency in the approach to be taken.
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5.6.1.6 The component shall be designed to accommodate the loading from the connected pipeline section
and vice versa with appropriate level of safety. If the standard or recommended practice used in the design
of a component does not take into account forces other than the internal pressure, additional evaluations,
e.g. FE analyses according to; ASME VIII Division 2/EN 13445/PD 5500 are required in order to address
the maximum forces that can be transferred to the component from the connecting pipeline sections under
installation and operation.
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The strength shall, as a minimum be:
— equivalent to the connecting pipeline, or
— sufficient to accommodate the most probable maximum 100-year load effect that will be transferred to
the component from the connecting pipeline under installation and operation, see Sec.4.
5.6.1.7 The use of other standards and recommended practices for structural design and construction will
require code breaks. The code break shall be maintained for all phases (i.e. not changed from design to
construction phase).
Guidance note:
The code break between line pipe and the relevant component standard may be located at the component weld neck, see Figure
5-3(a).
In practice, the component is likely to be thicker than the pipeline. This requires a transition length, see Figure 5-3(b). The code
break may be located within the component provided the part of the component covered by the pipeline standard or recommended
practice satisfies the material requirements of the pipeline code. Stress and strain concentrations at the girth weld may be avoided
by including a constant wall thickness section. This pipe section (or nib) is recommended to be minimum 4 times the elastic length
of the pipeline section at code break, see DNVGL-RP-C203 App.D. The length may be reduced provided detailed analyses show
nominal pipe section stresses at shorter length.
The elastic length is defined as:
(5.43)
where:
r =
radius to mid surface of the pipeline dimension
t
all thickness of the pipeline
=
v =
Poisson's ratio.
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Figure 5-3 Code breaks between the line pipe and component connection; (a) material-based code
break, and (b) geometry-based code break
5.6.1.8 The same design standard or recommended practice should be applied for all phases, i.e. design,
fabrication, NDT, FAT, installation, commissioning, operation. E.g. if the weld at the code break is performed
according to the component standard or recommended practice, it should also be factory acceptance tested
according to the component standard or recommended practice.
5.6.1.9 The load scenarios as described in Sec.4 as well as particular loads associated with the component
shall be analysed. This implies that also external hydrostatic pressure shall be considered in the design with
respect to both strength and internal leakage when relevant.
5.6.1.10 For material susceptible to HISC, see [6.4.5].
5.6.1.11 Sealing systems should be designed to allow testing without pressurising the pipeline.
5.6.1.12 The pigging requirements in [E.8.4.3] and [3.4.1.2] shall be considered for the component.
5.6.1.13 Transitions in C-Mn and low alloy steels where the nominal material thickness or yield stress is
unequal shall be in accordance with ASME B 31.8 Appendix I, Figure I-5 or equally recognised standard or
recommended practice. Transition in C-Mn line pipe by means of an external or internal taper shall be no
steeper than 1:4. If transitions to these requirements are not feasible, a transition piece shall be inserted.
5.6.1.14 Transitions in duplex stainless steels and 13Cr martensitic stainless steels shall be such that the
local stresses will not initiate HISC. Recommended practice for design of duplex stainless steels is given in
DNVGL-RP-F112.
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5.6.1.15 Internal transitions between different wall thicknesses and internal diameters for girth welds in
pipes of equal SMYS may be made in the base material provided radiographic examination only is specified.
5.6.1.16 For welds to be examined by ultrasonic testing, transition tapering in the base material should be
avoided. If tapering is unavoidable the pipe ends shall be machined to provide parallel external and internal
surfaces before the start of the taper. The length of the parallel surfaces shall at least be sufficient to allow
scanning from the external surface and sufficient for the required reflection off the parallel internal surface.
5.6.1.17 Specifications for installation and make-up of the component shall be established.
5.6.1.18 For pressure testing requirements of components, see Sec.8.
5.6.2 Induction bends
5.6.2.1 This standard does not provide any limit state criteria for pipeline bends.
Guidance note:
Bends exposed to bending moments behave differently from straight pipes. Ovalisation becomes the first order of deformation and
changes the stress pattern considerably compared to straight pipes.
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5.6.2.2 As an alternative to recognised standards or recommended practices the following simplified
Allowable Stress Design (ASD) check may be used provided that:
— The pressure containment criterion in [5.4.2] based on the bend minimum thickness is fulfilled.
— The applied moment and axial load can be considered displacement controlled.
— The moment and axial loads are calculated based on pipe elements, not including the benefit of reduced
stiffness in bends.
— The bend is exposed to internal over pressure or that the bend has no potential for collapse. This can
be considered fulfilled if the system collapse design capacity is three times the external overpressure in
question. The external pressure differential for the collapse limit state, pe - pmin, shall hence be multiplied
by a factor of 3 in Equation (5.10).
Guidance note:
Calculation of t1 is shown in Table 5-5. The wall thickness tolerances should include the effect of thinning and thinning will
therefore not affect the determination of t1. If an excessive thinning is agreed the effect of this is considered minor.
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— That the imposed shape distortion (e.g. ovalisation) is acceptable.
The ASD criteria read:
σe ≤ η · fy
(5.44)
|σl| ≤ η · fy
(5.45)
where:
(5.46)
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(5.47)
(5.48)
η = usage factor as given by Table 5-14
pi = design pressure in line with ISO 13623
N = pipe wall force
M = bending moment, the most critical of tensile or compressive side shall be used.
Guidance note:
The ovalisation of the bend has typically to be determined by finite element calculation. The acceptable distortion will typically be
governed by the bullet points in [5.4.12].
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Table 5-14 Usage factors for equivalent stress check
Safety class
η
Low
Medium
High
1.00
0.90
0.80
5.6.3 Fittings
5.6.3.1 Tees shall be of the extruded outlet, integral reinforcement type when exceeding the maximum of
2 inches (2 3/8”) or an intersection angle of 72°. The design shall be according to ASME B31.4, B31.8 or
equivalent.
5.6.3.2 Bars of barred tees should not be welded directly to the high stress areas around the extrusion neck.
The bars transverse to the flow direction should be welded to a pup piece, and the bars parallel to the flow
direction should be welded to the transverse bars only. If this is impracticable, alternative designs should be
considered in order to avoid peak stresses at the ends.
5.6.3.3 Wyes- and tees where the axis of the outlet is not perpendicular to the axis of the run (lateral tees)
shall not be designed to ASME B31.4 or B31.8, as these items require special consideration, i.e. design by
finite element analysis.
5.6.3.4 Standard butt welding fittings complying with ANSI B16.9, MSS SP-75 or equivalent standards may
be used provided that:
—
—
—
—
the weld is qualified as full penetration weld in compliance with requirements given in App.C.
the weld is examined by RT or UT meeting the requirements given in App.D.
the sweepolet meets the fabrication requirements and mechanical properties outlined in Sec.8.
the geometrical restraints shall be determined based on external nominal dimensions of the branch pipe
(i.e. covering less than 20% of the primary pipe circumference
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— the weld shall be considered equivalent to a girth weld w.r.t toe-to-toe distance etc.
5.6.4 Valves
5.6.4.1 The design shall ensure that internal gaskets are able to seal, and shall include a documented safety
margin which is valid during all relevant pipeline operating conditions. Sealing will be sensitive to internal
deflections, enlargement of gaps and changes in their support conditions. Valve operation will be sensitive to
friction and clearances.
Guidance note:
Guidance on sealing pressure may be found in ISO 13628-7
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5.6.4.2 Consideration should be given to requirements for durability when exposed to abrasive material (e.g.
weld scale, sand etc.) or to fire loads.
5.6.4.3 Valves with requirements for fire durability shall be qualified by applicable fire tests. Reference may
be made to API 6FA and ISO 10497 for test procedures.
5.6.4.4 Valve control systems and actuators shall be designed and manufactured in accordance with
recognised standards. The valve actuator specification should define torque requirements for valve operation,
with a suitable safety margin to accommodate deterioration and friction increase during service.
5.6.4.5 If the standard or recommended practice used for design of a component does not take into account
the possibility for internal leakage due to forces transferred to the component from the connecting pipeline
sections, the additional calculations or qualification tests shall be performed.
5.6.5 Insulating joints
5.6.5.1 CP insulating joints shall be of the boltless, monolithic coupling type and shall be provided with a
double seal system.
5.6.5.2 Insulating joints shall be fitted with pup pieces with mechanical properties and dimensions identical
to that of the adjoining pipeline.
5.6.5.3 Insulating joints shall be capable of meeting the test requirements given in [8.2.9] and to withstand
the effects of the environment without loss of performance.
5.6.5.4 To protect insulating joints and CP equipment from lightning effects, lightning protection shall be
installed. Surge arrestors should be mounted across insulating joints and output terminals of D.C. voltage
sources. Such measures should take into account the need for potential equalisation between the pipeline,
anodes, power supplies, reference electrodes, etc. during lightning strikes. Alternative devices to the spark
gap type can be used if documented to be reliable.
5.6.5.5 Bolting shall meet the requirements of [6.3.4].
5.6.5.6 All elastomeric materials used shall have a documented performance. The sealing materials shall
have documented decompression, creep and temperature properties. O-ring seals shall be resistant to
explosive decompression and AED certified. AED certification is not required for seals other than O-rings,
provided they are enclosed in a completely confined space.
Sealing surfaces exposed to sea water shall be made of materials resistant to sea water at ambient
temperature.
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5.6.5.7 The insulating materials, including dielectric strength, compressive strength and suitability for use at
the design temperatures shall be documented by testing in accordance with ASTM D 695.
5.6.6 Pig traps
5.6.6.1 The design of closures and items such as nozzle reinforcements, saddle supports, vent- kick and
drain branches shall comply with the applied design standard.
5.6.6.2 Closures shall be designed such that the closure cannot be opened while the pig trap is pressurised.
An interlock arrangement with the main pipeline valve should be provided.
5.7 Supporting structure
5.7.1 General
5.7.1.1 Structural items such as support and protective structures that are not welded onto pressurized
parts are considered as structural elements.
5.7.1.2 Steel structural elements shall be designed according to DNVGL-OS-C101Design of offshore steel
structures, general (LRFD method).
5.7.2 Stability of gravel supports and gravel covers
5.7.2.1 This applies to all types of gravel supports and covers, such as free span supports for installation
and operating phases (excessive bending and fatigue), separation and pipeline stabilisation at crossings,
suppressing of upheaval buckling, axial restraints/locking, stabilisation of pipeline etc.
5.7.2.2 The design of the gravel supports and covers shall consider the consequence of failure.
5.7.2.3 The design of the gravel supports and covers shall consider:
—
—
—
—
—
—
—
—
weight of gravel supports and/or covers and pipeline
loads imposed by pipeline (e.g. due expansion)
seabed slope, both longitudinal and horizontal
uncertainty in soil characteristics
resistance against hydrodynamic loads
slope failure (e.g. due to earthquakes)
uncertainty in survey data
subsea gravel installation tolerances, both horizontal and vertical.
5.8 Installation and repair
5.8.1 General
5.8.1.1 The line pipe transportation should comply with the requirements of API RP 5L1 and API RP 5LW.
5.8.1.2 The pipeline strength and stability shall be documented according to the limit states in [5.4] and to
the scenarios in [5.5] above.
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Guidance note:
According to this standard, equivalent limit states are used for all phases. Hence the design criteria in this section also apply to the
installation phase. Installation is usually classified as a lower safety class (safety class low) than operation, corresponding to lower
partial safety factors (higher failure probability).
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5.8.2 Installation analyses
5.8.2.1 The design analysis for the submarine pipeline system shall include both installation and repair
activities, in order to ensure that they can be installed and repaired without suffering damage or requiring
hazardous installation or repair work.
5.8.2.2 The design shall verify adequate strength during all relevant installation phases and techniques to be
used, including:
—
—
—
—
—
—
—
—
—
—
initiation of pipe laying operation
normal continuous pipe laying
pipe lay abandonment and pipeline retrieval
termination of laying operation
tow out operations (bottom tow, off-bottom tow, controlled depth tow and surface tow)
pipeline reeling and unreeling
trenching and back filling
spool installation
tie-in operations
landfalls.
5.8.2.3 The configuration of pipeline sections under installation shall be determined from the laying vessel
to the final position on the seabed. The configuration shall be such that the load effect levels are acceptable
when all relevant effects are taken into account. Discontinuities due to weight coating, buckle arrestors, inline assemblies etc. shall be considered.
5.8.2.4 Critical sea states and directions versus laying parameter ranges shall be determined for the
installation limit condition. The design load effect shall be determined from the characteristic load effects
multiplied by load effect factors as given in [4.3.6] and [10.6.1].
The design load effects shall meet the criteria in Table 5-15.
Guidance note:
During installation, the whole pipeline will be exposed to the same deformation unless larger environmental loads are imposed.
Without environmental loads, system effects are present as failure will occur at the weakest point. With environmental loads there
are no system effects as the failure will occur for the highest load. These considerations are included by check of load combination
a), when system effects are present and load combination b) when system effects are not present. The higher load effect factor in
load combination a is therefor used with a nominal thickness, t2, instead of a minimum wall thickness t1.
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Table 5-15 Installation limit state criteria
Design condition
Equation no.
Safety factors
On-reeling
Equation (5.29)
Load combination a:
γF = 1.2, γc = 0.77 (Seamless pipes)
Alternatively
γF = 1.2, γc = 0.82 (Welded pipes)
Design by detailed analyses considering statistical strength mis-match between pipe
joints
2
Equation (5.28)
γSC,LB = 1.0 , γc = 0.80
3
Equation (5.35)
-
2
Equation (5.28)
-
Equation (5.28)
Benefit of partial displacement controlled condition
may be included if documented
Over bend (S-lay)
Over bend (alternatively)
Stinger tip
Sag bend
2
1
4
1)
When allowing a higher failure probability in compliance with [5.4.6.10]
2)
Effect of point load in accordance with Equation (5.25) – Equation (5.27) applies in line with [5.8.2.5] below.
3)
Effect of point load in accordance with Equation (5.34) applies in line with [5.8.2.5] below.
4)
To be determined considering the effect of point load and varying stiffness, subject to agreement
5.8.2.5 The moment and curvature capacities of the pipeline shall be reduced due to the effect of point load
by Equation (5.25) – Equation (5.27) or Equation (5.34). This typically applies to the rollers of the stinger
and at touch down point in case of a mechanical support or similar. For V-rollers where the contact force
is equally balanced from the two rollers such reduction is not required and applies to the over bend with
exception of the last V-rollers in contact with the pipe.
Guidance note:
The last v-roller in contact with the pipeline will take lateral reactions from vessel movements and will therefore not be equally
balanced by the two rollers.
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5.8.2.6 The local buckling criteria referred to i Table 5-15 applies to line pipe only. For in-line components
and line pipe welded to in-line components, criteria that provides sufficient integrity in the relevant sea-state
shall be determined.
5.8.2.7 Influence from different applied design concepts from vessel to seabed shall be allowed for
throughout the design life.
Guidance note:
Examples hereof may be;
—
influence of increased ovalisation caused by large bending strains during reeling or on over bend on collapse capacity,
—
influence of permanent curvature caused by plastic bending strains during reeling or on over bend on operational condition.
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5.8.2.8 The flattening due to a permanent bending curvature, together with the out-of-roundness tolerances
from fabrication of the pipe shall meet the requirements defined in [5.4.12].
5.8.2.9
If the installation and repair analyses for the submarine pipeline system show that the required parameters
cannot be obtained with the equipment to be used, the submarine pipeline system shall be modified
accordingly.
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5.8.3 Pipe straightness and rotation instability
5.8.3.1 The primary requirement regarding permanent deformation during construction, installation
and repair is the resulting straightness of the pipeline. This shall be determined and evaluated with due
considerations of effects on:
— instability
— positioning of pipeline components e.g. valves and Tee-joints
— operation.
5.8.3.2 The possibility of instability due to out of straightness during installation (twisting) and the
corresponding consequence shall be determined.
5.8.3.3 If in-line assemblies are to be installed potential rotation of the pipe due to out of straightness shall
be controlled such that the load effects are acceptable and no damage to the pipeline or the in-line assembly
occurs, and positioned on the seabed within defined limits.
5.8.3.4 Other effects can also give rotation (curved lay route, eccentric weight, hydrodynamic loads, reduced
rotational resistance during pulls due to lateral play/elasticity in tensioners/pads/tracks etc.) and need to be
considered.
5.8.3.5 Instability during operation, due to out of straightness caused by the installation method and the
corresponding consequences, shall be determined. Residual stresses affecting present and future operations
and modifications shall also be considered.
5.8.3.6 The requirement for straightness applies to the assumed most unfavourable functional and
environmental load conditions during installation and repair. This requirement also applies to sections of
a pipeline where the strains are completely controlled by the curvature of a rigid ramp (e.g. stinger on
installation vessel), whether or not environmental loads are acting on the pipe.
Guidance note:
Rotation of the pipe may take place within the tensioner clamps due to elasticity of the rubber.
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5.8.4 Weight coating
5.8.4.1 Concrete crushing due to excessive compressive forces for static conditions in the concrete during
bending at the overbend is not acceptable. See [5.5.9] for thermal insulation.
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SECTION 6 DESIGN - MATERIALS ENGINEERING
6.1 General
6.1.1 Objective
6.1.1.1 This section provides requirements and recommendations to the selection of materials for submarine
pipeline systems and to the external and internal corrosion control of such systems. Also covered is
the specification of line pipe, pipeline components, coatings and cathodic protection. Finally, general
considerations for fabrication applicable to the design phase are addressed.
6.1.1.2 The purpose of performing materials selection is to assess the feasibility of different candidate
materials (including CRA’s) to meet functional requirements for line pipe and for other components of a
pipeline system. It may also include a cost comparison between candidate materials, including the calculated
costs for operation and any associated risk cost (see [6.4.6.1]). This activity is generally carried out during
conceptual design of submarine pipeline systems.
6.1.2 Application
6.1.2.1 This section is applicable to the conceptual and design phases for submarine pipeline systems. It
contains both normative requirements and information. (Subsections containing only informative text are
indicated Informative in heading).
6.1.2.2 Functional requirements for materials and manufacturing procedures for line pipe and pipeline
components are contained in Sec.7 and Sec.8, respectively. Manufacture and installation of systems for
external corrosion control is addressed in Sec.9. Sec.9 also contains functional requirements to any concrete
coating.
6.1.3 Systematic review
6.1.3.1 The overall requirement to systematic review in Sec.2 will for this section imply:
— Identification and evaluation of threats, the consequences of single failures and series of failures in the
pipeline system applicable for the material selection and corrosion protection philosophy.
— Identification and evaluation of needs for supplementary requirements defined in this standard.
— Identification and evaluation of needs for supplementary requirements not accounted for in this standard.
E.g. for CRA materials, and in particular for lined and clad pipes, it is possible that project specific
requirements and design assumptions lead to requirements and technical solutions that are not fully
accounted for in this standard.
— Review of potential contractors, evaluation of their capabilities and identification of special needs, e.g.
manufacturing procedure qualification, technical audits, follow-up during manufacturing, etc.
6.2 Materials selection for line pipe and pipeline components
6.2.1 General
6.2.1.1 Materials for pipeline systems shall be selected with due consideration of the fluid to be transported,
loads, temperature and possible failure modes during installation and operation. The selection of materials
shall ensure compatibility of all components of the pipeline system. The following material characteristics
shall be considered:
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mechanical properties
hardness
fracture toughness
fatigue resistance
weldability
corrosion resistance.
6.2.1.2 Materials selection shall include identification of the following supplementary requirements for line
pipe given in [7.9] as required:
— supplementary requirement S, H2S service (see [6.2.2])
— supplementary requirement F, fracture arrest properties (see [7.5.1])
— supplementary requirement P, line pipe exposed to plastic deformation exceeding the thresholds specified
in Table 5-10 (see Table 6-1 and ) [E.8.8.10]
— supplementary requirement D, more stringent dimensional requirements (see [E.8.7.5])
— supplementary requirement U, increased utilisation (see [8.7.4.5]).
6.2.1.3 The mechanical properties, chemical composition, weldability and corrosion resistance of materials
used in components shall be compatible with the part of the pipeline system where they are located. Low
internal temperatures due to system depressurisation shall be considered during the material selection.
6.2.2 H2S service
6.2.2.1 Pipelines to route fluids containing hydrogen sulphide (H2S) shall be evaluated for H2S service
(also referred to as sour service) according to ISO 15156. For all pipeline components exposed to such
internal fluids, materials shall be selected for compliance with this standard. For materials specified for
H2S service in ISO 15156, specific hardness requirements always apply. These are applicable both to
manufactured materials as-delivered after manufacture and after fabrication (e.g. welding). For certain
materials, restrictions for manufacture (e.g. heat treatment) and fabrication (e.g. cold forming) apply).
6.2.2.2 Any materials to be used that are not covered by ISO 15156 (e.g. C-Mn and low alloy steels with
SMYS > 450 MPa, 13Cr martensitic stainless steels), shall be qualified according to the said standard. The
same applies if a material specified for H2S service is to be used beyond the conditions specified (e.g. max.
hardness). In accordance with ISO 15156-2/3, the pipeline operator shall verify and retain the qualification
records in case the testing was initiated by a contractor or supplier.
Guidance note:
Purchaser may consider to specify SSC testing of material grades meeting all requirements for H2S service in ISO 15156 as a part
of a program for pre-qualification of line pipe manufacturing or pipeline installation procedures. For such testing, the methods and
acceptance criteria in ISO 15156-2/3 apply.
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6.2.2.3 ISO 15156, Sec.1, states that the standard is only applicable to the qualification and selection of
materials for equipment designed and constructed using conventional elastic design criteria. Any detrimental
effects of induced loading will only apply if these are imposed during exposure to an H2S-containing
environment. ISO 15156 is thus not required to be fulfilled if H2S is not present (e.g. for manufacture and
installation of pipelines). Any restrictions for maximum allowable strain during operation are beyond the
scope of this standard.
6.2.2.4 Supplementary requirements to H2S service in this standard are given in [7.9.1] and [8.3.6].
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6.2.3 Corrosion resistant alloys
6.2.3.1 Type 13Cr martensitic stainless steels (i.e. proprietary alloys developed for oil/gas pipelines) are
generally considered fully resistant to CO2-corrosion, provided welds have adequate PWHT. 22Cr and 25Cr
duplex stainless steel and austenitic CRAs are also fully resistant and do not require PWHT. Duplex (ferriticaustenitic) and martensitic stainless steels may be less tolerant than C-Mn steel to well stimulation acids.
Corrosion inhibitors for such acids developed for C-Mn steels may not be effective for CRAs.
6.2.3.2 Under conditions when water, oxygen and chloride can be present in the fluid, e.g. water injection,
stainless steels can be susceptible to localised corrosion. Hence, the corrosion resistance shall be considered
for each specific application. For special applications, corrosion testing should be considered to qualify the
material for the intended use.
6.2.3.3 Alloy 625 (UNS N06625) is generally considered immune to ambient temperature seawater. Also
type 25Cr duplex (e.g. UNS S32750/S32760) are generally resistant to ambient temperature seawater but
require more stringent control of microstructure in base material and weld, consequently corrosion testing
are often included for the qualification of manufacturing and fabrication procedures of these materials. Type
22Cr duplex, AISI 316 and Alloy 825 (UNS N08825) are not resistant to corrosion by raw seawater but are
applicable for components exposed to treated seawater (deoxygenated to max. 10 ppb and max. 100 ppb as
max monthly and daily residual concentrations of oxygen). For the latter materials, corrosion testing is not
normally included in specifications for manufacture and fabrication.
6.2.3.4 Duplex and martensitic stainless steel line pipe and pipeline components require special
considerations of the susceptibility of environmentally assisted cracking, primarily (HISC), see [6.4.5.2].
Guidance note:
In particular concerns of HISC apply to material subjected to plastic straining during installation, commissioning (in particular
pressure testing) and operation with cathodic protection applied. PWHT is known to reduce the HISC susceptibility of welds for
13Cr martensitic stainless steel. Recommended practice for duplex stainless steel and HISC design is given in DNVGL-RP-F112.
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6.2.3.5 In addition to resistance to internal corrosion and environmentally assisted cracking, the following
major parameters shall be considered:
— mechanical properties
— ease of fabrication, particularly weldability.
Guidance note:
Procurement conditions such as availability, lead times and costs should also be considered.
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6.2.4 Line pipe
6.2.4.1 Acceptance criteria and inspection requirements for line pipe, including pipe mill manufacturing
welds, are given in Sec.7, with supplementary requirements specified in [7.9]. Additional information,
relevant for the selection and specification of line pipe is provided in Table 6-1.
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Table 6-1 Additional information for selection and specification of line pipe
Considered aspect
Remark
Uniform elongation
Uniform elongation will in many cases be more relevant than elongation-atbreak. Uniform elongation is the plastic deformation that takes place before
necking starts. With information of the uniform elongation for a material it
will be possible to more accurately determine how much safety margin is in a
structure.
The uniform elongation can be determined by taking the total deformation
at maximum load (i.e. the highest point of the stress-strain curve) and
subtracting the elastic deformation (i.e. draw a line parallel to the initial
loading curve down from the high point).
Dimensional tolerances
The most prominent benefit of specifying Supplementary requirement D is
the eased fit-up prior to welding. Improved fit-up implies reduced stress
concentrations and improved structural integrity. The tolerances specified in
[7.9.4] are considered to be in the uppermost range of what may be achieved
by reputable pipe mills. Stricter tolerances and additional requirements such
as e.g. pipe eccentricity may be specified for further improvements, but may
be costly as machining may be required. Supplementary requirement D is also
beneficial when the pipe is exposed to high plastic straining due to reduced
possibility for local buckling (reduced wall thickness difference between two
adjoining pipes).
Corrosion testing of the CRA material of
clad or lined line pipe
For Alloy 625 (UNS N06625) clad or lined pipe specified to be seawater
resistant, testing according to ASTM G48, Method A, should be considered,
with acceptance criteria as for 25Cr duplex, see [7.3.4.9].
Gripping force of lined line pipe
The gripping force (see [D.2.1.5]) should be determined with due
consideration of the project requirements, especially the level of installation
and operational bending stresses. If no particular requirements are identified,
the requirement should be based on the gripping force obtained during MPQT.
Influence of coating application on
mechanical properties
Pipe tensile properties may be affected by high temperature during coating
application. During pipe coating, including field coating, the pipes might be
exposed to temperatures up to approximately 250°C. For TMCP processed
pipes and cold formed pipes not subjected to further heat treatment
mechanical properties may change due to strain aging, causing e.g. increased
yield stress. This may further affect the critical defect size considerably if the
pipe is strained above the yield stress.
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Considered aspect
Remark
Fracture arrest properties
Supplementary requirements to fracture arrest properties (F) are given in
[7.9.2] and are valid for gas pipelines carrying essentially pure methane up to
80% usage factor, up to a pressure of 15 MPa, 30 mm wall thickness and 1120
mm diameter.
For conditions outside the above limitations the required fracture arrest
properties should be based on calculations which reflect the actual conditions
or on full-scale tests. The fracture toughness required to arrest fracture
propagation for rich gas, i.e. gas mixtures that enter the two-phase state
during decompression can be much higher than for essentially pure methane.
Calculations should be carried out by use of the Battelle Two Curve Method
(TCM) and the appropriate correction factor for calculated required Charpy
values ≥ 95 J. The Battelle TCM should be calibrated by use of data from fullscale test which are as close as possible to the actual pipeline conditions with
regard to gas pressure, pipeline dimensions and gas composition. Although the
Battelle TCM is based on physical models of the speed of crack propagation
and the speed of decompression, it includes constants that are based on fitting
data and calculations within a limited range of test conditions.
Reeling of longitudinally welded pipes
and clad pipes
Due to the limited field experience, special considerations should be made for
longitudinally welded pipes to ensure that both the longitudinal weld, heat
affected zone and base material of such pipes are fit for intended use after
significant straining.
The weld metal strength of the pipe longitudinal weld should overmatch the
strength of the base material. It is further recommended to have a limited cap
reinforcement of the longitudinal weld in order to avoid strain concentrations.
Supplementary requirement U qualification in retrospect
The purchaser may in retrospect upgrade a pipe delivery to be in accordance
with supplementary requirement U. The requirements for such upgrade are
stated in [7.9.5].
6.2.5 Pipeline components
6.2.5.1 Materials for components should be selected to comply with internationally recognised standards
meeting the requirements given in Sec.7 and Sec.8. Modification of the chemical composition given in
such standards may be necessary to obtain a sufficient combination of weldability, hardenability, strength,
ductility, toughness and corrosion resistance.
6.2.5.2 A component should be forged rather than cast whenever a favourable grain flow pattern, a
maximum degree of homogeneity, and the absence of internal flaws are of importance.
6.2.5.3 For component material delivered in the quenched and tempered condition, the tempering
temperature should be sufficiently high to allow effective post weld heat treatment during later manufacture/
installation. The minimum tempering temperature should, if lower than 610°C, be specified by the purchaser.
If welds between the component and other items such as line pipe are to be post weld heat treated at a
later stage, or if any other heat treatment is intended, a simulated heat treatment of the test piece should, if
required, be specified by the purchaser.
6.2.5.4 If the chemical composition and the delivery condition of components require qualification of a
specific welding procedure for welding of the joint between the component and the connecting line pipe, then
the component should be fitted with pup pieces of the line pipe material in order to avoid field welding of
these components.
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Alternatively, rings of the component material should be provided for welding procedure qualification of the
field weld.
6.2.5.5 Particular consideration should be given to the suitability of elastomers and polymers for use in the
specific application and service conditions. NORSOK M-710 and ISO 23936-2 give suitable description of
methodology for establishing chemical compatibility and service life and may be used.
6.2.6 Bolts and nuts
6.2.6.1 For selection of bolting materials, see [8.3.5], plus [6.2.6.3] and [6.2.6.4] of this section.
6.2.6.2 When bolts and nuts shall be used at elevated temperature strength de-rating shall be applied, see
[5.3.3]. See also guidance note in [8.3.5.2].
6.2.6.3 Stainless steel according to ASTM A193/ASTM A320 grade B8M (type AISI 316) is applicable but
requires efficient cathodic protection for subsea use. UNS N06625 or other Ni-based solution hardening alloys
with equivalent or higher PRE are applicable as subsea bolting material without cathodic protection. These
bolts shall only be used in the solution annealed condition (ASTM B446) or cold-worked to SMYS 720 MPa
maximum. Restrictions for H2S service according to ISO 15156 shall apply when applicable.
6.2.6.4 To restrict damage by HISC for low alloy and carbon steels, the hardness for any bolts and nuts to
receive cathodic protection shall not exceed 35 HRC or 350 HV, as specified for the standard grades in Sec.8,
Table 8-3. The same restriction shall apply for solution annealed or cold-worked type AISI 316 austenitic
stainless steel and any other cold-worked austenitic alloys. Precipitation hardening Fe-or Ni-base alloys,
duplex and martensitic stainless steels should not be specified as bolting material if subject to cathodic
protection. For certification and traceability of bolts, see [6.3.4].
6.2.6.5 Any coating of bolts and nuts shall be selected with due considerations of how such coatings affect
tensioning and as-installed properties.
Guidance note:
Zinc coating, phosphatising and epoxy based coatings are applicable; however, there have been concerns that hot-dip zinc
coating may cause loss of bolt tensioning and that polymeric coatings may prevent efficient cathodic protection by electrically
insulating the bolt from a cathodically protected surface. PTFE coatings have low friction coefficient and the torque has to be
applied accordingly.
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6.2.7 Welding consumables
6.2.7.1 Requirements to welding are covered in App.C. Requirements that are specific for pipeline installation
welding are given in Sec.10. Below is provided guidance regarding the influence of weld metal strength on
allowable defect size as determined by ECA (if applicable).
6.2.7.2 The requirement for welds to have strength level equal to or higher than (overmatching properties)
the base material is to minimise deformation in the area adjacent to any possible defects.
6.2.7.3 For pipes exposed to global yielding, i.e. when girth welds are exposed to strain εl,nom ≥ 0.4%,
it is required to perform an ECA according to DNVGL-RP-F108. The ECA generally requires that the weld
metal yield stress is matching or overmatching the longitudinal yield stress of the pipe. An ECA involving
undermatching weld metal will require special considerations, see DNVGL-RP-F108.
6.2.7.4 It shall be noted that the reduction in yield stress at elevated temperature may be higher for
the weld metal than the base material. Hence, undermatching may be experienced for high operation
temperatures (e.g. snaking scenario). This is particularly relevant when welding clad or lined line pipe.
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Whenever such situations occur, it will be required to perform transverse all weld tensile testing of the weld
metal and fracture toughness testing at the relevant temperature.
6.3 Materials specification
6.3.1 General
6.3.1.1 Requirements to the manufacture of line pipe and pipeline components are covered in Sec.7 and
Sec.8, respectively. This includes requirements to all relevant manufacturing steps from steel making to
dispatch from the pipe mill or component manufacturing facility, but excluding any permanent external/
internal coating.
6.3.2 Line pipe specification
6.3.2.1 A specification reflecting the results of the materials selection according to this section and
referring to Sec.7, shall be prepared by the purchaser. The specification shall state any options, additional
requirements to and/or deviations from this standard pertaining to materials, manufacture, fabrication and
testing of line pipe.
6.3.2.2 The material specification may be a Material Data Sheet referring to this standard.
6.3.2.3 The materials specification shall as a minimum include the following (as applicable):
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quantity (e.g., total mass or total length of pipe)
manufacturing process (see [7.1.4])
type of pipe (see [7.1.2.1])
SMYS
if the strain ageing effect achieved during external coating should be addressed (see Table 6-1)
outside or inside diameter
wall thickness
wall thickness tolerances (see [4.7.4.6] and Table 7-20/Table 7-21)
whether data of the wall thickness variation (tmax and tmin) or the standard deviation in wall thickness
variation shall be supplied to facilitate girth welds AUT (see [E.2.1.7])
length and type of length (random or approximate)
application of supplementary requirements (S, F, P, D or U), see [6.2.1.2] and [6.2.1.3]
delivery condition (see Sec.7, Table 7-1 and [7.8.2])
minimum design temperature
range of sizing ratio for cold-expanded pipe
chemical composition for wall thickness > 25 mm (applicable to C-Mn steel pipe with delivery condition N
or Q)
chemical composition for wall thickness > 35 mm (applicable to C-Mn steel pipe with delivery condition M)
if additional tensile testing in the longitudinal direction with stress strain curves shall be performed
production tensile testing of base material at elevated temperatures is not required by this standard,
however, if this is requested by purchaser, temperature (e.g. maximum design temperature), acceptance
criteria and test frequency shall be defined
CVN test temperature for wall thickness > 40 mm
liner/cladding material (UNS number)
mechanical and corrosion properties of liner/cladding material
type of seal weld for lined line pipe
thickness of carrier pipe and liner/cladding material
any project specific requirements to gripping force of lined line pipe
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if the ultrasonically lamination checked zone at the pipe ends shall be wider than 50 mm
if diameter at pipe ends shall be measured as ID or D
if pipes shall be supplied with other than square cut ends (see [7.2.3.38])
if criteria for reduced hydrostatic test pressure, as given in [7.5.1.4], is fulfilled, and if it may be applied
if the outside weld bead shall be ground flush at least 250 mm from each pipe end to facilitate girth welds
AUT (see Table 7-22)
if inside machining of pipe ends is applicable, and the distance from pipe end to tapered portion (see
[7.2.3.39], and [E.2.1.8])
if pipes shall be supplied with bevel protectors, and in case of what type (see [7.8.3])
if weldability testing is required
if qualification testing shall be conducted after the pipe material has been heated to the expected coating
temperature when fusion bonded epoxy is used (see Table 6-1 and [7.4.7.10])
application of the alternative weld cap hardness of C-Mn steel pipe according to supplementary
requirement S (see [7.9.1.7])
if SSC testing shall be performed during MPQT for pipes conforming to supplementary requirement S
if supplementary requirement P apply, the relevant straining for the installation process, possible
corrective actions (e.g. reel on and reel off twice) and post installation conditions/operations introducing
plastic deformation shall be specified.
6.3.3 Components specification
6.3.3.1 A specification reflecting the results of the materials selection according to this section and
the pressure test philosophy in [5.2.2] and referring to Sec.8, shall be prepared by the purchaser. The
specification shall state any options, additional requirements to and/or deviations from this standard
pertaining to materials, manufacture, fabrication and testing of the components.
6.3.3.2 The materials specification shall as a minimum include the following (as applicable):
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quantity (i.e the total number of components of each type and size)
design standard
required design life
material type, delivery condition, chemical composition and mechanical properties at design temperature
nominal diameters, D or ID, out of roundness and wall thickness for adjoining pipes including required
tolerances
bend radius, see [8.2.3.15]
type of component, piggable or not piggable
gauging requirements, see [10.10.2.10]
minimum design temperature (local)
maximum design temperature (local)
design pressure (local)
water depth
pipeline operating conditions including fluid characteristics
details of field environmental conditions
external loads and moments that will be transferred to the component from the connecting pipeline under
installation and operation and any environmental loads
functional requirements
material specification including, material type, delivery condition, chemical composition and mechanical
properties at design temperature
required testing
required weld overlay, corrosion resistant or hardfacing
if pup pieces of the line pipe material shall be fitted
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— coating/painting requirements.
6.3.4 Specification of bolts and nuts
6.3.4.1 .Bolts and nuts shall be supplied with certificates to EN 10204 Type 3.1 or ISO 10474 type 3.1.B.
Bolts and nuts for pressure containing applications shall be marked for traceability to such certificates.
Transfers of test results obtained by specific inspection on primary or incoming products shall not be
acceptable for mechanical properties. Fasteners originating from different manufacturing lots shall not be
commingled.
6.3.4.2 Bolts and nuts for pressure containing and main structural applications should be specified to have
rolled threads.
6.3.4.3 Any coating of bolts shall be specified in the purchase document for bolting. Bolts to be installed
continuously submerged in seawater shall be designed to receive cathodic protection and do not need any
coating for corrosion control.
Guidance note:
See [6.2.6] for more information regarding use of bolts and nuts exposed to cathodic protection. For bolts to be exposed in splash
zone or atmospheric zone corrosion protective coating may be considered.
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6.3.5 Coating specification
6.3.5.1 As a part of detailed design, project specific requirements to as-applied coating properties and
to quality control of the manufacture of coating materials and of coating application shall be defined in a
purchase specification.
6.3.5.2 The specification of line pipe coating, field joint coating and any weight coating shall include
requirements to the qualification of coating materials, coating application and repair procedures, dimensions
of the line pipe cut-back (including tolerances) and to documentation of inspection and testing. Cut-backs
shall be defined to accommodate any AUT equipment.
6.3.5.3 For specific line pipe and field joint coating systems the minimum requirements in ISO 21809 (part
1-3) shall apply with some additional requirements given in [9.2] in this standard. For concrete coating
the minimum requirements in ISO 21809-5 shall apply with additional requirements given in [9.3] in this
standard.
6.3.5.4 Recommended practice for application of line pipe and field joint coating systems (some additional
systems to those defined in ISO 21809) are given in DNVGL-RP-F106 and DNVGL-RP-F102.
Guidance note:
The above RPs complies with and refers to ISO 21809 and give some additional requirements and guidance to coating design and
quality control of application.
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6.3.6 Galvanic anode specification
6.3.6.1 As a part of design, specifications for manufacture and installation of galvanic anodes shall be
prepared. These documents shall define requirements to materials, properties of anodes and anode
fastening (including any special provisions for electrical continuity), and associated quality control. Detailed
requirements are given in Sec.9.
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6.3.7 Concrete coating specification
6.3.7.1 If concrete coating is applicable, project specific requirements to concrete coating shall be defined in
a purchaser specification as part of detail design. ISO 21809-5 gives requirements to information that shall
be supplied by the purchaser and additional requirement given in [6.3.7.2] to [6.3.7.3] shall be included.
Requirements to materials and concrete coating application are specified in Sec.9.
6.3.7.2 The amount of reinforcement shall be designed for the specific project; i.e. take into account the
actual installation, laying and operation conditions for the pipeline. The percentage of reinforcement specified
in [9.3] should be considered as absolute minimum amounts.
6.3.7.3 Minimum shear resistance capacity between concrete coating and corrosion coating shall be specified
by the offshore laying contractor and included in the concrete coating specification.
For coal tar asphalt/coal tar enamel line pipe coating the effect of operating temperature (>40°C) on shear
strength capacity should be considered to prevent axial sliding of pipeline inside concrete coating.
6.4 Corrosion control
6.4.1 General
6.4.1.1 All components of a pipeline system shall have adequate corrosion control both externally and
internally to avoid failures caused or initiated by corrosion.
Guidance note:
Any corrosion damage may take the form of a more or less uniform reduction of pipe wall thickness, but scattered pitting and
grooving corrosion oriented longitudinally or transversally to the pipe axis is more typical. Stress corrosion cracking is another form
of damage. Uniform corrosion and corrosion grooving may interact with internal pressure or external operational loads, causing
rupture by plastic collapse or brittle fracture. Discrete pitting attacks are more likely to cause a pinhole leakage once the full pipe
wall has been penetrated.
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6.4.1.2 Pipeline systems may be exposed to a corrosive environment both internally and externally.
Options for corrosion mitigation include use of corrosion protective coatings and linings, cathodic protection
(externally only), and chemical treatment or fluid processing (internally only).
6.4.2 Corrosion allowance
6.4.2.1 For submarine pipeline systems a corrosion allowance may serve to compensate for internal and/
or external corrosion and is mostly applied for control of internal or external pressure. For C-Mn steel
components, a corrosion allowance may be applied either alone or in addition to some system for corrosion
mitigation. However, for external corrosion protection of continuously submerged components, cathodic
protection is mandatory and a corrosion allowance for external corrosion control is then superfluous.
Guidance note:
A requirement for wall thickness determined by installation forces and exceeding that needed for pressure containment at the
initial design pressure, or wall thickness not needed for pressure containment due to a later down rating of operational pressure
can be utilised for corrosion control but is not referred to in this document as a corrosion allowance.
A corrosion allowance is primarily used to compensate for forms of corrosion attack affecting the pipeline's pressure containment
resistance, i.e. uniform attack and, to a lesser extent, corrosion damage as grooves or pits. Such damage is unlikely to affect the
pipeline's pressure containment resistance but will cause a pinhole leak when the full wall thickness is penetrated. Any extra wall
thickness will then only delay leakage in proportion to the increase in wall thickness.
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6.4.2.2 The needs for, and benefits of, corrosion allowance shall be evaluated, taking into account the
following factors as a minimum:
— design life and potential corrosivity of fluid and/or external environment
— expected form of corrosion damage (see guidance note above)
— expected reliability of planned techniques and procedures for corrosion mitigation (e.g. chemical
treatment of fluid, external coating, etc.)
— expected sensitivity and damage sizing capability of relevant tools for integrity monitoring, time to first
inspection and planned frequency of inspection
— consequences of sudden leakage, requirements to safety and reliability
— any extra wall thickness applied during design for installation forces and not needed for control of internal
and external pressure
— any potential for down-rating (or up-rating) of operating pressure.
6.4.2.3 An internal corrosion allowance of minimum 3 mm should be used for C-Mn steel pipelines of safety
class medium and high carrying hydrocarbon fluids likely to contain liquid water during normal operation. For
nominally dry gas and for other fluids considered as non-corrosive, no corrosion allowance is required.
6.4.3 Temporary corrosion protection
6.4.3.1 The need for temporary corrosion protection of external and internal surfaces during storage and
transportation shall be considered during design/engineering for later inclusion in fabrication and installation
specifications. Optional techniques include end caps or bevel protectors, temporary thin film coating and rust
protective oil/wax.
Guidance note:
Outdoor storage of unprotected pipes for a period of up to about a year will not normally cause any significant loss of wall
thickness. However, superficial rusting may cause increased surface roughness affecting pipeline coating operations. Conditions
for storage should be such that water will not accumulate internally, or externally at any supports. End caps may retain water
internally if damaged or lost at one end, allowing entry of rain water or condensation. Temporary coating applied at coating cutbacks may interfere with pipeline girth welding.
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6.4.3.2 The needs for corrosion protection during flooding shall be assessed for inclusion in installation
specifications. Special precautions are required to avoid corrosion damage to CRA pipelines during system
pressure testing using seawater. Type 13Cr line pipe may suffer superficial corrosion attack during outdoor
storage.
Guidance note:
The use of a biocide for treatment of water for flooding is most essential (even with short duration) as incipient bacterial growth
established during flooding may proceed during operation and cause corrosion damage (pipelines for dry gas are excluded). For
uncoated C-Mn steel pipelines, an oxygen scavenger may be omitted since oxygen dissolved in sea-water will become rapidly
consumed by uniform corrosion with-out causing significant loss of wall thickness. Film forming or passivating corrosion inhibitors
are not actually required and may even be harmful. Type 13Cr steel is highly susceptible to damage by raw seawater or marginally
treated seawater even at a short exposure period. Use of fresh water should be considered or seawater treated to a pH of 9
minimum.
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6.4.4 External pipeline coatings
6.4.4.1 Line pipe coating (also referred to as factory coating or parent coating) refers to factory applied
external coating systems (mostly multiple-layer, with a total thickness of some millimetres) with a corrosion
protection function, either alone or in combination with a thermal insulation function. Some coating systems
may further include an outer layer for mechanical protection, primarily during laying and any rock dumping
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or trenching operations. Concrete coating for anti-buoyancy (weight coating, see [9.3]) is, however, not
covered by the term line pipe coating.
6.4.4.2 Field joint coating (FJC) refers to single or multiple layers of coating applied to protect girth welds
and the associated cut-back of the line pipe coating, irrespectively of whether such coating is actually applied
in the field or in a factory (e.g. pipelines for reel laying). Coating field repairs refers to repairs of factory
coating performed in the field (typically by the FJC contractor).
6.4.4.3 The line pipe (external) coating system should be selected based on consideration of the following
major items:
— general corrosion-protective properties dictated by permeability for water, dissolved gases and salts,
adhesion, freedom from pores, etc.
— resistance to physical, chemical and biological degradation leading to e.g. cracking or disbondment,
primarily in service but also during storage prior to installation (temperature range and design life are
decisive parameters)
— requirements for mechanical properties, primarily those related to adhesion and flexibility, during
installation (min. temperature) and operation (max. temperature)
— coating system’s compatibility with specific fabrication and installation procedures, including field joint
coating and coating field repairs
— coating systems compatibility with concrete weight coating (see [9.3]), if applicable
— coating system’s compatibility with CP, and capability of reducing current demand for CP, if applicable
— line pipe material’s compatibility with CP considering susceptibility to HISC; see [6.2.3.4]
— line pipe material’s susceptibility to corrosion in the actual environment, including stress corrosion
cracking in the atmospheric zone and any onshore buried zone
— environmental compatibility and health hazards during coating application, fabrication/installation and
operation.
6.4.4.4 For thermally insulating coatings, properties related to flow assurance also apply; e.g. specific heat
capacity, thermal conductivity and the degradation of such properties by high operating external pressure
and internal fluid temperature.
6.4.4.5 Pipeline components should have external coatings matching the corrosion protective properties
of those to be used for line pipe. If this is not practical, CP design may compensate for inferior properties.
However, risks associated with HISC by CP shall be duly considered (see [6.2.3.4] and [6.4.5.2] guidance
note).
6.4.4.6 For the selection of FJC, the same considerations as for pipeline and riser coatings as in [6.4.4.3],
[6.4.6.5] and [6.4.6.6] apply. In addition, sufficient time for application and cooling or curing is crucial during
barge laying of pipelines.
6.4.4.7 For pipes with a weight coating or thermally insulated coating, the field joint coating (FJC) is typically
made up of an inner corrosion protective coating and an in-fill. The objective of the in-fill is to provide a
smooth transition to the pipeline coating and mechanical protection to the inner coating. For thermally
insulated pipelines, requirements for adequate insulating properties may also apply. The requirements and
guidelines to FJC are also applicable to any field repairs of factory coating
6.4.4.8 The design and quality control of field joint coatings is essential to the integrity of pipelines in HISC
susceptible materials, including ferritic-austenitic (duplex) and martensitic stainless steel. Recommended
practice for design and quality control of field joint coatings is given in DNVGL-RP-F102.
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6.4.5 Cathodic protection
6.4.5.1 Pipelines in the submerged zone shall be furnished with a cathodic protection (CP) system to provide
adequate corrosion protection for any defects occurring during coating application (including field joints), and
also for any subsequent damage to the coating during installation and operation. The design of submarine
pipeline CP systems shall meet the minimum requirements in ISO15589-2. See DNVGL-RP-F103 for some
additional amendments and guidelines.
Guidance note:
CP may be achieved using either galvanic (sacrificial) anodes, or impressed current from a rectifier. Galvanic anodes are normally
preferred.
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6.4.5.2 The CP systems shall be capable of suppressing the pipe-to-seawater (or pipe-to-sediment)
electrochemical potential into the range -0.80 to -1.15 V rel. Ag/AgCl/ seawater. A less negative potential
may be specified for pipelines in CRA materials.
Guidance note:
Potentials more negative than -1.15 V rel. Ag/AgCl/ seawater can be achieved using impressed current. Such potentials may
cause detrimental secondary effects, including coating disbondment and HISC of line pipe materials and welds. Pipeline system
components in high-strength steel, and particularly in martensitic or ferritic-austenitic (duplex) stainless steel, subject to high
local stresses during subsea installation activities (e.g. pre-commissioning) or operation can suffer HISC by CP, also within the
potential range given above. Such damage is primarily to be avoided by restricting straining subsea by design measures. In
addition, special emphasis should be laid on ensuring adequate coating of components that may be subject to localised straining. It
is essential that the coating systems to be applied (i.e. factory applied coating and field joint coating) for materials that are known
to be susceptible to HISC have adequate resistance to disbonding by mechanical effects during installation as well as chemical/
physical effects during operation. Overlay welding of critical areas with austenitic CRA filler materials may be considered when
organic coatings are not applicable. Thermally sprayed aluminium coating has also been applied for this purpose. Other measures
to reduce or eliminate the risk of HISC include control of galvanic anodes by diodes and use of special anode alloys with less
negative closed circuit potential. (These techniques require that the pipeline is electrically insulated from conventional CP systems
on electrically connected structures). In case conventional bracelet anodes are still to be used, welding of anodes to any pressure
containing components in these materials should be avoided.
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6.4.5.3 Galvanic anode CP systems should be designed to provide corrosion protection throughout the
design life of the protected object.
Guidance note:
As retrofitting of galvanic anodes is generally costly (if practical at all), the likelihood of the initial pipeline design life being
extended should be duly considered.
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6.4.5.4 Pipeline systems connected to other offshore installations shall have compatible CP systems unless
an electrically isolating joint is to be installed. At any landfall of an offshore pipeline with galvanic anodes and
with impressed current CP of the onshore section, the needs for an isolation joint shall be evaluated.
Guidance note:
Without isolating joints, some interaction with the CP system of electrically connected offshore structures cannot be avoided.
As the design parameters for subsea pipelines are typically more conservative than that of other structures, some current drain
from riser and pipeline anodes to the CP system of the connecting system cannot be avoided, sometimes leading to premature
consumption. When the structure has a correctly designed CP system such current drain is not critical as the net current drain will
decrease with time and ultimately cease; i.e. unless the second structure has insufficient CP.
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6.4.5.5 Pipelines should be designed with a self-sustaining CP system based on bracelet anodes installed
with a maximum distance of 300 m (in accordance with ISO 15589-2) and with electrical connections to the
pipeline by pin brazing or aluminothermic welding of cable connections to the pipe wall. (See [C.5.5]).
For shorter pipelines (up to 30 km approximately), CP may be achieved by anodes installed on structures at
the end of the pipeline (e.g. platform sub-structure, subsea template or riser base) electrically connected to
the pipeline. This concept requires, however, that the design and quality control of factory applied coatings,
field joint coatings and coating field repairs are closely defined (e.g. as in DNVGL-RP-F106 Sec.6 and DNVGLRP-F102). A recommended procedure to calculate the protective length of anodes on an adjacent structure is
given in DNVGL-RP-F103.
Guidance note:
ISO 15589-2 gives an alternative procedure but, contrary to DNVGL-RP-F103, does not define the primary parameters to be used
for calculation of the protective length.
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CP by anodes located on adjacent structures significantly reduces the cost of anode installation in case the pipeline installation
concept would otherwise require anode installation offshore. Moreover, for buried pipelines in general and for hot buried lines in
particular, the anode electrochemical efficiency and current output capacity increases since the anodes on such structures are
freely exposed to seawater. The condition of such anodes can also be monitored. The concept of basing pipeline CP on anodes
installed on adjacent structures further reduces the risk of HISC damage to pipelines in susceptible materials (e.g. martensitic and
ferritic-austenitic stainless steels).
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6.4.5.6 Bracelet pipeline anodes are to be designed with due considerations of forces induced during pipeline
installation. For anodes to be installed on top of the pipeline coating, this may require use of bolts for
tensioning or welding of anode tabs with pressure applied on the bracelet assembly during the mounting.
Connector cables shall be adequately protected; e.g. by locating the cables to the gap between the anode
bracelets and filling with a moulding compound.
6.4.5.7 A calculation procedure for pipeline CP design using conventional bracelet anodes and a maximum
anode spacing of 300 m is given in ISO 15589-2 and in DNVGL-RP-F103.
Guidance note:
The latter document generally refers to ISO 15589-2 for design parameters and design procedures to be used and recommends
some default values which represent minimum requirements that do not need to be verified by special considerations and
testing. DNVGL-RP-F103 emphasizes the importance of coating design and quality control of coating application when defining
the CP current reducing effects of such coatings. It further contains additional guidance to the CP design. For alternative design
procedures, see [6.4.5.5] and [6.4.5.6] above.
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6.4.5.8 The detailed engineering documentation of galvanic anode CP systems shall contain the following:
— design premises, including design life and reference to relevant project specifications, standards or
recommended practices
— calculations of average and final current demands for individual sections of the pipeline
— calculations of total anode net mass for the individual sections, to meet the mean current demand
— calculation of final current anode output to verify that the final current demand can be met for the
individual sections of the pipeline (applies to a conventional bracelet anode concept with max. 300 m
anode spacing)
— number of bracelet anodes for the individual pipeline sections, and resulting net anode mass to be
installed on each section
— outline drawing(s) of bracelet anodes with fastening devices and including tentative tolerances
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— calculations of pipeline metallic resistance to verify the feasibility of CP by anodes on adjacent structure(s)
or a bracelet anode concept exceeding a spacing of 300 m in case any of these options apply (see DNVGLRP-F103)
— documentation of CP capacity on adjacent installation(s) to be utilized for CP of pipeline, if applicable.
Guidance note:
The above requirements for documentation of CP design is an amendment to ISO 15589-2.
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6.4.5.9 Recommended practice for CP design of pipeline system components with major surfaces in
structural steel (e.g. riser bases) is given in DNVGL-RP-B401.
6.4.5.10 Design of any impressed current CP systems installed at land falls shall comply with ISO 15589-1.
Requirements to electrically isolation joints are given in [8.2.8].
Guidance note:
Design of impressed current CP systems at landfalls is not covered by this standard. Some general guidance is given in ISO 15889.
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6.4.6 Internal corrosion control
6.4.6.1 Options for internal corrosion control should be evaluated aiming for the most cost-effective solution
meeting the overall requirements of safety and environmental regulations. The selection of the most costeffective strategy for corrosion control requires that all major costs associated with operation of the pipeline
system, as well as investment costs for corrosion control, are evaluated (life cycle cost analysis). When
fluid corrosivity and efficiency of corrosion mitigation cannot be assessed with any high degree of accuracy,
a risk cost may be added for a specific option being evaluated. The risk cost is the product of estimated
probability and consequences (expressed in monetary units) of a particular failure mode (e.g. rupture or
pinhole leakage) due to malfunction of the corrosion control system being considered (e.g. inhibitor addition
to a potentially corrosive fluid). The probability of such failures should reflect the designer's confidence in
estimating the fluid corrosivity and the efficiency of options for corrosion control being evaluated. Depending
on the failure mode, consequences of failure may include costs associated with increased maintenance,
repairs, lost capacity and secondary damage to life, environment and other investments.
6.4.6.2 The selection of a system for internal corrosion protection of pipelines has a major effect on detailed
design and shall therefore be evaluated during conceptual design. The following options for corrosion control
may be considered:
—
—
—
—
processing of fluid for removal of liquid water and/or corrosive agents
use of line pip or internal (metallic) lining/cladding with intrinsic corrosion resistance (see [6.2.3])
use of organic corrosion protective coatings or linings (normally in combination with a) or d))
chemical treatment, i.e. addition of chemicals with corrosion mitigating function.
In addition, the benefits of a corrosion allowance (see [6.4.2]) should be duly considered for the above
points.
6.4.6.3 Corrosion control by fluid processing may involve removal of water from gas/oil (dehydration),
or of oxygen from seawater for injection (deoxygenation), for example. Consequences of operational
upsets on material degradation should be taken into account. The necessity for corrosion allowance and
redundant systems for fluid processing should be considered. On-line monitoring of fluid corrosion properties
downstream of processing unit is normally required. For oil export pipelines carrying residual amounts of
water, a biocide treatment should be considered as a back up for prevention of bacterial corrosion. Periodic
pigging for removal of water and deposits counteracts internal corrosion in general and bacterial corrosion in
particular.
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6.4.6.4 If internal coatings or linings are to be evaluated as an option for corrosion control, the following
main parameters shall be considered:
— chemical compatibility with all fluids to be conveyed or contacted during installation, commissioning and
operation, including the effects of any additives for control of flow or internal corrosion (see [6.4.6.6])
— resistance to erosion by fluid and mechanical damage by pigging operations
— resistance to rapid decompression
— reliability of quality control during coating application
— reliability of (internal) field joint coating systems, if applicable
— consequences of failure and redundant techniques for corrosion mitigation.
6.4.6.5 Internal coating of pipelines (e.g. by thin film of epoxy) has primarily been applied for the purpose of
friction reduction in dry gas pipelines (flow coatings or anti-friction coatings). Any such coatings should have
a minimum specified thickness of 40 μm and should comply with the minimum requirements in API RP 5L2
or ISO 15741. Although such coatings can not be expected to be efficient in preventing corrosion attack if
corrosive fluids are conveyed, any coating with adequate properties may still be beneficial in reducing forms
of attack affecting membrane stresses and hence, the pressure retaining capacity of the pipeline.
6.4.6.6 Chemical treatment of fluids for corrosion control may include:
—
—
—
—
—
—
corrosion inhibitors (e.g. film forming)
pH-buffering chemicals
biocides (for mitigation of bacterial corrosion)
glycol or methanol (added at high concentrations for hydrate inhibition, diluting the water phase)
dispersants (for emulsification of water in oil)
scavengers (for removal of corrosive constituents at low concentrations).
6.4.6.7 The reliability of chemical treatment should be evaluated in detail during the conceptual design.
Important parameters to be considered are:
— anticipated corrosion mitigating efficiency for the actual fluid to be treated, including possible effects of
scales, deposits, etc. associated with this fluid
— capability of the conveyed fluid to distribute inhibitor in the pipeline system along its full length and
circumference
— compatibility with all pipeline system and downstream materials, particularly elastomers and organic
coatings
— compatibility with any other additives to be injected,
— health hazards and environmental compatibility
— provisions for injection and techniques/procedures for monitoring of inhibitor efficiency
— consequences of failure to achieve adequate protection, and redundant techniques.
For pipelines carrying untreated well fluid or other fluids with high corrosivity and with high requirements to
safety and reliability, there is a need to verify the efficiency of chemical treatment by integrity monitoring
using a tool allowing wall thickness measurements along the full length of the pipeline (see Sec.12).
Corrosion probes and monitored spools are primarily for detection of changes in fluid corrosivity and are not
applicable for verification of the integrity of the pipeline.
6.4.6.8 The design of corrosion control based on fluid processing and/or chemical treatments should be
reviewed by operator’s operational organisation.
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SECTION 7 CONSTRUCTION – LINEPIPE
7.1 General
7.1.1 Objective
7.1.1.1 This section specifies the requirements for manufacture, testing and documentation of linepipe. All
mechanical properties and dimensional tolerances shall be met after heat treatment, expansion or impansion,
and final shaping.
Guidance note:
Coating application of fusion bonded epoxy involves heating the material to 200-250 ˚C, but this is not considered a heat
treatment by this standard. It is a low temperature for steel materials, still it may have a minor effect on the material properties.
Test results prior to coating application can be considered representative of the final condition. During qualification it may be
considered to perform some additional testing after coating application and compare with results obtained before coating. In case
the difference is non-negligible, it indicates that the material is too sensitive to temperature increase and the chemical composition
and manufacturing process should be reviewed. Typically the YS/TS ratio will have most noticeable variation, if any.
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7.1.1.2 Materials selection shall be performed in accordance with Sec.6.
7.1.1.3 This section does not cover any activities taking part after the pipes have been dispatched from the
pipe mill, e.g. coating and girth welding.
7.1.1.4 The requirements stated herein for Carbon-Manganese (C-Mn) steel linepipe conform in general to
ISO 3183 Annex J: PSL 2 pipe ordered for offshore service, with some additional and modified requirements.
7.1.1.5 Manufacturers shall have an implemented quality assurance system. For linepipe manufacturers a
quality assurance system according to ISO 9001 is considered to meet requirements in Table D-4.
7.1.2 Application
7.1.2.1 The requirements are applicable for linepipe made of:
— C-Mn steel
— clad or lined steel
— corrosion resistant alloys (CRA) including ferritic - austenitic (duplex) stainless steels, austenitic stainless
steels, martensitic stainless steels (13Cr), other stainless steels and nickel based alloys.
The principles from this standard may be applied for other materials, e.g. 9Ni steel. In such cases, specific
material requirements shall be defined in the project specification.
7.1.2.2 Materials, manufacturing methods and procedures that comply with recognised practices or
proprietary specifications will normally be acceptable provided they comply with the requirements of this
section.
7.1.3 Systematic review
7.1.3.1 The overall requirements to systematic review in Sec.2 will apply for the linepipe manufacturers to
review this section and evaluate if the requirements in the purchase order and this standard can be met.
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7.1.4 Process of manufacture
7.1.4.1 C-Mn linepipe shall be manufactured according to one of the following processes:
Seamless (SMLS)
Pipe manufactured by a hot forming process without welding. In order to obtain the required dimensions, the
hot forming may be followed by sizing or cold finishing.
High frequency welded (HFW)
Pipe formed from strip and welded with one longitudinal seam formed by electric-resistance welding applied
by induction or conduction with a welding current frequency ≥ 70 kHz, without the use of filler metal. The
forming may be followed by cold expansion or reduction.
Submerged arc-welded (SAW)
Pipe manufactured by forming from strip or plate and with one longitudinal (SAWL) or helical (SAWH) seam
formed by the submerged arc process, with at least one pass made on the inside and one pass from the
outside of the pipe. The forming may be followed by cold expansion or reduction.
7.1.4.2 CRA linepipe may, in addition to SMLS and SAWL, be manufactured according to one of the following
processes:
Electron beam welded (EBW) and laser beam welded (LBW)
Pipe formed from strip and welded with one longitudinal seam, with or without the use of filler metal. The
forming may be followed by cold expansion or reduction to obtain the required dimensional tolerances. These
welding processes shall be subject to pre-qualification testing according to App.C.
Multiple welding processes (MWP)
Pipe formed from strip or plate and longitudinally welded using a combination of two or more welding
processes. If the combination of welding processes has not been used previously, pre-qualification testing
should be conducted according to App.C.
7.1.4.3 The backing steel of lined linepipe shall comply with [7.4].
7.1.4.4 The liner pipe of lined linepipe shall be manufactured in accordance with API 5LC.
7.1.4.5 Clad linepipe shall be manufactured from CRA clad C-Mn steel plate by application of a single
longitudinal weld. With respect to the backing steel, the pipe manufacturing shall be in general compliance
with one of the manufacturing routes for SAW pipe as given in Table 7-1. The longitudinal weld shall be MWP
(see [7.1.4.2]).
7.1.5 Supplementary requirements
7.1.5.1 When requested by the purchaser and stated in the materials specification (as required in [7.1.6]),
linepipe to this standard shall meet supplementary requirements given in subsection [7.9], for:
—
—
—
—
—
H2S service (also referred to as sour service), suffix S (see [7.9.1])
fracture arrest properties, suffix F (see [7.9.2])
linepipe for plastic deformation, suffix P (see [7.9.3])
enhanced dimensional requirements for linepipe, suffix D (see [7.9.4])
high utilisation, suffix U (see [7.9.5]).
7.1.6 Linepipe specification
7.1.6.1 A linepipe specification reflecting the results of the materials selection (see [6.3.2]), referring to
this section of the offshore standard, shall be prepared by the purchaser. The specification shall state any
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additional requirements to and/or deviations from this standard related to materials, manufacture, fabrication
and testing of linepipe.
7.1.7 Manufacturing procedure specification
7.1.7.1 Prior to start of production, the manufacturer shall prepare a manufacturing procedure specification
(MPS). The MPS shall demonstrate how the specified properties may be achieved and verified throughout the
proposed manufacturing route.
The MPS shall address all factors that influence the quality and consistency of the product. All main
manufacturing steps from control of received raw material to shipment of finished pipe, including all
examination and check points, shall be outlined in detail.
References to the procedures established for the execution of all the individual production steps shall be
included.
7.1.7.2 The MPS shall as a minimum contain the following information (as applicable):
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
steel producer
plan(s) and process flow description/diagram
project specific quality control plan
manufacturing process
target chemical composition
steel making and casting techniques
ladle treatments (secondary refining), degassing, details of inclusion shape control, super heat
method used to ensure that sufficient amount of intermixed zones between different orders are removed
details and follow-up of limiting macro, as well as micro segregation, e.g. soft reduction and electro
magnetic stirring (EMS) used during continuous casting
manufacturer and manufacturing location of raw material and/or plate for welded pipes
billets reheating temperature for seamless
allowable variation in slab reheating temperature, and start and stop temperatures for finishing mill and
accelerated cooling
methods for controlling the hydrogen level (e.g. stacking of slabs and/or plates)
pipe-forming procedure, including preparation of edges and control of alignment and shape (including
width of strip for HFW)
procedure for handling of welding consumable and flux, including frequency of flux moisture testing
all activities related to production and repair welding, including welding procedures and qualification
heat treatment procedures (including in-line heat treatment of the weld seam) including allowable
variation in process parameters
method for cold expansion/reduction/sizing/finishing, target and maximum sizing ratio
hydrostatic test procedures
NDT procedures (also for strip/plate as applicable)
list of specified mechanical and corrosion testing
dimensional control procedures
pipe number allocation
pipe tracking procedure (traceability procedure)
marking, coating and protection procedures
handling, loading and shipping procedures
for coiled line pipe; strip end and circumferential welds (if applicable) welding and NDT procedures.
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7.1.8 Manufacturing procedure qualification test
7.1.8.1 The MPS shall be qualified for each nominal pipe diameter; either as part of first-day production
or as a separate MPQT prior to full-scale production. For C-Mn steels with SMYS < 485 MPa that are not
intended for H2S service, relevant documentation may be agreed in lieu of qualification testing providing all
essential variables in [7.1.8.7] are adhered to.
Guidance note:
Depending on the criticality of the project, it is recommended for all projects to carefully evaluate if the MPQT should be conducted
prior to start of production.
It is not necessary to perform repeated qualification testing during one and the same project, even if the fabrication is interrupted
by some weeks. This is provided that all procedures and equipment remain unchanged, and that all essential variables are adhered
to.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
7.1.8.2 For C-Mn steels with SMYS > 450 MPa, the qualification of the MPS should be completed prior to
start of production.
7.1.8.3 Each MPQT shall include full qualification of one pipe from two different test units of different heats
(a total of two pipes). If the entire production is limited to one heat, the MPQT may be performed on a single
pipe from that heat. The minimum type and extent of chemical, mechanical, and non-destructive testing are
given in this section. This includes all production tests plus additional tests given in Table 7-8. Table 7-13 and
Table 7-15.
7.1.8.4 For pipes delivered as coiled line pipe, qualification of strip end welds shall also be included as part of
the MPQT.
7.1.8.5 If the cold forming of C-Mn steel exceeds 5% strain after heat treatment, ageing tests shall be
performed as part of the qualification testing. The cold forming shall take into account all operations on the
steel, including but not limited to levelling of plate, pipe forming and expansion. The tests shall be performed
on the actual pipe without any straightening or additional deformation, see [B.2.11.1]. The absorbed Charpy
V-notch impact energy in the aged condition shall meet the requirements in Table 7-5.
7.1.8.6 Additional MPS qualification testing may be required by purchaser (e.g. weldability testing, analysis
for trace elements for steel made from scrap), as part of the qualification of the MPS (see [7.1.8.1]).
Weldability tests should be performed using the same welding equipment as used during installation or on
the lay barge.
7.1.8.7 The validity of the MPQT shall be limited to the steelmaking, rolling, and manufacturing/fabrication
facilities used during the qualification.
7.1.8.8 In addition to the requirements stated above, the following changes (as applicable) to the
manufacturing processes will require re-qualification of the MPS (essential variables):
— any change in steelmaking practice
— for C-Mn steel, change in the superheat exceeding ±20˚C, change in the slab thickness exceeding
±20%, change in the casting speed exceeding ±30%, any change in the use of soft reduction and
electromagnetic stirring.
— changes beyond the allowable variation for rolling practice, accelerated cooling and/or QT process
— for C-Mn steel plate, changes exceeding for slab reheating ±60˚C, final rolling temperature ±30˚C,
accelerated cooling start temperature ±40˚C, accelerated cooling stop temperature ±60˚C
— change in nominal wall thickness exceeding + 5% to -10%
— change in ladle analysis for C-Mn steels outside ± 0.02% C, ± 0.03 CE and/or ± 0.02 in Pcm
— any change in pipe forming process, between UOE, JCOE, three-roll bend or other forming method,
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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—
—
—
—
—
—
—
any change in sr > ±0.0025 (see [7.2.3.34] and [7.2.3.35])
any change in alignment and joint design for welding
change in welding heat input ± 15%
any change in welding wire type, thickness and configuration (including number of wires)
any change in welding flux
any change in shielding gas
any change in make, type and model of welding equipment.
The following additional essential variable applies to HFW, EBW and LBW pipe:
—
—
—
—
any change in nominal thickness
change in welding heat coefficient Q = (amps × volts)/(travel speed × thickness) ± 5%
addition or deletion of an impeder
change in rollers position and strip width outside agreed tolerances.
In case issues only related to the welding process have been changed, the re-qualification of the MPS may be
limited to the weld and HAZ only (e.g. not base material testing).
7.1.8.9 If one or more tests in the MPQT fail, the MPS shall be reviewed and modified accordingly, and a
complete re-qualification performed. Re-testing may be allowed subject to agreement. In the specific case
of failed fusion line CVN tests (with reference to local brittle zones), retesting of further 2 sets removed from
the failed MPQ pipe (at the same position relative to the wall thickness) is permitted prior to declaring the
MPQT as having failed (see [7.2.5.10]).
Guidance note:
For toughness in fusion line there is general industry understanding that the results can have very large variation – and this does
not necessarily mean that the general material properties are unacceptable. Local brittle zones (LZB) are known to be present in
the heat affected zone (HAZ) of welds with high heat input. Such LBZs are inevitable, and their extent should be kept as low as
possible. Even a very low amount of LBZs can lead to some unacceptable toughness results.
The standard allows retesting of the same pipe if there is a low toughness result in the fusion line (FL), and it can be attributed
to LBZs. Retesting gives a larger set of results, and will clearly show whether the quantity of LBZs is low (i.e. few low toughness
results) or high (i.e. many low toughness results). Since LBZs are most likely present in all pipes, rejecting pipes with few low
toughness results does not improve the quality of the products. The neighbouring pipes will most likely have similar properties.
The intention of allowing retesting the same pipe in case of low toughness in FL is to have a realistic approach to quality assurance
and integrity control – while not rejecting pipes that are in principle acceptable.
Local brittle zones may influence all types of toughness tests, not only Charpy impact toughness testing.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
7.2 Carbon Manganese (C-Mn) steel linepipe
7.2.1 General
7.2.1.1 C-Mn steel linepipe fabricated according to this standard generally conform to the requirements in
ISO 3183 Annex J: PSL 2 pipe ordered for offshore service. Any additional or modified requirements to ISO
3183 Annex J are highlighted in this subsection ([7.2]) as described in [7.2.1.2] and [7.2.1.3].
7.2.1.2 Paragraphs with additional requirements to ISO 3183 are marked at the end of the relevant
paragraph with AR.
Paragraphs with modified requirements compared to ISO 3183 are marked at the end of the relevant
paragraph with MR.
7.2.1.3 Additional or modified requirements when given in tables are marked in accordance with [7.2.1.2]
with AR and MR in the relevant table cells.
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7.2.2 Pipe designation
7.2.2.1 C-Mn steel linepipe shall be designated with:
—
—
—
—
DNV GL
process of manufacture
SMYS
supplementary requirement suffix (see [7.9]), as applicable. MR
Guidance note:
E.g. “DNVGL SMLS 450 SP” designates a seamless pipe with SMYS 450 MPa, meeting the supplementary requirements for H2S
service and plastic deformation (e.g. reeling installation) properties.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
7.2.3 Manufacturing
7.2.3.1 C-Mn steel linepipe shall be manufactured in accordance with the processes given in [7.1.4] using
the starting materials and corresponding forming methods and final heat treatment as given in Table 7-1.
7.2.3.2 All manufacturing including steel making and the raw materials used shall be in accordance with the
qualified MPS, follow the same activity sequence, and stay within the agreed allowable variations.
7.2.3.3 All steels shall be made by an electric or one of the basic oxygen processes. C-Mn steel shall be fully
killed and made to a fine grain practice. The final product should have a maximum hydrogen content of 2
ppm. The hydrogen content in the ladle shall be determined by direct measurements or by a relevant model.
If a model is used, the input parameters shall be stated. The maximum allowable hydrogen content in the
ladle shall be determined by the manufacturer, and justified by relevant data.
7.2.3.4 SMLS pipe shall be manufactured from continuously (strand) cast or ingot steel.
7.2.3.5 If the process of cold finishing is used, this shall be stated in the inspection document.
7.2.3.6 Pipe ends shall be cut back sufficiently after rolling to ensure freedom from defects. AR
7.2.3.7 Strip and plate used for the manufacture of welded pipe should be rolled from continuously (strand)
cast or pressure cast slabs. Strip or plate shall not contain any repair welds.
7.2.3.8 The strip width for spiral welded pipes should not be less than 0.8 and not more than 3.0 times the
pipe diameter. Strip and plate shall be inspected visually after rolling, either of the plate, of the uncoiled strip
or of the coil edges.
7.2.3.9 If agreed, strip and plate shall be inspected ultrasonically for laminar imperfections or mechanical
damage, either before or after cutting the strip or plate, or the completed pipe shall be subjected to full-body
inspection, including ultrasonic inspection, see Table 7-16.
7.2.3.10 Plate or strip shall be cut to the required width and the weld bevel prepared by milling or other
agreed methods before forming. AR
7.2.3.11 Cold forming (i.e. below 250°C) of C-Mn steel shall not introduce a plastic deformation exceeding
5%, unless heat treatment is performed or ageing tests show acceptable results (see [7.1.8.5]). AR
7.2.3.12 Normalising forming of materials and weldments shall be performed as recommended by the
manufacturers of the plate/strip and welding consumables. AR
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7.2.3.13 Welding personnel for execution of all welding operations shall be qualified by in-house training.
The in-house training program shall be available for review on request by purchaser. AR
7.2.3.14 Welding and repair welding procedures for the seam weld shall be qualified as part of MPQT. AR
7.2.3.15 The following types of repair welding procedure shall, as a minimum, be qualified:
— Arc stop/restart
— Shallow repair (single pass is not allowed, a minimum of 2 passes)
— Deep repair (minimum 10% of WT, but not covering through thickness repair). The depth of the groove
should be set by the manufacturer.
Other repair procedures may be qualified, if agreed. Repair welding shall be qualified in a manner realistically
simulating the repair situation to be qualified. AR
7.2.3.16 Welds containing defects may be locally repaired by welding, after complete removal of all defects.
AR
7.2.3.17 The manufacturer shall ensure stable temperature conditions during welding. A minimum prewelding temperature shall be established. If SAW seam welding is done in more than one pass per side, then
a maximum interpass temperature shall be qualified. AR
7.2.3.18 Low hydrogen welding consumables shall be used and shall give a diffusible hydrogen content
of maximum 5 ml/100 g weld metal. Unless comparative tests result of diffusible hydrogen versus flux
moisture content are provided to meet this requirement for SAW, the maximum residual moisture content of
agglomerated flux shall be 0.03%. AR
7.2.3.19 Welding consumables shall be individually marked and supplied with an inspection certificate
according to EN 10204 or an equivalent material certification scheme. Welding wire shall be supplied with
certificate type 3.1, while certificate type 2.2 is sufficient for SAW Flux. AR
7.2.3.20 Handling of welding consumables and the execution and quality assurance of welding shall meet
the requirements of in-house quality procedures. AR
7.2.3.21 Any lubricant and contamination on the weld bevel or the surrounding areas shall be removed
before making the seam welds of SAWL pipes or SAWH pipes.
7.2.3.22 Tack welds shall be made by: manual or semi-automatic submerged-arc welding, electric welding,
gas metal-arc welding, gas tungsten-arc welding, flux-cored arc welding; or shielded metal-arc welding using
a low hydrogen electrode. Tack welds shall be melted and coalesced into the final weld seam or removed by
machining.
7.2.3.23 Intermittent tack welding of the SAWL groove shall not be used unless purchaser has approved
data furnished by manufacturer to demonstrate that all mechanical properties specified for the pipe are
obtainable at both the tack weld and intermediate positions.
7.2.3.24 For linepipe welding, the flux moisture needs to be controlled. Flux sampling should be from the
weld head, rotating between welding machines on a regular basis. Test frequency should take into account
risk of moisture fluctuation due to environmental conditions, storage conditions and handling practice. The
acceptance criteria for flux moisture shall be determined by the manufacturer, based on correlation with
diffusable hydrogen content in final product, see [7.2.3.18]. For agglomerated flux, a maximum residual
moisture content of 0.03% can be used, unless comparative test results justify a higher limit. For fused flux,
no suggested limit has been established.
7.2.3.25 General requirements to repair welding:
— Any repair welding shall be carried out prior to cold expansion and final heat treatment.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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—
—
—
—
Repeated repairs shall be subject to agreement.
Repair welding of cracks is not permitted.
A local weld repair shall be at least 50 mm long or 4 times the repair depth, whichever is longer.
The excavated portion of the weld shall be large enough to ensure complete removal of the defect, and
the ends and sides of the excavation shall have a gradual taper from the bottom of the excavation to the
surface. If air-arc gouging is used, the last 3 mm shall be removed by mechanical means to remove any
carbon enriched zones. Removal of less than 3 mm may be accepted if it can be documented that the
carbon enriched zones has been satisfactorily removed.
— Weld repairs shall be ground to merge smoothly into the original weld contour.
7.2.3.26 Qualification testing of repair welds shall be described in the MPS. It shall be documented that the
repair weld metal, including all transition zones (e.g. interface between new and old weld metal) meets the
same requirements as the original weld metal and HAZ. AR
Guidance note:
It is recommended to review the test and qualification regime described in Table C-4.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
7.2.3.27 The abutting edges of the strip or plate should be milled or machined immediately before welding
of HFW pipes. The weld flash shall be removed on both external and internal surface as required in Table D-4.
7.2.3.28 The width of the strip or plate should be continuously monitored during production of HFW pipes.
AR
7.2.3.29 The weld seam and the HAZ shall be fully normalized subsequent to welding of HFW pipes. MR
7.2.3.30 For pipes to be supplied as coiled line pipe, strip/plate end welds are permitted and shall be at an
acute angle to the edges of the strip. Strip/plate end welds shall comply with all applicable requirements in
this section given to helical welded pipes and NDT requirements given in [7.6].
7.2.3.31 If used, circumferential welds between coiled pipes shall be qualified according to requirements for
pipeline girth welds given in App.C. See also DNVGL-RP-F108 for considerations when fracture mechanics
testing is not possible due to size limitations for such circumferential welds.
7.2.3.32 Heat treatments of SMLS and welded pipe shall be performed according to documented procedures
used during MPQT.
7.2.3.33 The documented procedures shall be in accordance with any recommendations from the material
manufacturer with regard to heating and cooling rates, soaking time, and soaking temperature. AR
7.2.3.34 The extent of cold sizing and cold forming expressed as the sizing ratio sr, shall be calculated
according to the following formula:
s
r
= |Da - Db| / Db
(7.1)
where:
Da
Db
= the actual outside diameter after sizing
= the actual outside diameter before sizing.
The actual outside diameter should be measured with a tape measure (i.e. perimeter as an average of all
possible diameters). The sizing ratio should be checked every shift, preferably at both ends of the pipe. MR
7.2.3.35 The sizing ratio of cold expanded pipe should be within the range 0.003 < sr ≤ 0.015. Expansion
shall not introduce high local deformations.
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7.2.3.36 Pipes may be cold sized to their final dimensions by expansion or reduction. This shall not produce
excessive permanent strain. The sizing ratio, sr , shall not exceed 0.015 if no subsequent heat treatment or
only heat treatment of the weld area is performed.
7.2.3.37 The sizing ratio, sr , for cold sizing of pipe ends shall not exceed 0.015 unless the entire pipe ends
are subsequently stress relieved.
7.2.3.38 Pipe ends should be cut square and be free from burrs. MR
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Table 7-1 C-Mn steels, acceptable manufacturing routes
Type of
pipe
SMLS
Starting material
Ingot, bloom or billet
Pipe forming
Final heat treatment
Normalising forming
None
Hot forming
Hot forming and cold finishing
Normalising rolled strip
Thermo-mechanical rolled strip
HFW
Cold forming
Cold forming
Cold forming and hot reduction
under controlled temperature,
resulting in a normalised condition
2)
Thermo-mechanical rolled plate
or strip
SAW
QT
2)
Heat treating of weld
area
M
Heat treating of weld
area and stress relieving
of entire pipe
M
Normalising of entire
pipe
N
of entire pipe
2)
Q
N
None
M
N
Cold forming
None, unless required
due to degree of cold
forming
plate or strip
As-rolled, QT , normalised or
normalising rolled plate or strip
N or Q
N
Cold forming followed by
thermomechanical forming of pipe
Normalised or normalising
rolled plate or strip
N or Q
Normalising of weld area
2)
1)
N
Normalising or QT
QT
Hot rolled or normalising rolled
strip
Delivery
condition
M
Q
Normalising forming
Cold forming
None
N
Normalising
N
QT
2)
Q
Notes
1)
The delivery conditions are:
— N - normalised
— Q - quenched and tempered
— M - thermo-mechanical rolled or formed.
2)
Quenched and tempered.
7.2.3.39 If agreed, internal machining or grinding may be carried out. In case of machining, the following
requirements shall be adhered to:
— if required in the purchase order the internal taper shall be located at a defined minimum distance from
future bevel to facilitate UT or AUT
— the angle of the internal taper, measured from the longitudinal axis shall not exceed 7.0° for welded pipe.
For SMLS pipe the maximum angle of the internal taper shall be as given in Table 7-2. MR
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Table 7-2 Maximum angle of internal taper for SMLS pipe
Wall thickness t [mm]
Max. angle of taper [°]
< 10.5
7.0
10.5 ≤ t < 14.0
9.5
14.0 ≤ t < 17.0
11.0
≥ 17.0
14.0
7.2.3.40 Jointers should not be used.
7.2.3.41 If used, the jointer circumferential weld shall be qualified according to the requirements for pipeline
girth welds given in App.C. Production testing requirements for jointers shall be in accordance with ISO 3183.
Other manufacturing requirements shall comply with Annex A of ISO 3183.
7.2.3.42 Apart from linepipe supplied as coiled tubing, strip/plate end welds should not be permitted. see
[7.2.3.30]. MR
7.2.3.43 In case any mechanical tests fail during production of pipe from delivery condition N or Q, it
is acceptable to conduct one re-heat treatment cycle of the entire test unit. All mechanical testing shall
be repeated after re-heat treatment. No re-processing is allowed of delivery condition M material unless
otherwise agreed. AR
7.2.3.44 A system for traceability of the heat number, heat treatment batch and test unit number and the
records from all required tests to each individual pipe shall be established and described in the MPS (see
[7.1.7.2]). Required repairs and records of dimensional testing and all other required inspections shall be
included. Care shall be exercised during storage and handling to preserve the identification of materials. MR
7.2.4 Acceptance criteria
7.2.4.1 The chemical compositions given in Table 7-3 are applicable to pipes with delivery condition N or Q
(normalised or quenched and tempered according to Table 7-1), with nominal wall thickness t ≤ 25 mm.
7.2.4.2 The chemical compositions given in Table 7-4 are applicable to pipes with delivery condition M
(thermomechanical formed or rolled according to Table 7-1), with nominal thickness t ≤ 35 mm. MR
7.2.4.3 For pipes with nominal wall thickness larger than the limits indicated in [7.2.4.1] and [7.2.4.2], the
chemical composition shall be subject to agreement.
7.2.4.4 For pipe with a carbon content ≤ 0.12% (product analysis), carbon equivalents shall be determined
using the Pcm formula as given in Table 7-3 and Table 7-4. If the heat analysis for boron is less than
0.0005%, then it is not necessary for the product analysis to include boron, and the boron content may be
considered to be zero for the Pcm calculation.
7.2.4.5 For pipe with a carbon content > 0.12% (product analysis) carbon equivalents shall be determined
using the CE formula as given in Table 7-3.
7.2.4.6 The tensile properties shall be as given in Table 7-5.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Guidance note:
The elongation requirements in Table 7-5 are based on a formula identical in API 5L and ISO 3183. The formula is calibrated for
use with tensile test specimens prepared according to ASTM A370 (i.e. API test specimens). It should be noted that the same
material tested with specimens based on ASTM A370 and ISO 6892 can give different elongation results due to the different
specimen geometries.
In general it should be considered to use ASTM A370 specimens for normal tensile testing, since this would give the best
correspondence with the requirements in Table 7-5.
Tensile specimens based on ISO 6892 can be used, but then the acceptance criteria should be reviewed. Some options are; (i)
use the values from Table 7-5, (ii) during qualification perform a number of tests on both types of specimens to establish an
empirical correspondence for the specific material or (iii) define elongation criteria based on relevant testing experience and
existing documentation.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e--Guidance note:
There is increasing interest among operators and installation contractors for digital/electronic version of the stress-strain curves.
The advantage of digitally stored tensile test data is the ease of further analysis and use in calculations – both statistical for a
production run and also in load/strain simulations.
Manufacturers should make preparations in case a project-specific requirement is included in a contract or specification. As a
minimum all tensile tests during qualification should be stored and transmitted electronically.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
7.2.4.7 For transverse weld tensile testing, the ultimate tensile strength shall be at least equal to the SMTS.
7.2.4.8 The hardness in the base material (BM), weld metal (WM) and the heat affected zone (HAZ) shall
comply with Table 7-5. AR
7.2.4.9 Requirements for Charpy V-notch impact properties for linepipe BM, WM and HAZ are given in Table
7-5. These values shall be met when tested at the temperatures given in Table 7-6. MR
7.2.4.10 Testing of Charpy V-notch impact properties shall, in general, be performed on test specimens 10
× 10 mm. Where test pieces of width < 10 mm are used, the measured average impact energy (KVm) and
2
the test piece cross-section measured under the notch (A) (mm ) shall be reported. For comparison with the
values in Table 7-5, the measured energy shall be converted to the impact energy (KV) in Joules using the
formula:
(7.2)
AR
7.2.4.11 From the set of three Charpy V-notch impact specimens, only one is allowed to be below the
specified average value and shall meet the minimum single value requirement. AR
7.2.4.12 For flattening test of HFW pipe with SMYS ≥ 415 MPa and wall thickness ≥ 12.7 mm, there shall
be no opening of the weld before the distance between the plates is less than 66% of the original outside
diameter. For flattening test of all other combinations of pipe grade and specified wall thickness, there shall
be no opening of the weld before the distance between the plates is less than 50% of the original outside
diameter.
7.2.4.13 For flattening test of HFW pipe with a D/t2 > 10, there shall be no cracks or breaks other than in
the weld before the distance between the plates is less than 33% of the original outside diameter.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Guidance note:
The weld extends to a distance, on each side of the weld line, of 6.4 mm for D < 60.3 mm, and 13 mm for D ≥ 60.3 mm.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
7.2.4.14 The guided-bend test pieces shall not:
— fracture completely
— reveal any cracks or ruptures in the weld metal longer than 3.2 mm, regardless of depth, or
— reveal any cracks or ruptures in the parent metal, HAZ, or fusion line longer than 3.2 mm or deeper than
12.5% of the specified wall thickness.
However, cracks that occur at the edges of the test piece during testing shall not be cause for rejection,
provided that they are not longer than 6.4 mm.
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Table 7-3 Chemical composition for C-Mn steel pipe with delivery condition N or Q, applicable for
seamless and welded pipe
Carbon
equivalents
Product analysis, maximum. wt.%
SMYS
C
1)
Si
Mn
1)
P
S
V
Ti
Other
2)
0.04
Notes
6,7)
0.36
0.19
8)
7)
0.36
0.19
8)
6,7)
0.38
0.20
8)
6)
0.43
0.22
8)
Nb
CE
3)
P
cm
4)
Pipe with delivery condition N (normalised according to Table 7-1)
Note
5)
Note
5)
245
0.14
0.40
1.35
0.020
0.010
290
0.14
0.40
1.35
0.020
0.010
0.05
0.05
0.04
Note
320
0.14
0.40
1.40
0.020
0.010
0.07
0.05
0.04
Notes
360
0.16
0.45
1.65
0.020
0.010
0.10
0.05
0.04
Note
Pipe with delivery condition Q (quenched and tempered according to Table 7-1)
245
0.14
0.40
1.35
0.020
0.010
0.04
0.04
0.04
Note
7)
0.34
0.19
8)
290
0.14
0.40
1.35
0.020
0.010
0.04
0.04
0.04
Note
7)
0.34
0.19
8)
320
0.15
0.45
1.40
0.020
0.010
0.05
0.05
0.04
Note
7)
0.36
0.20
8)
360
0.16
0.45
1.65
0.020
0.010
0.07
0.05
0.04
Notes
6,9)
0.39
0.20
8)
390
0.16
0.45
1.65
0.020
0.010
0.07
0.05
0.04
Notes
6,9)
0.40
0.21
8)
415
0.16
0.45
1.65
0.020
0.010
0.08
0.05
0.04
Notes
6,9)
0.41
0.22
8)
450
0.16
0.45
1.65
0.020
0.010
0.09
0.05
0.06
Notes
6,9)
0.42
0.22
8)
485
0.17
0.45
1.75
0.020
0.010
0.10
0.05
0.06
Notes
6,9)
0.42
0.23
8)
555
0.17
0.45
1.85
0.020
0.010
0.10
0.06
0.06
Notes
6,9)
As agreed
Notes
1)
For each reduction of 0.01% below the specified maximum for carbon, an increase of 0.05% above the specified
maximum for manganese is permissible, up to a maximum increase of 0.20%.
2)
Al total ≤ 0.060%; N ≤ 0.012%; Al/N ≥ 2:1 (not applicable to titanium-killed steel or titanium-treated steel).
3)
4)
5)
The sum of the niobium and vanadium contents should be ≤ 0.06%.
6)
The sum of the niobium, vanadium, and titanium contents shall be ≤ 0.15%.
7)
Cu ≤ 0.35%; Ni ≤ 0.30%; Cr ≤ 0.30%; Mo ≤ 0.10%; B ≤ 0.0005%.
8)
For SMLS pipe, the listed value is increased by 0.03, up to a maximum of 0.25.
9)
Cu ≤ 0.50%; Ni ≤ 0.50%; Cr ≤ 0.50%; Mo ≤ 0.50%; B ≤ 0.0005%.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
DNV GL AS
Page 156
Table 7-4 Chemical composition for C-Mn steel pipe with delivery condition M (thermo-mechanical
formed or rolled according to Table 7-1)
Carbon
equivalent
Product analysis, maximum. wt.%
SMYS
C
1)
Si
Mn
1)
P
S
V
Nb
Ti
Other
2)
P
3)
cm
245
0.12
0.40
1.25
0.020
0.010
0.04
0.04
0.04
Note
4)
0.19
290
0.12
0.40
1.35
0.020
0.010
0.04
0.04
0.04
Note
4)
0.19
4)
0.20
320
0.12
0.45
1.35
0.020
0.010
0.05
0.05
0.04
Note
360
0.12
0.45
1.65
0.020
0.010
0.05
0.05
0.04
Notes
5,6)
0.20
Notes
5,6)
0.21
Notes
5,6)
0.21
Notes
5,6)
0.22
0.22
7)
0.24
7)
390
0.12
415
0.12
450
0.12
0.45
0.45
0.45
1.65
1.65
1.65
0.020
0.020
0.020
0.010
0.010
0.010
0.06
0.08
0.10
0.08
0.08
0.08
0.04
0.06
0.06
485
0.12
0.45
1.75
0.020
0.010
0.10
0.08
0.06
Notes
5,6)
555
0.12
0.45
1.85
0.020
0.010
0.10
0.08
0.06
Notes
5,6)
Notes
1)
For each reduction of 0.01% below the specified maximum for carbon, an increase of 0.05% above the specified
maximum for manganese is permissible, up to a maximum increase of 0.20%.
2)
Al total ≤ 0.060%; N ≤ 0.012%; Al/N ≥ 2:1 (not applicable to titanium-killed steel or titanium-treated steel).
3)
4)
Cu ≤ 0.35%; Ni ≤ 0.30%; Cr ≤ 0.30%; Mo ≤ 0.10%; B ≤ 0.0005%.
5)
The sum of the niobium, vanadium, and titanium contents shall be ≤ 0.15%.
6)
Cu ≤ 0.50%; Ni ≤ 0.50%; Cr ≤ 0.50%; Mo ≤ 0.50%; B ≤ 0.0005%.
7)
For nominal wall thickness t > 25 mm the carbon equivalent may be increased with 0.01.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
DNV GL AS
Page 157
Table 7-5 C-Mn steel pipe, mechanical properties
Yield strength
R
Tensile strength
Ratio
Rm
R t0,5
/R m
t0,5
[MPa]
SMYS
min.
245
245
290
290
320
[MPa]
max.
450
3)
min.
2)
max.
max.
Elongation
in 50.8 mm
A
f
[%]
Hardness
[HV10]
BM, WM
min.
Charpy V-notch
energy (KVT) for
1)
BM, WM and HAZ
HAZ
max.
[J]
average
Min.
415
760
270
27
22
495
415
760
270
30
24
320
520
435
760
270
32
27
360
360
525
460
760
270
36
30
390
390
540
490
760
39
33
415
415
565
520
760
270
42
35
450
450
570
535
760
270
45
38
485
485
605
570
760
300
50
40
555
555
675
625
825
300
56
45
0.93
Note 4)
270
300
Notes
1)
The required KVL (longitudinal direction specimens) values shall be 50% higher than the required KVT values.
2)
If tested in the longitudinal direction, a minimum tensile strength 5% less than the required value is acceptable
(does not apply to all weld tensile tests).
3)
For pipe with specified outside diameter < 219.1 mm, the yield strength shall be ≤ 495 MPa.
4)
The specified minimum elongation in 50.8 mm, Af, expressed in percent, rounded to the nearest percent shall be as
determined using the following equation:
where:
C = 1940 for calculations using SI units;
A = the applicable tensile test piece cross-sectional area, as follows:
XC
2
2
— for circular cross-section test pieces, 130 mm for 12.7 mm and 8.9 mm diameter test pieces; and 65 mm for 6.4
mm test pieces
2
— for full-section test pieces, the lesser of a) 485 mm and b) the cross-sectional area of the test piece, calculated using
2
the specified outside diameter and the specified wall thickness of the pipe, rounded to the nearest 10 mm
2
— for strip test pieces, the lesser of a) 485 mm and b) the cross-sectional area of the test piece, calculated using the
2
specified width of the test piece and the specified wall thickness of the pipe, rounded to the nearest 10 mm
U
is the specified minimum tensile strength, in MPa.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
DNV GL AS
Page 158
Table 7-6 C-Mn steel linepipe, Charpy V-notch impact testing temperatures T0 (°C) as a function
of Tmin (°C) (minimum design temperature)
Nominal wall thickness (mm)
Pipelines and risers
t ≤ 20
T0 = Tmin
20 < t ≤ 40
T0 = Tmin – 10
t > 40
T0 = to be agreed in each case
7.2.4.15 The measured fracture toughness shall as a minimum have a CTOD value of 0.15 mm, when tested
at the minimum design temperature. AR
7.2.4.16 The macro section shall show a sound weld merging smoothly into the base material without weld
defects according to Table D-4. Complete re-melting of tack welds shall be demonstrated for double sided
SAW pipes. MPQT welds shall meet the requirements of ISO 5817 quality level C. AR
7.2.4.17 The misalignment of the axes of internal and external weld seams and the weld interpenetration
of double sided SAW pipes shall be verified on the macro section and meet the requirements given in Table
7-22.
7.2.4.18 The metallographic examination shall be documented by micrographs at sufficient magnification
and resolution to demonstrate that no detrimental oxides from the welding process are present along the
weld line. AR
7.2.4.19 It shall be verified that the entire HAZ has been appropriately heat treated over the full wall
thickness and that no untempered martensite remains.
7.2.4.20 The pipe shall withstand the hydrostatic test without leakage through the weld seam or the pipe
body.
7.2.4.21 Linepipe joints that fails the hydrostatic test shall be rejected. AR For pipes delivered as coiled
line pipe, the failed section may be removed, butt welded, and retested subject to agreement. Prior to any
retesting a root cause analysis shall be submitted for approval.
7.2.4.22 Requirements to visual examination performed at the plate mill are given in [D.7]. Requirements
for visual inspection of welds and pipe surfaces are given in [D.8.5]. MR and AR
7.2.4.23 Requirements to dimensions, mass and tolerances shall be as given in [7.7].
7.2.4.24 If agreed, the manufacturer shall supply weldability data or perform weldability tests. The details
for carrying out the tests and the acceptance criteria shall be as specified in the purchase order.
7.2.4.25 If requested, the linepipe supplier shall provide information regarding the maximum post weld heat
treatment (PWHT) temperature for the respective materials. AR
7.2.5 Inspection
7.2.5.1 Compliance with the requirements of the purchase order shall be checked by specific inspection in
accordance with EN 10204. Records from the qualification of the MPS and other documentation shall be in
accordance with the requirements in Sec.12.
The inspection frequency during production shall be as given in Table 7-7 and the frequency of testing for
MPQT as given in Table 7-8. Reference to the relevant acceptance criteria is given in these tables. Pipes for
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
DNV GL AS
Page 159
testing should be evenly distributed, both throughout the production period and between welding stations.
MR
Pipes for production testing shall be representative of all pipes produced. This means that sample pipes
should be taken from as many work shifts as possible (distributing the sampling throughout the production
period), and sampling should be rotated between the different welding stations.
It is not acceptable practice to select one plate from a number of heats in order to concentrate the production
of pipes for sampling.
7.2.5.2 A test unit is a prescribed quantity of pipe that is made to the same specified outside diameter and
specified wall thickness, by the same pipe-manufacturing process, from the same heat, and under the same
pipe-manufacturing conditions.
7.2.5.3 For coiled line pipe, all required mechanical testing in Table 7-7 shall be performed at each pipe
end or for each heat, whichever gives the highest number of tests. Strip end welds for coiled tubing shall be
tested according to tests specified for strip end welds for SAWH in ISO 3183 Annex J. AR
7.2.5.4 Sampling for mechanical and any corrosion testing shall be performed after heat treatment,
expansion and final shaping, but may be carried out before pipe end sizing process for pipes subjected to
heat treatment and when the associated sizing ratio is below 0.015 [7.2.3.36]. The number and orientation
of the samples for mechanical testing are given in Table 7-9. The samples shall not be prepared in a manner
that may influence their mechanical properties.
7.2.5.5 In case of large quantities of longitudinally welded large diameter and heavy wall thickness pipe,
where the test unit is governed by the heat size, it may be agreed that pipes from several heats represents
one test unit. The first 30 000 tons shall be tested with a frequency according to normal practice of this
standard. After exceeding 30 000 tons, the below testing philosophy may be applied:
— each test unit may consist of pipes from maximum 3 heats
— in case of test failure, the test frequency shall revert to the normal rate of testing until again 30 000 tons
with satisfactory results are documented.
7.2.5.6 In order to accept or reject a test unit as a result of a test unit release failure, re-testing shall be
conducted in accordance with [7.2.5.7] through [7.2.5.11].
7.2.5.7 If a test fails to meet the requirements, two re-tests shall be performed (for the failed test only)
on samples taken from two different pipes within the same test unit. Both re-tests shall meet the specified
requirements. The test unit shall be rejected if one or both of the re-tests do not meet the specified
requirements.
7.2.5.8 The reason for the failure of any test shall be established and the appropriate corrective action to
prevent re-occurrence of the test failures shall be taken accordingly.
7.2.5.9 If a test unit has been rejected, the manufacturer may conduct individual testing of all the remaining
pipes in the test unit. If the total rejection of all the pipes within one test unit exceeds 25%, the test unit
shall be rejected. In this situation the manufacturer shall investigate and report the reason for failure and
shall change the manufacturing process if required. Re-qualification of the MPS is required if the agreed
allowable variation of any parameter is exceeded (see [7.1.8.8] and [7.1.8.9]).
7.2.5.10 Re-testing of failed pipes shall not be permitted. If a pipe fails due to low CVN values in the fusion
line (HAZ) or weld line in HFW pipe, testing of samples from the same pipe may be performed subject to
agreement (see 7.1.8.9 for guidance on local brittle zones (LBZ)). Refer to [7.2.3.43] for re-processing of
pipe.
7.2.5.11 For any of the mechanical tests, any test piece that shows material imperfections unrelated to the
intent of the particular mechanical test, whether observed before or after testing, may be discarded and
replaced by another test piece from the same pipe. If the test results are influenced by improper sampling,
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
DNV GL AS
Page 160
machining, preparation, treatment or testing, the test sample shall be replaced by a correctly prepared
sample from the same pipe and a new test performed.
7.2.5.12 Heat and product analysis shall be performed in accordance with App.B. MR
7.2.5.13 If the value of any elements, or combination of elements, fails to meet the requirements, two retests shall be performed on samples taken from two different pipes from the same heat. If one or both retests fail to meet the requirements, the heat shall be rejected. MR
7.2.5.14 All mechanical testing shall be performed according to App.B. MR
7.2.5.15 Macro examination and metallographic examination shall be performed in accordance with App.B.
7.2.5.16 Hydrostatic testing shall be performed in accordance with [7.5]. MR
7.2.5.17 NDT, including visual inspection, shall be carried out in accordance with [7.6]. AR and MR
7.2.5.18 Dimensional testing shall be performed according to [7.7]. MR
7.2.5.19 Surface imperfections and defects shall be treated according to [D.8.3]. MR
Table 7-7 Inspection frequency for C-Mn steel linepipe during production 1, 2)
Applicable to
All pipe
SAWL, SAWH, HFW
Type of test
Frequency of testing
Heat analysis
One analysis per heat
Product analysis
Two analyses per heat
(taken from separate
product items)
Tensile testing of the pipe
body
Once per test unit of
3)
not more than 50/100
pipes with the same coldexpansion ratio
Table 7-5
CVN impact testing of the
7)
pipe body
Once per test unit of
4)
not more than 50/100
pipes with the same coldexpansion ratio
Table 7-5 and Table 7-6
Hardness testing
Once per test unit of
3)
not more than 50/100
pipes with the same coldexpansion ratio(AR)
Table 7-5
Hydrostatic testing
Each pipe
[7.2.4.20] to [7.2.4.21]
Pipe dimensional testing
See [7.7]
See [7.7]
NDT including visual
inspection
See [7.6] (MR and AR)
See [7.6] (MR and AR)
Tensile testing of the seam
weld (cross weld test)
Once per test unit of
5)
not more than 50/100
pipes with the same coldexpansion ratio (MR)
[7.2.4.6] and [7.2.4.7]
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
DNV GL AS
Acceptance criteria
Table 7-3 or Table 7-4
Page 161
Applicable to
SAWL, SAWH
Type of test
Frequency of testing
Acceptance criteria
CVN impact testing of the
seam weld of pipe with
specified wall thickness as
given in Table 22 of ISO
3183
Once per test unit of
4)
not more than 50/100
pipes with the same coldexpansion ratio (MR)
Table 7-5 and Table 7-6
Hardness testing of hard
spots
Any hard spot exceeding 50
mm in any direction
[D.8.5]
Macrographic testing of
seam weld
At least once per operating
6)
shift
[7.2.4.16]
Guided-bend testing of the
seam weld of welded pipe
Once per test unit of
3)
not more than 50/100
pipes with the same coldexpansion ratio (MR)
[7.2.4.14]
Flattening test
As shown in Figure 6 of
ISO3183
[7.2.4.12] and [7.2.4.13]
Metallographic examination
At least once per operating
6)
shift
[7.2.4.18] and [7.2.4.19]
(MR)
CVN impact testing of the
7)
coil/plate end weld
At least once per 50 coil/
plate end welds from
pipe with the same cold8)
expansion ratio
Table 7-5 and Table 7-6
HFW
Pipes supplied as coiled line
pipe
Notes
1)
Sampling of specimens and test execution shall be performed in accordance with App.B. For tensile, CVN, hardness,
guided-bend and flattening testing App.B refers to ISO 3183 without additional requirements.
2)
The number orientation and location of test pieces per sample for mechanical tests shall be in accordance with Table
7-9.
3)
Not more than 100 pipes with D ≤ 508 mm and not more than 50 pipes for D > 508 mm.
4)
Not more than 100 pipes with 114.3 mm ≤ D ≤ 508 mm and not more than 50 pipes for D > 508 mm.
5)
Not more than 100 pipes with 219.1 mm ≤ D ≤ 508 mm and not more than 50 pipes for D > 508 mm.
6)
At least once per operating shift plus whenever any change of pipe size occurs during the operating shift.
7)
Applicable to pipes with wall thickness > 6 mm.
8)
Testing shall be performed on finished pipe.
where
D = Specified outside diameter
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
DNV GL AS
Page 162
Table 7-8 Additional testing for manufacturing procedure qualification test for C-Mn steel pipe 1)
Applicable to
Type of test
All production tests as stated
in Table 7-7
All pipe
SMLS pipe
mm
Frequency of testing
See Table 7-7
Base metal longitudinal
2)
tensile test , AR
3, 4)
with t > 25
SAWL, SAWH pipe
25 mm
4)with
Welded pipe (all types)
t>
CVN testing at ID of
quenched and tempered
seamless pipe with t > 25
mm AR
CVN testing at ID of the
seam weld
Acceptance criteria
Table 7-5 and Table 7-6
One test for each pipe
provided for manufacturing
5)
procedure qualification
All-weld tensile test AR
Table 7-5
Fracture toughness (CTOD)
6, 7)
test of weld metal
AR
[7.2.4.15]
Ageing test
AR
8)
, see [7.1.8.5]
9)
Table 7-5
Notes
1)
Sampling of specimens and test execution shall be performed in accordance with App.B.
2)
Additional longitudinal test specimen is not necessary if already required by Table 7-7 and Table 7-9 for production
testing.
3)
Only applicable to pipe delivered in the quenched and tempered condition.
4)
Sampling shall be 2 mm from the internal surface, see [B.2.4].
5)
One pipe from two different test units of different heats shall be selected for the MPQT, see [7.1.8] (a total of 2
pipes).
6)
CTOD testing is not required for pipes with t < 13 mm. CTOD testing is not required of HAZ, only the centre of the
weld.
7)
For HFW pipe the testing applies to the fusion line (weld centre line).
8)
Only when cold forming during pipe manufacture exceeds 5% strain.
9)
Only SMYS, SMTS and elongation applies.
where
t = specified nominal wall thickness
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
DNV GL AS
Page 163
Table 7-9 Number, orientation, and location of test specimens per tested pipe
1, 2)
Wall thickness
Applicable to
Sample location
Type of test
≤ 25 mm
> 25 mm
Specified outside diameter
Specified outside diameter
< 219.1 mm
Tensile
SMLS, not cold
expanded pipe
Pipe body
Pipe body
Pipe body
HFW pipe
Seam weld
Pipe body and
weld
Pipe body
Seam weld
Pipe body
SAWH pipe
Seam weld
1L
1L
≥ 219.1 mm
3)
1L
3T
3T
3T
3T
Hardness
1T
1T
1T
1T
1L
3)
CVN
3T
Hardness
1T
Tensile
CVN
4)
1T
1L
3T
1L90
1T180
4)
1T
3T
1T
3)
3)
3T
1T
4)
1T
3)
1L90
1T180
4)
3T90
3T90
3T90
3T90
Tensile
—
1W
—
1W
CVN
3W and 3HAZ
MR
6W and 6HAZ
Hardness
1W
1W
1W
Flattening
Tensile
CVN
Tensile
SAWL pipe
3)
< 219.1 mm
CVN
Tensile
SMLS, cold
expanded pipe
1L
≥ 219.1 mm
5)
MR
1W
As shown in Figure 6 of ISO 3183
3)
1L90
3T90
1T180
3W and 6HAZ
Guided-bend
Hardness
4)
3)
1L90
3T90
3T90
1W
—
—
CVN
Tensile
5)
6)
1T180
3T90
1W
6)
MR
6W and 12HAZ
2W
2W
2W
2W
1W
1W
1W
1W
3)
4)
3)
1L
1T
1L
MR
4)
1T
CVN
3T
3T
3T
3T
Tensile
—
1W
—
1W
CVN
3W and 6HAZ
Guided-bend
Hardness
6)
6)
MR
6W and 12HAZ
2W
2W
2W
2W
1W
1W
1W
1W
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
DNV GL AS
4)
MR
Page 164
Wall thickness
Applicable to
Sample location
Type of test
≤ 25 mm
> 25 mm
Specified outside diameter
Specified outside diameter
< 219.1 mm
≥ 219.1 mm
< 219.1 mm
≥ 219.1 mm
Notes
1)
See Figure 5 of ISO 3183 for explanation of symbols used to designate orientation and location.
2)
All destructive tests may be sampled from pipe ends.
3)
Full-section longitudinal test pieces may be used at the option of the manufacturer, see App.B.
4)
If agreed, annular test pieces may be used for the determination of transverse yield strength by the hydraulic ring
expansion test in accordance with ASTM A370.
5)
For the HF weld seam, W means that the notch shall be located in the FL, while HAZ means that the notch shall be
located in FL +2 (see Figure B-6).
6)
HAZ means that the notch shall be located in FL and FL +2 (see Figure B-5).
7.3 Corrosion resistant alloy linepipe
7.3.1 General
7.3.1.1 All requirements of this subsection are applicable to welded and seamless linepipe in duplex stainless
steel and seamless martensitic 13Cr stainless steel.
7.3.1.2 Austenitic stainless steel and nickel based corrosion resistant alloy (CRA) linepipe shall be supplied
in accordance with a recognised standard that defines the chemical composition, mechanical properties,
delivery condition and all the details listed in Sec.6 and as specified in the following. If a recognised standard
is not available, a specification shall be prepared that defines these requirements.
7.3.2 Pipe designation
7.3.2.1 CRA linepipe to be used to this standard shall be designated with:
—
—
—
—
DNVGL
process of manufacture (see [7.1.4])
grade (see Table 7-11 or [7.3.1.2], as applicable)
supplementary requirement suffix (see [7.1.5]).
Guidance note:
e.g. “DNVGL SMLS 22Cr D” designates a seamless 22Cr duplex steel linepipe meeting the supplementary requirements for
enhanced dimensional requirements.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
7.3.3 Manufacturing
7.3.3.1 CRA linepipe shall be manufactured in accordance with the processes given in [7.1.4.2] using the
raw materials stated in the qualified MPS, follow the same activity sequence, and stay within the agreed
allowable variations. The manufacturing practice and instrumentation used to ensure proper control of the
manufacturing process variables and their tolerances shall be described in the MPS.
7.3.3.2 All steels shall be made by an electric or one of the basic oxygen processes.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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7.3.3.3 In addition to the requirements in [7.3.3.4] and [7.3.3.5] below, the following requirements given
for C-Mn steel pipe are also applicable for CRA pipes:
—
—
—
—
[7.2.3.4]- [7.2.3.6]for seamless pipe
[7.2.3.7]-[7.2.3.10]and [7.2.3.13]-[7.2.3.20]for all welded pipes
[7.2.3.21]-[7.2.3.26]for SAW and MWP pipe
[7.2.3.32]-[7.2.3.44]for all pipe.
7.3.3.4 Before further processing, the slabs/ingots shall be inspected and fulfil the surface finish
requirements specified in the MPS.
7.3.3.5 Duplex and austenitic stainless steel pipe shall be delivered in solution-annealed and waterquenched condition.
7.3.4 Acceptance criteria
7.3.4.1 The chemical composition of duplex stainless steel and martensitic 13Cr stainless steel parent
materials shall be according to Table 7-10. Modifications are subject to agreement. The limits and tolerances
for trace elements for martensitic 13Cr stainless steels, i.e. elements not listed in Table 7-10, shall be subject
to agreement.
7.3.4.2 Requirements for tensile, hardness and Charpy V-notch properties are given in Table 7-11. Weldment
shall meet the requirement for KVT impact properties. The Charpy V-notch specimens shall be tested at the
temperatures given in Table 7-6.
7.3.4.3 In addition to the requirements in [7.3.4.4] and [7.3.4.5] below, the following acceptance criteria
given for C-Mn steel pipe are also applicable to CRA pipe (as applicable):
—
—
—
—
[7.2.4.7] for transverse weld tensile testing
[7.2.4.10] and [7.2.4.11] for Charpy V-notch impact testing
[7.2.4.14] for guided-bend testing
[7.2.4.15] for fracture toughness testing of the seam weld.
7.3.4.4 For the flattening test of pipe with wall thickness ≥ 12.7 mm, there shall be no opening of the weld,
including the HAZ, until the distance between the plates is less than 66% of the original outside diameter.
For pipe with wall thickness < 12.7 mm there shall be no opening of the weld, including the HAZ, until the
distance between the plates is less than 50% of the original outside diameter.
7.3.4.5 For pipe with a D/t2 > 10, there shall be no cracks or breaks other than in the weld, including the
HAZ, until the distance between the plates is less than 33% of the original outside diameter.
7.3.4.6 The macro examination of weld seam shall meet the requirements in [7.2.4.16] and [7.2.4.17].
7.3.4.7 The microstructure of duplex stainless steel shall be essentially free from grain boundary carbides,
nitrides and intermetallic phases after solution heat treatment. Essentially free implies that occasional strings
of detrimental phases along the centreline of the base material is acceptable given that the phase content
within one field of vision (at 400X magnification) is < 1.0% (max. 0.5% intermetallic phases).
7.3.4.8 The base material ferrite content of duplex stainless steel shall be within the range 35-55%. For weld
metal the ferrite content shall be within the range 30-65%.
7.3.4.9 Pitting corrosion test according to ASTM G48 is only required for 25Cr duplex stainless steel. The
2
maximum allowable weight loss for is 4.0 g/m tested for 24 hours at 50°C and there shall be no pitting at
20 X magnification.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Table 7-10 Duplex
Element
1)
- and martensitic stainless steel linepipe, chemical composition
2)
Product analysis, wt.%
Grade
Grade
Grade
Grade
22Cr duplex
25Cr duplex
13Cr - 2 Mo
13Cr - 2.5 Mo
0.030 max
0.030 max
0.015 max
0.015 max
Mn
2.00 max
1.20 max
-
-
Si
1.00 max
1.00 max
-
-
P
0.030 max
0.035 max
0.025 max
0.025 max
S
0.020 max
0.020 max
0.003 max
0.003 max
Ni
4.50 - 6.50
6.00 – 8.00
4.50 min
6.00 min
Cr
21.0 - 23.0
24.0 – 26.0
12.0 min
12.0 min
Mo
2.50 – 3.50
3.00 – 4.00
2.00 min
2.50 min
N
0.14 – 0.20
0.20 – 0.34
-
-
-
-
C
PRE
-
min. 40
3)
Notes
1)
It is acknowledged that there are other duplex stainless steels commercially available, e.g. UNS S82551, which may
be considered subject to agreement provided all mechanical and corrosion properties, as relevant.
2)
If other alloying elements than specified in this table are being used, the elements and the maximum content shall
be agreed in each case.
3)
PRE = %Cr+3.3%(Mo+0.5W)+16%N.
Table 7-11 Duplex and martensitic 13Cr stainless steel linepipe, mechanical properties
SMYS
Grade
SMTS
MPa
MPa
Ratio
R
t0.5
/R
m
Maximum
hardness
(HV10)
Elongation
in 50.8 mm
A
f
Charpy V-notch energy (KVT)
1)
for BM, WM and HAZ
[%]
[J]
BM
WM
HAZ
Mean
Single
45
35
55
45
55
45
22Cr
450
620
0.92
290
350
25Cr
550
750
0.92
330
350
13Cr-2 Mo and
13Cr-2.5 Mo
550
700
0.92
300
na
Note
2)
Notes
1)
The required KVL (longitudinal direction specimens) values shall be 50% higher than the required KVT values.
2)
See note 4) in Table 7-5
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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7.3.5 Inspection
7.3.5.1 Compliance with the requirements of the purchase order shall be checked by specific inspection in
accordance with EN 10204, or an equivalent material inspection scheme. Records from the qualification of the
MPS and other documentation shall be in accordance with the requirements in Sec.12.
7.3.5.2 The inspection frequency during production and MPQT shall be as given in Table 7-12 and Table 7-13,
respectively. Reference to the relevant acceptance criteria is given in the tables.
7.3.5.3 A test unit is a prescribed quantity of pipe that is made to the same specified outside diameter and
specified wall thickness, by the same pipe-manufacturing process, from the same heat, and under the same
pipe-manufacturing conditions.
7.3.5.4 Sampling for mechanical and corrosion testing shall be performed after heat treatment, expansion
and final shaping. The samples shall not be prepared in a manner that may influence their mechanical
properties. See [7.2.5.5] for reduced frequency of testing in case of large quantities of pipe.
7.3.5.5 The number and orientation of the samples for SMLS and SAWL/SAWH pipe shall be according to
Table 7-9.
7.3.5.6 For EBW and LBW pipe, the number and orientation of the samples shall be as for HFW in Table 7-9.
7.3.5.7 For MWP pipe, the number and orientation of the samples shall be as for SAWL pipe in Table 7-9.
7.3.5.8 Requirements for retesting shall be according to [7.2.5.7] to [7.2.5.11].
7.3.5.9 Heat and product analysis shall be performed in accordance with App.B.
7.3.5.10 All elements listed in the relevant requirement/standard shall be determined and reported. Other
elements added for controlling the material properties may be added, subject to agreement.
7.3.5.11 If the value of any elements, or combination of elements, fails to meet the requirements, two retests shall be performed on samples taken from two different pipes from the same heat. If one or both retests fail to meet the requirements, the heat shall be rejected.
7.3.5.12 All mechanical testing shall be performed according to App.B.
7.3.5.13 Metallographic examination shall be performed in accordance with App.B.
7.3.5.14 Corrosion testing of 25Cr duplex stainless steels according to ASTM G48 shall be performed in
accordance with [B.3.2]. ASTM G48 testing is not applicable for 22Cr duplex or other CRAs with PRE lower
than 40.
7.3.5.15 Hydrostatic testing shall be performed in accordance with [7.5].
7.3.5.16 NDT, including visual inspection, shall be in accordance with [7.6].
7.3.5.17 Dimensional testing shall be performed according to [7.7].
7.3.5.18 Surface imperfections and defects shall be treated according to [D.8.3].
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Table 7-12 Inspection frequency for CRA linepipe
1)
Acceptance
criteria
Applicable to
Type of test
Frequency of testing
All pipe
All tests in Table 7-7 applicable to all
pipe
As given in Table 7-7
Table 7-10 and
Table 7-11
SAWL and MWP pipe
All tests in Table 7-7 applicable to SAWL
Flattening test
As shown in Figure 6 of ISO3183
[7.3.4.4] and
[7.3.4.5]
Metallographic examination
Once per test unit of not more
3)
than 50/100
[7.3.4.7] and
[7.3.4.8]
EBW and LBW pipe
2)
Duplex stainless steel pipe
25Cr duplex stainless steel Pitting corrosion test (ASTM G48 Method Once per test unit of not more
3)
pipe
A)
than 50/100
[7.3.4.9]
Notes
1)
Sampling of specimens and test execution shall be performed in accordance with App.B. The number orientation and
location of test pieces per sample for mechanical tests shall be according to [7.3.5.5] to [7.3.5.7].
2)
For EBW and LBW pipes the testing applies to the fusion line.
3)
Not more than 100 pipes with 114.3 mm ≤ D ≤ 508 mm and not more than 50 pipes for D > 508 mm.
1)
where :
D = specified outside diameter.
Table 7-13 Additional testing for manufacturing procedure qualification test of CRA linepipe
Applicable to
Type of test
Frequency of testing
All pipe
All production tests as stated in Table 7-12
All-weld tensile test
Welded pipe (all types)
Fracture toughness (CTOD) test of weld
2)
metal
1)
Acceptance
criteria
[7.3.4]
One test for each pipe provided
for manufacturing procedure
3)
qualification
Table 7-11
[7.2.4.15]
Notes
1)
Sampling of specimens and test execution shall be performed in accordance with App.B. The number, orientation
and location of test pieces per sample for mechanical tests shall be according to [7.3.5.5] to [7.3.5.7].
2)
CTOD testing is not required for pipes with t < 13 mm.
3)
Two pipes shall be provided for MPQT. The two pipes provided shall be from two different test units of different
heats.
7.4 Clad or lined steel linepipe
7.4.1 General
7.4.1.1 The requirements below are applicable to linepipe consisting of a C-Mn steel backing material with a
thinner internal CRA layer.
7.4.1.2 The backing steel of lined pipe shall fulfil the requirements in [7.2].
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7.4.1.3 The manufacturing process for clad or lined linepipe shall be according to [7.1.4.3] to [7.1.4.5].
7.4.1.4 Cladding and liner materials shall be specified according to recognised standards. If a recognised
standard is not available, a specification shall be prepared that defines chemical composition. If agreed
corrosion testing and acceptance criteria shall be specified.
7.4.1.5 The cladding/liner material thickness should not be less than 2.5 mm.
7.4.2 Pipe designation
7.4.2.1 In addition to the designation of the backing material (see [7.1.4]) clad/lined pipes shall be
designated with:
— C, for clad pipe, or
— L, for lined pipe
— UNS number for the cladding material or liner pipe (B) and end weld (E), when applicable.
Guidance note:
e.g. “DNVGL MWPL 415 D L - UNS S31600 (B) UNS N06625 (E)” designates a longitudinal welded pipe using multiple welding
processes with SMYS 415 MPa, meeting the supplementary requirements for dimensions, lined with a UNS designated material for
pipe body of stainless steel 316 and pipe ends of nickel alloy 625.
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7.4.3 Manufacturing procedure specification
7.4.3.1 In addition to the applicable information given in [7.1.7] and [7.1.8], the MPS for clad linepipe shall
as a minimum contain the following information (as applicable):
For roll bonded clad plates:
— slab reheating temperature and initial rolling practice of cladding alloy and backing material prior to
sandwich assembly
— method used to assemble the sandwich or one-sided-open package, as applicable, prior to reheating and
rolling
— package (sandwich or one-side-open) reheating temperature, start and stop rolling temperatures, means
of temperature and thickness control, start and stop temperatures for accelerated cooling (if applicable)
and inspection
— final plate heat treatment, e.g. quench and tempering (if applicable)
— method used to cut and separate the metallurgically roll bonded plates after rolling (separation of the
sandwich between the CRA layers
— details regarding any CRA clad welding to pipe ends.
For explosion welded clad plates:
— details for fabrication of backing and CRA layer (separate MPS can be submitted by the rolling mills)
— quality control checks for the pre-bond, explosion weld and post-bond process
— details of data to be recorded (e.g. CRA layer seam welding, surface preparation, plate assembly, standoff, surface finish)
— final plate heat treatment, e.g. quench and tempering (if applicable)
— cutting of side and end scrap.
7.4.3.2 In addition to the applicable information given in [7.1.7] and [7.1.8], the MPS for lined linepipe shall
as a minimum contain the following information (as applicable):
— details for fabrication of backing pipe and liner
— quality control checks for the lining process
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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—
—
—
—
details of data to be recorded (e.g. expansion pressure/force, strain, deformation)
procedure for cut back prior to seal welding or cladding to attach liner to carrier pipe
seal welding procedures
details regarding any CRA clad welding to pipe ends.
7.4.3.3 The following additional essential variables apply to the qualification of the MPS for clad linepipe (see
[7.1.8.8]]):
For roll bonded clad plates:
— sequence of welding.
For explosion welded clad plates:
—
—
—
—
stand-off distance between backing plate and CRA layer
type of explosive powder
explosive load
location for ignition point on plate.
7.4.4 Manufacturing
7.4.4.1 During all stages of manufacturing, contamination of CRA with carbon steel shall be avoided. Direct
contact of the CRA layer with carbon steel handling equipment (e.g. hooks, belts, rolls, etc.) is prohibited.
Direct contact may be allowed providing subsequent pickling is performed.
7.4.4.2 All work shall be undertaken in clean areas and controlled environment to avoid contamination and
condensation.
7.4.4.3 In addition to the requirements stated in [7.2.3] and [7.3.3] (as applicable), the following shall
apply:
7.4.4.4 The welding consumables for seam welds and liner seal welds shall be selected taking into
consideration the reduction of alloying elements by dilution of iron from the base material. The corrosion
properties of the weld consumable shall be equal or superior to the clad or liner material.
7.4.5 General requirements to manufacture of clad pipelines
7.4.5.1 The cladding alloy shall be produced from plate, and shall be supplied in a solution or soft annealed
condition, as applicable.
7.4.5.2 The steel backing material and the cladding alloy shall be cleaned, dried and inspected to ensure
that the level of humidity and particles between the respective plates are equal to or less than for the MPQT
plates.
7.4.5.3 The mating plate surfaces should as a minimum be blast cleaned to a surface cleanliness of ISO
8501 Sa2.
7.4.5.4 The metallurgical bonding of base and CRA layer shall be ensured by hot rolling of the sandwich (or
one-side-open packages, as applicable) or by explosion welding of the backer steel plate and the CRA layer.
If a seam weld (pre-weld) of the CRA layer is applied (prior to explosion bonding), the WPS shall be qualified
prior to start of any production welding. Qualification and production welding shall follow the principles in
App.C and testing in accordance with Table C-3, except all-weld testing is not required.
7.4.5.5 The package assembly for roll bonding consisting of sandwich or one-side-open, shall be
manufactured through a TMCP route, or receive a final heat treatment (e.g. QT). For explosion welded
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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clad material the backing steel plate shall be manufactured through a TMCP route, or receive a final heat
treatment (e.g. QT).
7.4.5.6 In addition to the applicable requirements given in [7.2.3.7] to [7.2.3.33], the following
requirements shall apply for welding of clad linepipe:
— the corrosion properties of the CRA weld consumable (e.g. root and hot pass) shall be equal or superior to
the clad material
— except for single pass per side welds, the longitudinal weld shall be back purged with welding grade inert
gas and be free from high temperature oxides
— tack welds shall be made using GTAW, GMAW, G-FCAW or SMAW using low hydrogen electrodes
— weld seam tracking of continuous welding shall be automatically controlled.
7.4.6 General requirements to manufacture of lined pipeline
7.4.6.1 The liner for lined pipe shall be manufactured according to API 5LC.
7.4.6.2 The internal surface of the C-Mn steel backing pipe shall be blast cleaned to a surface cleanliness of
ISO 8501 Sa2 along the complete length of the pipe prior to fabrication of lined pipe. The external surface of
the liner pipe shall be blast cleaned as specified above or pickled.
7.4.6.3 The liner pipe shall be inserted into the backing C-Mn steel pipe after both pipes have been carefully
cleaned, dried and inspected to ensure that the level of humidity and particles in the annular space between
these two pipes are equal to or less than for the MPQT pipes.
7.4.6.4 The humidity during assembly shall be less than 80%, and the carbon steel and CRA surfaces shall
be maintained at least 5°C above the dew point temperature. Temperature and humidity shall continuously
be measured and recorded.
7.4.6.5 After having lined up the two pipes, the liner shall be expanded by a suitable method to ensure
adequate gripping. The carbon steel pipe shall not receive a sizing ratio, sr , exceeding 0.015 during the
expansion process (see [7.2.3.34]).
7.4.6.6 The liner for lined pipe shall be welded according to API 5LC.
7.4.6.7 Seal welds, i.e. pipe end clad welds or fillet welds, shall be qualified according to [C.5.4], [C.5.6.5]
and [C.5.6.6], respectively. Production welding shall follow the principles in App.C.
7.4.6.8 Subsequent to expansion, the liner or backing pipe shall be machined at each end and further fixed
to the backing pipe by a seal weld (clad or fillet weld) to ensure that no humidity can enter the annulus
during storage, transportation and preparation for installation.
7.4.6.9 In addition to the applicable requirements given in [7.2.3.7] to [7.2.3.33], the following
requirements shall apply for welding of lined linepipe:
— the corrosion properties of the CRA weld consumable (e.g. fillet or clad weld) shall be equal or superior to
the liner material
— the weld shall be purged with welding grade inert gas and be free from high temperature oxides.
7.4.7 Acceptance criteria
7.4.7.1 The backing material of the manufactured clad or lined linepipe shall comply with the requirements
for C-Mn steel given in [7.2]. H2S service requirements according to [7.9.1] shall not apply to the backing
material unless required according to [7.9.1.15].
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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7.4.7.2 The cladding/liner material shall be removed from the test pieces prior to mechanical testing of the
backing material.
7.4.7.3 The hardness of the base material, cladding material, HAZ, weld metal and the metallurgical bonded
area shall meet the relevant requirements of this standard.
7.4.7.4 After bend testing in accordance with [B.2.5.9] (see Table 7-14), there shall be no sign of cracking or
separation on the edges of the specimens.
7.4.7.5 After longitudinal weld root bend testing in accordance with [B.2.5.7] (see Table 7-16), the bend test
specimen shall not show any open defects in any direction exceeding 3 mm. Minor ductile tears less than 6
mm, originating at the specimen edge may be disregarded if not associated with obvious defects.
7.4.7.6 The minimum shear strength shall be 140 MPa.
7.4.7.7 The CRA material shall meet the requirements of the relevant reference standard, e.g. API 5LD.
7.4.7.8 The chemical composition of the longitudinal seam weld (or overlay weld if applicable) of clad
pipes, pipe end clad welds, and the liner seal welds (if exposed to the pipe fluid), shall be analysed during
MPQT. The composition of the deposited weld metal as analysed on the exposed surface should meet the
requirements of the base material specification.
The calculated PRE (see Table 7-10, note 2) for alloy 625 weld metal should not be less than for the clad pipe
base material or liner material.
7.4.7.9 The weld metal and the HAZ in the root area of the clad pipe seam welds, any pipe end clad
welds and the seal welds of lined pipe shall be essentially free from grain boundary carbides, nitrides and
intermetallic phases.
7.4.7.10 Acceptance criteria for gripping force production testing of lined linepipe shall be agreed based on
project specific requirements (see [6.2.4]) and/or test results obtained during MPQT.
7.4.7.11 After the test for presence of moisture in the annulus between the liner and the backing material,
the pipe shall be inspected and no ripples or buckles in the liner or carbon steel pipe shall be in evidence
when viewed with the naked eye.
7.4.8 Inspection
7.4.8.1 Compliance with the requirements of the purchase order shall be checked by specific inspection in
accordance with EN 10204. Records from the qualification of the MPS and other documentation shall be in
accordance with the requirements in Sec.12.
7.4.8.2 The inspection frequency during production and MPQT shall be as given in Table 7-14 and Table 7-15,
respectively.
7.4.8.3 For clad pipe, the number and orientation of the samples shall be as for SAWL pipe in Table 7-9
7.4.8.4 For lined pipe, the number and orientation of the samples for the backing steel shall be according to
Table 7-9. Testing of the liner for lined pipe shall be according to API 5LC.
7.4.8.5 Requirements for retesting shall be according to [7.2.5.7] to [7.2.5.11].
7.4.8.6 Heat and product analysis shall be performed in accordance with [7.2.5] and [7.3.5] for the backing
steel and the CRA liner or cladding, respectively.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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7.4.8.7 All mechanical testing of clad pipe and the backing steel of lined pipe shall be performed according to
App.B. Mechanical testing of the liner for lined pipe shall be according to API 5LC.
7.4.8.8 Hardness testing of welded linepipe shall be performed on a test piece comprising the full crosssection of the weld. Indentations shall be made in the base material, cladding material and the metallurgical
bonded area as detailed in App.B.
7.4.8.9 Unless specified by purchaser, corrosion testing of roll bonded clad pipes or any longitudinal weld
seams is not required.
Guidance note:
ASTM G48 Method A testing is relevant in case flooding with raw sea water of material clad/lined with Alloy 625 is a design
requirement/assumption. Such testing is not relevant if the CRA material is UNS S31600, UNS S31603 or UNS N08825.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
7.4.8.10 Metallographic examination shall be performed in accordance with App.B.
7.4.8.11 Moisture between liner and backing steel may evaporate during coating and cause external
pressure to the liner and thereby implosion of the liner. To check for the presence of moisture in the annulus,
one finished pipe or a section thereof (minimum length of 6 m) shall be heated to 200°C for 15 minutes and
air cooled. This pipe shall be within the first 10 pipes produced.
7.4.8.12 Gripping force of lined pipe shall be measured in accordance with API 5LD. Equivalent tests may
be applied subject to agreement. Inspection frequency for production testing shall be agreed based on test
results obtained during the MPQT (see [7.4.3]).
7.4.8.13 Hydrostatic testing shall be performed in accordance with [7.5].
7.4.8.14 NDT, including visual inspection, shall be in accordance with [7.6].
7.4.8.15 Dimensional testing shall be performed according to [7.7].
7.4.8.16 Surface imperfections and defects shall be treated according to [D.8.3].
Table 7-14 Inspection frequency for clad or lined steel linepipe
Applicable to
Type of test
Frequency of testing
All pipe
All tests in Table 7-7 applicable to all pipe
All tests in Table 7-7 applicable to SAWL
Clad pipe
Bend tests (2 specimens)
Shear strength
Acceptance criteria
See Table 7-7 and [7.4.6]
[7.4.7.1]
Once per test unit of not more than 50
pipes
[7.4.7.5]
[7.4.7.6]
CRA material
According to reference standard (see [7.4.7.7])
of clad pipe
Liner pipe
Lined pipe
According to API 5LC (see [7.4.7.7])
Macrographic examination of seal weld
Once per test unit of not more than 50
pipes
[C.6.4.5]
Gripping force test
To be agreed, see [7.4.8.12]
[7.4.7.10]
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Table 7-15 Additional testing for manufacturing procedure qualification test of clad or lined steel
1)
linepipe
Applicable to
Type of test
Frequency of testing
All production tests in Table 7-14
All pipe
See Table 7-14
Relevant qualification tests in Table 7-8
See Table 7-8
Corrosion testing of welds, if agreed, see [7.4.8.9]
Chemical composition of seam weld and clad weld
Clad pipe
To be agreed
2)
Metallographic examination of the seam weld and clad weld
Longitudinal weld root bend test
Chemical composition of seal or clad welds
Lined pipe
Acceptance criteria
2)
Metallographic examination of seal welds
Liner collapse test
2)
One test for each
pipe provided for
manufacturing
procedure
qualification
[7.4.7.8]
[7.4.7.9]
[7.4.7.5]
[7.4.7.8]
[7.4.7.9]
[7.4.7.11]
Notes
1)
Sampling of specimens and test execution shall be performed in accordance with App.B. The number, orientation
and location of test pieces per sample for mechanical tests shall be according to [7.4.8.3] and [7.4.8.4].
2)
As applicable, according to [7.4.7.8] and [7.4.7.9].
7.5 Hydrostatic testing
7.5.1 Mill pressure test
7.5.1.1 Each length of linepipe shall be hydrostatically tested, unless the alternative approach described in
[7.5.1.6] is used. The water for testing should be clean and free from any suspended or dissolved substance
that can be harmful to the linepipe material.
7.5.1.2 The mill test pressure, pmpt, should be:
(7.3)
where:
(7.4)
(7.5)
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
DNV GL AS
Page 175
The following values are relevant for k for a mill pressure test:
— 1.00 for pipelines without end-cap (set up not introducing axial stresses)
— 1.15 for a mill pressure test with end cap effect transferred to the pipe.
7.5.1.3 In case a lower mill test pressure than specified in [7.5.1.2] is applied, a reduction in system test
pressure and incidental pressure in line with [5.4.2.1] shall be applied with the exception of the corrosion
allowance as discussed in [7.5.1.4] and waiving of mill pressure test in [7.5.1.6].
Guidance note:
A reduction in mill test pressure in line with this paragraph may be applicable for ultra deep water pipelines or where the wall
thickness is governed by other limit states, e.g. for reeling installation.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
7.5.1.4 In case significant corrosion allowance has been specified (as stated by the purchaser in the material
specification) or significant temperature de-rating of the mechanical properties take place, the mill test
pressure may be significantly higher than the incidental pressure. For such conditions and where the mill
pressure test capacity is limited, the mill test pressure may be limited to ph= 1.4·pli, (where pli is the local
incidental pressure).
7.5.1.5 The test configuration shall permit bleeding of trapped air prior to pressurisation of the pipe. The
pressure test equipment shall be equipped with a calibrated recording gauge. The applied pressure and the
duration of each hydrostatic test shall be recorded together with the identification of the pipe tested. The
equipment shall be capable of registering a pressure drop of minimum 2% of the applied pressure. The
holding time at test pressure shall be minimum 10 seconds. Calibration records for the equipment shall be
available.
7.5.1.6 Subject to agreement, the hydrostatic testing may be omitted for expanded pipes manufactured by
the UOE process. It shall in such situations be documented that the expansion process and subsequent pipe
inspection will:
— ensure that the pipe material stress-strain curve is linear up to a stress corresponding to [7.5.1.2]
— identify defects with the potential for through-thickness propagation under pressure loading
— identify pipes subject to excessive permanent deformation under pressure loading to a degree equivalent
to that provided by hydrostatic testing.
Workmanship and inspection shall be at the same level as for hydrostatically tested pipe.
The expansion process parameters and inspection results shall be recorded for each pipe.
7.5.1.7 For pipe classified as coiled line pipe, the mill pressure test of the finished coiled line pipe shall be
performed at a pressure corresponding to [7.5.1.2] using tmin. Pressure shall be held for not less than two
hours.
7.6 Non-destructive testing
7.6.1 Visual inspection
7.6.1.1 Visual inspection shall be in accordance with [D.8.5].
7.6.1.2 If visual inspection for detection of surface imperfections is substituted with alternative inspection
methods then the substitution shall conform to the requirements in [D.8.5.5].
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
DNV GL AS
Page 176
7.6.2 Non-destructive testing
7.6.2.1 Requirements for non-destructive testing (NDT) of linepipe are given in [D.8].
7.6.2.2 Requirements for NDT (laminar imperfections) and visual examination of plate, coil and strip
performed at plate mill are given in [D.7].
7.6.2.3 Table 7-16 lists the required NDT of linepipe including lamination check for welded linepipe.
For welded pipe, lamination checks may be performed on linepipe or plate/strip at the discretion of the
manufacturer.
7.6.2.4 Alternative test methods may be accepted subject to agreement according to [D.8.4.1] and
[D.8.4.2].
Table 7-16 Type and extent of non-destructive testing 1)
Applicable to
Scope of testing
Visual inspection
All
Residual magnetism
Imperfections in un-tested ends
Pipe ends of all pipe
SMLS
HFW, EBW and LBW
Reference
-
100%
[D.8.5]
-
3)
[D.8.5]
2)
5%
UT+ST
100% or
cut off
UT
100%
Laminar imperfections pipe end face/bevel
ST
100%
Laminar imperfections in pipe body
UT
100%
Longitudinal imperfections in pipe body
UT
100%
Transverse imperfections in pipe body
UT
100/10%
Wall thickness testing
UT
100%
Longitudinal surface imperfections in pipe
5)
body
ST
100/10%
Laminar imperfections in pipe body
UT
100%
Laminar imperfections in area adjacent to
weld
UT
100%
Longitudinal imperfections in weld
UT
100%
Laminar imperfections pipe ends
4)
Laminar imperfections in pipe body
Laminar imperfections in area adjacent to
weld
Coiled line pipe
Frequency
of testing
Type of test
UT or EC
8)
UT
100%
Skelp end weld – imperfections in weld
UT or RT
100%
Skelp end weld – surface imperfections
ST
Submarine pipeline systems
DNV GL AS
6)
[D.8.8]
6)
[D.8.9]
100%
100%
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
[D.8.7]
7)
UT or EC
Longitudinal imperfections in weld
[D.8.6]
[D.8.9]
9)
100%/R
Page 177
SAWL,
SAWH and MWP
Laminar imperfections in pipe body
UT
100%
Laminar imperfections in area adjacent to
weld
UT
100%
Imperfections in weld
UT
100%
ST
100%/R
Surface imperfections in weld area
5)
Imperfections at weld ends
CRA liner pipe
Lined pipe
10)
RT+UT
100%
11)
UT
100%
Laminar imperfections in pipe body
UT
100%
Longitudinal and transverse imperfections in
weld
UT
100%
Laminar imperfections in area adjacent to
weld
UT
100%
Surface imperfections in weld area
ST
100%/R
Imperfections in welds
RT
100%
Longitudinal and transverse imperfections in
weld
EC or RT
100%
[D.8.10]
As required for the type of backing material
used, see above
-
100%
-
Seal and clad welds
ST
100%
Clad welds (bonding imperfections)
UT
100%
Lack of bonding in pipe body and pipe ends
Clad pipe
[D.8.13]
[D.8.12]
12)
[D.8.11]
Notes
1)
The indicated test methods are considered to be industry standard. Alternative methods may be used as required in
[D.8.4].
2)
Nomenclature: UT = ultrasonic testing, ST = surface testing, e.g. magnetic particle testing or EMI (flux leakage)
for magnetic materials and liquid penetrant testing for non-magnetic materials, RT = radiographic testing and EC =
eddy current testing, see App.D.
3)
5% = testing of 5% of the pipes produced but at least once per 4 hour per operating shift.
4)
Laminar inspection is not applicable to pipe with t ≤ 5 mm. Standard width of band to be tested is 50 mm, but a
wider band may be tested if specified by the purchaser.
5)
Applicable to external surface only.
6)
100/10% = 100% testing of the first 20 pipes manufactured and if all pipes are within specification, thereafter
random testing (minimum five pipes per 8-hour shift) during the production of 10% of the remaining pipes.
7)
The wall thickness shall be controlled by continuously operating measuring devices.
8)
EC for lamination inspection is acceptable for WT < 10 mm.
9)
100%/R = 100% testing of the first 20 strip end welds. If all welds are within specification, thereafter random
testing of a minimum of one weld per 8-hour shift.
10) 100%/R = 100% testing of the first 20 pipes manufactured. If all pipes are within specification, thereafter random
testing of a minimum of one pipe per 8-hour shift.
11) Applies to pipe ends irrespective if clad welds are applied to pipe ends or not.
12) For external weld note 10) shall apply. For internal weld the frequency shall be 100%.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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DNV GL AS
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7.7 Dimensions, mass and tolerances
7.7.1 General
7.7.1.1 Linepipe shall be delivered to the dimensions specified in the linepipe specification, subject to
the tolerances in this standard or client specification (whichever are more stringent). Dimensions shall be
checked in final delivery condition and one dimensional feature shall be considered at a time.
Guidance note:
In practice dimensional control can be done at different stages in the pipe production. The key consideration is that the dimension
to be checked is in its final delivery condition at the time of measurement. For instance the weld reinforcement geometry of
welded pipe will not be influenced by pipe end bevelling – consequently it can be measured at an intermediary stage of production.
Consequently each dimension can be checked upon completion of all operations that can influence on the measured parameter.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e--Guidance note:
When measuring the linepipe dimensions and geometrical features it is reasonable to consider that each parameter (e.g. wall
thickness, diameter, out-of-roundness etc) is fully independent of the others. This means that the linepipe should be considered to
have nominal values for all parameters, except the one parameter being measured.
This might not fully reflect the reality; the pipe out-of-roundness may very well influence the diameter, and the wall thickness
variations can influence offset measurements and diameter measurements. Still, in order to have a common approach to linepipe
dimensions and geometry inspection it is important to consider one feature at a time.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
7.7.1.2 Suitable methods shall be used for the verification of conformance with the dimensional and
geometrical tolerances. Unless particular methods are specified in this standard or in the client specification,
the methods to be used shall be at the discretion of the manufacturer.
The manufacturer shall ensure sufficient training and instruction of the personnel, in order to provide a stable
and repeatable inspection practice.
7.7.1.3 All test equipment shall be calibrated, and the measurement resolution shall be sufficient to properly
evaluate the tolerances. Dimensional testing by automatic measuring devices is acceptable, and may replace
manual methods specified in this standard, provided the accuracy and precision of the measuring devices is
documented and found to be at least equal to relevant manual measurements.
Guidance note:
There are no explicit requirements to the measurement resolution and accuracy of equipment and methods for geometry control. It
is recommended that the manufacturer should be able to demonstrate a resolution of 10% of the allowed tolerance/variation (i.e. if
the allowed tolerance/variation is 1 mm, then the measurements should distinguish between features that differ by 0.1 mm).
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e--Guidance note:
The accuracy and error of a measurement practice depends on equipment, method and personnel. There is no requirement to
determine the overall accuracy/error of a measurement practice over time.
For manual practices this may be impossible, because the human factor plays a dominating role. Probably the best that can be
achieved is to approximate the measurement error to the calibration tolerance of the equipment, and rather in design calculations
keep in mind that there are limits to the practice accuracy that can be achieved (e.g. out-of-roundness can be difficult to measure
manually, and it would not be reasonable to require a maximum OoR on the order of 2-3 millimeters).
For automated practices it is quite feasible to establish an overall accuracy of the equipment and document the stability of
measurements over time. This can be achieved by using a reference object that is characterised at the start of a production run,
and later regularly measured during the production. Some statistical analysis of these data will give a good indication of the global
accuracy and error for the given measurement practice.
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Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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7.7.2 Tolerances
7.7.2.1 The diameter and out-of-roundness shall be within the tolerances given in Table 7-17 to Table 7-19.
7.7.2.2 The wall thickness shall be within the tolerances given in Table 7-20 and Table 7-21. This also applies
for grinded areas, see [D.8.3.8] and [D.8.3.9]. For welded pipes, the plus tolerances do not apply for the
weld.
7.7.2.3 Pipe length, including tolerances and statistical distribution (if relevant), shall be specified by the
purchaser. The application and/or installation approach should be considered.
Guidance note:
Typically an average length of 12.1 m may be the optimum length for handling on several S-lay barges in operation, but this could
change in the course of time. An average length of 12.1 m is not necessarily optimum for deepwater J-lay practice and can vary
according to the J-lay system used. It is the responsibility of the purchaser to agree with both the linepipe manufacturer and the
pipe-lay contractor the length range to be supplied. Pipe used for other applications, such as mother pipe for bends, may have
different length requirements.
The following should be considered:
- Will the installation method benefit from another standard linepipe length?
- Should a significant quantity of the delivered linepipes (subject to agreement) be within ±0.2m or ±0.1m of the required
standard linepipe length?
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
7.7.2.4 Other parameters shall be within the tolerances given in Table 7-22.
7.7.2.5 Tolerances for the weld seam of welded pipe, i.e.:
—
—
—
—
—
—
—
—
—
—
—
—
root penetration MR*
weld interpenetration (for double-sided SAW only) MR*
cap and root concavity
misalignment of weld beads for double sided welds
undercut
arc burns
start/stop craters/poor restart
surface porosity
cracks
lack of penetration/lack of fusion
systematic imperfections
burn through
shall be within the tolerances given in Table D-4.
*) MR indicates that the requirement is modified compared to ISO 3183.
7.7.2.6 Requirements for dents are given in [D.8.5].
7.7.3 Inspection
7.7.3.1 The frequency of dimensional testing shall be according to Table 7-23.
7.7.3.2 All specified tests shall be recorded as acceptable or non-acceptable. Recording frequency of actual
measured value shall be according to Table 7-23. During MPQT the actual value of all parameters for all
inspected pipes shall be recorded.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
DNV GL AS
Page 180
7.7.3.3 Diameter measurements shall be based on measurements using circumferential tape, if done by
manually. MR
7.7.3.4 Diameter values at pipe ends shall be determined based on inside (i.e. pipe internal surface)
measurements. For linepipe with internal diameter less than 150 mm outside measurements are allowed.
Pipe body diameter shall be measured towards the middle of the pipe and the choice between inside or
outside measurements is at the manufacturer’s discretion. When measurements are done on inside, the
tolerances applied shall be calculated based on nominal outside diameter (same as for outside diameter
measurements).MR
7.7.3.5 The out-of-roundness is the difference between the largest and smallest diameter in a given crosssectional plane (i.e. plane perpendicular to the pipe longitudinal axis). The out-of roundness should be
measured using a rod gauge or similar equipment and rotate this around the circumference in a given crosssection in order to search for the largest and smallest diameter. The measurements shall evaluate the full
circumference of the pipe. For welded pipes the measurements shall exclude only the weld itself. MR
7.7.3.6 Out-of-roundness values at pipe ends shall be determined from inside (i.e. pipe internal surface)
measurements. For linepipe with internal diameter less than 150 mm outside measurements are allowed.
Pipe body out-of-roundness shall be measured towards the middle of the pipe and the choice between inside
or outside measurements is at the manufacturer’s discretion. MR
7.7.3.7 For welded pipes where wall thickness measurements have been done on the plate or strip, the final
pipe shall be measured as follows;
— One measurement on each pipe end for every pipe
— One measurement on the pipe body for minimum three pipes per eight hours of production
For seamless pipes, wall thickness measurements shall be done on each pipe with a suitable method and
with measurement locations sufficient to properly document that the pipe wall thickness is within acceptable
limits.
For pipe with clad or lined CRA material, the WT shall be measured and reported for each material layer.
7.7.3.8 Wall thickness measurements shall be made with an automatic or manual non-destructive device, or
mechanical calliper. In case of dispute, the measurement determined by use of the mechanical calliper shall
govern. The mechanical calliper shall be fitted with contact pins having circular cross-sections of 6.35 mm in
diameter. The end of the pin contacting the inside surface of the pipe shall be rounded to a maximum radius
of 38.1 mm for pipe of size 168.3 mm or larger, and up to a radius of d/4 for pipe smaller than size 168.3
mm with a minimum radius of 3.2 mm. The end of the pin contacting the outside surface of the pipe shall be
either flat or rounded to a radius of not less than 38.1 mm.
7.7.3.9 Geometric deviations from the nominal cylindrical contour of the pipe (e.g. flat spots and peaks)
resulting from the pipe forming or manufacturing operations (i.e. not including dents) shall not exceed the
criteria in Table 7-22. Geometric deviations shall be measured as the gap between the extreme point (i.e.
deepest or highest) of the deviation and the prolongation of the contour of the pipe. A template with a
curvature equal to the nominal ID or OD of the pipe to be inspected shall be used. The length of the gauges
shall be 200 mm or 0.25 D, whichever is less. The gauges shall be made with a notch so that it can fit over
the weld cap.
At pipe ends the full internal circumference shall be inspected, over a length of minimum 100 mm from the
pipe end bevel.
Inspection of the external surface shall be performed along the weld and around the circumference whenever
indicated by visual inspection. MR
7.7.3.10 Straightness shall be measured according to Figure 1 and Figure 2 in ISO 3183. Measuring full
length straightness should be done at the concave orientation of the pipe, with a straight reference line (e.g.
a string) lifted equally above the surface at both ends (e.g. 10-15 mm).
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Page 181
7.7.3.11 Out-of squareness at pipe ends shall be measured according to Figure 3 in ISO 3183.
7.7.3.12 The pipe length shall be measured individually.
7.7.3.13
The weight of each pipe with D ≥ 141.3 mm shall be measured individually. For pipe with D < 141.3 mm, the
linepipes shall be weighed either individually or in convenient lots selected by the manufacturer.
7.7.3.14 The mass per unit length, rl, shall be used for the determination of pipe nominal weight and shall
be calculated using the following equation:
r
l
= t(D-t) · C
(7.6)
where:
r l is the mass per unit length, in kg/m
D is the nominal outer diameter, expressed in mm
t is the nominal wall thickness, in mm
C is 0.02466.
7.7.3.15 The cap reinforcement height shall be measured relative to the base metal immediately next to the
weld toe.
7.7.3.16 At the pipe ends the weld cap shall be removed (e.g. by machining or grinding), in order to allow
for AUT of the girth weld during installation. The height of the remaining weld metal shall be measured
relative to the base metal at the weld toe. The transition between areas with and without weld cap shall be
rounded (i.e. not a sharp feature). For external surface, the transition to the base material/pipe body shall be
smooth.
Guidance note:
The purpose of removing weld cap at the ends is to allow UT probes to pass without snagging (external surface).
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
7.7.3.17 The radial offset shall be measured as the difference in height (i.e. radial difference) of the base
metal within 100 mm of the weld toes. This can be measured either at external or internal surface, at the
manufacturer’s discretion.
7.7.3.18 A straight line shall be oriented parallel to the longitudinal axis of the weld (e.g. the longitudinal
axis of the pipe). The distance from this line to the weld toe shall be determined, and the difference between
the point closest and farthest from the line shall not exceed the acceptance criteria.
Guidance note:
The intention is to determine the presence of both waving bead/dogleg and widening/narrowing of the weld cap - both of which
indicates unstable welding process. This should not be a reason to reject the pipe, since the cap can be ground. Pipe purchaser can
require to be informed before any grinding, and require implementation of measures to improve the welding practice.
This control can be performed with a straight ruler of length 300 mm.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
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Page 182
7.7.3.19 The weld flash on HFW pipes shall be removed on both external and internal surfaces as required in
Table 7-22.
Table 7-17 Diameter tolerances, SMLS pipe
Diameter [mm]
Pipe body
D < 66.7
±0.5 mm
1)
66.7 ≤ D < 100
100 ≤ D < 320
±0.0075*D
320 ≤ D ≤ 610
610 < D < 1422
Pipe ends
2), 3)
±0.5 mm
±0.005*D
±1.6 mm
±0.01*D
±2.0 mm
D = Nominal outside diameter
1) Dimensions of pipe body shall be measured approximately in the middle of the pipe length.
2) The pipe end includes a length of 100 mm at each of the pipe extremities.
3) The tolerances apply for t ≤ 25.0 mm. For heavier wall thickness the tolerances shall be agreed between purchaser
and supplier, but in any case not larger than ±2.0 mm .
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Table 7-18 Diameter tolerances, welded pipe
1)
Pipe body
Diameter [mm]
Pipe end
-
D < 66.7
-
±0.5 mm
2)
±0.5 mm
±0.005*D
±0.0075*D
200 ≤ D < 320
Pipe end lined/clad
Suppl. req. D
±0.5 mm
66.7 ≤ D < 100
100 ≤ D < 200
2)
320 ≤ D < 426.7
426.7 ≤ D ≤ 610
±3.2 mm
610 < D < 800
±0.005*D
800 ≤ D ≤ 1422
±4.0 mm
±1.0 mm
±1.6 mm
1422 < D
As agreed
D = Nominal outside diameter
1) Dimensions of pipe body shall be measured approximately in the middle of the pipe length.
2) The pipe end includes a length of 100 mm at each of the pipe extremities.
Table 7-19 Out-of-roundness tolerances, all pipes
Diameter [mm]
Pipe end
2)
D < 60.3
1)
Pipe body
Pipe end all pipe,
except lined/clad
3)
-
Suppl. req. D
Included in the diameter tolerance
60.3 ≤ D < 400
0.01*D
0.015*D
0.0075*D
0.01*D
400 ≤ D < 450
450 ≤ D ≤ 610
610 < D < 666.7
0.01*D
4.5 mm
3.0 mm
1000 ≤ D < 1066.7
1422 ≤ D
Suppl. req. D
0.0075*D
666.7 ≤ D < 1000
1066.7 ≤ D < 1422
Pipe end lined/clad
10 mm
5.0 mm
8 mm
As agreed
D = Nominal outside diameter
1) For pipes with both D > 610 mm and D/t > 75, the tolerances shall be agreed between purchaser and supplier.
2) The pipe end includes a length of 100 mm at each of the pipe extremities.
3) For SMLS pipe body, the tolerances apply for t ≤ 25.0 mm, and the tolerances for heavier wall pipe shall be agreed
between purchaser and supplier.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
DNV GL AS
Page 184
Table 7-20 Wall thickness tolerances, seamless pipes
1, 2)
Wall thickness [mm]
Normal tolerances
t < 4.0
+0.6 mm ; -0.5 mm
4.0 ≤ t < 10.0
+0.15*t ; -0.125*t
10.0 ≤ t < 25.0
±0.125*t
+0.125*t ; -0.10*t
25.0 ≤ t < 30.0
+3.7 mm ; -3.0 mm
± 3.0 mm
30.0 ≤ t < 37.0
+3.7 mm ; -0.10*t
t ≥ 37.0
±0.10*t
t
Suppl. req. D
= specified nominal wall thickness
1)
If the purchase order specifies a minus tolerance for wall thickness smaller than the applicable value given in this
table, the plus tolerance for wall thickness shall be increased by an amount sufficient to maintain the applicable
tolerance range.
2)
For pipe with D ≥ 355.6 mm and t ≥ 25.0 mm, the tolerance is ±0.125*t.
Table 7-21 Wall thickness tolerances, welded pipes
1, 2, 3)
Wall thickness [mm]
Normal tolerances
Suppl. req. D
t ≤ 6.0
± 0.5 mm
± 0.4 mm
6 < t ≤ 10
± 0.7 mm
± 0.6 mm
10 < t ≤ 20
± 1.0 mm
± 0.8 mm
t > 20.0
+1.5, -1.0
± 1.0 mm
t
= specified nominal wall thickness
1) If the purchase order specifies a minus tolerance for wall thickness smaller than the applicable value given in this
table, the plus tolerance for wall thickness shall be increased by an amount sufficient to maintain the applicable tolerance
range.
2) Subject to agreement a larger plus tolerance for metallurgically clad pipes may be applied.
3) The plus tolerance for wall thickness does not apply to the weld area.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
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Table 7-22 Tolerances for pipe geometric properties not covered in Tables 7-18 to Table 7-21
Characteristic to be tested
Tolerances
Geometric deviations (peaking and flats). Only applicable to 0.005 D or 2.5 mm, whichever is less
welded pipes.
Suppl. req. D: 0.005 D or 1.5 mm, whichever is less
Straightness, max. for full length of pipe
≤ 0.0015 L
Straightness, max. deviation for pipe end region. End
region is 1.0 m at each of the pipe extremities.
3 mm
Out-of squareness at pipe ends
≤ 1.6 mm from true 90°
Length
See [7.7.2.3]
Weight of each single pipe/pipe bundle
-3.5% / +10% of nominal weight
Cap reinforcement height (longitudinal weld)
External weld:
For t < 13 mm: max 3.0 mm.
For t ≥ 13 mm: max 4.0 mm
Internal weld:
Max 3.5 mm
Cap reinforcement height (longitudinal weld) – pipe ends
both external and internal. Not applicable to HFW linepipes.
After grinding, the specified minimum WT shall be met.
Maximum height 0.5 mm
Minimum height 0.0 mm
Length of cap to be removed, measured from pipe end
bevel;
External weld: minimum 250 mm
Internal weld: minimum 100 mm
Radial offset of strip/plate edges (longitudinal weld)
For t ≤ 15 mm: max 1.3 mm
For 15 mm < t ≤ 25 mm: max 0.1 t
For t > 25 mm: max 2.0 mm
The radial offset of HFW linepipe shall not reduce the
thickness of the weld to less than t min.
For welds in clad/lined material, the radial offset shall not
reduce the effective thickness of the cladding/liner in the
root area.
Deviation of weld toe from a straight line (double-sided
SAW in pipe mills)
The weld toe shall run parallel to the weld longitudinal axis.
The maximum deviation within any section of 300 mm
length is 0.20 t, but not more than 4.0 mm.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Page 186
Weld flash (HFW longitudinal welds only)
The flash trimming shall not reduce the wall thickness to
below tmin.
External surface : Removed to be essentially flush with the
pipe surface, without any noticeable radial step.
Internal surface : Removed to be maximum 0.3 mm +
0.05t above the contour of the pipe.
The resulting internal groove shall have a smooth transition
to the base metal without notches. The groove depth shall
be maximum 0.05t (see also ISO 3183 Table 15).
Table 7-23 Inspection and recording frequency, all pipes
Inspection frequency
Normal
Suppl. req. D
Record test values, as
frequency of inspected pipes
5 %, but minimum 3 pipes
per 8-hour shift
For D ≤ 168.3 mm; once
per test unit of not more
than 100 lengths of pipe,
but minimum one (1) and
maximum 6 pipes per 8hour shift.
Each pipe end
10 %
5 %, but minimum 3 pipes
per 8-hour shift
10 %
Wall thickness
Each pipe
Each pipe
10 %
Geometric deviations (only
welded pipes)
10 %
10 %
Straightness, full length and
pipe end region
5 %, but minimum 3 pipes
per 8-hour shift
For D ≤ 168.3 mm;
maximum 6 pipes per 8hour shift.
5 %, but minimum 3 pipes
per 8-hour shift
100 %
100 %
Cap reinforcement height
(longitudinal weld)
5 %, but minimum 3 pipes
per 8-hour shift
5 %, but minimum 3 pipes
per 8-hour shift
Cap reinforcement height
(longitudinal weld) – pipe
ends
100 %
100 %
Radial offset of strip/plate
edges (longitudinal weld)
5 %, but minimum 3 pipes
per 8-hour shift
5 %, but minimum 3 pipes
per 8-hour shift
Characteristic to be tested
Diameter, pipe end
Out-of-roundness, pipe end
Diameter and out-ofroundness, pipe body
Out-of-squareness
Length
10 %
-
-
Weight
Deviation of weld toe from
a straight line (double-sided
SAW in pipe mills)
100 %
100 %
-
100%
Weld flash (HFW longitudinal
welds only)
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
DNV GL AS
Page 187
7.8 Marking, delivery condition and documentation
7.8.1 Marking
7.8.1.1 All marking shall be easily identifiable and durable in order to withstand pipe loading, shipping, and
normal installation activities.
7.8.1.2 Marking shall include DNV GL linepipe designation (see [7.2.2], [7.3.2] and [7.4.2]). Other type of
marking shall be subject to agreement.
7.8.1.3 Each linepipe shall be marked with a unique number. The marking shall reflect the correlation
between the product and the respective inspection document.
7.8.2 Delivery condition
7.8.2.1 The delivery condition of C-Mn steel pipe shall be according to Table 7-1.
7.8.2.2 The internal surface of CRA pipes shall be pickled in accordance with the purchase order. If agreed
the external surface of CRA pipes shall be cleaned.
7.8.3 Handling and storage
7.8.3.1 On customer's request, each linepipe shall be protected until taken into use.
7.8.3.2 For temporary storage see [6.4.3].
7.8.4 Documentation, records and certification
7.8.4.1 Linepipe shall be delivered with inspection certificate 3.1 according to European Standard EN 10204
(Metallic Products - Types of Inspection Documents) or an accepted equivalent.
7.8.4.2 Inspection documents shall be in printed form or in electronic form as an EDI transmission that
conforms to any EDI agreement between the purchaser and the manufacturer.
7.8.4.3 The inspection certificate shall identify the products represented by the certificate, with reference
to product number, heat number and heat treatment batch. The specified outside diameter, specified wall
thickness, pipe designation, type of pipe, and the delivery condition shall be stated.
7.8.4.4 The certificate shall include or refer to the results of all specified inspection, testing and
measurements including any supplementary testing specified in the purchase order. For HFW pipe, the
minimum temperature for heat treatment of the weld seam shall be stated.
7.8.4.5 Records from the qualification of the MPS and other documentation shall be in accordance with the
requirements in [12.3.1].
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
DNV GL AS
Page 188
7.9 Supplementary requirements
7.9.1 Supplementary requirement, H2S service (S)
7.9.1.1 Linepipe for H2S service (also referred to as sour service) shall conform to the requirements below.
[6.2.2] provides guidance for material selection.
7.9.1.2 All mandatory requirements in ISO 15156-2/3 shall apply, in combination with the additional
requirements of this standard.
Guidance note:
ISO 15156-1/2/3, Sec.1, states that the standard is only applicable to the qualification and selection of materials for equipment
designed and constructed using conventional elastic design criteria. Any detrimental effects of induced strain will only apply if
these are imposed during exposure to an H2S-containing environment; hence, for manufacture and installation of pipelines the
restrictions imposed in the ISO standard are applicable also to strain based design. Any restrictions for maximum allowable strain
during operation are beyond the scope of this standard.
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7.9.1.3 C-Mn steel linepipe for H2S service shall conform to [7.2], and to the modified and additional
requirements below, which conform to the requirements in ISO 3183 Annex H.
7.9.1.4 The chemical compositions given in Table 7-3 and Table 7-4 shall be modified according to Table 7-24
and Table 7-25, respectively.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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DNV GL AS
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Table 7-24 Chemical composition for SMLS and welded C-Mn steel pipe with delivery condition N
or Q for Supplementary requirement, H2S service
SMYS
Product analysis, maximum. weight %
1)
C
Mn
1)
S
2)
Other
3)
Pipe with delivery condition N - according to Table 7-1
245
-
-
0.003
-
290
-
-
0.003
-
320
-
-
0.003
-
360
-
-
0.003
-
Pipe with delivery condition Q - according to Table 7-1
245
-
-
0.003
-
290
-
-
0.003
-
320
-
-
0.003
-
360
-
-
0.003
-
390
-
-
0.003
-
415
-
-
0.003
Note
4)
450
-
-
0.003
Note
4)
485
0.16
1.65
0.003
Notes
4, 5)
Notes
1)
For each reduction of 0.01% below the specified maximum for carbon, an increase of 0.05% above the specified
maximum for manganese is permissible, up to a maximum increase of 0.20%.
2)
If agreed the sulphur content may be increased to ≤ 0.008% for SMLS and ≤ 0.006% for welded pipe, and in such
cases lower Ca/S may be agreed.
3)
Unless otherwise agreed, for welded pipe where calcium is intentionally added, Ca/S ≥ 1.5 if S > 0.0015%. For
SMLS and welded pipe Ca ≤ 0.006%.
4)
If agreed Mo ≤ 0.35%.
5)
The maximum allowable Pcm value shall be 0.22 for welded pipe and 0.25 for SMLS pipe.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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DNV GL AS
Page 190
Table 7-25 Chemical composition for welded C-Mn steel pipe with delivery condition M for
supplementary requirement, H2S service
SMYS
Product analysis, maximum. weight %
C
1)
Mn
1)
S
2)
3)
Other
245
0.10
-
0.002
-
290
0.10
-
0.002
-
320
0.10
-
0.002
-
360
0.10
1.45
0.002
-
390
0.10
1.45
0.002
-
415
0.10
1.45
0.002
Note
450
0.10
1.60
0.002
Notes
4)
485
0.10
1.60
0.002
Notes
4)
4)
Notes
1 to 4) See Table 7-24.
7.9.1.5 Vacuum degassing or alternative processes to reduce the gas content of the steel should be applied.
7.9.1.6 The molten steel shall be treated for inclusion shape control.
7.9.1.7 The requirements for mechanical properties in [7.2.4] shall apply, except for the hardness.
7.9.1.8 During MPQT and production, the hardness in the pipe body, weld and HAZ shall not exceed 250
HV10. If agreed, (see ISO 15156-2) and provided the parent pipe wall thickness is greater than 9 mm and
the weld cap is not exposed directly to the H2S environment, 275 HV10 is acceptable for the weld cap area.
Guidance note:
It is recommended to specify a maximum hardness of 235 HV10 for the base material in order to allow for hardness increase
during installation girth welding. If 275 HV10 is allowed in the cap area, the hardness in the corresponding base metal should be
limited to 250 HV10.
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7.9.1.9 Any hard spot larger than 50 mm in any direction, see Table 7-7, shall be classified as a defect if its
hardness, based upon individual indentations, exceeds:
— 250 HV10 on the internal surface of the pipe, or
— 275 HV10 on the external surface of the pipe.
Pipes that contain such defects shall be treated in accordance with [D.8.3].
7.9.1.10 The acceptance criteria for the HIC test shall be the following, with each ratio being the maximum
permissible average for three sections per test specimen when tested in solution (Environment) A (see Table
B.3 of ISO 15156-2):
— crack sensitivity ratio (CSR) ≤ 2%
— crack length ratio (CLR) ≤ 15%, and
— crack thickness ratio (CTR) ≤ 5%.
If HIC tests are conducted in alternative media (see [B.3.3.2]) to simulate specific service conditions,
alternative acceptance criteria may be agreed.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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DNV GL AS
Page 191
7.9.1.11 By examination of the tension surface of the SSC specimen under a low power microscope at X10
magnification there shall be no surface breaking fissures or cracks, unless it can be demonstrated that these
are not the result of sulphide stress cracking.
7.9.1.12 CRA linepipe for H2S service shall conform to [7.3], and the recommendations given in [6.2.2].
7.9.1.13 Linepipe grades, associated hardness criteria, and requirements to manufacturing/fabrication shall
comply with ISO 15156-3.
7.9.1.14 Clad or lined steel or linepipe for H2S service shall conform to [7.4], and to the modified and
additional requirements below.
7.9.1.15 Materials selection for cladding/liner, the associated hardness criteria, and requirements to
manufacturing and fabrication shall comply with ISO 15156-3. The same applies to welding consumables for
weldments exposed to the internal fluid. For selection of the C-Mn steel base material the considerations in
A13.1 of ISO 15156-3 shall apply.
7.9.1.16 During qualification of welding procedures and production, hardness measurements shall be
performed as outlined in App.B. The hardness in the internal heat-affected zone and in the fused zone of the
cladding/lining shall comply with relevant requirements of ISO 15156-3.
7.9.1.17 The frequency of inspection shall be as given in Table 7-7, Table 7-8, Table 7-12, Table 7-13, Table
7-14 and Table 7-15 as relevant, and with additional testing given in Table 7-26.
7.9.1.18 HIC testing during production shall be performed on one randomly selected pipe from each of
the three (3) first heats, or until three consecutive heats have shown acceptable test results. After three
consecutive heats have shown acceptable test results, the testing frequency for the subsequent production
may be reduced to one test per casting sequence of not more than ten (10) heats.
7.9.1.19 If any of the tests during the subsequent testing fail, three pipes from three different heats of the
last ten heats, selecting the heats with the lowest Ca/S ratio (based on heat analysis), shall be tested, unless
the S level is below 0.0015. For heat with S level greater than 0.0015 heats shall be selected with the lowest
Ca/S ratio. Providing these three tests show acceptable results, the ten heats are acceptable. However, if any
of these three tests fail, then all the ten heats shall be tested. Further, one pipe from every consecutive heat
shall be tested until the test results from three consecutive heats have been found acceptable. After three
consecutive heats have shown acceptable test results, the testing frequency may again be reduced to one
test per ten heats.
7.9.1.20 SSC testing is required unless the pipe material is pre-qualified in ISO 15156, see [6.2.2.2]. If
the material is pre-qualified, the purchaser may specify SSC testing. SSC testing shall be performed in
accordance with ISO 15156 2/3 as applicable. (see [6.2.2.2]).
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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DNV GL AS
Page 192
Table 7-26 Applicable testing for supplementary requirement S 1)
Type of pipe
Type of test
Frequency of testing
Acceptance criteria
Production tests
Welded C-Mn steel pipe
HIC test
In accordance with
[7.9.1.18] and
[7.9.1.18]
Tests for manufacturing procedure qualification test
2
Type of pipe
Type of test
Frequency of testing
Welded C-Mn steel pipe
HIC test
One test (3 test pieces)
for each pipe provided
for manufacturing
procedure qualification
All pipe
3)
SSC test
[7.9.1.10]
Acceptance criteria
[7.9.1.10]
[7.9.1.11]
Notes
1)
Sampling of specimens and test execution shall be performed in accordance with App.B.
2)
To be performed on strain and aged material if Supplementary requirement P (see [7.9.3.7]) has been specified
3)
SSC testing is required for C-Mn and low alloy steels with SMYS > 450 MPa, 13Cr martensitic stainless steels and
other materials not listed for H2S service in ISO 15156. (See [6.2.2.2].
7.9.2 Supplementary requirement, fracture arrest properties (F)
7.9.2.1 The requirements to fracture arrest properties are valid for gas pipelines carrying essentially pure
methane up to 80% usage factor (see Table 13-1), up to a pressure of 15 MPa, 30 mm wall thickness and
1120 mm diameter
Testing shall be according to Table 7-28.
7.9.2.2 A Charpy V-notch transition curve shall be established for the linepipe base material. The Charpy
V-notch energy value in the transverse direction at Tmin shall, as a minimum, meet the values given in
Table 7-27. Five sets of specimens shall be tested at different temperatures, including Tmin, and the results
documented in the qualification report.
7.9.2.3 This paragraph does not apply to C-Mn linepipes delivered with a final heat treatment (e.g.
normalising or quench and tempering), or 22Cr and 25Cr linepipes. A Charpy V-notch transition curve
shall be established for the linepipe base material in the aged condition. The plastic deformation shall be
equal to the actual deformation introduced during manufacturing (no additional straining is required). The
samples shall be aged for 1 hour at 250°C. Five sets of specimens shall be tested at different temperatures,
including Tmin. The Charpy V-notch energy value in the transverse direction, at Tmin, shall as a minimum
meet the values given in Table 7-27 in the aged condition. Values obtained at other test temperatures are for
information.
7.9.2.4 Drop Weight Tear Testing (DWTT) shall only be performed on all linepipes with outer diameter >
400 mm, wall thickness > 8 mm and SMYS > 360 MPa. A DWTT transition curve shall be established for the
linepipe base material. Minimum five sets of specimens shall be tested at different temperatures, including
Tmin. Each set shall consist of two specimens taken from the same test coupon. The test shall be performed
in accordance with App.B. The specimens tested at the minimum design temperature and all temperatures
above, shall as a minimum, meet an average of 85% shear area with one minimum value of 75%.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
DNV GL AS
Page 193
Guidance note:
It is globally recognised that inversed fracture appearance may occur in high toughness pipeline materials which could negatively
affect the test results. DNV GL supports the statement given in API RP 5L3, section 4.2.
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7.9.2.5 If supplementary requirements for H2S service as in [7.9.1] are specified for linepipe material with
SMYS ≥ 450 MPa the acceptance criteria stated in [7.9.2.4] (average and minimum shear area) may be
subject to agreement.
Table 7-27 Charpy V-notch impact test requirements for fracture arrest properties tested at T min
(joules; transverse values; average value of three full size base material specimens) 1, 2)
Wall thickness
≤30 mm
3)
D (mm)
SMYS
≤610
≤820
≤1120
245
40
40
40
290
40
43
52
360
50
61
75
415
64
77
450
73
485
555
4)
Notes
1)
Minimum individual results to exceed 75% of these
values, (max 1 specimen per set)
2)
The values obtained in the longitudinal direction, when
tested, shall be at least 50% higher than the values
required in the transverse direction.
95
3)
89
109
Fracture arrest properties for larger wall thicknesses and
diameters shall be subject to agreement (see [5.4.9])
4)
SMYS 550 for 22Cr, 25Cr and 13Cr
82
100
124
103
126
155
Table 7-28 Applicable testing for supplementary requirement F
Production tests
Type of pipe
Type of test
All pipe
DWT testing (with limitations give to dimensions in [7.9.2.4])
Tests for manufacturing procedure qualification test
Frequency of
testing
Acceptance
criteria
Once per test
unit of not more
1)
than 50/100
pipes
[7.9.2.4] (see
also Table 7-28)
One test for
each pipe
provided for
manufacturing
procedure
qualification
Table 7-27
3)
Table 7-27
3)
2
All pipe
CVN impact testing of the pipe body for establishment of
transition curve
Welded pipe
except CRA pipe
CVN impact testing of the pipe body for establishment of
3)
transition curve, aged condition
All pipe
DWT testing of the pipe body for establishment of transition
curve (with limitations give to dimensions in [7.9.2.4])
[7.9.2.4] (see
also [7.9.2.5])
Notes
1)
Not more than 100 pipes with D ≤ 508 mm and not more than 50 pipes for D > 508 mm.
2)
To be performed on strain and aged material if Supplementary requirement P (see [7.9.3.7]) has been specified
3)
The values obtained in the longitudinal direction, when tested, shall at least be 50% higher than the values required
in the transverse direction.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
DNV GL AS
Page 194
7.9.3 Supplementary requirement, linepipe for plastic deformation (P)
7.9.3.1 The objectives of supplementary requirement P are to:
— mitigate the effect of variations in mechanical and geometrical properties along the pipe, in particular
across the girth welds (between two adjacent line pipes), through
— reduced variation in mechanical properties
— reduced variation in geometrical tolerances at the pipe ends
— increased strain hardening
— ensure that the level of straining not cause sub-standard specific material properties.
7.9.3.2 Supplementary requirement (P) is applicable to line pipe (including C-Mn backing steel for lined/
clad pipes) when the total nominal strain in longitudinal direction from a single event exceeds 1.0% or the
accumulated nominal plastic strain in longitudinal direction exceeds 2.0%, see Table 5-10. The requirements
are only applicable to single event strains below 5%.
7.9.3.3 Supplementary requirement (D) should be specified.
Table 7-29 Additional testing for supplementary requirement P
1)
As manufactured condition
Type of pipe
All pipe
Type of test
Frequency of testing
Acceptance criteria
Production testing:
Max(YS) 5)
Min(YS)≤100 MPa
Once per test unit of not more
3)
than 50/100
pipes
Tensile testing of the pipe body,
longitudinal specimen of proportional
2)
type
Manufacturing procedure
qualification:
6)
YS/TS≤0.90
UEL > 5%
9)
One test for one of the pipes
Strained and aged condition
Type of pipe
Type of test
7
Frequency of testing
UTS (Rm)> YS
8)
(Rt0.5)
Tensile testing of the pipe
2)
body, longitudinal specimen
UEL > 5%
All pipe
CVN impact testing of the pipe body
Manufacturing procedure
qualification:
Hardness testing
One test for one of the pipes
Tensile testing of weld filler
10)
metal (all weld test)
Welded pipe
CVN impact testing of the seam weld
Acceptance criteria
Table 7-5 or Table
7-11, as relevant
UTS (Rm)> YS
8)
(Rt0.5)
UEL > 5%
4)
Hardness testing of the seam weld
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
DNV GL AS
9)
9)
Table 7-5 or Table
7-11, as relevant
Page 195
Notes
1)
Mechanical and corrosion testing shall be performed in accordance with App.B.
2)
Proportional type specimens according to ISO 6892 should be tested, see [B.2.3.8]. For smaller diameter pipes
tensile testing may be performed using full sized specimens (full pipe if it is impossible to prepare proportional type
specimen due to size constraints.
3)
Not more than 100 pipes with D < 508 mm and not more than 50 pipes for D ≥ 508 mm.
4)
CVN testing performed unless excepted, see [B.2.4.2].
5)
Applicable for C-Mn steel with SMYS up to and including 450 MPa, otherwise subject to agreement.
6)
See [7.9.3.5].
7)
See [7.9.3.6].
8)
For material with last cycle in tension.
9)
See [6.2.4.1]. Subject to agreement, lower UEL for strained and aged condition can be applied. A lower UEL should
conservatively reflect the strain level in the pipeline in operation, and should not be lower than 2.5%.
10) This applies to pipes with weld filler material
7.9.3.4 Mechanical testing shall be performed both in the as-manufactured (prior to any reeling) and in the
strained and aged condition in accordance with Table 7-29.
7.9.3.5 As an alternative to the requirements in Table 7-29, all relevant failure modes in [5.4] shall be
evaluated for the relevant maximum YS/TS ratio and variations in YS, TS and wall thickness, but the YS/TS
ratio shall not exceed 0.98.
7.9.3.6 As part of qualification of the pipe material, the line pipe material shall be strained and aged to
simulate the representative plastic deformation during installation. The plastic deformation shall either
be simulated by full scale testing of a pipe or strip specimens extracted from pipes (see [B.2.11.2] to
[B.2.11.10]). Mechanical testing shall be performed on material which has been subjected to last strain
increment in tension. Recommended practice for straining of strips is given in DNVGL-RP-F108. The samples
shall be artificially aged at 250°C for one hour before testing.
7.9.3.7 If the supplementary requirement for H2S service (S) and/or fracture arrest properties (F) is
required, the testing for these supplementary requirements shall be performed on samples that are removed,
strained and artificially aged in accordance with [7.9.3.6]. Testing shall be performed on material which has
been subjected to last strain increment in tension. The relevant acceptance criteria shall be met.
7.9.3.8 Qualification for supplementary requirement P may be based on historical data to be documented by
the manufacturer, subject to agreement. This may be applied if all relevant parameters are identical (WT, ID,
chemical composition, deformation scenario (e.g. same or less onerous deformation scenario), steelmaking/
rolling practice, heat treatments).
7.9.4 Supplementary requirement, dimensions (D)
7.9.4.1 Supplementary requirements for enhanced dimensional requirements for linepipe (D) are given in
Table 7-18 to Table 7-23. Implementing supplementary requirement D should be done by the purchaser
considering the influence of dimensions and tolerances on the subsequent fabrication/installation activities
and the welding facilities to be used.
Guidance note:
Supplementary requirement D is beneficial for local buckling during reel-lay installation. The requirements of D are applicable to as
milled pipe prior to reeling.
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Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
DNV GL AS
Page 196
7.9.5 Supplementary requirement, high utilisation (U)
7.9.5.1 Supplementary requirement U is required in order to apply a material strength factor αU of 1.00. The
purpose of supplementary requirement U is to have sufficient confidence that there are no pipes with yield
strength below the minimum required value (i.e. insignificant tail below the requirement).
This supplementary requirement is only valid for:
— material yield strength
— both tensile and compressive testing
— both transverse and longitudinal direction.
The supplementary requirement can be applied to one or several of the properties mentioned above. In
this sub-section requirements are related to SMYS. If supplementary requirement is applied to compressive
strength, the agreed minimum requirement value shall be used, as relevant. Compressive testing is not
required by this standard, but may be relevant for some projects.
Guidance note:
When applied, supplementary requirement U is typically relevant for transverse tensile yield strength in cases where pressure
containment is a governing limit state. When installation loads are a concern, supplementary requirement U can be applied to
longitudinal tensile yield strength.
Supplementary requirement U may be relevant for transverse compressive yield strength in case of large water depth.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
7.9.5.2 There are two separate approaches to achieve supplementary requirement U, and it is sufficient to
use only one of them:
— modified testing regime during production, as described in this subsection
— retrospective documentation.
Review and analysis of records from fabrication and testing may justify an increase of the SMYS. This shall be
done only by agreement, and based on an evaluation of the fabrication process and documentation. It may
be allowed to increase the SMYS up to but not including the next material grade.
Guidance note:
The purpose of both approaches is the same. However, it is not guaranteed that the modified testing regime will give an average
yield strength value that is two standard deviations above the minimum required value.
The modified testing regime has been designed so that the confidence in the desired outcome is high. It is an approach based on
probability functions and expected distribution –there will always be some uncertainty.
Consequently supplementary requirement U should be considered fulfilled if the modified testing regime has been followed – even
if a retrospective analysis of the pipes may show that the actual average value is somewhat less than 2.0 standard deviations from
the minimum required value.
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7.9.5.3 The modified testing regime has a set of re-testing steps, based on the results.
Re-testing of failed pipes is not permitted. However, if the test results are influenced by improper sampling,
machining, preparation, treatment or testing, the test sample shall be replaced by a correctly prepared
sample from the same pipe, and a new test performed.
7.9.5.4 The production test of the modified testing regime shall have:
— testing frequency as stated in Table 7-7 or Table 7-12.
— result equal to or larger than SMYS x 1.03 times.
If the result meets the requirement, the test unit is accepted. If the result does not meet the requirement,
then retesting shall be carried out – or the test unit shall be rejected.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Page 197
7.9.5.5 If the production test result is below SMYS, the tested pipe shall be rejected. Four additional pipes
within the same test unit shall be sampled, for a total of four new tests. If all four re-tests meet SMYS, the
test unit is acceptable. If at least one of the re-tests is below SMYS, the test unit shall be rejected.
7.9.5.6 If the production test result is between 1.03 x SMYS and SMYS, the tested pipe is acceptable. In
addition, two pipes within the same test unit shall be sampled, for a total of two confirmatory tests. If both
confirmatory tests meet SMYS, the test unit is acceptable. If at least one of the confirmatory tests is below
SMYS, further re-testing is allowed.
If one or both of the confirmatory tests fall below SMYS, the re-test program given in [7.9.5.8] shall apply.
7.9.5.7 If one or both of the confirmatory tests fail to meet SMYS, two re-tests taken from two additional
pipes within the same test unit shall be tested (a total of four tests). If all re-tests meet SMYS, the test unit
is acceptable. If any of the re-tests fall below SMYS, the test unit shall be rejected.
7.9.5.8 If a test unit has been rejected after re-testing, the manufacturer may conduct individual testing of
all the remaining pipes in the test unit. If the total rejection of all the pipes within one test unit exceeds 15%,
including the pipes failing the production and/or confirmatory tests, the test unit shall be rejected.
7.9.5.9 Retrospective documentation, see [7.9.5.2], shall meet the following requirements;
— More than 50 test units: The average yield strength shall be at least 2.0 standard deviations above SMYS.
— From 21 to 50 test units: The average yield strength shall be at least 2.1 standard deviations above
SMYS.
— From 10 to 20 test units: The average yield strength shall be at least 2.3 standard deviations above
SMYS.
— Less than 10 test units: supplementary requirement U is not applicable.
The statistical analysis shall be based on a group of test units that are all within the same MPQT essential
variables (e.g. different supply routes shall be analysed separately).
The statistical analysis shall take into account all test results from the test units proposed for supplementary
requirement U. This includes test results for pipes rejected from the test units. All test results shall be
considered as an individual data point (e.g. the results from a double re-test shall be considered as two
separate values).
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SECTION 8 CONSTRUCTION - COMPONENTS AND PIPELINE
ASSEMBLIES
8.1 General
8.1.1 Objective
8.1.1.1 This section specifies requirements to the construction of the components as defined in Table 8-1
and pipeline assemblies, see Table 6-1.
8.1.2 Application
8.1.2.1 This section is applicable to pressure containing components listed in Table 8-1 used in the
submarine pipeline system. Design of components shall be in accordance with [5.6].
Table 8-1 Manufacture and testing of pipeline components and pipeline assemblies
Requirements for
manufacture and testing
given in this section
Components
Bends
2)
Reference standards or recommended
practices and applicable class or
1)
designation
Pressure strength
test in accordance
with [8.7]
[8.2.3]
ISO 15590-1, PSL 2 for non-H2S and
PSL 2S for H2S service
Mill pressure
test of mother
6)
pipe .Hydrostatic
test of bend may be
specified
FAT /
8)
Qualification /Mill
10)
pressure test
Fittings
2), 3), 4)
[8.2.4]
ISO 15590-2, class C for non-sour and
class CS for sour service
Flanges
2), 4)
[8.2.5]
ISO 15590-3, designation (L) for nonsour and designation (LS) for sour
service, Norsok L-005
[8.2.6]
ISO 14723
[8.2.7]
ASME VIII Div.2/EN 13445/PD5500
5)
Qualification
[8.2.8]
ASME VIII Div.2/EN 13445/PD5500
5)
FAT
[8.2.9]
See Table 5-13
Valves
2), 4)
Mechanical connectors
CP Isolation joints
Anchor flanges
2), 4)
2), 4)
2), 4)
Buckle and fracture arrestors
4)
Pig traps
2), 4)
Repair clamps and repair
2), 4)
couplings
Pipeline assemblies
7)
8)
Qualification
7)
FAT in accordance
with ISO 14723
Clause 11
8)
7)
8)
Qualification
[8.2.10]
6)
Mill pressure test
[8.2.11]
ASME VIII Div.2/EN 13445/PD5500
[8.2.12]
DNVGL-RP-F113 Sec.8
5)
5)
7)
FAT
8)
Qualification
9)
[8.6]
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Notes
1)
The listed reference standards or recommended practices only cover C-Mn steels, for other materials reference is
given to this section. The listed standards or recommended practices shall be used within the applicability of the
standards or recommended practices.
2)
Supplementary requirements F, P, D or U are not applicable.
3)
Fittings include: Elbows, caps, tees, wyes, single or multiple extruded headers, reducers and transition sections.
4)
Where components are constructed from C-Mn or low alloy steel forgings, forgings complying with the requirements
in DNVGL-RP-0034 for steel forging class SFC 2 or SFC 3 may be considered as equivalent and therefore an
acceptable alternative to the corresponding requirements in this standard.
5)
Not covered by specific reference standards or recommended practices, however, these codes are listed as relevant
standards or recommended practices.
6)
See [7.5.1]
7)
Shall be pressure tested in accordance with applied design standard. This is often higher than the pressure test
requirement of this standard which is typically 15% above the design pressure. This implies that the pressure
testing has to be performed within the code breaks, i.e. typically before the transition piece and pup-pieces are
added.
8)
Shall be qualified or type approved. Recommended practice on qualification is given in DNVGL-RP-A203
9)
The benefit of detection leakage early is beneficial and the current industry practice of hydrostatic testing of pipeline
assemblies are reflected in Table 8-5.
10) Mill test may be performed of mother pipe to original size, prior to machining
8.1.2.2 Materials selection for components shall be in accordance with Sec.6.
8.1.3 Systematic review
8.1.3.1 The overall requirements to systematic review in Sec.2 will for this section apply for the component
manufacturers and imply:
— Review of this section and evaluate if the requirements in the purchase order and of this standard can be
met.
— Identify any possible threats, evaluate the possible consequences and define necessary remedial
measures.
8.2 Component requirements
8.2.1 General
8.2.1.1 References to requirements are listed in Table 8-1.
8.2.1.2 In paragraphs of subsection [8.2.2] to [8.2.6], ISO references are given between slashes, e.g.: /
Annex A/. The paragraph text shall be read as either additional or modified requirement to ISO 15590/ISO
14723.
8.2.2 Component specification
8.2.2.1 A component specification reflecting the results of the materials selection (see [6.2]), and referring
to this section of the offshore standard, shall be prepared by the purchaser. The specification shall state
any additional requirements to and/or deviations from this standard pertaining to materials, manufacture,
fabrication and testing of linepipe. For components covered by ISO 15590, see Table 8-1, the component
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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specification should preferably refer to the applicable ISO standard with necessary modifications in line with
this section.
8.2.3 Induction bends – additional and modified requirements to ISO
15590-1:2009
8.2.3.1 /Annex A/ The following additional requirements shall be stated in the MPS:
— the number and location of the pyrometers used (minimum two, located 120 to 180° apart) and the
allowable temperature difference between them
— the centring tolerances for the coil
— the number of water nozzles and flow rate.
8.2.3.2 /9.1/ The chemical composition of C-Mn steel mother pipe, including the backing steel of clad mother
pipe, shall be in agreement with the composition for the linepipe grades listed in Table 7-3, Table 7-4, Table
7-24 or Table 7-25. The maximum carbon equivalent (CE) of quenched and tempered or normalised CMn steel mother pipe (delivery condition N or Q, respectively) shall be according to Table 8-2. The carbon
equivalent (Pcm) of thermo-mechanical formed or rolled C-Mn steel mother pipe (delivery condition M) shall
be maximum 0.02 higher than as required in Table 7-4.
Guidance note:
Hot expanded mother pipe may experience dimensional instability after post bending heat treatment.
Bends may be made from spare sections of normal linepipe. It should be noted that linepipe, particularly pipe manufactured from
TMCP plate, may not have adequate hardenability to achieve the required mechanical properties after induction bending and
subsequent post bending heat treatment.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
Table 8-2 Carbon equivalent values for mother pipe
SMYS
CE
1)
, max.
245
0.36
290
0.38
320
0.40
360
0.43
390
0.43
415
0.44
450
0.45
485
0.46
555
0.47
Note
1)
8.2.3.3 /9.1/ The chemical composition of mother pipe for CRA materials shall meet the applicable
requirements for the relevant material type and grade given in Sec.7.
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8.2.3.4 /9.1/ Mother pipe shall be subjected to NDT as required for linepipe in Sec.7, except NDT of mother
pipe ends if the ends will be cut off during bend fabrication.
8.2.3.5 /9.1/ Induction bends shall not be produced from CRA lined steel pipe.
8.2.3.6 /9.1/ All mother pipes shall be mill pressure tested in accordance with [7.5], where [7.5.1.6] does
not apply.
8.2.3.7 (/9.2/ and /Table 1/) The following parameters shall be additional to or modification of the essential
variables given in /Table 1/:
— Heat of steel: This essential variable shall be replaced by: Change in ladle analysis for C-Mn steels outside
± 0.02% C, ± 0.03 CE and/or ± 0.02 in Pcm, or any change in nominal chemical composition for CRA's.
— Bending radius: Qualified MPS qualifies all larger radii, but not smaller.
— Any change in number and position of pyrometers used and in the allowable temperature difference
between the pyrometers.
— Any change in the stated tolerances for coil centring.
— Any change in the number and size of cooling nozzles and flow rate or water pressure.
8.2.3.8 /9.4/ Heat treatment equipment and procedures shall be in accordance with [8.4.5].
8.2.3.9 /10.4.4.2/ Hardness shall be measured in Hardness Vickers.
8.2.3.10 /Table 2/ and /10.4.3/ For bends from mother pipe with nominal wall thickness greater than 25
mm, additional CVN testing shall during MPQT be performed at mid thickness for CRA and 2 mm below inner
surface for C-Mn in the following locations:
—
—
—
—
transition zones base metal extrados start and stop
bend extrados base metal
bend intrados base metal
bend weld metal.
Acceptance criteria for mechanical testing shall meet the requirements given in applicable mother pipe
material specification.
8.2.3.11 /10.4.5/ Surface hardness testing using portable equipment shall be performed in accordance with
App.B.
8.2.3.12 /10.4.6/ For metallographic evaluation of CRA or clad induction bends, the acceptance criteria shall
be in accordance with in [7.3.4] and [7.3.5].
8.2.3.13 /10.5/ Additional NDT shall be performed in accordance with [D.8] as applicable.
Acceptance criteria for the additional testing shall be according to [D.8].
8.2.3.14 /10.6/ Ovality of cross-sections shall be kept within the specified tolerances. The bend radius shall
be as specified by the purchaser, and large enough (e.g. 5× outer diameter) to allow passage of inspection
vehicles when relevant.
Dimensional control shall include the following additional or modified tests and acceptance criteria:
—
—
—
—
—
ID at bend ends (always measure ID) shall be as specified for mother pipe body
out-of-roundness of bend ends shall be maximum 1.5% and maximum 3% for the body
the bend angle shall be within ±0.75°
weld seam location ± 15° from the neutral axis
end squareness shall be as specified for mother pipe end (only applicable for final dimension).
8.2.3.15 /10.7/ Gauging shall be performed as specified in the Component specification, see [6.3.3].
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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8.2.3.16 /12.0/ Marking requirements shall be specified to distinguish between bends manufactured and
tested to the requirements above and unmodified ISO 15590-1 bends.
8.2.4 Fittings - additional and modified requirements to ISO 15590-2
8.2.4.1 /1/ The following components shall be defined as fittings: Elbows, caps, tees, wyes, single or
multiple extruded headers, reducers and transition sections.
8.2.4.2 /6.2/ Tees and headers shall be of the integral (non-welded) reinforcement type. Outlets should
be extruded. Bars of barred tees and wyes shall not be welded directly to the high stress areas around the
extrusion neck. The bars transverse to the flow direction should be welded to a pup piece, and the bars
parallel to the flow direction should be welded to the transverse bars only. If this is impractical, alternative
designs shall be considered in order to avoid peak stresses at the bar ends.
8.2.4.3 /7/ The information required in [6.3.3.2] shall be provided.
8.2.4.4 /8/ The following additional information shall be provided:
The MPS should specify the following items, as applicable:
— For the starting material
— delivery condition
— chemical composition, and
— NDT procedures for examination of starting materials.
— For fitting manufacture
—
—
—
—
—
—
NDT procedures
hydrostatic test procedures
dimensional control procedures
coating and protection procedures
handling, loading and shipping procedures, and
at-site installation recommendations.
For one-off fittings designed and manufactured for a specific purpose, the following additional information
shall be provided:
— plan and process flow description/diagram
— order specific quality plan including supply of material and subcontracts, and
— manufacturing processes including process- and process control procedures.
8.2.4.5 /8.2/ Starting material shall be subject to 100% NDT at an appropriate stage of manufacture
according to:
—
—
—
—
—
—
C-Mn steel and duplex stainless steel pipe shall be tested as required in Sec.7 or [D.3.2].
[D.2.2], for RT of welds in starting materials other than pipe
[D.2.3] or [D.2.4] as applicable, for UT of welds in starting materials other than pipe
[D.4.2], for C-Mn steel forgings
[D.4.3], for duplex stainless steel forgings
[D.3.2], for UT of plate material
with acceptance criteria according to the corresponding requirements of App.D.
Subject to agreement, equivalent NDT standards with regard to method and acceptance criteria may be
applied.
8.2.4.6 /8.3.2/ Welding and repair welding shall be performed in accordance with qualified procedures
meeting the requirements in App.C.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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8.2.4.7 /8.3.3/ Heat treatment equipment and procedures shall be in accordance with [8.4.5].
8.2.4.8 /9.2/ Testing requirements shall be in accordance with [8.5.1].
8.2.4.9 /Table 2/ Inspection, testing and acceptance criteria shall be in accordance with class C with the
following additional and modified requirements:
— the level of hardeneability elements, e.g Ni, Cr, Mo, Cu, may be adjusted based on a hardeneability
assessment, providing requirements in [8.3.2.5] to carbon equivalent is maintained
— the chemical composition of duplex stainless steel materials shall be according to [8.3.3]
— mechanical and hardness testing of weld seams shall be performed in accordance with App.B and
acceptance criteria shall be in accordance with [8.5.2] and [8.5.3] as applicable
— surface hardness testing of fittings of class CS shall be performed with acceptance criteria according to
Table 6-1
— metallographic examination for welds and body of duplex stainless steel fittings shall be performed in
accordance with App.B and with acceptance criteria according to [8.5.3]
— HIC testing shall be performed on fittings in class CS manufactured from rolled material as required in
Table 8-4
— 25Cr duplex stainless steel fittings shall be corrosion tested as required in Table 8-4, and
— NDT of fitting bodies shall be performed according to [8.2.5.12].
8.2.4.10 /Table 3/ The extent of testing and examination shall comprise the following additional
requirements:
— the test unit definition shall be amended to: Fitting or test piece of the same designation, starting material
wall thickness, heat, manufacturing procedure specification and heat treatment batch
— surface hardness tests shall be performed on two fittings per test unit
— metallography of duplex stainless steel fittings with the largest thickness exceeding 25 mm shall be
performed as one per test unit
— HIC testing shall be performed for qualification of the MPS for fittings in class CS manufactured from
rolled material, and
— 25Cr duplex stainless steel fittings shall be corrosion tested for qualification of the MPS, in accordance
with Table 8-4.
8.2.4.11 /Table 2/ and /9.5/ NDT of each completed fitting shall be performed in accordance with the /Table
2/, class C with the following additional requirements:
— the body of fittings manufactured from plates and pipes shall be subject to 100% magnetic particle testing
for C-Mn steels and 100% dye penetrant/eddy current testing for duplex stainless steel
— the extrusion area for tees and headers with adjoining pipe wall thickness ≥ 12 mm shall be subject to
100% volumetric ultrasonic and 100% magnetic particle testing for C-Mn steels and 100% volumetric
ultrasonic and 100% dye penetrant/eddy current testing for duplex stainless steel
— the extrusion area for tees and headers with adjoining pipe wall thickness < 12 mm shall be subject to
100% magnetic particle testing for C-Mn steels and 100% dye penetrant/eddy current testing for duplex
stainless steel
— overlay welds shall be tested 100%.
8.2.4.12 NDT shall be performed in accordance with App.D (as applicable):
—
—
—
—
—
—
[D.3.4], for visual inspection
[D.4.2], for UT and MT of C-Mn/low alloy steel forgings
[D.4.3], for UT and PT of duplex stainless steel forgings
[D.3.2.6] through [D.3.2.13], for UT of a 50 mm wide band inside ends/bevels
[D.3.2.21], for MT of ends/bevels
[D.3.2.22], for PT of ends/bevels
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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—
—
—
—
—
—
—
—
—
[D.2.2],
[D.2.3],
[D.2.4],
[D.2.5],
[D.2.6],
[D.3.3],
[D.4.4],
[D.2.8],
[D.3.5],
for
for
for
for
for
for
for
for
for
RT of welds
UT of welds in C-Mn/low alloy steel
UT of welds in duplex stainless steel
MT of welds in C-Mn/low alloy steel
DP of welds in duplex stainless steel
NDT of overlay welds
visual inspection of forgings
visual inspection of welds, and
residual magnetism.
Acceptance criteria shall be according to the corresponding requirements of App.D.
8.2.4.13 /11/ Marking requirements shall be specified to distinguish between fittings manufactured and
tested to the requirements above and unmodified ISO 15590-2 fittings.
8.2.5 Flanges and flanged connections - additional requirements to ISO
15590-3
8.2.5.1 /7/ The following additional information shall be provided:
— required design life
— nominal diameters, D or ID, out of roundness and wall thickness for adjoining pipes including required
tolerances
— dimensional requirements and tolerance if different from ISO 7005-1
— minimum design temperature (local)
— maximum design temperature (local)
— external loads and moments that will be transferred to the component from the connecting pipeline under
installation and operation and any environmental loads (e.g. nominal longitudinal strain)
— material type and grade, delivery condition, chemical composition and mechanical properties at design
temperature
— required testing
— corrosion resistant weld overlay.
8.2.5.2 /8/ Overlay welding shall be performed according to qualified welding procedures meeting the
requirements of App.C.
8.2.5.3 /8.1/ The MPS shall be in accordance with [8.4.1].
8.2.5.4 /8.2/ and /Table 4/
— the level of hardeneability elements, e.g Ni, Cr, Mo, Cu, may be adjusted based on a hardeneability
assessment, providing requirements in [8.3.2.5] to Carbon Equivalent is maintained
— The chemical composition of duplex stainless steel materials shall be according to [8.3.3].
8.2.5.5 /8.4/ Heat treatment equipment and procedures shall be in accordance with [8.4.5].
8.2.5.6 /Table 3/ Mechanical testing shall be performed with the following additional requirements:
— Tensile, impact and through thickness hardness shall be performed once per test unit with the test unit
defined as; Flanges of the same size, heat, manufacturing procedure specification and heat treatment
batch.
— Surface hardness testing shall be performed once per test unit for flanges in class LS.
— Mechanical, hardness and corrosion testing of flanges shall be performed as required by [8.5.1],
acceptance criteria to [8.5.2] or [8.5.3] as applicable.
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— Metallographic examination for duplex stainless steel flanges shall be performed according to [8.5.1], with
acceptance criteria according to [8.5.3].
8.2.5.7 /Table 5/ The impact test temperature for C-Mn steel and low alloy flanges shall be 10°C below the
minimum design temperature for all thicknesses and categories.
8.2.5.8 /9.4.4/ Hardness indentation locations shall be according to Table 8-4.
8.2.5.9 /9.4.5/ Metallographic examination of duplex stainless steel shall be performed in accordance with
App.B, with acceptance criteria according to [7.3.4].
8.2.5.10 /9.4.6/ and /9.4.7/ Corrosion testing of duplex stainless steel shall be according to Table 8-4.
8.2.5.11 /9.5.4/ The extent of NDT shall be 100% magnetic particle testing of ferromagnetic materials and
100% liquid penetrant testing of non magnetic materials. A percentage test is not permitted.
8.2.5.12 /9.5.5/ 100% ultrasonic testing of the final 50 mm of each end of the flange shall be performed.
100% ultrasonic testing of the first 10 flanges of each type and size ordered. If no defects are found during
the testing of the first 10 flanges of each type and size ordered the extent of testing may be reduced to
10% of each size and type. If defects are found in any tested flange, all flanges of the same size, heat,
manufacturing procedure specification and heat treatment batch shall be 100% tested.
All flanges shall be subject to 100% visual inspection.
8.2.5.13 NDT shall be performed in accordance with App.D or ISO (as applicable):
—
—
—
—
—
—
Magnetic particle testing shall be performed in accordance with [D.4.2] or ISO 13664
Liquid penetrant testing shall be performed in accordance with [D.4.3] or ISO 12095
Ultrasonic testing of C-Mn/low alloy steel forgings shall be performed in accordance with [D.4.2]
Ultrasonic testing of duplex stainless steel forgings shall be performed in accordance with [D.4.3]
Testing of overlay welds shall be performed in accordance with [D.3.3]
Visual examination shall be in accordance with [D.4.4]
Acceptance criteria for forgings shall be in accordance with the corresponding requirements of [D.4.5] and for
overlay welds only, in accordance with [D.3.6].
Subject to agreement, equivalent NDT standards with regard to method and acceptance criteria may be
applied.
8.2.5.14 /9.6/ For flanges with specified dimensions and tolerances different from ISO 7005-1, these
specified requirements shall be met.
8.2.5.15 /9.9/ Repair welding of flange bodies is not permitted.
8.2.5.16 /11/ Marking requirements shall be specified to distinguish between flanges manufactured and
tested to the requirements above and unmodified ISO 15590-3 flanges.
8.2.5.17 Sealing rings shall be compatible with the finish and surface roughness of the flange contact faces.
8.2.5.18 Sealing rings shall be capable of withstanding the maximum pressure to which they could be
subjected, as well as installation forces if flanges are laid in-line with the pipeline. Sealing rings for flanges
shall be made from metallic materials that are resistant to the fluid to be transported in the pipeline system.
Mechanical properties shall be maintained at the anticipated in service pressures and temperatures.
8.2.5.19 Bolts shall meet the requirements given in [8.3.5].
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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8.2.5.20 For the use of ANSI, RTJ and orifice flanges it shall be ensured that the flanges are suitable for
subsea use, e.g. by means of materials compatibility and use of vent holes to avoid water trapping and
pressure build up in the groove area for gaskets.
8.2.6 Valves – additional requirements to ISO 14723
8.2.6.1 /Annex B/ The following additional information shall be provided:
—
—
—
—
—
—
—
design standard
required design life
minimum design temperature (local)
maximum design temperature (local)
design pressure (local)
water depth, and
weld overlay, corrosion resistant and/or wear resistant.
8.2.6.2 /8.1/ A manufacturing procedure specification in accordance with [8.4.1] shall be documented.
8.2.6.3 /8.1/, /8.4/ and /8.7/ Materials shall be specified to meet the requirements given in [8.3].
8.2.6.4 /8.5/ The impact test temperature shall be 10°C below the minimum design temperature
8.2.6.5 /8.6/ Bolting shall meet the requirements of [8.3.5].
8.2.6.6 /8/ Welding shall be performed according to qualified welding procedures meeting the requirements
of App.C.
8.2.6.7 /9.4/ The extent, method and type of NDT of C-Mn/low alloy steels shall be in accordance with ISO
14723, Annex A, QL 2 requirements.
The extent and type of NDT of duplex stainless steels shall be in accordance with ISO 14723, Annex A, QL 2
requirements. Methods shall be according to App.D of this standard.
The extent and type of NDT of weld overlay shall be in accordance with ISO 14723, Annex A, QL 2
requirements. the method shall be according to App.D.
Acceptance criteria for NDT shall be in accordance with ISO 14723, Annex A with the following amendments:
For UT 2, VT 2 and VT 3 the acceptance criteria shall be in accordance with App.D of this standard.
8.2.6.8 /9.5/ Repair welding of forgings is not permitted.
8.2.6.9 /10.2/ Hydrostatic shell tests shall be performed in accordance with ISO 14723, Clause 11, or
according to specified requirements in compliance with [5.2.2.1] as outlined in [8.7].
8.2.6.10 /11/ Marking requirements shall be specified to distinguish between valves manufactured and
tested to the requirements above and unmodified ISO 14723 valves.
8.2.6.11 Valves with requirements for fire durability shall be qualified by applicable fire tests. Refer to API
6FA and BS 6755 Part 2 for test procedures.
8.2.7 Mechanical connectors
8.2.7.1 This section applies to end connections, such as hub and clamp connections connecting a pipeline to
other installations.
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Requirements to material, manufacture and mechanical testing of pressure containing parts shall be in
accordance with [8.3], [8.4] and [8.5].
8.2.7.2 Bolting shall meet the requirements of [8.3.5].
8.2.7.3 End connections shall be forged.
8.2.7.4 The extent of NDT shall be:
— 100% magnetic particle testing of ferromagnetic materials and 100% liquid penetrant testing of non
magnetic materials
— 100% ultrasonic testing of forgings and castings
— 100% RT of critical areas of castings
— 100% ultrasonic or radiographic testing of welds
— 100% magnetic particle testing/liquid penetrant testing of welds
— 100% visual inspection.
NDT shall be performed in accordance with App.D (as applicable):
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
[D.3.4], for visual inspection
[D.4.2], for UT and MT of C-Mn/low alloy steel forgings
[D.4.3], for UT and PT of duplex stainless steel forgings
[D.5.2], for UT and MT of C-Mn/low alloy steel castings
[D.5.3], for UT and PT of duplex stainless steel castings
[D.5.4], for RT of castings
[D.3.2.21], for MT of ends/bevels
[D.3.2.22], for DP of ends/bevels
[D.2.2], for RT of welds
[D.2.3], for UT of welds in C-Mn/low alloy steel
[D.2.4], for UT of welds in duplex stainless steel
[D.2.5], for MT of welds in C-Mn/low alloy steel
[D.2.6], for DP of welds in duplex stainless steel
[D.3.3], for overlay welds
[D.4.4], for visual inspection of forgings
[D.5.5], for visual examination of castings
[D.2.8], for visual inspection of welds
[D.3.5], for residual magnetism.
Acceptance criteria shall be according to the corresponding requirements of App.D.
8.2.8 CP Isolation joints
8.2.8.1 These requirements apply to manufacture and testing of boltless, monolithic coupling type of
isolation joints for onshore applications.
8.2.8.2 CP isolation joints shall be manufactured from forgings. Requirements to material, manufacture and
mechanical testing shall be in accordance with [8.3], [8.4] and [8.5].
8.2.8.3 Isolation joints shall be protected from electrical high current high voltage from welding and
lightening etc. in the construction period. If high voltage surge protection is not provided in the construction
period isolation joints shall be fitted with a temporary short-circuit cable clearly tagged with the instruction
not to be removed until installation of permanent high voltage surge protection.
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8.2.8.4 For manufacturers without previous experience in the design, manufacture and testing of isolation
joints, one joint should be manufactured and destructively tested for the purpose of qualifying the design and
materials of the joint.
The qualification programme should as a minimum contain the following elements:
—
—
—
—
bending to maximum design bending moment
tension to maximum design tension
pressure testing to 1.5 times the design pressure
pressure cycling from minimum to maximum design pressure 10 times at both minimum and maximum
design temperature.
Before and after testing the resistance and electrical leakage tests should show the same and stable values.
In addition, after full tests the joint should be cut longitudinally into sections to confirm the integrity of the
insulation and fill materials and the condition of the O-ring seals.
8.2.8.5 Isolation joint shall be forged close to the final shape (if applicable). Machining of up to 10% of the
local wall thickness at the outside of the component is allowed.
8.2.8.6 The extent of NDT shall be:
— 100% magnetic particle testing of ferromagnetic materials and 100% liquid penetrant testing of non
magnetic materials
— 100% ultrasonic testing of forgings
— 100% ultrasonic or radiographic testing of welds
— 100% magnetic particle testing/liquid penetrant testing of welds
— 100% visual inspection.
NDT shall be performed in accordance with App.D (as applicable):
—
—
—
—
—
—
—
—
—
—
—
—
—
—
[D.3.4], for visual inspection
[D.4.2], for C-Mn/low alloy steel forgings
[D.4.3], for duplex stainless steel forgings
[D.3.2.21], for MT of ends/bevels
[D.3.2.22], for DP of ends/bevels
[D.2.2], for RT of welds
[D.2.3], for UT of welds in C-Mn/low alloy steel
[D.2.4], for UT of welds in duplex stainless steel
[D.2.5], for MT of welds in C-Mn/low alloy steel
[D.2.6], for DP of welds in duplex stainless steel
[D.3.3], for overlay welds
[D.4.4], for visual inspection of forgings
[D.2.8], for visual inspection of welds, and
[D.3.5], for residual magnetism.
Acceptance criteria shall be according to the corresponding requirements of App.D.
8.2.8.7 Prior to hydrostatic testing, hydraulic fatigue test and the combined pressure-bending test/electrical
leakage tests shall be performed and the results recorded.
8.2.8.8 Hydraulic fatigue testing of each isolation joint shall be performed. The test shall consist of 40
consecutive cycles with the pressure changed from 10 barg to 85 percent of the hydrostatic test pressure.
At the completion of the test cycles the pressure shall be increased to the hydrostatic test pressure and
maintained for 30 minutes. For acceptance criterion, see [E.4.5.6].
8.2.8.9 One isolation joint per size/design pressure shall also be tested to meet the specified bending
moment requirements. The joint shall be pressurised to the specified hydrostatic test pressure and
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simultaneously be subjected to an external 4 point bending load sufficient to induce a total (bending plus
axial pressure effect) longitudinal stress of 90% of SMYS in the adjoining pup pieces. The test duration shall
be 2 hours. The acceptance criteria are no water leakage or permanent distortion.
8.2.8.10 After hydrostatic testing, all isolation joints shall be leak tested with air or nitrogen. The joints shall
be leak tested at 10 barg for 10 minutes. The tightness shall be checked by immersion or with a frothing
agent. The acceptance criterion is: no leakage.
8.2.8.11 The FAT shall be performed according to the accepted FAT programme. The FAT shall consist of:
— dielectric testing
— electrical resistance testing
— electrical leakage tests.
8.2.8.12 Prior to FAT isolation joints shall be stored for 48 hours at an ambient temperature between 20 and
25°C and a relative humidity of max. 93%.
8.2.8.13 Dielectric testing shall be performed by applying an AC sinusoidal current with a frequency of
50 - 60 Hz to the joint. The current shall be applied gradually, starting from an initial value not exceeding
1.2kV increasing to 5.0kV in a time not longer than 10 seconds and shall be maintained at peak value for 60
seconds. The test is acceptable if no breakdown of the isolation or surface arcing occurs during the test.
8.2.8.14 Electrical resistance testing shall be carried out at 1000 V DC. The test is acceptable if the electrical
resistance is minimum 25 MOhm.
8.2.8.15 Electrical leakage tests shall be performed to assess any changes which may take place within a
joint after hydrostatic testing, hydraulic fatigue test and the combined pressure-bending test. No significant
changes in electrical leakage shall be accepted.
8.2.9 Anchor flanges
8.2.9.1 Anchor flanges shall be forged. Requirements to material, manufacture and mechanical testing shall
be in accordance with [8.3], [8.4] and [8.5].
8.2.9.2 The extent of NDT shall be:
— 100% magnetic particle testing of ferromagnetic materials and 100% liquid penetrant testing of non
magnetic materials
— 100% ultrasonic testing of forgings
— 100% ultrasonic or radiographic testing of welds
— 100% magnetic particle testing/liquid penetrant testing of welds
— 100% visual inspection.
NDT shall be performed in accordance with App.D (as applicable):
—
—
—
—
—
—
—
—
—
—
[D.3.4], for visual inspection
[D.2.2], for C-Mn/low alloy steel forgings
[D.2.3], for duplex stainless steel forgings
[D.3.2.21], for MT of ends/bevels
[D.3.2.22], for DP of ends/bevels
[D.2.2], for RT of welds
[D.2.3], for UT of welds in C-Mn/low alloy steel
[D.2.4], for UT of welds in duplex stainless steel
[D.2.5], for MT of welds in C-Mn/low alloy steel
[D.2.6], for DP of welds in duplex stainless steel
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— [D.4.4], for visual inspection of forgings
— [D.2.8], for visual inspection of welds, and
— [D.3.5], for residual magnetism.
Acceptance criteria shall be according to the corresponding requirements of App.D.
8.2.10 Buckle- and fracture arrestors
8.2.10.1 The material for buckle and fracture arrestors and manufacture, inspection and testing shall be in
accordance with [8.3], [8.4] and [8.5] (if forged/cast), or Sec.7 (if linepipe).
8.2.11 Pig traps
8.2.11.1 Materials shall comply with the requirements of the design standard or recommended practice or
with the requirements of this section, including [8.3], [8.4] and [8.5], if more stringent.
8.2.11.2 Testing and acceptance criteria for qualification of welding procedures shall comply with the
requirements of the design standard or recommended practice or with the requirements of App.C, if more
stringent.
Essential variables for welding procedures and production welding shall comply with the requirements of
App.C.
8.2.11.3 The extent, methods and acceptance criteria for NDT shall comply with the requirements of the
design standard or recommended practice. In addition the requirements of [D.1] and [D.2.1] shall apply.
8.2.12 Repair clamps and repair couplings
8.2.12.1 Repair clamps and repair couplings to be installed according to DNVGL-RP-F113 shall be
manufactured and tested in accordance with this section, including [8.3], [8.4] and [8.5].
8.3 Materials
8.3.1 General
8.3.1.1 The materials used shall comply with internationally recognised standards, provided that such
standards have acceptable equivalence to the requirements given in Sec.7 and this section. Modification of
the chemical composition given in such standards may be necessary to obtain a sufficient combination of
weldability, hardenability, strength, ductility, toughness, and corrosion resistance.
8.3.1.2 Sampling for mechanical and corrosion testing shall be performed after final heat treatment, i.e. in
the final condition. The testing shall be performed in accordance with App.B and [8.5.1].
8.3.2 C-Mn and low alloy steel forgings and castings
8.3.2.1 These requirements are applicable to C-Mn and low alloy steel forgings and castings with SMYS ≤
555 MPa. Use of higher strength materials shall be subject to agreement.
8.3.2.2 All steels shall be made by an electric or one of the basic oxygen processes. C-Mn steel shall be fully
killed and made to a fine grain practice.
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8.3.2.3 The chemical composition for hot-formed, cast and forged components shall be in accordance with
recognised international standards. The chemical composition shall be selected to ensure an acceptable
balance between sufficient hardenability and weldability.
8.3.2.4 For materials to be quenched and tempered, a hardenability assessment shall be performed to
ensure that the required mechanical properties can be met.
8.3.2.5 For C-Mn steels the maximum carbon equivalent (CE) shall not exceed 0.50, when calculated in
accordance with:
(8.1)
8.3.2.6 Acceptance criteria for tensile, hardness and Charpy V-notch impact properties are given in [8.5.2].
8.3.2.7 Forgings shall be delivered in normalised or quenched and tempered condition.
8.3.2.8 Castings shall be delivered in homogenised, normalised and stress relieved or homogenised,
quenched and tempered condition.
8.3.2.9 For C-Mn and low alloy materials delivered in the quenched and tempered condition, the minimum
tempering temperature shall be 610°C when PWHT will be applied, unless otherwise specified.
8.3.3 Duplex stainless steel, forgings and castings
8.3.3.1 All requirements with regard to chemical composition for 22Cr and 25Cr duplex stainless steel shall
be in accordance with [7.3.4].
8.3.3.2 Acceptance criteria for tensile, hardness, Charpy V-notch impact properties and corrosion tests are
given in [8.5.3].
8.3.3.3 Duplex stainless steel castings and forgings shall be delivered in the solution annealed and water
quenched condition.
8.3.4 Pipe and plate material
8.3.4.1 Pipe and plate material shall meet the requirements in Sec.7.
8.3.4.2 For welded pipe it shall be assured that the mechanical properties of the material and longitudinal
welds will not be affected by any heat treatment performed during manufacture of components.
8.3.4.3 In case PWHT is required, the mechanical testing should be conducted after simulated heat
treatment.
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8.3.5 Bolting materials
8.3.5.1 In general, bolting material selection shall be in line with the applicable design standards or
recommended practices supplemented with [6.2.6] and [6.3.4], with limitations and additional requirements
as given in [8.3.5.2] to [8.3.5.10].
8.3.5.2 For components based on ASME design codes, carbon and low alloy steel bolts and nuts for pressure
containing and main structural applications shall be selected in accordance with Table 8-3.
For components based on other design standards or recommended practices, equivalent carbon and low alloy
steel bolts in line with the design standards or recommended practices shall be selected.
The bolting materials listed in Table 8-3 may be used in combination with other design standards or
recommended practices than ASME if properly considered by the designer. This shall include assessment of
allowable utilisation and derating for elevated temperature applications, if relevant. Applicable ASME design
codes list pre-defined allowable stresses, which are not necessarily based on SMYS and SMTS, while other
design standards or recommended practices define utilisation based on safety factors on SMYS and SMTS.
This shall be considered when mixing ASTM bolting materials with other standards or recommended practices
than ASTM.
Table 8-3 Carbon and low alloy steel bolts and nuts for ASME design code applications
Temperature range (
o
C)
Bolt
Nut
Size range
-100 to + 400
ASTM A320, Grade L7
ASTM A194, Grade
4/S3/S4/S5 or
Grade 7/S3/S4/S5
< 65 mm
-100 to + 400
ASTM A320,
Grade L7M
ASTM A194, Grade
7M/S3/S4/S5
< 65 mm
-100 to + 400
ASTM A320,
Grade L43
ASTM A194,
Grade 7/S3/S4/S5
< 100 mm
8.3.5.3 Carbon and low alloy steel bolting materials shall be Charpy-V impact tested. The bolting materials
shall meet the requirements for the bolted connection, i.e. the materials to be bolted. See [8.5.1.5] and
[8.5.2.1] for test temperature and acceptance criteria.
8.3.5.4 Stainless steel bolts according to ASTM A193/A320 grade B8M (type AISI 316) are applicable but
require efficient cathodic protection for subsea use.
8.3.5.5 Ni-based bolts according to ASTM B446 type UNS N06625 or other Ni-based solution hardening
alloys with equivalent or higher PRE are acceptable. However, these bolting materials shall only be used in
the solution annealed condition, or cold worked to SMYS 720 MPa maximum.
8.3.5.6 Maximum hardness shall not exceed 35 HRC for carbon and low alloy steels, in addition to solution
annealed or cold-worked type AISI 316 or any other cold-worked austenitic stainless steel (only applicable if
the bolts will be exposed to cathodic protection).
8.3.5.7 Restrictions for H2S service (also referred to as sour service) according to ISO 15156 shall apply
when applicable.
8.3.5.8 The hardness of bolts and nuts shall be verified for each lot (i.e. bolts of the same size and material,
from each heat of steel and heat treatment batch) and be traceable back to heat number.
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Guidance note:
In order to ensure acceptable traceability, several Companies require higher frequency for hardness testing than one per lot for
verification of subsea fasteners. The party installing the bolts should also consider to perform random testing of bolt properties.
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8.3.5.9 For acid cleaned and/or electrolytically plated bolts and nuts, baking at 200°C for a minimum of 2
hours is required in order to prevent hydrogen embrittlement.
8.3.5.10 Only unused bolting materials shall be applied.
8.3.6 H2S service
8.3.6.1 For components in pipeline systems to be used for fluids containing hydrogen sulphide and defined
as H2S service according to ISO 15156, all requirements to chemical composition, maximum hardness, and
manufacturing and fabrication procedures given in the above standard shall apply.
8.3.6.2 The sulphur content of C-Mn and low alloy steel forgings and castings shall not exceed 0.010%.
8.3.6.3 Pipe and plate material used for fabrication of components shall meet the requirements given in
[7.9.1].
8.4 Manufacture
8.4.1 Manufacturing procedure specification
8.4.1.1 The requirements of this subsection are not applicable to induction bends and fittings that shall be
manufactured in accordance with [8.2.3] and [8.2.4]
8.4.1.2 Components shall be manufactured in accordance with a documented and approved manufacturing
procedure specification (MPS).
8.4.1.3 The manufacturing procedure specification (MPS) shall demonstrate how the fabrication will be
performed and verified through the proposed fabrication steps. The MPS shall address all factors which
influence the quality and reliability of production. All main fabrication steps from control of received material
to shipment of the finished product(s), including all examination and check points, shall be covered in detail.
References to the procedures and acceptance criteria established for the execution of all steps shall be
included.
8.4.1.4 The MPS should be project specific and specify the following items as applicable:
— Starting materials
—
—
—
—
—
—
—
manufacturer
steel making process
steel grade
product form, delivery condition
chemical composition
welding procedure specification (WPS)
NDT procedures.
— Manufacturing
— supply of material and subcontracts
— manufacturing processes including process- and process control procedures
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—
—
—
—
—
—
—
—
—
—
—
welding procedures
heat treatment procedures
NDT procedures
list of specified mechanical and corrosion testing
hydrostatic test procedures
functional test procedures
dimensional control procedures
FAT procedures
marking, coating and protection procedures
handling, loading and shipping procedures
at-site installation recommendations.
For one-off components and other components designed and manufactured for a specific purpose, the
following additional information shall be provided:
— plan and process flow description/diagram
— order specific quality plan including supply of material and subcontracts
— manufacturing processes including process- and process control procedures.
8.4.2 Forging
8.4.2.1 Forging shall be performed in compliance with the accepted MPS. Each forged product shall be hot
worked as far as practicable, to the final size with a minimum reduction ratio of 4:1.
8.4.2.2 The work piece shall be heated in a furnace to the required working temperature.
8.4.2.3 The working temperature shall be monitored during the forging process.
8.4.2.4 If the temperature falls below the working temperature the work piece shall be returned to the
furnace and re-heated before resuming forging.
8.4.2.5 The identity and traceability of each work piece shall be maintained during the forging process.
8.4.2.6 Weld repair of forgings is not permitted.
8.4.3 Casting
8.4.3.1 Casting shall be performed in general compliance with ASTM A352.
8.4.3.2 A casting shall be made from a single heat and as a single unit.
8.4.3.3 Castings may be repaired by grinding to a depth of maximum 10% of the actual wall thickness,
provided that the wall thickness in no place is below the minimum designed wall thickness. The ground areas
shall merge smoothly with the surrounding material.
8.4.3.4 Defects deeper than those allowed by [8.4.3.3] may be repaired by welding. The maximum extent
of repair welding should not exceed 20% of the total surface area. Excavations for welding shall be ground
smooth and uniform and shall be suitably shaped to allow good access for welding.
8.4.3.5 All repair welding shall be performed by qualified welders and according to qualified welding
procedures.
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8.4.4 Hot forming
8.4.4.1 Hot forming shall be performed according to an agreed procedure containing:
—
—
—
—
—
—
—
—
—
—
—
—
—
—
sequence of operations
heating equipment
material designation
pipe diameter, wall thickness and bend radius
heating/cooling rates
maximum and minimum temperature during forming operation
temperature maintenance/control
recording equipment
position of the longitudinal seam
methods for avoiding local thinning
post bending heat treatment (duplex stainless steel: full solution annealing and water quenching)
hydrostatic testing procedure
NDT procedures
dimensional control procedures.
8.4.4.2 Hot forming of C-Mn and low alloy steel, including extrusion of branches, shall be performed below
1100°C. If microalloying elements have been added to prevent grain growth (e.g. Ti), the hot forming
temperature may be increased to 1150°C. The temperature shall be monitored. The component shall be
allowed to cool in still air.
8.4.4.3 For duplex stainless steel material, the hot forming shall be conducted between 1000 and 1150°C.
8.4.5 Heat treatment
8.4.5.1 Heat treatment procedures for furnace heat treatment shall as a minimum contain the following
information:
—
—
—
—
—
—
—
—
—
—
—
—
—
heating facilities
furnace
insulation (if applicable)
measuring and recording equipment, both for furnace control and recording of component temperature
calibration intervals for furnace temperature stability and uniformity and all thermocouples
fixtures and loading conditions
heating and cooling rates
temperature gradients
soaking temperature range and time
maximum time required for moving the component from the furnace to the quench tank (if applicable)
cooling rates (conditions)
type of quenchant (if applicable)
start and end maximum temperature of the quenchant (if applicable).
8.4.5.2 If PWHT in an enclosed furnace is not practical, local PWHT shall be performed according to [C.7.4].
8.4.5.3 The heat treatment equipment shall be calibrated at least once a year in order to ensure acceptable
temperature stability and uniformity. The uniformity test shall be conducted in accordance with a recognised
standard (e.g. ASTM A991). The temperature stability and uniformity throughout the furnace volume shall be
within ± 10°C.
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8.4.5.4 Whenever practical, thermocouple(s) should be attached to one of the components during the heat
treatment cycle.
8.4.5.5 Components should be rough machined to near final dimensions prior to heat treatment. This is
particularly important for large thickness components.
Guidance note:
The extent and amount of machining of forgings and castings prior to heat treatment should take into account the requirements for
machining to flat or cylindrical shapes for ultrasonic examination. See also App.D.
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8.4.5.6 For components that shall be water quenched, the time from the components leave the furnace until
being immersed in the quenchant shall not exceed 90 seconds for low alloy steel, and 60 seconds for duplex
stainless steels.
8.4.5.7 The volume of quenchant shall be sufficient and shall be heavily agitated, preferably by cross flow
to ensure adequate cooling rate. The maximum temperature of the quenchant shall never exceed 40°C.
Temperature measurements of the quenchant shall be performed.
8.4.5.8 The hardness of the accessible surfaces of the component shall be tested. The hardness for C-Mn or
low alloy steels and duplex stainless steels shall be in accordance with [8.5.2] and [8.5.3], respectively.
8.4.6 Welding
8.4.6.1 Welding and repair welding shall be performed in accordance with qualified procedures meeting the
requirements of App.C.
8.4.7 NDT
8.4.7.1 NDT shall be performed in accordance with App.D.
8.5 Mechanical and corrosion testing
8.5.1 General testing requirements
8.5.1.1 Mechanical testing after hot forming, casting or forging shall be performed on material taken from
a prolongation or sacrificial component from each test unit, i.e. components of the same size and material,
from each heat and heat treatment batch. Number, orientation and location of test specimens shall be as
given in Table 8-4, as far as geometry permits.
8.5.1.2 Sampling for mechanical and corrosion testing shall be conducted after final heat treatment. Testing
shall be performed in accordance with App.B.
8.5.1.3 If agreed, separate test coupons may be allowed providing they are heat treated together with the
material they represent, and the material thickness, forging reduction, and mass are representative of the
actual component.
8.5.1.4 A simulated heat treatment of the test piece shall be performed if welds between the component and
other items such as linepipe are to be PWHT at a later stage or if any other heat treatment is intended.
8.5.1.5 The CVN test temperature shall be 10°C below the minimum design temperature.
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8.5.1.6 A sketch indicating the final shape of the component and the orientation and location of all
specimens for mechanical testing shall be issued for review and acceptance prior to start of production.
8.5.1.7 For 25Cr duplex stainless steels corrosion testing according to ASTM G48 shall be performed in order
to confirm that the applied manufacturing procedure ensures acceptable microstructure. Testing shall be
performed in accordance with App.B at 50°C. The test period shall be 24 hours.
8.5.2 Acceptance criteria for C-Mn and low alloy steels
8.5.2.1 Tensile, hardness and Charpy V-notch impact properties shall meet the requirements for linepipe
with equal SMYS as given in [7.2.4].
8.5.2.2 The hardness for components intended for non- H2S service shall not exceed 300 HV10. For
components intended for H2S service the hardness shall be according to [7.9.1].
Table 8-4 Number, orientation, and location of test specimens per tested component
Type of test
No. of tests
Test location, e.g. as shown in Figure 8-1
1, 2)
One specimen in tangential direction from the thickest
section 1/2T below the internal surface.
Tensile test for components having
maximum section thickness T ≤ 50
mm
3
One specimen in both tangential and axial direction from the
area with highest utilisation at 1/2T (after final machining),
3)
e.g. the weld neck area.
Test specimens shall have the mid-length at least T or 100
mm, whichever is less from any second surface.
One specimen in tangential direction from the thickest
section 1/4T below the internal surface.
Tensile test for components having
maximum section thickness T > 50
mm
3
One specimen in both tangential and axial direction from the
area with highest utilisation at 1/2T (after final machining),
3
e.g. the weld neck area.
Test specimens shall have the mid-length at least T or 100
mm, whichever is less from any second surface.
One set in tangential direction from the thickest section at
1/2T.
CVN impact testing for components
having maximum section thickness T
4, 5)
≤ 50 mm
3 sets
One specimen in both tangential and axial direction from the
area with highest utilisation at 1/2T (after final machining),
3
e.g. the weld neck area.
Test specimens shall have the mid-length at least 50 mm
from any second surface.
One specimen in tangential direction from the thickest
section 1/4T below the internal surface.
CVN impact testing for components
having maximum section thickness T
4, 5)
> 50 mm
3 sets
One specimen in both tangential and axial direction from the
area with highest utilisation at 1/2T (after final machining),
3
e.g. the weld neck area.
Test specimens shall have the mid-length at least T or 100
mm, whichever is less from any second surface.
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Type of test
No. of tests
CVN impact testing for components
³
having maximum section thickness 30
4, 5, 6)
mm 4, 5, ,6)
Metallographic sample
Hardness testing
HIC and SSC test
ASTM G48
7)
8)
9)
10)
Test location, e.g. as shown in Figure 8-1
1, 2)
1 set
One set in the tangential direction 2 mm below the internal
surface at the thickest section for hollow forgings. For solid
forgings, one set in the tangential direction 2 mm below the
surface at the thickest section.
2 or 3
As for the CVN impact testing sets
3
As for the CVN impact testing sets
1
In accordance with ISO 15156
1
See [8.5.1.7]
Notes
1)
For welded components, the testing shall also include testing of the welds in accordance with App.C.
2)
Internal and external surface refers to the surfaces of the finished component.
3)
For Tees and Wyes both main run and branch weld necks shall be tested.
4)
For CVN impact testing one set consists of three specimens.
5)
The base of the notch shall be perpendicular to the component's surface.
6)
Only applicable to C-Mn and low alloy steel. The section thickness is in the radial direction in the as-heat treated
condition.
7)
2 samples for section thickness < 30 mm (only one sample from mid thickness location) and 3 samples for section
thickness ≥ 30 mm.
8)
A minimum of 3 hardness measurements shall be taken on each sample.
9)
Only applicable for rolled C-Mn steels not meeting the requirements in [8.3.6].
10) Only applicable for 25Cr duplex steels.
1 Axial tensile specimen 1/2 T
1 Tangential tensile specimen 1/4 T
1 Tangential CVN (set) 1/2 T
1 Axial CVN (set) 1/2 T
1 Tangential CVN (set) 2 mm
below internal surface
1 Tangential CVN (set) 1/4 T
1 Tangential tensile specimen 1/2 T
Figure 8-1 Location of tensile and CVN specimens, exemplified on a flange with maximum section
thickness ≥ 50 mm
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8.5.2.3 Specimens for hardness testing shall be examined, prior to testing, at a magnification of not
less than X100. Grain-size measurement shall be performed in accordance with ASTM E112. The type of
microstructure and actual grain size shall be recorded on the materials testing report.
8.5.3 Acceptance criteria for duplex stainless steels
8.5.3.1 Tensile, hardness and Charpy V-notch impact properties shall meet the requirements for linepipe as
given in [7.3.4].
8.5.3.2 The metallographic samples shall comply with the requirements of [7.3.4].
2
8.5.3.3 For ASTM G48 testing the acceptance criteria is: maximum allowable weight loss 4.0 g/m .
8.6 Pipeline assemblies
8.6.1 General
8.6.1.1 This subsection is applicable for the fabrication of pipe strings (stalks) for reeling and towing, rigid
risers, spools and expansion loops.
8.6.1.2 The fabrication shall be performed according to a specification giving the requirements for fabrication
methods, procedures, extent of testing, acceptance criteria and required documentation. The specification
shall be subject to agreement prior to start of production.
8.6.2 Materials
8.6.2.1 Linepipe shall comply with the requirements, including supplementary requirements (as applicable)
given in Sec.7.
8.6.2.2 Induction bends shall comply with the requirements in this section, see [8.2.3].
8.6.2.3 Forged and cast material shall as a minimum meet the requirements given in this section.
8.6.3 Fabrication procedures, planning and mobilisation
8.6.3.1 The construction site shall establish the following:
—
—
—
—
organisation and communication
health, safety and environment manual
emergency preparedness
security plan including ISPS.
8.6.3.2 The construction site shall establish the following:
— material handling and storage (see [8.6.4])
— material receipt, identification and tracking (see [8.6.5])
— maintenance system.
8.6.3.3 All personnel shall be familiarized with the operation to be performed at the fabrication site. More
detailed familiarization shall be performed for personnel specific work tasks.
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8.6.3.4 Personnel involved in critical operations shall participate in a risk assessment for the specific
operation.
8.6.3.5 Equipment needed for the operations at the fabrication site shall be defined and mobilised.
8.6.3.6 Before production commences, the fabricator shall prepare a manufacture procedure specification
(MPS). The MPS shall be issued for review and acceptance prior to start of fabrication.
8.6.3.7 The MPS shall demonstrate how the fabrication will be performed and verified through the proposed
fabrication steps. The MPS shall address all factors which influence the quality and reliability of production.
All main fabrication steps from control of received material to shipment of the finished product(s), including
all examination and check points, shall be covered in detail. References to the procedures and acceptance
criteria established for the execution of all steps shall be included.
Guidance note:
The MPS will as a minimum typically contain the following information:
—
fabrication plan(s) and process flow description/diagram
—
supply of material, i.e. manufacturer and manufacturing location of material
—
fabrication process procedures
—
dimensional and weight control procedures
—
welding procedures including repair
—
heat treatment procedures
—
NDT procedures
—
coating procedures including repair and field joint coating
—
marking and protection procedures and
—
reeling procedures
—
stalk drawings
—
handling, lifting, loading and shipping procedures
—
cleaning and gauging of pipes
—
pressure test procedures, if applicable.
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8.6.3.8 Due consideration shall be given to the access and time required for adequate inspection and testing
as fabrication proceeds.
8.6.3.9 Due consideration during fabrication shall be given to the control of weight and buoyancy distribution
of pipe strings for towing.
8.6.4 Linepipe temporary storage and transportation
8.6.4.1 Temporary storage of pipes, both single joints or several joints, shall consider potential corrosion
damage. Corrosion damage may affect quality of NDT and pipeline integrity.
8.6.4.2 It shall be documented that storage facilities have the sufficient foundation for the weight of the
pipes. Each pipe joint and pipe stack shall withstand relevant weight and environmental loading (e.g. wind,
waves, earth quakes). Drainage of water shall be ensured. Potential icing shall be considered and appropriate
counter-active measures taken where found necessary.
8.6.4.3 Transportation and lifting of pipe joints shall be conducted safely to avoid damage to personnel,
equipment and pipe joints. The equipment used for transportation and lifting shall not impose damage to the
pipe joints.
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8.6.4.4 Acceptable stacking heights shall be established and documented for temporary storage and
transportation.
8.6.5 Material receipt, identification and tracking
8.6.5.1 All material shall be inspected for damage upon arrival. Quantities and identification of the material
shall be verified. Damaged items shall be clearly marked, segregated and disposed of properly.
8.6.5.2 A system for ensuring correct traceability to the material shall be established. The identification of
material shall be preserved during handling, storage and for all fabrication activities.
8.6.5.3 A pipe tracking system shall be used to maintain records of weld numbers, NDT records, pipe
numbers, pipe lengths, bends, cumulative length, weight, anode installation, in-line assemblies and repair
numbers. The system shall be capable of detecting duplicate records.
8.6.5.4 Pipes shall be inspected for loose material, debris, and other contamination, and shall be cleaned
both internally and at the pipe ends before being added to the assembly. The cleaning method shall not
cause damage to any internal coating.
8.6.5.5 The pipeline ends shall be protected against ingress of dust, water or any other material after
cleaning and prior to being added to the assembly.
8.6.5.6 All debris caused by the welding shall be removed from the inside of the pipeline.
8.6.5.7 The individual pipes of pipe strings shall be marked in accordance with the established pipe tracking
system using a suitable marine paint. The location, size and colour of the marking shall be suitable for
reading by ROV during installation. In case installation of in-line assemblies or piggy back cables, it may be
required to mark a band on top of the pipe string to verify if any rotation has occurred.
8.6.6 Hydrostatic testing
8.6.6.1 Detecting leakage early is beneficial and the current industry practice of hydrostatic testing of
pipeline assemblies prior to installation in Table 8-5 may be applied. If the pipeline assembly not is part of
the system pressure test, hydrostatic test shall be performed.
Table 8-5 Hydrostatic pressure test of pipeline assemblies
2
1)
Pipeline assemblies
Pressure
Holding time
Risers
σ e=0.96 SMYS
See Table 8-6
Spools
Stalks
PLEM/PLET's and other end terminations
1)
These hydrostatic tests may be performed prior to installation as a risk reduction measure, to reduce the probability
of installing assemblies with leaks, which are discovered during the system test. The tests shall be performed if an
assembly is not part of the system pressure test.
2)
The differential pressure shall be minimum equal to the system test pressure. The stated pressure will always be
higher than this and may be applied for simplicity.
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8.6.7 Welding and non-destructive testing
8.6.7.1 Requirements for welding processes, welding procedure qualification, execution of welding and
welding personnel are given in App.C.
8.6.7.2 Requirements for mechanical and corrosion testing for qualification of welding procedures are given
in App.B.
8.6.7.3 Requirements for methods, equipment, procedures, acceptance criteria and the qualification and
certification of personnel for visual examination and non-destructive testing (NDT) are given in App.D.
Selection of non-destructive methods shall consider the requirements in [D.1.4].
8.6.7.4 Requirements to automated ultrasonic testing (AUT) are given in App.E.
8.6.7.5 Members to be welded shall be brought into correct alignment and held in position by clamps, other
suitable devices, or tack welds, until welding has progressed to a stage where the holding devices or tack
welds can be removed without danger of distortion, shrinkage or cracking. Suitable allowances shall be made
for distortion and shrinkage where appropriate.
8.6.7.6 The fabrication and welding sequence shall be such that the amount of shrinkage, distortion and
residual stress is minimised.
8.6.7.7 For production testing, see [C.7.5.25] to [C.7.5.31].
8.6.7.8 The extent of NDT for installation girth welds shall be 100% ultrasonic or radiographic testing.
Radiographic testing should be supplemented with ultrasonic testing in order to enhance the probability of
detection and/or characterisation/sizing of defects.
8.6.7.9 All welds shall be subject to 100% visual inspection.
8.6.7.10 For wall thickness > 25 mm, automated ultrasonic testing should be used.
8.6.7.11 Ultrasonic testing (UT) or automated ultrasonic testing (AUT) shall be used in the following cases:
— whenever sizing of flaw height and/or determination of the flaw depth is required (see Table 5-10).
— 100% lamination checks of a 50 mm wide band at ends of cut pipe.
Exception to this requirement may be given for wall thickness < 8 mm provided that it can be technically
justified that alternative NDT processes provide sufficient inspection performance for the expected
imperfections for the applied welding procedure, see [D.2.10.11].
8.6.7.12 When radiographic testing is the primary NDT method UT or AUT shall be used in the following
cases:
— For the first 10 welds for welding processes with high potential for non-fusion type defects, when starting
installation or when resuming production after suspension of welding
— to supplement radiographic testing for unfavourable groove configurations
— for wall thickness above 25 mm:
— to provide additional random local spot checks during installation
— to supplement radiographic testing to aid in characterising and sizing of ambiguous indications.
8.6.7.13 If UT reveals defects not discovered by radiography, the extent of UT shall be 100% for the next
10 welds. If the results of this extended testing are unsatisfactory, the welding shall be suspended until the
causes of the defects have been established and rectified.
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8.6.7.14 For welds where allowable defect sizes are based on an ECA, UT shall supplement radiographic
testing, unless AUT is performed.
8.6.7.15 All NDT shall be performed after completion of all cold forming and heat treatment.
8.6.8 Cutting, forming and heat treatment
8.6.8.1 Attention shall be paid to local effects on material properties and any activities causing
carbon contamination where this is relevant. Preheating of the area to be cut may be required. Carbon
contamination shall be removed by grinding off the affected material.
Forming of material shall be according to agreed procedures.
8.6.9 Verification of dimensions and weight
8.6.9.1 Verification of dimensions should be performed in order to establish conformance with the required
dimensions and tolerances.
8.6.9.2 Verification of dimensions verification of pipe strings for towing and spools shall include weight, and
the distribution of weight and buoyancy.
8.6.10 Corrosion protection and thermal insulation
8.6.10.1 Application of coatings and installation of anodes shall meet the requirements of Sec.9.
8.6.10.2 Acceptable temperature ranges for spooling operations shall be defined.
Guidance note:
Undesired events such as cracking of field joints may occur for low temperatures.
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8.7 Hydrostatic testing
8.7.1 Preparations
8.7.1.1 Prior to performing hydrostatic testing the test object shall be cleaned and gauged.
8.7.1.2 The extent of the section to be tested shall be shown on drawings or sketches. The limits of the test,
temporary blind flanges, end closures and the location and elevation of test instruments and equipment shall
be shown. The elevation of the test instruments shall serve as a reference for the test pressure.
8.7.1.3 End closures and other temporary testing equipment shall be designed, fabricated, and tested to
withstand the maximum test pressure, and in accordance with a recognised standards or recommended
practices.
8.7.1.4 Testing should not be performed against in-line valves, unless possible leakage and damage to the
valve is considered, and the valve is designed and tested for the pressure test condition. Blocking off or
removal of small-bore branches and instrument tappings should be considered in order to avoid possible
contamination.
Considerations shall be given to pre-filling valve body cavities with an inert liquid unless the valves have
provisions for pressure equalisation across the valve seats.
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8.7.1.5 Welds shall not be coated, painted or covered, if the purpose of the test is 100% visual inspection.
However, thin primer coatings may be used where agreed.
8.7.1.6 Welds may be coated or painted if the acceptance criterion is based on pressure observations.
8.7.2 Instrumentation
8.7.2.1 Instruments and test equipment used for measurement of pressure, volume, and temperature shall
be calibrated for accuracy, repeatability, and sensitivity. All instruments and test equipment shall possess
valid calibration certificates with traceability to reference standards within the 6 months preceding the test. If
the instruments and test equipment have been in frequent use, they should be calibrated specifically for the
test.
8.7.2.2 Gauges and recorders shall be checked for correct function immediately before each test. All test
equipment shall be located in a safe position outside the test boundary area.
8.7.2.3 The following requirements apply for instruments and test equipment:
— testers shall have a range of minimum 1.25 times the specified test pressure, with an accuracy better
than ± 0.1 bar and a sensitivity better than 0.05 bar.
°
— temperature-measuring instruments and recorders shall have an accuracy better than ± 1.0 C
— pressure and temperature recorders shall be used to provide a graphical record of the pressure test for
the total duration of the test.
8.7.3 Test medium and filling
8.7.3.1 The test medium should be fresh water or adequately treated sea water, as applicable.
Filling procedure shall ensure minimum air pockets.
8.7.4 Testing
8.7.4.1 Pressurisation shall be performed as a controlled operation with consideration for maximum
allowable velocities in the inlet piping up to 95% of the test pressure. The final 5% up to the test pressure
shall be raised at a reduced rate to ensure that the test pressure is not exceeded. Time shall be allowed for
confirmation of temperature and pressure stabilisation before the test hold period begins.
8.7.4.2 The test pressure shall be according to the applied standards or recommended practices.
8.7.4.3 Leakage may be detected by visual observations or by pressure variations. When the test acceptance
is based on observation of pressure variations, calculations showing the effect of temperature changes on
the test pressure shall be developed prior to starting the test. Temperature measuring devices, if used, shall
be positioned close to the test object and the distance between the devices shall be based on temperature
gradients along the test object.
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8.7.4.4 Hydrostatic pressure test hold times is given in Table 8-6
Table 8-6 Hydrostatic pressure test holding times (from DNVGL-RP-F113)
Item
Hold time
Volume
2)
3
Pipelines
>1000 m
Short pipelines
100-1000 m
Local repair sec.
10-100 m
Pipeline Assemblies
1-10 m
Pipeline Components
Back-seal tests
3
3
3
0.1-1 m
1)
3
3
0.01-0.1 m
Visual detection
Pressure monitoring
NA
≥24 hrs
NA
8 hrs
2 hrs
8 hrs
15 min
8 hrs
15 min
8 hrs
15 min
15 min
1)
For unsupported seals supported by friction towards pipe wall and fitting surface (e.g. inflated- and tongue seal,
without any grove or equivalent) additional holding time to document acceptable resistance against slippage needs
to be assessed.
2)
The holding time at test pressure shall be until 100% visual inspection is complete or the specified hold time,
whichever is longer.
8.7.4.5 The pressure test is acceptable for:
— 100% visual inspection when there are no observed leaks (e.g. at welds, flanges, mechanical connectors)
and the pressure has at no time during the hold period fallen below 99% of the test pressure. 100%
visual inspection shall only be acceptable where there is no risk that a leak may go undetected due to
prevailing environmental conditions
— 100% pressure observation when the pressure profile over the test hold period shows a clear convergence
to a fixed value above 99% of the specified test pressure. This may required an extension of the holding
time.
8.7.5 Alternative test pressures
8.7.5.1 For components fitted with pup pieces of material identical to the adjoining pipeline, the test
pressure can be reduced to a pressure that produce an equivalent stress of 96% of SMYS in the pup piece.
8.7.5.2 If the alternative test pressure in [8.7.5.1] cannot be used and the strength of the pup piece is not
sufficient:
— Testing shall be performed prior to welding of pup pieces. The weld between component and pup piece is
regarded a pipeline weld and will be tested during pipeline system testing.
8.8 Documentation, records, certification and marking
8.8.1 General
8.8.1.1 All base material, fittings and, flanges, etc. shall be delivered with inspection certificate 3.1
according to European Standard EN 10204 or accepted equivalent.
The inspection certificate shall include:
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— identification the products covered by the certificate with reference to heat number, heat treatment batch
etc.
— dimensions and weights of products
— the results (or reference to the results) of all specified inspections and tests
— the supply condition and the temperature of the final heat treatment.
8.8.1.2 Records from the qualification of the MPS and other documentation shall be in accordance with
Sec.12.
8.8.1.3 Each equipment or component item shall be adequately and uniquely marked for identification. The
marking shall, as a minimum, provide correlation of the product with the related inspection documentation.
8.8.1.4 The marking shall be such that it easily will be identified, and retained during the subsequent
activities.
8.8.1.5 Other markings required for identification may be required.
8.8.1.6 Equipment and components shall be adequately protected from harmful deterioration from the time
of manufacture until taken into use.
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SECTION 9 CONSTRUCTION - CORROSION PROTECTION AND
WEIGHT COATING
9.1 General
9.1.1 Objective
9.1.1.1 This section gives requirements and recommendations on:
—
—
—
—
application (manufacture) of external pipeline coatings including field joint coatings and infill
application (manufacture) of concrete weight coatings
manufacture of galvanic anodes
installation of galvanic anodes.
9.1.1.2 The objectives are to ensure that the external corrosion control system and any weight coating
are designed and fabricated to ensure proper function for the design life of the systems. As to the last item
above, it is a further objective to ensure that the fastening does not impose any damage or hazards affecting
the integrity of the pipeline system.
9.1.2 Application
9.1.2.1 This section is applicable to the preparation of specifications for manufacture/installation of external
corrosion control systems and for the manufacture of concrete weight coating during the construction phase.
Such specifications shall define the requirements to properties of the coatings and anodes, and to the
associated quality control.
9.1.2.2 Manufacture/installation of any impressed current CP systems for landfalls is not covered by this
standard. The requirements in ISO 15589-1 shall then apply.
9.1.3 Systematic review
9.1.3.1 An overall requirement to systematic review in Sec.2 shall for this section imply:
— The selection of coating system and its detailed design shall take into considerations e.g. the pipe laying
method, pipe loading conditions and pipeline operating conditions in service.
— The selection of coating system and its detailed design shall take into consideration compatibility between
linepipe coating system, field joint coating system, infill and concrete coating (when applicable).
— In the coating purchase specification, as-applied coating properties shall be defined and requirements to
methods, frequency and acceptance criteria for their verification shall be specified.
— Prior to start of coating application, essential application process parameters shall be defined by the
coating applicator. The essential process parameters shall be project specific and should be verified in
a procedure qualification trial (PQT, see [9.2.2.2] and [9.3.4.2] below) to ensure that specified coating
properties can be fulfilled. Quality control during production shall verify that the essential process
parameters are maintained during production.
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Guidance note:
Examples of how inadequate coating properties may result in failures are:
—
Poor adhesion between steel surface and corrosion protective coating may result in partly or completely detachment of coating
during storage or operation.
—
Insufficient bonding to steel substrate/between coating layers, in combination with low ductility of as-applied coating may
cause cracking of linepipe and/or field joints/infill during reeling of pipelines.
—
Insufficient shear resistance capacity between corrosion coating and concrete coating may result in a safety risk during
installation due to sudden sliding of the concrete coating relative to steel pipe, and/or damage to field joints and anodes during
operation due to thermal axial expansion of the steel pipe relative to the concrete coating.
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9.2 External corrosion protective coatings
9.2.1 General
9.2.1.1 Properties of the coating (as-applied) and requirements to quality control during application shall be
defined in a purchase specification (see [6.3.5]).
9.2.1.2 For application of 3-layer polyolefin coatings (3-layer polyethylene/polypropylene), single layer
fusion-bonded epoxy coatings and field joint coatings, requirements in ISO 21809 (part 1-3) shall apply with
the additional requirements as specified below.
9.2.1.3 Recommended practice for application of line pipe coatings and field joint coating are given in
DNVGL-RP-F106 Sec.9 and DNVGL-RP-F102, respectively.
Guidance note:
DNVGL-RP-F106 Sec.9 and DNVGL-RP-F102 have emphasis on quality control procedures and documentation. They comply with
and refer to ISO 21809 with some additional requirements for relevant coating systems (including some additional systems to
those defined in ISO 21809). DNVGL-RP-F102 also covers field repairs of line pipe coating and infill, see [6.4.4]. These documents
are applicable to the preparation of coating specifications and can also be used as a purchase document if amended to include
project and any operator specific requirements.
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9.2.1.4 The design and quality control during application of field joint coatings is essential to the integrity of
pipelines in HISC susceptible materials, including ferritic-austenitic (duplex) and martensitic stainless steel.
Recommended practice for design and quality control during application of field joint coatings is given in
DNVGL-RP-F102.
9.2.2 Coating materials, surface preparation, coating application and
inspection/testing of coating
9.2.2.1 All coating work shall be carried out according to a project specific application procedure specification
(APS, also referred to as manufacturing procedure specification, MPS). The following items shall be described
in the procedure specification:
—
—
—
—
—
—
—
receipt, handling and storage of coating materials
surface preparation and inspection
coating application and monitoring of essential process parameters
inspection and testing of coating
coating repairs and stripping of defect coating
preparation of cut-backs (for linepipe coating)
marking, traceability and handling of non-conformities
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— handling and storage of coated pipes (for linepipe coating)
— documentation.
Material data sheets for coating, blasting and any other surface preparation materials may either be included
in the APS or in a separate document. The purchaser may specify that the above documentation shall be
submitted for approval prior to the start of production and any PQT (see [9.2.2.2]).
9.2.2.2 A coating procedure qualification trial (PQT; also referred to as an application procedure qualification
test or pre-production qualification test) should be executed and accepted by purchaser before starting
the coating work, especially for coating systems which rely on a curing process to achieve the specified
properties. For field joint coating (FJC) and infill, a pre-production trial (PPT) should also be performed. The
purpose of the qualification is to confirm, prior to the start of regular production, that the coating application
procedure specification (APS), coating materials, tools/equipment and personnel to be used for production
are adequate to achieve the specified properties of the coating.
9.2.2.3 An inspection and testing plan (ITP; sometimes referred to as an inspection plan or quality plan)
shall be prepared and submitted to purchaser for acceptance. The ITP shall refer to the individual application
and inspection/testing activities in consecutive order, define methods/standards, frequency of inspection/
testing, checking/calibrations, and acceptance criteria. Reference shall further be made to applicable
reporting documents and procedures for inspection, testing and calibrations.
9.2.2.4 Inspection and testing data, essential process parameters, repairs and checking/calibrations of
equipment for quality control shall be recorded in a daily log that shall be updated on a daily basis and be
available to purchaser on request at any time during coating production.
9.2.2.5 The daily log format and final documentation index should be prepared for acceptance by purchaser
prior to start of production.
9.3 Concrete weight coating
9.3.1 General
9.3.1.1 The objectives of a concrete weight coating are to provide negative buoyancy to the pipeline, and
to provide mechanical protection of the corrosion coating and linepipe during installation and throughout the
pipeline's operational life.
9.3.1.2 The concrete weight coating (thickness, strength, density, amount of reinforcement) shall be
designed for the specific project; i.e. the actual installation, laying and operation conditions for the pipeline
shall then be taken into consideration.
9.3.1.3 For materials and application of concrete weight coating requirements in ISO 21809-5 shall apply
with the additional requirements (AR) or modified requirements (MR) as specified below.
9.3.2 Materials
9.3.2.1 Cement shall be moderate sulphate resistant Portland cement equivalent to type II according to
ASTM C150. MR
9.3.2.2 The tricalcium aluminate (C3A) content of the cement shall not exceed 8%. MR
9.3.2.3 The percentage of the recycled concrete used as aggregate shall not exceed 7% by weight. MR
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9.3.2.4 The reclaimed concrete content in the concrete mix should not exceed 10% by weight. Use of
higher amounts shall be verified by testing confirming that the required concrete coating properties can be
achieved. AR
9.3.3 Concrete mix
9.3.3.1 The content of chloride in the concrete mix, calculated as free CaCl2 shall not exceed 0.4% of the
weight of the cement. AR
9.3.4 Coating application
9.3.4.1 All coating work shall be carried out according to an application procedure specification (APS), AR.
The following items shall be described in the APS:
—
—
—
—
—
—
—
—
raw materials, including receipt, handling and storage
concrete mix design
reinforcement percentage and placement
coating application and curing
inspection and testing, including calibrations of equipment
coating repairs
pipe tracking, marking and coating documentation
handling and storage of coated pipes.
Purchaser may specify that the APS shall be subject to approval prior to start of production and any PQT. AR
9.3.4.2 A coating procedure qualification trial (PQT; in ISO 21809-5 referred to as qualification test) shall be
executed and accepted by purchaser before starting the coating work.
9.3.4.3 Changes in type of linepipe coating and/or applicator and/or changes in concrete constituent
materials and/or concrete mix shall require a new PQT. AR
9.3.4.4 Repair methods shall be included in the PQT. AR
9.3.4.5 The following inspections and tests shall also be carried out during PQT. AR:
—
—
—
—
—
Testing aggregates according to ASTM C33 or equivalent
Determining water content in the concrete mix
Determining cement content in the concrete mix and water/cement ratio
Inspection of linepipe coating (holiday detection)
Calibration/verification of all measuring and weighting equipment
Guidance note:
Purchaser may consider performing a full scale water absorption test, shear resistance test and/or impact resistance test as an
integral part of PQT. Also, purchaser may consider a requirement on production of several pipes to demonstrate the applicator
capability of continuous production of conforming pipes.
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9.3.4.6 The following modification of acceptance criteria for inspections and tests during PQT shall apply.
MR:
— The thickness of the concrete coating shall not be less than 40 mm.
— The minimum in-situ compressive strength of the concrete coating shall not be less than 40 MPa. The
mean strength shall be calculated from compressive test results of three drilled cores obtained from one
pipe, with no single test results less than 34 MPa.
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9.3.4.7 The concrete coating shall be reinforced by steel bars welded to cages or by wire mesh steel. The
minimum percentage of the steel reinforcement shall be 0.5% circumferentially and 0.08% longitudinally of
the cross-sectional area of the concrete coating. MR
9.3.4.8 The minimum diameter of circumferential cage reinforcement shall be 5 mm. MR
9.3.4.9 The maximum spacing between circumferential and longitudinal cage reinforcement shall be 125 mm
and 250 mm, respectively. AR
9.3.4.10 The minimum diameter of wire mesh reinforcement shall be 2 mm. MR
9.3.4.11 The minimum overlap of wire mesh reinforcement shall be 1.5 x distance between the wires or 25
mm (whichever is greater). AR
9.3.4.12 Minimum concrete cover to the reinforcement shall be 15 mm for concrete thickness less or equal
to 50 mm and minimum 20 mm for concrete thickness greater than 50 mm. MR
9.3.4.13 The thickness of the concrete coating shall not be less than 40 mm. MR
9.3.5 Inspection and testing
9.3.5.1 An inspection and testing plan (ITP) shall be prepared and submitted to purchaser for acceptance in
due time prior to start of production. The ITP shall define the methods and frequency of inspection, testing
and calibrations, acceptance criteria and requirements to documentation. Reference shall further be made to
applicable reporting documents and procedures for inspection, testing and calibration. AR
9.3.5.2 Other standards for testing than those specified in this standard may be used, provided that it is
documented during PQT that the quality of materials and applied concrete weight coating will not be lower
than when testing according to the standards specified in this rule. AR
9.3.5.3 The dimensions of cube and cylinder specimens (cast from fresh concrete) for testing the concrete
compressive strength shall be 100 mm × 100 mm × 100 mm cubes or 100 mm × 100 mm cylinders. AR
9.3.5.4 For hardened concrete drill cores specimens, the diameter of the cylinder shall not be less than 38
mm and the preparation shall be according to ASTM C31 or EN 12390-2. AR
9.3.5.5 The following inspections and tests shall also be carried out during production. AR:
—
—
—
—
inspection of linepipe coating (holiday detection) before concrete coating application
calibration of all measuring and weighing equipment
content of recycled and reclaimed materials in the concrete mix
sounding test.
Guidance note:
Purchaser may consider performing a full scale water absorption test as part of production testing.
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9.3.5.6 The following modification of acceptance criteria for inspections/tests during production shall apply.
MR:
— Concrete coating thickness: minimum 6 measurements on each pipe.
9.3.5.7 Inspection and testing data, repairs, essential process parameters and calibrations of equipment for
quality control shall be recorded in a daily log that shall be updated on a daily basis and be available to the
purchaser on request at any time during coating production. AR
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9.3.5.8 The daily log format and final documentation index should be prepared for acceptance by purchaser
prior to start of production.
9.4 Manufacture of galvanic anodes
9.4.1 Anode manufacture
9.4.1.1 Requirements to anode manufacture shall be detailed in a purchase specification (anode
manufacturing specification). A manufacturing specification for pipeline bracelet anodes shall cover all
requirements in ISO 15589-2.
Recommended practice for anode manufacture with some additional requirements and guidance to ISO,
primarily for quality control, is given in DNVGL-RP-F103.
9.4.1.2 The manufacturer of bracelet anodes shall prepare a manufacturing procedure specification (MPS)
describing anode alloy (e.g. limits for alloying and impurity elements) and anode core materials, anode
core preparations, anode casting, inspection and testing, coating of bracelet anode surfaces facing the pipe
surface, marking and handling of anodes, and documentation.
9.4.1.3 An inspection and testing plan (ITP) for manufacture of bracelet anodes, shall be prepared and
submitted to the purchaser for acceptance. It is further recommended that the inspection and testing results
are compiled in a daily log
See DNVGL-RP-F103 for requirements and guidance for preparation of these documents and to a procedure
qualification trial (PQT). For manufacture of other types of anodes than pipeline bracelet anodes, see DNVGLRP-B401.
Guidance note:
The requirement for an ITP is an amendment to ISO 15589-2.
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9.4.1.4 For each anode type/size, the manufacturer shall prepare a detailed drawing showing location and
dimensions of anode inserts, anode gross weight and other details as specified in a purchase document
9.4.1.5 The anode manufacturer shall prepare a detailed procedure for electrochemical testing in compliance
with the agreed standard. An outline procedure for electrochemical testing of anode material performance
during anode manufacture is given in DNVGL-RP-B401 App.B and in Annex D of ISO 15589-2.
9.4.1.6 Marking of anodes shall ensure traceability to heat number. Anodes should be delivered according to
ISO 10474, inspection certificate 3.1.B or EN 10204, inspection certificate 3.1.
9.5 Installation of galvanic anodes
9.5.1 Anode installation
9.5.1.1 Installation of anodes shall meet the requirements in ISO 15589-2. Recommended practise for
installation of anodes with some additional requirements and guidelines, primarily for quality control, are
given in DNVGL-RP-F103.
9.5.1.2 For martensitic and ferritic-austenitic (duplex) stainless steels and for other steels with SMYS >
450 MPa, no welding for anode fastening (including installation of doubling plates) should be carried out on
linepipe or other pressure containing components.
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Guidance note:
The requirement above is an amendment to ISO 15589-2. Most CP related HISC damage to pipeline components in CRA’s have
occurred at welded connections of galvanic anodes to the pipe walls. To secure adequate fastening of pipeline bracelet anodes
for compatibility with the applicable installation techniques, forced clamping of anodes is applicable in combination with electrical
cables attached to anodes and pipeline by brazing. However, for many applications, CP can be provided by anodes attached to
other structures electrically connected to the pipeline (see [6.4.5]). For installation of anodes on such structures, see DNVGL-RPB401.
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9.5.1.3 All welding or brazing of anode fastening devices and connector cables shall be carried out according
to a qualified procedure (see App.C of this standard) to demonstrate that the requirements in ISO 13847 to
maximum hardness (welding/brazing) and copper penetration (brazing including aluminothermic welding) are
met.
9.5.1.4 For linepipe to be concrete weight coated, electrical contact between concrete reinforcement and
the anodes shall be prevented. The gaps between the anode half shells may be filled with asphalt mastic,
polyurethane or similar. Any spillage of filling compound on the external anode surfaces shall be removed.
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SECTION 10 CONSTRUCTION – OFFSHORE
10.1 General
10.1.1 Objective
10.1.1.1 This section provides requirements as to studies, analyses and documentation shall be prepared
and agreed for the offshore construction, and further to provide requirements for the installation and testing
of the complete submarine pipeline system. For associated marine operations reference is also made to
DNVGL-ST-N001.
10.1.2 Application
10.1.2.1 This section is applicable to offshore construction of submarine pipeline systems designed and
constructed according to this standard.
10.1.3 Systematic review
10.1.3.1 The overall requirement to systematic review in Sec.2 shall be reflected in the offshore construction
of the pipeline.
10.1.3.2 Systematic analyses of equipment and offshore construction shall be performed in order to identify
possible critical items or activities which could cause or aggravate a hazardous condition, and to ensure that
effective remedial measures are taken.
10.1.3.3 The extent of systematic review shall depend on criticality of operations and experience from
previous similar operations.
10.1.3.4 The systematic analyses should be carried out as a failure mode effect analysis (FMEA) for
equipment and hazard and operability studies (HAZOP) for critical operations. Recommended practice for
FMEA and HAZOP is given in DNVGL-RP-N101. For HAZOP, see also API RP 17N.
Guidance note:
Typical items to be covered for HAZOP include:
—
simultaneous operations
—
lifting operations including pipe joints transportation and storage
—
dry and wet buckles including flooding of pipe
—
initiation and lay down including shore pull
—
operations inside safety zones
—
critical operations (laying in short radii curves, areas with steep slopes etc.)
—
failure of equipment and measuring and monitoring devices
—
tie-in operation
—
pre-commissioning activities
—
environmental conditions and weather criteria
—
emergency abandonment
—
loss of station keeping capabilities
—
survey.
It is desired to mitigate potential hazards by engineering measures.
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10.1.3.5 The results of the FMEA analysis or HAZOP studies shall also be used in determining the extent and
depth of verification of equipment and procedures.
10.1.4 Installation manual
10.1.4.1 An installation manual shall be prepared by the contractor, see [10.12].
10.1.5 Quality assurance
10.1.5.1
The contractor shall as a minimum have an implemented quality assurance system as outlined in [2.2.5].For
installation contractors a quality assurance system according to ISO 9001 is considered to meet requirements
in [2.2.5].
10.1.5.2
The installation contractor shall demonstrate compliance with QA/QC system.
10.1.5.3
The Contractor shall use competent personnel at all stages of the project. Permanent technical, managerial
and planning personnel shall have adequate education, training and experience commensurate with their
duties and level of supervision under which the work is performed. These requirements shall be part of the
contractor’s quality management system.
10.1.5.4
All engineering analysis and calculations required to support installation procedures shall be performed by
technical staff with the appropriate educational qualifications and experience. Such work shall be discipline
checked and approved by responsible engineers in the contractor’s organization or external consultants.
10.1.5.5
For offshore personnel, contractor shall have a competence assurance program similar to the IMCA
Competence Assurance and Assessment framework or equivalent, for all personnel involved in marine,
diving, offshore survey, remote operations and ROV work.
10.1.5.6
A master language for communications shall be defined. Platforms for where master language shall be used
shall be defined.
Guidance note:
The purpose of defining a master language is to avoid miscommunications and to ensure that all parties may receive and
understand communications. The master language is normally defined by the operator. For platforms where master language is not
required, other languages may be used as appropriate.
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10.1.5.7
Key personnel shall have sufficient verbal communication skills in the common language used during
operations.
10.2 Pipe assemblies onshore
10.2.1 Pipe assemblies onshore
10.2.1.1 For pipe assemblies onshore, see [8.6].
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10.2.1.2 For linepipe temporary storage and transportation, see [8.6.4].
10.3 Pipeline route, pre-installation survey and preparation
10.3.1 Pre-installation route survey
10.3.1.1 A pre-installation survey of the pipeline route should be performed in addition to the route survey
required for design purposes covered by [3.3.6] if:
—
—
—
—
—
the time elapsed since the previous survey is significant
a change in seabed conditions is likely to have occurred
the route is in areas with heavy marine activity
new installations or facilities are present in the area
seabed preparation work is performed within the route corridor after previous survey.
10.3.1.2 The pre-installation survey should determine:
— potential new/previously not identified hazards to the pipeline and the installation operations
— location of wrecks, submarine installations and other obstructions such as mines, debris, rocks and
boulders that might interfere with, or impose restrictions on, the installation operations
— that the present seabed conditions confirm those of the survey required in Sec.3
— any other potential hazards due to the nature of the succeeding operations.
10.3.1.3 The extent of, and the requirements for, the pre-installation route survey shall be specified.
10.3.2 Seabed preparation including shore approaches
10.3.2.1 Seabed preparation may be required to:
— remove obstacles and potential hazards interfering with the installation operations
— prevent loads or load effects that occur as a result of seabed conditions or shore area such as unstable
slopes, sand waves, deep valleys and possible erosion and scour from exceeding the design criteria
— prepare for pipeline and cable crossings
— infill depressions and remove high-spots to prevent unacceptable free spans
— carry out any other preparation due to the nature of the succeeding operations
— avoid damage to coating and anodes and other attachments to the pipeline.
10.3.2.2 The extent of, and the requirements for, seabed preparation shall be specified. The laying
tolerances shall be considered when the extent of seabed preparation is determined.
10.3.2.3 Where trench excavation is required before pipelaying, trench shall be excavated to a sufficiently
smooth profile.
10.3.3 Existing pipelines and cables including crossings
10.3.3.1 The location of any other pipelines, cables or other infrastructure shall be identified.
10.3.3.2 Preparations for crossing of pipelines and cables shall be carried out according to a specification
detailing the measures adopted to avoid damage to both installations. The operations should be monitored to
confirm proper placement and configuration of the supports. Support and profile over the existing installation
shall be in accordance with the accepted design.
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10.3.3.3 The specification shall state requirements concerning:
—
—
—
—
—
—
—
—
—
—
—
—
—
minimum separation between existing installation and the pipeline
co-ordinates of crossing
marking of existing installation
confirmation of position and orientation of existing installations on both sides of the crossing
lay-out and profile of crossing
depth of cover
vessel anchoring
installation of supporting structures or gravel beds
methods to prevent scour and erosion around supports
monitoring and inspection methods
tolerance requirements
condition of landfall
any other requirements.
10.4 Installation spread
10.4.1 General
10.4.1.1 These requirements are applicable for vessels performing pipeline and riser installation and
supporting operations. Specific requirements for installation equipment onboard vessels performing
installation operations are given in the relevant subsections.
10.4.1.2 The organisation of key personnel with defined responsibilities and lines of communication shall be
established prior to start of the operations. Interfaces with other parties shall be defined.
10.4.1.3 All personnel shall be qualified for their assigned work. Key personnel shall have sufficient verbal
communication skills in the common language used during operations.
10.4.1.4 Manning level should comply with IMO Res. A.1047 (27) - Principles of minimum safe manning.
Non-self propelled vessels shall have similar manning and organisation as required for self propelled units of
same type and size.
10.4.1.5 Vessels and equipment shall have a documented maintenance programme covering all systems
vital for the safety and operational performance of the vessel, related to the operation to be performed. The
maintenance programme shall be presented in a maintenance manual or similar document.
10.4.2 Vessels
10.4.2.1 All vessels shall have valid class with a recognised classification society. The valid class shall cover
all systems of importance for the safety of the operation. Further requirements to vessels shall be given in a
specification stating requirements for:
—
—
—
—
—
—
—
—
anchors, anchor lines and anchor winches
anchoring systems
thrusters in case of thruster assisted mooring
positioning and survey equipment
dynamic positioning equipment and reference system
alarm systems, including remote alarms when required
general seaworthiness of the vessel for the region
cranes and lifting appliances
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— pipeline installation equipment
— any other requirement due to the nature of the operations.
10.4.2.2 Status reports for any recommendations or requirements given by national authorities and/or
classification societies, and status of all maintenance completed in relation to the maintenance planned for a
relevant period, shall be available for review.
10.4.2.3 An inspection or survey shall subject to agreement be performed prior to mobilisation of the vessels
to confirm that the vessels and their principal equipment meet the specified requirements and are suitable
for the intended work.
10.4.2.4 The scale of fire fighting and lifesaving appliances on board shall, as a minimum, be in accordance
with the scales prescribed in SOLAS corresponding to the number of personnel on board the vessel.
10.4.3 Positioning systems
10.4.3.1 The installation barge/vessel shall have a position/heading keeping system able to maintain a
desired position/heading within the accuracy and reliability required for the planned operation and the
environmental conditions. See [10.4.4] and [10.4.5] for more details.
10.4.3.2 The operation/installation shall be planned and executed with use of position/heading reference
system(s) of suitable type, accuracy and reliability required for the operation(s) and type of vessel(s)
involved.
10.4.3.3 The positioning/heading reference systems shall be calibrated and capable of operating within the
specified limits of accuracy prior to start of the installation operations.
10.4.3.4 Installation in congested areas and work requiring precise relative location may require local
systems of greater accuracy, such as acoustic transponder array systems. Use of ROV’s to monitor and assist
the operations is recommended and should be considered.
10.4.3.5 The positioning/heading reference system shall as a minimum provide information relating to:
—
—
—
—
—
position relative to the grid reference system used
geographical position
heading
offsets from given positions
vertical reference datum(s).
10.4.4 Anchoring systems, anchor patterns and anchor handling
10.4.4.1 Anchoring systems for vessels kept in position/heading by anchors (with or without thruster
assistance) while performing marine operations shall meet the following requirements:
— Instruments for reading anchor line tension and length of anchor lines shall be fitted in the operations
control room or on the bridge, and also at the winch station.
— Remotely operated winches shall be monitored from the control room or bridge, by means of cameras or
equivalent.
— Instrumentation for reading thruster output and available electrical power for thrusters shall be available
at bridge and/or in the operation control room.
10.4.4.2 Anchor handling vessels shall be equipped with:
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— a surface positioning reference system of sufficient accuracy. High accuracy is required for anchor drops
in areas with strict requirements to control of anchor position, typical within safety zone of existing
installations, proximity of pipelines or areas of archeological or environmental importance
— computing and interfacing facilities for interfacing with lay vessel, trenching vessel or other anchored
vessels
— latest revision of charts for the whole area of operation.
10.4.4.3 Procedures for the anchor handling shall be established, ensuring that:
— anchor locations are in compliance with the anchor pattern for the location
— requirements of operators of other installations and pipelines for anchor handling in the vicinity of the
installation are known, and communication lines established
— position prior to anchor drop is confirmed
— anchor positions are monitored at all times, particularly in the vicinity of other installations and pipelines
— any other requirement due to the nature of the operations is fulfilled.
Guidance note:
In order to ensure correct positioning of anchors, the line length measurements should be reset at the point of the anchor shackle
being at the stern roller and accurate information of line tension should be ensured.
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10.4.4.4 All mooring equipment shall hold a valid certificate. There shall be procedures in place for handling
and regular inspection of all mooring equipment.
10.4.4.5 For mooring systems using synthetic fibre lines, instructions for handling, use and storage as
provided by manufacturer and/or stated on certificate shall be followed. Contact with the seabed shall be
avoided at any time unless the fibre ropes have been certified for such contact.
10.4.4.6 Anchor patterns shall be predetermined for each vessel using anchors to maintain position.
Different configurations for anchor patterns may be required for various sections of the pipeline, especially in
the vicinity of fixed installations and other subsea installations or other pipelines or cables.
10.4.4.7 The minimum allowable number of anchors to be used during pipeline installation shall be
established.
10.4.4.8 Anchor patterns shall be according to the results of mooring analyses and shall be verified to have
the required capacity for the proposed location, time of year and duration of operation. Safe distance to
other installation and non-anchoring zones shall be established, and the possibility to leave the site in an
emergency situation shall be considered.
Guidance note:
For weather restricted operations and mooring, see DNVGL-ST-N001. For non-weather restricted operations and mooring, see
DNVGL-OS-E301.
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10.4.4.9 The mooring system shall as a minimum be analysed for:
— an ultimate limit state (ULS) to ensure that the individual lines and anchors have adequate strength to
withstand the load effects imposed by extreme environmental actions
— an ultimate limit state (ULS) to ensure that the individual lines have the adequate strength and the
vessel/barge is kept within acceptable positions for the environmental limiting conditions for the operation
— an accidental limit state (ALS) to ensure that the mooring system has the adequate capacity to withstand
the failure of one mooring line, or in case of thruster assisted mooring, failure of one truster or failure in
trusters’ control or power systems.
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10.4.4.10 Holding capacity of anchor shall be documented, and potential dragging of anchors shall be
assessed. The anchor holding capacity shall be based on actual soil condition and type of anchors to be used.
Various anchors may have various performance in different soils, and evaluation of the appropriate anchor
type shall be performed. Special caution should be paid to holding capacity on sand.
10.4.4.11 Each anchor pattern shall be clearly shown on a chart of adequate scale. The pattern should
include allowable tolerances. All subsea installations, infrastructure and other anchor restricted zones shall be
shown in the chart.
10.4.4.12 If using anchor handling tug as live anchor, the tug should as a minimum hold a DP class
according to DP equipment class 2. The winch and DP system should be linked ensuring winch tension to be
considered in the system. Live anchor should not be used in critical operations and inside the safety zone.
10.4.4.13 Station-keeping systems based on anchoring shall have adequate redundancy or back-up systems
in order to ensure the pipeline integrity and that other vessels and installations are not endangered by partial
failure.
Guidance note:
The pipeline integrity check should, as a minimum, include the following cases:
- Worst case for mooring failure
- Mooring failure for the most loaded case for pipeline as identified in dynamic analysis.
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10.4.4.14 Safe distances are to be specified between an anchor, its cable and any existing fixed or subsea
installations and infrastructure, both for normal operations and emergency conditions.
Guidance note:
Minimum clearances may vary depending on requirements of operators of other installation/pipeline and national requirements.
Additional guidance can be found in DNVGL-ST-N001.
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10.4.4.15 The anchor position, drop zone and wire catenary should be established taking into account the
water depth, wire tension and wire length. Confirmation of anchor positioning after installation shall be
confirmed at regular intervals depending on required accuracy and criticality, and counteractive measures
taken when found required. Monitoring systems shall be considered.
10.4.4.16 During anchor running, attention shall be paid to the anchor cable and the catenary of the cable,
to maintain minimum clearance between the anchor cable and any subsea installations and infrastructure or
obstacles.
10.4.4.17 All anchors transported over subsea installations and infrastructure shall be secured on deck of
the anchor handling vessel.
10.4.5 Dynamic positioning
10.4.5.1 Vessels performing pipelaying activities using dynamic positioning systems for station keeping and
location purposes shall be designed, equipped and operated in accordance with IMO MSC/Circ.645 Guidelines
for Vessels with Dynamic Positioning Systems or MSC 1./Circ.1580 Guideline for Vessels and Units with
Dynamic Positioning (DP) Systems and the corresponding class notations from a recognised classification
society.
10.4.5.2 Selection of required DP equipment class for the operation shall comply with national requirements
and in addition be based upon a risk assessment of the actual installation and location.
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Guidance note:
The following DP equipment class should apply:
—
Minimum equipment class 2 for operations outside the safety zone for live installation (surface or subsea)
—
Equipment class 3 for operations inside the safety zone for live installations
—
Equipment class 3 for manned subsea operations or other operations where a sudden horizontal displacement of the vessel
may have severe consequences for personnel.
For operations inside the safety zone, vessels with lower equipment classes may be accepted subject to agreement on a case by
case basis. Elements to evaluate with regard to acceptance of lower equipment class are:
—
the vessel does not exceed the vessel size of which the facility is designed for with regard to withstanding collision.
—
the consequences of single failures, including fire and flooding, will not increase significantly
—
availability of reliable positioning reference systems
—
possibility of operating with open waters on leeward side
—
risk reducing measures as extra DP manning, engine room manning and fire watch.
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10.4.5.3 Sufficient DP capacity shall be documented by capability plots. The plots shall be relevant for the
planned project based on correct vessel lay-out, including project specific modifications, and relevant pipeline
and tension. The plots shall cover normal operation as well as worst case single failure from FMEA.
Guidance note:
The capacity plots should be provided for two scenarios for the same weather conditions:
—
all system fully functional
—
worst case failure mode, or an amalgamation of the worst cases
For capacity plots, see IMCA M140. See also DNVGL-ST-O111.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e--Guidance note:
For worst single failure concept, see DNVGL-RU-SHIP Pt.6 Ch.3Navigation, manoeuvring and position keeping, and in IMO MSC/
circ. 645 or MSC 1./Circ.1580 Guideline for Vessels and Units with Dynamic Positioning (DP).
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10.4.5.4 For critical operations monitoring/displaying of actual DP capacity for actual weather conditions at
site are recommended.
Guidance note:
Equipment classes 2 and 3 has a software function, normally known as consequence analysis, which continuously verifies that
the vessel will remain in position even if the worst case failure occurs. This analysis should verify that the thrusters remaining in
operation after the worst case failure can generate the same resultant thruster force and moment as required before the failure.
The consequence analysis should provide an alarm if the occurrence of a worst case failure would lead to a loss of position due to
insufficient thrust for the prevailing environmental conditions. For operations which will take a long time to safely terminate, the
consequence analysis should include a function which simulates the thrust and power remaining after the worse case failure, based
on manual input of weather trend.
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10.4.5.5 Due consideration should be given to the reference systems limitations regards reliability,
accessibility and quality.
10.4.5.6 The DP operators shall be familiar with the vessel specific FMEA as well as the contingency plans for
the operation in question.
10.4.5.7 Key elements of the contingency planning measures should be located in the vicinity of the DP
operator station, so that situation specific required actions are immediately available to the DP operator.
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10.4.5.8 DP operation station and tensioner system operation station should be located in the vicinity
of each other ensuring close communication between the operators and availability/monitoring of vital
information.
10.4.6 Cranes and lifting equipment
10.4.6.1 Cranes and lifting equipment shall meet applicable statutory requirements. Certificates for the
equipment, valid for the operations and conditions under which they will be used, shall be available on board
for review.
10.4.7 Layvessel arrangement, laying equipment and instrumentation
10.4.7.1 The tensioning system shall operate in a fail-safe mode and shall have adequate pulling force,
holding force, braking capacity and squeeze pressure to maintain the pipe under controlled tension. The
forces applied shall be controlled such that no detrimental damage to the pipeline or coating will occur.
10.4.7.2 The installation vessel tensioning system arrangement shall therefore be such that:
— the tensioning system capacity shall have sufficient redundancy to allow failure of individual components
— in case of failure in the tensioning system, the pipeline installation shall not re-start before the system has
been repaired or have enough redundancy to allow for additional failures.
10.4.7.3 The pipe joints, stalks and pipeline shall be sufficiently supported by rollers, tracks or guides that
allow the pipe to move axially. Supports shall prevent damage to coating, field joint coatings, anodes and inline assemblies, and rollers shall move freely. The vertical and horizontal adjustment of the supports shall
ensure a smooth transition from the vessel onto the stinger, ramp or lay tower, to maintain the loading on the
pipeline within the specified limits. The support configuration shall be related to a clear and easily identifiable
datum.
10.4.7.4 The abandonment and recovery system (A&R) should be able to abandon the pipeline safely if
waterfilled. In case the recovery system is incapable of recovering the pipeline, alternative methods should
be available.
10.4.7.5 A sufficient amount of instrumentation and measuring devices shall be installed to ensure that
monitoring of essential equipment and continuous digital storage of all relevant parameters required for
configuration control and control of the operating limit conditions can be performed.
The following minimum instrumentation and monitoring is required:
Tensioning system:
— actual tension, tension settings and variance to set point
— squeeze pressure.
Stinger, ramp:
—
—
—
—
pipeline and A&R wire position with respect to the last roller or guide
roller reaction loads on the roller introducing the stinger curvature
roller reaction loads (vertical and horizontal), as a minimum for stinger tip
stinger and ramp configuration.
Guidance note:
Pipeline and wire position with respect to the last roller or guide may be monitored using underwater camera(s), sonar, ROV or
diver.
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Lay configuration:
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— lay parameter monitoring and recording as applicable to the installation method (see [10.6.1.11]).
Touch down monitoring:
— appropriate systems for touch down monitoring capable of operating under the expected weather
conditions.
Buckle detection:
— appropriate instrumentation and monitoring system for the applied buckle detection method
— pulling wire tension and length recorder in case buckle detector is chosen as buckle detection method.
Winches:
— abandonment and recovery system shall be equipped with wire tension and length recorder
— anchor winches shall meet the requirements given in [10.4.4].
Vessel:
—
—
—
—
—
—
vessel position
vessel movements such as roll, pitch, sway, heave
water depth
vessel draft and trim
wind strength and direction
direct or indirect indication of sagbend curvature and strain.
Vessels used for installation by towing:
— measuring equipment that continuously displays and records the towing speed and tensions
— measuring equipment that continuously displays and monitors the depth of the pipestring and its distance
from the seabed
— measuring equipment that continuously display the position of any ballast valves. The flow rates during
any ballasting and de-ballasting shall be displayed
— atrain gauges to monitor the stresses in the pipestring during tow and installation shall be considered.
10.4.7.6 All measuring equipment shall be calibrated and adequate documentation of calibration shall be
available onboard the vessel prior to start of work and during the whole operation. All measuring equipment
used shall be provided with an adequate amount of spares to ensure uninterrupted operation.
10.4.7.7 Direct reading and processing of stored records from all required essential instrumentation and
measuring devices, shall be possible at the vessels bridge.
10.4.7.8 Correlation of recorded data and pipe identifications numbers shall be possible.
10.4.7.9 The function of essential measuring devices shall be verified at regular intervals.
10.4.7.10 Other measuring and recording systems or equipment shall be required if they are essential for
the installation operation.
10.4.8 Mobilization
10.4.8.1 All personnel shall be familiarized with the operation to be performed. More detailed familiarization
shall be performed for personnel specific work tasks.
10.4.8.2 Personnel involved in critical operations should participate in a risk assessment for the specific
operation. Personnel involved in critical operations shall participate in a safe job analysis or toolbox talk
ensuring that an understanding of the involved risk related to the operation is understood.
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10.4.8.3 Equipment needed for the operation shall be defined in and mobilised according to the mobilisation
manual.
10.4.8.4 Stinger, ramp or lay tower shall be adjusted to the correct configuration to ensure a smooth
transition from the vessel to the outboard stinger, ramp or lay tower end, and to maintain the loading on the
pipeline within the specified limits. The pipeline support geometry shall be verified prior to laying, and the
accepted height and spacing of supports shall be permanently marked or otherwise indicated. If the stinger,
ramp or lay tower can be adjusted during laying operations, it shall be possible to determine the position and
configuration by reference to position markings or indicators.
10.4.8.5 Trim, tilt and ballasting shall also be verified to be according to procedures prior to laying.
10.4.8.6 Procedures for safe lifting operations shall be in place.
10.4.8.7 All pipes, anodes, consumables, equipment etc. shall be seafastened within the environmental
limits expected for the area of the operation.
10.4.9 Qualification of vessel and equipment
10.4.9.1 Vessel and equipment shall be qualified to do installation work within the specified operating limits.
Re-qualification is required if significant modification or alternation to the vessel, equipment or software has
been made.
10.4.9.2 Qualification shall be done according to a qualification plan based on a systematic review of the
specified operating limits for the vessel and all equipment.
10.4.9.3 Qualification shall be done based on a combination of desktop review, analyses, HAZID/HAZOP,
FMECA, simulation tests and test laying.
10.4.9.4 Combined positioning system/tensioning system tests shall be done by simulating pipeline pull,
tensioning system failures and redundancy tests during pull.
10.4.10 General calibration and testing
10.4.10.1 Essential equipment shall be calibrated against a certified load cell. If essential components for
the equipment such as load cells, amplifiers or software are replaced or modified the equipment shall be
tested and re-calibrated. Indications of equipment out of calibration should trigger a re-calibration.
Guidance note:
Typical essential equipment can be, but are not limited to, tensioners, clamps, reel, winches, cranes, lifting equipment, conveyor
system, bevelling machines, internal line-up clamp, field joint coating system, positioning systems.
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10.4.10.2 The certified load cell used for calibration shall have a certificate from a recognised certification
body. The certificate for the load cell used for calibration should not be older than 6 months.
Guidance note:
A recognised certification body will have a competent laboratory that can ensure traceability and adequate procedures. See ISO/
IEC 17025.
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10.4.10.3 Testing and calibration shall be done according to the test procedures. Test procedures shall be
subject to agreement.
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10.4.10.4 The test procedures shall provide documented acceptance criteria for the testing and calibration.
10.4.10.5 The acceptance criteria shall be evaluated and set according to the pipeline integrity. Any
deviation from the correct value shall be accounted for.
10.4.10.6 Calibration and testing should be performed and planned such that it can be witnessed in
agreement with operator.
10.4.10.7 Equipment should be tested and calibrated to the maximum equipment capacity or alternatively
up to maximum expected dynamic or accidental loads + 50%, whichever is less.
10.4.10.8 During testing and calibration the complete load range should be covered. For linear trends at
least five load steps should be applied up to maximum expected dynamic loads, more steps are required
when testing to maximum capacity. Non-linear trends require higher numbers of load steps. Cyclic loading
should be considered.
Guidance note:
Loss of main power and loss of signal should be tested by removing fuses or cables.
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10.4.11 Calibration and testing frequency
10.4.11.1 The calibration and testing of essential equipment should as a minimum be performed for each
project minimum once per year. the testing shall include:.
— Calibration checks.
— Tensioner system Review test. This includes test combinations of tensioners, clamps and reel, and testing
of single tensioner failure when running two or more tensioners, test redundancy of single tensioners, fail
safe actions, loss of main power and loss of signal.
— Pull test of the tensioning and pipe holding system to verify sufficient squeeze pressure and friction.
— Abandonment and recovery system test (fail safe actions, loss of main power and loss of signal).
— In-field dynamic positioning system test.
— Fail safe testing to max expected level of tension for the project.
— Buckle detection system, stinger control and monitoring devices including roller load cells.
10.4.11.2 For each specific project, the following shall be documented :
— Test results for the above testing.
— Calibration records of critical/essential equipment, including welding machines and automated NDT
equipment.
— Maintenance records for critical/essential equipment, including welding machines and automated NDT
equipment.
— Maintenance/calibration records of critical/essential equipment on support vessels.
—
10.4.11.3 Subject to agreement,testing and calibration for one project may be sufficient for similar project.
If testing is performed with a different set up (e.g. different clamps or pads or pipe diameter) re-testing
should be performed.
10.4.11.4 Re-testing should be performed in case equipment is maintained. In case re-testing is not
performed this shall be based upon an evaluation which shall be documented.
10.4.11.5 Re-testing shall be performed in case equipment is changed or modified.
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10.5 Welding and non-destructive testing
10.5.1 General
10.5.1.1 Requirements for welding processes, welding procedure qualification, execution of welding and
welding personnel are given in App.C.
10.5.1.2 Requirements for mechanical and corrosion testing for qualification of welding procedures are given
in App.B.
10.5.1.3 Requirements for methods, equipment, procedures, acceptance criteria and the qualification and
certification of personnel for visual examination and non-destructive testing (NDT) are given in App.D.
Selection of non-destructive methods shall consider the requirements in [D.1.4].
10.5.1.4 Requirements to automated ultrasonic testing (AUT) are given in App.E.
10.5.2 Welding
10.5.2.1 Pipes shall be bevelled to the correct configuration, checked to be within tolerance, and inspected
for damage. Internal line-up clamps should be used. Acceptable alignment, root gap and staggering of
longitudinal welds shall be confirmed prior to welding.
10.5.2.2 A weld repair analysis should be performed. Bending and tensile stresses shall be considered. The
analysis shall determine the maximum excavation length and depth combinations that may be performed,
taking into account all stresses acting at the area of the repair. The analysis shall be performed in accordance
with [5.4.8]. The analysis shall consider the reduction of yield and tensile strength in the material due
to the heat input from defect excavation, preheating, and welding and also dynamic amplification due to
weather conditions and reduced stiffness effect at field joints. Elevated temperature tensile testing should be
performed.
10.5.2.3 In case multiple welding stations on the installation vessel, the root and the first filler pass shall, as
a minimum, be completed at the first welding station before moving the pipe. Moving the pipe at an earlier
stage may be permitted if an analysis is performed showing that this can be performed without any risk of
introducing defects in the deposited weld material. This analysis shall consider the maximum misalignment
allowed, the height of the deposited weld metal, the possible presence of flaws, support conditions for the
pipe and any dynamic effects.
10.5.2.4 For production testing, see [C.7.5.25] to [C.7.5.31].
10.5.3 Non-destructive testing
10.5.3.1 The extent of NDT for installation girth welds shall be 100% ultrasonic or radiographic testing.
Radiographic testing shall be supplemented with ultrasonic testing in order to enhance the probability of
detection and/or characterisation/sizing of defects.
10.5.3.2 For wall thickness > 25 mm and for mechanized welds with weld bevel angles >6°, automated
ultrasonic testing shall be used.
10.5.3.3 Automated ultrasonic testing (AUT) shall be used in the following cases:
— whenever sizing of flaw height and/or determination of the flaw depth is required (see [5.4.8]).
— 100% lamination checks of a 50 mm wide band at ends of cut pipe.
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Exception to this requirement may be given for wall thickness < 8 mm provided that it can be technically
justified that alternative NDT processes provide sufficient inspection performance for the expected
imperfections for the applied welding procedure, see [D.2.10.11].
10.5.3.4 When radiographic testing is the primary NDT method UT or AUT shall be used in the following
cases:
— For the first 10 welds for welding processes with high potential for non-fusion type defects, when starting
installation or when resuming production after suspension of welding
— to supplement radiographic testing for unfavourable groove configurations
— for wall thickness above 25 mm:
— to provide additional random local spot checks during installation
— to supplement radiographic testing to aid in characterising and sizing of ambiguous indications.
10.5.3.5 If ultrasonic testing reveals defects not discovered by radiography, the extent of ultrasonic testing
shall be 100% for the next 10 welds. If the results of this extended testing are unsatisfactory, the welding
shall be suspended until the causes of the defects have been established and rectified.
10.5.3.6 For Golden Welds (critical welds e.g. tie-in welds that will not be subject to pressure testing, etc.)
100% ultrasonic testing, 100% radiographic testing, and 100% magnetic particle testing or 100% liquid
penetrant testing of non- ferromagnetic materials shall be performed. If the ultrasonic testing is performed
as automated ultrasonic testing, see App.E, the radiographic testing may be omitted subject to agreement.
10.5.3.7 Magnetic particle testing or liquid penetrant testing of non-ferromagnetic materials shall be
performed to verify complete removal of defects before commencing weld repairs, and for 100% lamination
checks at re-bevelled ends of cut pipe.
10.5.3.8 Visual Examination shall include:
— 100% examination of completed welds for surface flaws, shape and dimensions
— 100% examination of the visible pipe surface, prior to field joint coating.
10.6 Pipeline installation
10.6.1 General
10.6.1.1 The requirements of this subsection are generally applicable to pipeline installation, regardless
of installation method. Additional requirements pertaining to specific installation methods are given in the
following subsections.
10.6.1.2 This section addresses the main installation methods. Other installation methods may be suitable in
special cases. A thorough study shall be performed to establish the feasibility of the installation method and
the loads imposed during installation. Such methods are subject to agreement in each case.
10.6.1.3 Interfaces shall be established with other parties that may be affected by the operations or may
affect the operation. The responsibilities of all parties and lines of communication shall be established.
10.6.1.4 Handling and storage of pipes and materials on supply and laying vessels shall ensure that damage
to personnel, pipe, coatings, assemblies and accessories are avoided. Slings and other equipment used shall
be designed to prevent damage of product. Storage of pipes, in-line assemblies and other accessories shall
be seafastended to withstand design loads. All material shipped for installation shall be recorded.
10.6.1.5 All material shall be inspected for damage, quantity and identification upon arrival. Damaged items
shall be quarantined, repaired or clearly marked and returned onshore.
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10.6.1.6 Pipes and in-line assemblies shall be inspected for loose material, debris and other contamination
and cleaned internally before being added to the line. The cleaning method shall not cause damage to any
internal coating.
10.6.1.7 A pipe tracking system shall be used to maintain records of weld numbers, pipe numbers, NDT, pipe
lengths, cumulative length, anode installation, field joints, in-line assemblies and repair numbers. The system
shall be capable of detecting duplicate records.
10.6.1.8 The individual pipes of the pipeline shall be permanent marked in accordance with the established
pipe tracking system. The marking shall be suitable for reading by ROV. Means of monitoring possible pipeline
rotation may be applied. If damaged pipes are replaced, any sequential marking shall be maintained.
10.6.1.9 In-line assemblies shall be handled and stored to avoid damage prior to joining to the line, and
shall further be handled such that damage is avoided through tensioning system, pipe supports/rollers or
ramp, whichever is relevant. Any pipeline rotation shall be controlled.
10.6.1.10 Any applied field joint coating shall meet the requirements in Sec.9.
10.6.1.11 The lay configuration and loads shall be controlled in order to ensure that these are within
established design parameters during installation. The configuration and loads may be controlled by
various means, and these shall be clearly described including allowable ranges for the specific installation.
Redundancy is required.
Guidance note:
The lay configuration may typically be controlled by tension, stinger tip clearance and lay back distance/touch down monitoring.
Depending on the installation vessel and pipeline, the preferred methods may alter.
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10.6.1.12 Pipelay touch down monitoring shall be performed for critical operations and critical sections
representing a risk for the pipeline or for existing infrastructure. Critical operations and critical sections are
project specific, but will typically be initiation, laying of curves, narrow lay corridor, crossings, laying towards
counteracts, boulder areas and lay down.
10.6.1.13 Pipelay in congested areas, in the vicinity of existing installations and at pipeline and cable
crossings, shall be carried out using positioning systems with required accuracy. Measures shall be taken to
avoid damage to existing infrastructure. ROV should be used to continuously monitor such operations. ROVs
shall be capable of operating under the seastates expected for the operation in question.
10.6.1.14 The pipeline shall be installed within the lay corridor. Deviations to the lay corridor shall be
checked and verified or corrected before pipelaying continues.
10.6.1.15 Where a buckle detector is used, the buckle detector load chart shall be monitored. The buckle
detector shall be retrieved and inspected if there is reason to believe that buckling can have occurred. If the
inspection shows indications of buckling or water ingress, the situation shall be investigated and remedial
action performed.
10.6.1.16 The position of pipeline including start up and lay-down shall be verified as within their respective
target areas prior to departure of the lay vessel from site.
10.6.1.17 Prior to abandonment of the pipeline, all internal equipment except the buckle detector should be
removed. All welds, including the abandonment and recovery head welds, shall be filled to a level that the
pipe can be safely abandoned on and retrieved from the seabed, and shall be clearly defined in advance.
10.6.1.18 During abandonment, winch tension and cable lengths shall be monitored and the values shall
be within the specified range during the operation. The connection at the end of the wire shall be easily
recoverable independently of waves and current conditions.
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10.6.1.19 After abandonment and prior to recovery the pipeline shall be surveyed over a length away from
the abandonment and recovery head, sufficient to ensure that no damage has occurred.
10.6.1.20 Diving and underwater operations shall be performed in accordance with agreed procedures
covering applicable requirements.
10.6.1.21 In the event of buckling a survey of the pipeline shall be performed before repair to establish the
extent of damage and feasibility of the repair procedure. After completion of the repair, a survey shall be
performed of the pipeline over a length sufficient to ensure that no further damage has occurred.
10.6.1.22 If loss or major damage to weight and corrosion coating or anodes and their cables/connectors
are observed, repair shall be performed and inspected according to established procedures.
10.6.1.23 For temporary storage and transportation of linepipe, see [8.6.4].
10.6.1.24 Initiation of pipeline installation shall be performed using adequate start-up piles or anchors to
ensure safe operations.
10.6.1.25 Lay down of the pipeline should be performed such that the pipeline is inside the lay corridor and
with the desired approach angle.
10.6.2 Additional requirements for installation method S-lay
10.6.2.1 The stinger and rollers shall be positioned to avoid exceeding any limit state for the pipeline, and to
avoid damage to anodes or other attachments.
10.6.3 Additional requirements for installation method J-lay
10.6.3.1 The consequences in case losing internal welding clamp inside pipeline shall be established and
agreed.
10.6.4 Additional requirements for installation methods introducing
significant plastic strains
10.6.4.1 Additional requirements of this subsection are applicable to pipeline installation by methods which
give total single event nominal strain > 1.0% or accumulated nominal plastic strain > 2.0%.
10.6.4.2 Pipelines used for such installation methods shall meet the supplementary requirement, pipe for
plastic deformation (P), see [7.9.3].
10.6.4.3 Adequate support of the pipestring shall be provided when loading the reel. Sufficient tension shall
be applied during reeling in order to ensure that the successive layers on the reel are sufficiently tightly
packed to prevent slippage between the layers, and to control the curvature. Tension shall be monitored.
Adequate measures shall be taken to protect the coating during reeling. Vessel motion shall be controlled and
within acceptable limits during onshore tie-in weld between stalks.
10.6.4.4 The curvature of the pipe, peaking and sagging, between the point of departure from the reel and
entry into the straighteners shall not exceed the maximum values assumed in design and included in the
fracture assessment of the girth welds as per [5.4.8] and validated in the material testing of the girth welded
pipes.
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10.6.4.5 Anodes should be installed after the pipe has passed through the straightener and tensioner. The
electrical connection between anodes and pipe shall meet the specified requirements and shall be verified at
regular intervals, see Sec.9.
10.6.5 Towing
10.6.5.1 Tows may be performed as:
— surface or near-surface tows, with the pipestring supported by surface buoys
— mid-depth tows, where the pipestring is towed well clear away from the seabed
— bottom tows, where the pipestring is towed in contact with, or close to, the seabed.
10.6.5.2 For surface tows, all aspects pertaining to the tow are subject to agreement in each case.
10.6.5.3 For bottom or near bottom tows, the pipeline route shall be surveyed prior to the tow and the
route shall avoid rough seabed, boulders, rock outcrops and other obstacles that may cause damage to the
pipeline, coating or anodes during the tow and installation. During bottom and near bottom tows, adequate
monitoring with ROVs and of the pipeline position at critical phases is required. Satisfactory abrasion
resistance of the pipeline coating shall be demonstrated. All aspects pertaining to bottom tows are subject to
agreement in each case.
10.6.5.4 Launching of pipestrings shall be performed such that the pipestring is safe from damage and
damage to the coating and anodes are avoided. If pipestrings are moored inshore awaiting the tow, adequate
precautions shall be taken to avoid marine growth influencing pipestring buoyancy, weight and drag.
10.6.5.5 Notification of the tow shall be given to the relevant authorities, operators of subsea installations
crossed by the towing route and users of the sea.
10.6.5.6 During the tow a standby vessel shall be present to prevent interference with the tow by third party
vessels.
10.6.5.7 Tension in the towing line and the towing depth shall be kept within the specified limits during the
tow. If required, ballasting or de-ballasting shall be performed to adjust the towing depth to the specified
values.
10.6.5.8 Installation shall be performed by careful ballasting and de-ballasting. Care shall be exercised to
prevent over-stressing of the pipestring. The use of drag chains during the installation is recommended. The
installation operation shall be monitored by ROV.
10.6.6 Shore pull
10.6.6.1 The requirements of this subsection are applicable to the execution, inspection and testing of shore
pull when pipestrings are pulled either from a vessel onto the shore, or vice versa.
10.6.6.2 Detailed requirements for the execution, inspection and testing of shore pull shall be specified,
considering the nature of the particular installation site.
10.6.6.3 Cables, pulling heads and other equipment shall be dimensioned for the forces to be applied,
including any overloading, friction and dynamic effects that may occur.
10.6.6.4 Measuring devices shall be used to control the integrity of the pipeline during execution of the
shore pull. Continuous monitoring of the cable tension and pulling force shall be applied, and these shall be
within allowable limits. Monitoring with ROVs may be needed.
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10.6.6.5 The winches shall be equipped with wire tension and length indicators and recorders. All measuring
equipment shall be calibrated, and an adequate amount of spares to ensure uninterrupted operation shall be
provided.
10.6.6.6 It shall be documented that ROVs are able to operate under the seastate expected for the operation
in question. The ROVs shall, if used, be equipped as found necessary to perform the work in a safely manner
and controlled manner.
10.6.6.7 Satisfactory abrasion resistance of the pipeline coating shall be demonstrated for the installation
conditions.
10.6.6.8 Installation of the pulling head shall be made in a manner that does not compromise the integrity
of the pipeline and provides a secure connection.
10.6.6.9 Buoyancy aids may be used as a mean to keep pulling tension within allowable limits.
10.6.6.10 During the operation, continuous monitoring of cable tension and pulling force shall be performed.
Monitoring with ROVs may be needed.
10.6.7 Buckle detection
10.6.7.1 The consequences of buckles shall be evaluated as part of the HAZID/HAZOP (see [5.1.3] and
[10.1.3]), and in agreement between operator and contractor.
Guidance note:
The assessment of the consequences will typically include recovery (e.g. in case wet buckle), availability of repair methods and
time frames for repair. The consequences of a buckle not detected during installation will normally require inline repair methods
which can have large schedule and cost impact. Detection of buckles during installation will have less schedule and cost impact.
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10.6.7.2 Mitigation measures for consequences of buckles shall be based upon the outcome of the HAZID/
HAZOP. Buckle detection in accordance with Table 10-1 should be used.
Guidance note:
Buckle detection may be ensured by a buckle detector or equipment providing similar degree of detection.
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The buckle detector (or equipment providing same degree of detect ability) shall be positioned in such a way
that critical areas are monitored (normally a distance after the touch down point). If a buckle detector is
used the diameter of the disc shall be chosen with regard to the pipeline diameter and tolerances on ovality,
wall thickness, misalignment and internal weld bead.
Table 10-1 Buckle detection
Safety class
Buckle detection requirement
Additional requirements and consequence of buckle
Low
Buckle detection continuously
during laying
Medium
Buckle detection not required
Improved control of parameters controlling the lay configuration
required (e.g. lay tension, touch down point monitoring etc.) and
consequence of possible buckle is found acceptable.
High
Buckle detection not required
Improved control of parameters controlling the lay configuration
required (e.g. lay tension, touch down point monitoring etc.) and
consequence of possible buckle is found unacceptable.
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10.6.7.3 In case the parameters controlling the lay configuration indicates that unacceptable configuration is
experienced or other indications of buckle events, an inspection shall be performed. The inspection shall be
carried out such that it can be confirmed that buckling has not occurred.
10.6.8 Operating limit conditions
10.6.8.1 The installation operation shall be classified as weather restricted operation or unrestricted
operation, see [4.3.6]. An unrestricted operation is a temporary condition or permanent condition.
10.6.8.2 For weather restricted operations, operating limit conditions shall be established and agreed.
10.6.8.3 The operating limit conditions shall be based on detailed load effect analyses, vessel station
keeping capability, FMEA analysis or HAZOP study data, and shall refer to objective, critical values indicated
by measuring devices. The operating limit conditions shall be referred to in the procedure for configuration
control. Continuous monitoring and recording of the measuring devices required for control of the operating
limit conditions shall be performed during all phases of installation activities.
10.6.8.4 If a systematic deviation between the monitored response and predicted response from a seastate
is found this should be accounted for.
10.6.8.5 Start of weather restricted operations is conditional to an acceptable weather forecast. Uncertainty
in the weather forecast shall be considered.
10.6.8.6 For weather restricted operations, planning of operation shall be based on an operational reference
period. Further, the operational criteria shall account for uncertainties in both weather forecasts and
monitoring of environmental conditions. Regular weather forecasts from a recognised meteorological centre
shall be available onboard the lay vessel, and shall be supplemented by historical environmental data. See
DNVGL-ST-N001.
10.6.8.7 If the critical values are about to be exceeded, preparations for lay-down shall commence. If the
critical condition is weather dependent only, and if weather forecasts indicate that the weather condition will
subside, the lay-down may be postponed subject to agreement.
10.6.8.8 Decision to recover the pipeline shall be based on comparison of the actual seastate with the
limiting seastate, together with weather forecasts.
10.6.9 Spools and other in-line assemblies installed separately from
pipeline
10.6.9.1 In-line assemblies to be installed separately from the pipeline shall be sufficiently seafastened to
ensure no damage is occurring during transportation.
10.6.9.2 For operating limit conditions for such installations, see [10.6.8].
10.6.9.3 Lifting operations above existing infrastructure on the seabed should be avoided. Safe lifting and
installation zones shall be defined.
10.6.9.4 In-line assemblies to be installed separately from pipeline shall be installed inside the pre-defined
target areas and also within the pre-defined heading limitations, in all planes.
10.6.9.5 Recommended practice for modelling and analysis of offshore lifting operations are given in DNVGLRP-N103.
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10.7 As-laid survey
10.7.1 General
10.7.1.1 An as-laid survey covering the complete submarine pipeline system shall be performed. This can
be done either by continuous touch down point monitoring during pipe laying or by a separate survey. In
case continuous touch-down monitoring is used, pipeline positioning shall be confirmed after completion of
pipeline installation.
Guidance note:
Continuous touch down monitoring may not identify possible horizontal curve pull-out, and therefore positioning of pipeline have to
confirmed after completion of installation activities.
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10.7.1.2 Requirements to survey vessel, survey equipment, the extent of survey, tolerances for the aslaid pipeline, and the maximum acceptable length and gap height of free spans at various locations shall be
defined.
10.7.2 Survey requirements
10.7.2.1 The as-laid survey should include the following:
— position and depth of the pipeline, including location of in-line assemblies, anchoring and protective
structures, tie-ins, supports etc.
— identification and quantification of any free spans with length and gap height
— determination of position of start-up and lay down heads
— determination of the presence of debris
— video documentation of the submarine pipeline system.
Guidance note:
Where video coverage cannot be obtained due to environmental reasons, alternate methodologies should be utilised to ensure
100% coverage.
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10.7.2.2 The pipeline horizontal position and seabed and pipeline vertical profile/seabed shall as a minimum
be reported at intervals defined by the requirement for as-laid pipeline analyses. The data shall be reported
in an agreed format.
10.7.3 Survey of corrosion protection systems
10.7.3.1 In the case of damage to coating or anodes, consequences for long-term performance shall be
considered. Potential measurements at any bare surfaces should be carried out to confirm adequate corrosion
protection. Corrective actions may include retrofitting of anodes and coating repairs. Satisfactory level of
corrosion protection shall be documented after the corrective action has been performed.
10.7.3.2 Impressed current cathodic corrosion protection systems shall be inspected, including cables,
conduits, anodes and rectifiers. Readings from the corrosion monitoring system shall be verified by
independent potential measurements, and adequate electrical insulation from other installations (if
applicable) shall be confirmed installed and commissioned according to ISO 15589-2.
If the required protection level is not attained, the causes shall be identified and adequate corrective actions
performed. Satisfactory performance shall be documented after the corrective action.
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10.8 Post-lay intervention (seabed intervention and pipeline
protection)
10.8.1 General
10.8.1.1 The requirements of this subsection are applicable to free span rectification and the protection of
pipelines, e.g. by trenching and backfilling, gravel dumping, grout bags, concrete mattresses etc.
10.8.1.2 A specific survey of the work area should be performed, or supplementing, the as-laid survey if:
—
—
—
—
—
significant time has elapsed since the as-laid survey
a change in seabed conditions is likely
marine activity is present in the area
new installations are present in the area
the as-laid survey does not provide sufficient information.
10.8.1.3 The survey of the work area should as a minimum include:
—
—
—
—
a video inspection of the pipeline to identify any areas of damage to pipeline, coating and anodes
cross profiles of the pipeline and adjacent seabed at regular intervals
depth profiles along the pipeline and the seabed at both sides of the pipeline
any existing subsea installations.
The undisturbed seabed level shall be included in the cross profiles.
10.8.2 Span rectification and protection specification
10.8.2.1 The requirements applicable to the specific methods of span rectification and protection regarding
execution, monitoring and acceptance criteria shall be documented. Requirements for vessels, survey
equipment etc. shall be addressed in the installation and testing specifications and procedures. The extent of
procedures to be prepared and qualified shall be specified.
10.8.3 Free span rectification
10.8.3.1 Free span rectification is required for all spans exceeding the specified acceptable length or height
for the specific location. Rectification of other spans shall be considered if scour or seabed settlement could
enlarge the span length and gap height above maximum acceptable dimensions before the first planned
inspection of the pipeline.
10.8.3.2 Adequate rectification of free spans shall be documented by a video survey. All rectified free spans
shall be identified and the length, gap and height shall be within the requirements.
10.8.4 Trenching
10.8.4.1 Where trench excavation is performed after pipelaying, the trenching equipment shall be of a type
that does not place significant loads on the pipeline and minimises the possibility of damage to the pipeline.
10.8.4.2 Trenching equipment shall be equipped with sufficient instrumentation to ensure that damage and
excessive pipe contact is avoided.
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10.8.4.3 Special care shall be taken during trenching operations of piggy back/bundle pipelines, so that
strapping arrangements will not be disturbed/damaged during trenching.
10.8.4.4 Trenching shall not damage or dismantle the anodes.
10.8.4.5 Where mechanical backfilling is required, it shall be carried out in a manner that minimises the
possibility of damage or disturbance to the pipeline.
10.8.4.6 It shall be ensured that the trenching method for the given pipeline submerged weight and soil
properties is adequate to avoid pipeline floatation during trenching and backfilling.
10.8.4.7 The trenching equipment monitoring system shall be calibrated and include:
— devices to measure depth of pipe
— a monitoring system and control system preventing horizontal loads on the pipeline or devices to measure
and record all vertical and horizontal forces imposed on the pipeline by trenching equipment, and devices
to measure the proximity of the trenching equipment to the pipeline, horizontally and vertically relative to
the pipeline
— underwater monitoring systems enabling the trenching equipment operator to view the pipeline and
seabed profile forward and aft of the trenching equipment
— measuring and recording devices for trenching equipment tow force
— devices monitoring pitch, roll, depth, height and speed of the trenching equipment.
10.8.4.8 Jet sleds shall have a control and monitoring system for the position of the jetting arms and the
overhead frame, horizontally and vertically relative to the pipeline. The location of the sled shall not be
controlled by the force between sled and pipeline. Devices indicating tension in the tow line and showing the
depth of the trench shall be installed.
10.8.4.9 An allowable range of values, indicated by the measuring devices of the trenching equipment, shall
be established. The possibility of damage to coating shall be considered. During trenching operations the
measuring devices shall be continuously monitored.
10.8.4.10 A post-trenching survey should be performed after the trenching in order to determine if the
required depth of trench and/or pipe has been achieved and if any remedial work is required.
10.8.5 Post-installation gravel installation
10.8.5.1 Material used for gravel installation shall meet the specified requirements for specific gravity,
composition and grading.
10.8.5.2 Gravel installation shall be performed in a continuous and controlled manner. Existing infrastructure
should not be disturbed or interfered with.
10.8.5.3 The gravel installation operation shall ensure rectification of all free spans to meet the specified
requirements. Scouring effects shall be considered.
10.8.5.4 If the fall pipe technique is used for gravel installation, minimum clearances shall be specified
such that the fall pipe cannot touch the pipeline or any other subsea installation or the seabed. Deployment
operations shall be performed well away from the pipeline or any other subsea installation. Before the fall
pipe is moved to the installation location, the clearance beneath the fall pipe shall be verified. The clearance
shall be continuously monitored during gravel installation.
10.8.5.5 The completed gravel installation shall leave a mound on the seabed with a smooth contour and
profile and a slope not steeper than specified.
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10.8.5.6 If the gravel installation is performed over cable and pipeline crossings, the gravel mound shall
provide the specified depth of cover over both the crossing and the crossed pipeline. During the gravel
installation operations inspections shall be performed with a sonar survey system or with video when visibility
is restored, to determine the completeness and adequacy of the installation.
10.8.5.7 Upon completion of the gravel installation, a survey shall be performed to confirm compliance with
the specified requirements. The survey shall include:
—
—
—
—
—
—
video of the pipeline length covered
cross profiles of the mound and adjacent undisturbed seabed at regular intervals
length profiles of the mound
confirmation that minimum required buried depth is achieved
confirmation that maximum burial depth is not exceeded
any existing installations and their vicinity in order to ensure that the installation(s) have not suffered
damage.
10.8.6 Grout bags and concrete mattresses
10.8.6.1 Concrete mattresses and grout bags shall meet the specification with regard to size, shape and
flexibility of the material, location of filling points, and the specific gravity, composition and grading of grout.
10.8.6.2 Placing of grout bags and concrete mattresses shall be performed in a controlled manner, such that
the bags or mattresses are placed as required. Restrictions on vessel movements during the operation shall
be given.
10.8.6.3 During the placing operations, inspections shall be performed with a ROV-mounted video camera to
determine the completeness and adequacy of the installation.
10.8.6.4 Upon completion of the placing operation, a survey shall be performed to confirm compliance with
the specified requirements. The survey shall as a minimum include:
— video of the completed work
— cross profiles of the placed bags or mattresses and adjacent undisturbed seabed at regular intervals
— length profiles of the placed bags or mattresses and the seabed at both sides of the area.
10.9 Tie-in
10.9.1 General
10.9.1.1 The requirements of this subsection are applicable to tie-in operations using welding or mechanical
connectors. The operations can be performed onboard a laying vessel (in which case welding is the preferred
method) or underwater.
10.9.1.2 Tie-in operations by means of hot or cold taps are subject to special consideration and agreement.
10.9.1.3 Operating limit conditions with regard to the seastate, current and vessel movements shall be
established. Uncertainty in weather forecast shall be considered.
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10.9.2 Tie-in operations above water
10.9.2.1 The position of the tie-in shall be verified prior to start of operations. A survey shall be performed
to establish that the location is free of obstructions and that the seabed conditions will permit the tie-in to be
performed as specified.
10.9.2.2 Lifting and lowering of the pipeline sections shall be analysed to determine the critical parameters
and operational criteria for the operation. Critical parameters/operational criteria shall be monitored
continuously.
10.9.2.3 Lifting arrangements and equipment shall be designed taking into account the critical parameters
and operational criteria for the operations.
10.9.2.4 The operation should be monitored to confirm correct configuration of the pipeline sections from
the seabed and onto the vessel.
10.9.2.5 The alignment and position of the tie-in ends shall be within the specified tolerances before
completing the tie-in.
10.9.2.6 Installation of mechanical connectors shall be performed in accordance with the manufacturer's
procedure. For flanged connections hydraulic bolt tension equipment shall be used. During all handling, lifting
and lowering into the final position, open flange faces shall be protected against mechanical damage.
10.9.2.7 A local leak test to an internal pressure not less than the local incidental pressure should be
performed for all mechanical connections after make-up. This local leak test is additional to the normal
system pressure test.
10.9.2.8 Corrosion protection of the tie-in area shall be performed and inspected in accordance with
accepted procedures.
10.9.2.9 After completion of the tie-in, a survey of the pipeline on both sides of the tie-in, and over a length
sufficient to ensure that no damage has occurred, should be performed
10.9.2.10 It shall be verified that the position of the tie-in is within the target area prior to departure of the
vessel from site. The pipeline stability shall be ensured and adequate protection of pipeline provided.
10.9.2.11 Requirements for dry welding are given in App.C.
10.9.3 Tie-in operations below water
10.9.3.1 In addition to the requirements in [10.9.2], the requirements below are valid for tie-in operations
involving underwater activities.
10.9.3.2 Diving and underwater operations shall be performed in accordance with agreed procedures for
normal and contingency situations covering applicable requirements.
10.9.3.3 Requirements for underwater hyperbaric dry welding are given in App.C.
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10.10 Pre-commissioning
10.10.1 General
10.10.1.1 All work on the submarine pipeline system, including crossings, trenching, gravel installation,
artificial backfill, subsea assemblies, riser installation, tie-in etc., should be completed before precommissioning activities commences.
10.10.1.2 Disposal of cleaning and test fluids shall be performed in a manner minimising danger to the
environment. Any disposal of fluids shall be in compliance with requirements from national authorities.
10.10.1.3 Requirements for equipment, the extent of testing and preparation for operation, performance
of tests and preparation for operation and associated acceptance criteria shall be defined. The extent of
procedures to be prepared and qualified shall be specified.
10.10.1.4 All operations and tests shall be performed in accordance with agreed procedures.
10.10.1.5 Recommended practice on pre-commissioning is given in DNVGL-RP-F115.
10.10.2 Waterfilling, cleaning and gauging
10.10.2.1 Cleaning and gauging may be combined with the initial flooding of the pipeline, be run as a
separate operation, or be combined with the weld sphere removal after completion of hyperbaric tie-in.
10.10.2.2 Appropriate measures shall be taken to ensure that any suspended and dissolved substances in
the fluid used for cleaning operation are compatible with the pipe material and internal coating (if applied),
and that deposits are not formed within the pipeline.
10.10.2.3 Filling of the submarine pipeline system with water should be performed in a controlled manner,
using water behind one or more pigs. The pig(s) shall be capable of providing a positive air/liquid interface.
Considerations shall be given to pre-filling valve body cavities with an inert liquid, unless the valves have
provision for pressure equalisation across the valve seats. All valves shall be fully open during line filling. A
pig tracking system and the use of back-pressure to control the travel speed of the pig shall be considered if
steep gradients occur along the pipeline route.
10.10.2.4 Water to be used for flooding should have a minimum quality corresponding to filtration of 50μm,
3
and suspended matters should not have an average content exceeding 20 g/m .
10.10.2.5 If water quality or the water source is unknown, water samples shall be analysed and suitable
actions shall be taken to remove and/or inhibit harmful substances.
10.10.2.6 If water is to remain in the pipeline for an extended period of time, consideration shall be given to
control of bacterial growth and internal corrosion by chemical treatment (see [6.4.3.2]).
10.10.2.7 Added corrosion inhibitors, any chemical additives like oxygen scavengers, biocides, dyes, etc.
shall be considered for possible harmful interactions selected to ensure full compatibility and their impact on
the environment during and after disposal of the test water shall be considered.
10.10.2.8 The submarine pipeline system shall be cleaned. The pipeline cleaning concept shall consider:
— protection of pipeline components and facilities (e.g. valves) from damage by cleaning fluids and pigs
— testing devices such as isolation spheres etc.
— removal of substances that may contaminate the product to be transported
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—
—
—
—
particles and residue from testing and mill scale
organisms and residue resulting from test fluids
chemical residue and gels
removal of metallic particles that may affect future inspection activities.
10.10.2.9 Acceptance criteria for cleaning shall be established and agreed.
10.10.2.10 The submarine pipeline system shall be gauged. The main purpose of gauging the submarine
pipeline system is to prove that it is unlikely that any damages, dent or buckle exists in the submarine
pipeline system, and to provide basis for future operational pigging activities. The purpose is further to
document that no excessive dent or ovalisation exceeding the requirements in [5.4.11] and [5.4.12] has
taken place. The preferred gauging is by an intelligent gauging tool (calliper pig). As an alternative a running
a pig with a metallic gauge plate with a diameter of 95% of the largest nominal inner diameter, or 97%
of the minimum inner diameter of the largest nominal inner diameter. In case a gauge plate cannot be
used due to internal restrictions (e.g. variations in diameter, valves, bends etc.) an intelligent gauging tool
(calliper pig) shall be used. When gauging is carried out with an intelligent tool the tolerances of the diameter
measurements should be less than 0.2 mm and the diameter readings should be made minimum each 10mm
along the entire pipeline length. The tool shall also be able to report locations of the readings.
Guidance note:
The minimum inner diameter including uncertainties can be established as:
Dmin,tot = Dmin(1-O0/2)-2tmax-2hbead
Where hbead also allows for possible misalignment.
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10.10.2.11 Cleaning and gauging train design including number and type of pigs, train velocity shall be
decided based upon need for chemical cleaning, type and length of pipeline, steep gradients along the
pipeline route, type of service, construction method, downstream process, potential cleaning and gauging
already performed (see [8.6.5.4] and [8.7.1.1]) or other aspects.
10.10.2.12 For cleaning operations where the acceptance criteria for cleaning are not fulfilled, a rerun of the
cleaning pig train should be performed.
10.10.2.13 If cleaning is performed on separate sections of the submarine pipeline system prior to tie-in,
a minimum of one cleaning pig should be run through the completed submarine pipeline system prior to, or
during, product filling.
10.10.2.14 On completing of all tie-ins, a calliper pig or gauge plate should be run through the submarine
pipeline system.
10.10.3 System pressure testing
10.10.3.1 A pipeline system pressure test shall be performed based upon the system test pressure
determined according to [5.2.2.2] unless the test is waived as allowed by [5.2.2.3].
10.10.3.2 The submarine pipeline system may be tested as separate sections provided that the tie-in welds
between sections fulfil the requirements in [10.5.3.6].
10.10.3.3 The pipeline section under test shall be isolated from other pipelines and facilities. Pressure
testing should not be performed against in-line valves, unless possible leakage and damage to the valve is
considered, and the valve is designed and tested for the pressure test condition. Blocking off or removal of
small-bore branches and instrument tappings, should be considered to avoid possible contamination.
10.10.3.4 Temporary testing equipment such as end closures, temporary pigtraps and manifolds, shall be
designed and constructed according to a recognised standards or recommended practices and with design
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pressure equal to the pipeline design pressure. Such items shall be individually pressure tested to at least the
same test pressure as the pipeline.
10.10.3.5 Instruments and test equipment used for the measurement of pressure, volume and temperature
shall be calibrated for accuracy, repeatability and sensitivity. All instruments and test equipment shall possess
valid calibration certificates, with traceability to reference standards within the 6 months preceding the test.
If the instruments and test equipment have been in frequent use, calibration specifically for the test should
be performed.
10.10.3.6 Gauges and recorders shall be checked for correct function immediately before each test. All test
equipment shall be located in a safe position outside the test boundary area.
10.10.3.7 The test pressure shall be measured using a dead weight tester or a high accuracy pressure
transducer, in addition to a high accuracy large diameter pressure gauge. Dead weight testers shall not be
used before a stable condition is confirmed, and shall not be used offshore when positioned on a vessel. If
a high accuracy pressure transducer is used, it shall have sensitivity that is better than 4 times the target
pressure drop, i.e. 0.05%. Time history of the test pressure shall be recorded.
10.10.3.8 The following requirements apply for instruments and test equipment:
— dead weight testers shall have a range of minimum 1.25 times the specified test pressure, and shall have
an accuracy better than ±0.1 bar and a sensitivity better than 0.05 bar
— the volume of water added or subtracted during a pressure test shall be measured with equipment having
accuracy better than ± 1.0% and sensitivity better than 0.1%
— temperature measuring instruments and recorders shall have an accuracy better than ±1.0°C, and a
sensitivity better than 0.1°C
— pressure recorders and temperature recorders shall be used to provide a graphical record of the pressure
test continuously for the total duration of the test.
10.10.3.9 A correlation that shows the effect of temperature changes on the test pressure where relevant,
shall be developed and accepted prior to starting the test. Temperature measuring devices, if used, shall
be positioned close to the pipeline, and the distance between the devices shall be based on temperature
gradients along the pipeline route.
10.10.3.10 The test medium should be water meeting the requirements given in [10.10.2].
10.10.3.11 The air content of the test water shall be assessed by constructing a plot of the pressure against
volume during the initial filling and pressurisation, until a definite linear relationship is apparent, see Figure
10-1. This should be done at 35% of test pressure, or at maximum 35 bar. The assessed air content should
not exceed 0.2% of the calculated total volume of the pipeline under test. If the limit is exceeded, it shall be
documented that the amount of air, not will influence the accuracy of the test significantly.
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Figure 10-1 Determination of volume of air
10.10.3.12 Pressurisation of the submarine pipeline system shall be performed as a controlled operation
with consideration for maximum allowable velocities in the inlet piping. The last 5% up to the test pressure
shall be raised at a reduced rate to ensure that the test pressure is not exceeded. Time should be allowed
for stabilisation before the test hold period begins, in particular when testing operation occurs directly post
flooding/flushing of the pipeline system. Stabilisation time shall be based on the filling water temperature
difference with ambient temperature and on the possible presence of thermal insulation.
10.10.3.13 Subject to agreement shorter pressure hold periods may be accepted for pipelines with test
3
volumes less than 5000 m . In these cases the principles of [8.7] should apply.
10.10.3.14 The pressure and temperatures where relevant, shall be continuously recorded during the
pressurisation, stabilisation and test hold periods.
10.10.3.15 Flanges, mechanical connectors etc. under pressure should be visually inspected for leaks during
the pressure test, either directly or by monitors.
10.10.3.16 The pressure test is acceptable if the submarine pipeline system is free from leaks, and the
pressure variation is within ± 0.2% of the test pressure.
A pressure variation up to an additional ±0.2% of the test pressure is normally acceptable if the total
variation (i.e. ± 0.4%) can be documented to be caused by:
— temperature fluctuations not accounted for or
— tide in case the pressure is measured at a fixed elevation (fixed platform on onshore)
— if pressure variations greater than ± 0.4% of the test pressure are observed, the holding period shall be
extended until a hold period with acceptable pressure variations has occurred.
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Guidance note:
Corresponding criteria for flexible pipes are often less stringent. For a pipeline system comprising both rigid pipeline and flexible
parts (e.g. flexible riser or flexible tail), an equivalent pressure variation criterion should be determined by weighing the criteria for
the different parts w.r.t. the volume of water that they contain during the system pressure test.
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10.10.3.17 De-pressurisation of the submarine pipeline system shall be performed as a controlled operation
with consideration for maximum allowable velocities in the pipeline and the discharge piping.
10.10.4 De-watering and drying
10.10.4.1 De-watering should be performed before introducing the product fluid into the pipeline. Drying
may be required in order to prevent an increase in the corrosion potential or hydrate formation, or if omission
of drying is deemed to have an adverse effect on the product transported.
10.10.4.2 In case the product fluid is introduced prior to de-watering the separation pig train between the
test medium and the fluid shall be qualified in order to avoid contact between the residual test water and the
product.
10.10.4.3 Selection of de-watering and drying methods and chemicals shall include consideration of any
effect on valve and seal materials, any internal coating and trapping of fluids in valve cavities, branch piping,
instruments etc.
10.10.5 Systems testing
10.10.5.1 Prior to fluid product filling, safety and monitoring systems shall be tested in accordance with
accepted procedures. This includes testing of:
—
—
—
—
—
corrosion monitoring systems
alarm and shutdown systems
safety systems such and pig trap interlocks, pressure protection systems etc.
pressure monitoring systems and other monitoring and control systems
operation of pipeline valves.
10.11 As-built survey
10.11.1 General
10.11.1.1 An as-built survey covering the complete submarine pipeline system shall be performed. The
as-built survey shall be performed after all work on the submarine pipeline system, including crossings,
trenching, gravel dumping, artificial back-fill, tie-in, riser installation, etc., are completed. The as-built survey
of the installed and completed pipeline system is performed to verify that the completed installation work
meets the specified requirements, and to document any deviations from the original design. The as-built
survey shall include the corrosion protection system where potential damage to the coating and sacrificial
anodes shall be documented.
10.11.1.2 The as-built survey should include the following in addition to the requirements for as-laid survey:
—
—
—
—
out of straightness measurements as applicable
depth of cover or trench depth as applicable
location of areas of damage to pipeline, coating and anodes
location of any areas with observed scour or erosion along pipeline and adjacent seabed
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— verification that the condition of weight coating (or anchoring systems that provide for on-bottom
stability) is in accordance with the specification
— description of wreckage, debris or other objects which may affect the cathodic protection system or
otherwise impair the pipeline
— video documentation of the submarine pipeline system.
Guidance note:
The survey accuracy should reflect the requirements related to lay corridor, size of lay down target boxes, restrictions in design
related to out of straightness (in particular for uneven seabed) or other aspects that may influence pipeline integrity.
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10.12 Documentation
10.12.1 General
10.12.1.1 The documentation of the offshore construction including testing of the submarine pipeline system
shall be as a minimum include that given in Sec.12.
10.13 Installation manual
10.13.1 Installation manual
10.13.1.1 Installation manual is defined as a document or collection of documents required for performing
the project specific installation work including normal operations and contingency handling/operations and
acceptance criteria. In case the installation manual is a collection of documents, a master document shall be
prepared.
Guidance note:
The installation manual is prepared in order to demonstrate that methods and equipment used by the contractor will meet specified
requirements, and that the results can be verified. The installation manual will hence include all factors that influence quality,
reliability and safety of the installation work, including normal and contingency situations, and will address all installation steps,
including examinations and check points. The manual will reflect the results of the risk management studies performed for the
installation and will state requirements for the parameters to be controlled and the allowable range of parameter variation during
the installation.
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10.13.1.2 The installation contractor shall prepare an installation manual. In case several contractors are
used, the installation manuals shall be harmonised. A master installation manual may be required
10.13.1.3 The installation manual shall be agreed between contractor and operator, and updated and revised
as found necessary.
10.13.1.4 The installation manual shall contain documentation of fulfilment of all requirements in this
section.
10.13.1.5 The installation manual shall include the following:
—
—
—
—
—
quality system manual
mobilisation manual
construction manual
health, safety and environment manual
emergency preparedness manual.
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10.13.1.6 The installation manual shall cover:
—
—
—
—
—
—
—
—
—
—
—
—
—
—
organization, communications and reporting
navigation and positioning, including anchors and anchor handling or dynamic positioning
installation procedures, see [10.13.2]
pre-commissioning procedures, see [10.13.3]
contingency procedures, see [10.13.4]
spread, including modifications and upgrading, if any
pipeline configuration monitoring, positioning and control activities, including recording and reporting
operating limit conditions imposed by environmental loads
installation analyses including fatigue forming the basis for the operating limit conditions
installation of in-line assemblies
operations in areas of particular concern
limitations imposed by structural strength in accordance with the design
qualification of personnel
essential variable including acceptable limits.
Guidance note:
Areas of particular concern may typically include shipping lanes, existing or future subsea installation, shore approach or crossings.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e--Guidance note:
For towing operations the installation manualtypically include a description of towing vessel(s) including capacities, equipment and
instrumentation.
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10.13.1.7 Essential variables and their acceptable limits shall be established for cases where variations in
manner of performance of an activity may give undesirable results. Essential variables shall as minimum be
established for:
— allowable variations in configuration control parameters where variations beyond established limits may
cause critical conditions during installation
— variations in equipment settings/performance that can cause or aggravate critical conditions
— changes in welding joint design and process parameters beyond that allowed in App.C
— changes in NDT method, NDT equipment and NDT equipment calibration beyond that allowed in App.D
and App.E
— weld repair lengths/depths in areas where the pipe is subject to bending moments/axial stress. The
maximum length/depth of excavation shall be determined by stress analyses
— field joint coating procedure
— operating limit conditions
— any other requirement due to the nature of the operations.
10.13.1.8 The validity of the installation manual is limited to the lay-vessel/spread where the qualification
was performed and to the pipeline or section of pipeline in question.
10.13.2 Installation procedures
10.13.2.1 The installation contractor shall prepare installation procedures. In case several contractors are
used, the installation procedures shall be harmonised.
10.13.2.2 The installation procedures shall be agreed between contractor and operator, and updated and
revised as found necessary.
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10.13.2.3 The installation procedures shall describe the following:
—
—
—
—
—
purpose and scope of the activity
responsibilities
materials, equipment and documents to be used
how the activity is performed in order to meet specified requirements and acceptance criteria
how the activity is controlled and documented.
10.13.2.4 The installation procedures shall cover all requirements in this section.
10.13.2.5 The following procedures shall be established:
—
—
—
—
—
—
—
—
emergency procedures
mobilisation procedures
operational procedures covering all phases of installation work
verification procedures
welding and NDT equipment and procedures including repair
pipe and equipment handling and lifting, hauling, stacking and storage procedures
pipe tracking procedures
pre-commissioning and commissioning procedures.
Guidance note:
Operational procedures may typically include configuration and alignment control, anchor handling, field joint coating, tensioning
handling, ROV control, anode attachment, control of weight and buoyancy distribution, control of pipe rotations, installation of inline assemblies, loading and spooling pipe onto the reel, pipe straightening and underwater operations.
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10.13.3 Pre-commissioning procedures
10.13.3.1 The installation contractor shall prepare pre-commissioning procedures. In case several
contractors are used, the pre-commissioning procedures shall be harmonised.
10.13.3.2 The pre-commissioning procedures shall be agreed between contractor and operator, and updated
and revised as found necessary.
10.13.3.3 The pre-commissioning procedures shall be prepared for the pre-commissioning activities of
the submarine pipeline system, covering all testing activities that may be performed. The testing shall be
conducted to verify that the submarine pipeline system meet the requirements of this standard. The precommissioning procedures shall contain sufficient detail to enable full understanding of testing methods and
procedures, including acceptance criteria. It shall also provide references to relevant specifications, test plans
and engineering documents applicable for the submarine pipeline system.
10.13.3.4 The pre-commissioning procedures shall state the type and extent of verification, testing,
acceptance criteria, records, documentation and certification required for the components of the submarine
pipeline system. It shall also provide references to relevant specifications, test plans and engineering
documents applicable for the pipeline system.
10.13.4 Contingency procedures
10.13.4.1 The installation contractor shall prepare contingency procedures. In case several contractors are
used, the contingency procedures shall be harmonised.
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10.13.4.2 The contingency procedures shall be agreed between contractor and operator, and updated and
revised as found necessary. For installation methods introducing plastic strains restrictions to potential
contingency cyclic plastic loading shall be described.
10.13.4.3 Contingency procedures shall be prepared for all installation activities.
Guidance note:
Contingency procedures may typically include failure of dynamic positioning system, failure of anchors or anchor lines, coating
repair, anode repair, failure of tensioning system, ROV breakdown, breakdown of positioning system, weather conditions in excess
of operating limit conditions, third party marine activity and critical or emergency situations identified in FMEA or HAZOP studies.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
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SECTION 11 OPERATIONS AND ABANDONMENT
11.1 General
11.1.1 Objective
11.1.1.1 This section provides minimum requirements for the safe and reliable operation of submarine
pipeline systems for the whole service life with its main focus on the pipeline integrity management system
and the pipeline integrity management process.
11.1.1.2 Recommended practice for integrity management of submarine pipeline systems is given in DNVGLRP-F116.
11.1.1.3 Specific guidance on integrity management on pipe-in-pipe systems is given in [13.6.7].
11.1.2 Scope and application
11.1.2.1 The integrity management system comprises a core integrity management process and a number
of support elements (see Figure 11-1 and [11.3.1]).
Figure 11-1 Integrity management system
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11.1.2.2 The core pipeline integrity management process is the combined process of threat identification,
risk assessment, planning, monitoring, inspection, maintenance, etc. to maintain pipeline integrity.
11.1.2.3 Operating safely is interpreted as operating to meet the limit state criteria as established in design
and updated through the project phases and service life.
11.1.2.4 The PIM principles and methodology are applicable to pipeline systems in general.
11.1.3 Systematic review of risks
11.1.3.1 The overall requirement to systematic review of risks in Sec.2 is complied with through the risk
assessment and integrity management (IM) planning activity that is part of the integrity management
process – see [11.1.2.2] and [11.4.2]. The pipeline system threats shall be established (see DNVGL-RPF116 Table 4-1) and the risk for each threat determined. The risk assessment contributes to ensuring that
the safety level premised in the design phase is maintained throughout the original design life of the pipeline
system.
11.1.4 Responsibilities
11.1.4.1 Pipeline integrity management is the responsibility of the pipeline operator. The pipeline operator
shall ensure that the integrity of the pipeline is not compromised.
11.1.4.2 At all times during the operational life of the pipeline system, responsibilities shall be clearly
defined and allocated.
11.1.5 Authority and pipeline operator requirements
11.1.5.1 The relevant national requirements shall be identified and complied with.
11.1.5.2 The relevant company requirements should be complied with when developing, implementing and
maintaining the integrity management system.
11.1.6 Safety philosophy
11.1.6.1 The safety philosophy adopted in design shall apply. The original safety philosophy may be modified
as a result of company/operator, industry and society developments, improvements and better knowledge of
the pipeline system.
A change in the basis for design requires a re-qualification (see [11.5]) and/or a management of change
program.
11.1.6.2 It shall be verified that design and operating premises and requirements are fulfilled. If this is not
the case, appropriate actions shall be taken to bring the pipeline system back to a safe condition.
11.1.6.3 A risk based pipeline integrity management philosophy, which takes into account both probability of
failure and consequence of failure, shall be applied.
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11.2 Commissioning
11.2.1 General
11.2.1.1 Commissioning comprises activities associated with the initial filling of the pipeline system
with the fluid to be transported, and should be part of the operational phase. Requirements pertaining to
documentation and procedures for commissioning are specified in [12.5].
11.2.1.2 This sub-section shall also apply for pipeline re-commissioning.
11.2.2 Fluid filling
11.2.2.1 During fluid filling, care shall be taken to prevent explosive mixtures and, in the case of gas
or condensate, to avoid hydrate formation. The injection rate shall be controlled so that pressure and
temperature do not exceed allowable limits (as given in design or re-qualification) for the pipeline material or
dew point conditions.
11.2.3 Operational verification
11.2.3.1 Following commissioning of the system, it shall be verified that the operational limits are within
design conditions. Important issues that may need verification can be:
— flow parameters (pressure, temperature, dew point conditions, hydrate formation sensitivity, sand
production, chemical injection, etc.)
— CP-system
— expansion, movement, lateral snaking/buckling, upheaval buckling, free span and exposure.
11.2.3.2 Scheduling of the first inspection of the wall thickness for pipelines designed for inspection pigging
shall be evaluated based on the:
—
—
—
—
—
—
corrosivity of the fluid
expected operational parameters
robustness of the internal corrosion protection system (inhibitor system)
corrosion allowance used in the design
effectiveness of the QA/QC system applied during fabrication and construction, and
defect sizing capabilities of the inspection tool that will be used during operation of the pipeline.
11.3 Integrity management system
11.3.1 General
11.3.1.1 The operator shall establish, implement and maintain an integrity management system which
includes the following elements as a minimum (see Figure 11-1):
—
—
—
—
—
—
company policy
organisation and personnel
management of change
operational controls and procedures
contingency plans
reporting and communication
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— audit and review
— information management
— the integrity management process (see [11.4]).
The integrity management system shall in addition satisfy the requirements from:
— the specific pipeline systems' design documentation and safety philosophy
— the relevant authorities (see [11.1.5]) and the operating company itself
— other relevant external stakeholders.
The core of the integrity management system is the integrity management process. The other elements
support this core process.
11.3.1.2 Documents for the operational phase are specified in Sec.12.
11.3.1.3 Specification of work processes should be the basis for establishing procedures.
11.3.1.4 The detailed procedures for operation, inspection and repair shall be established prior to start-up of
operation.
11.3.1.5 Procedures covering non-routine or special activities, shall be prepared as required, e.g. for major
repairs, modifications, etc.
11.3.2 Pipeline operator policy
11.3.2.1 The pipeline operator policy for pipeline integrity management should set the values and beliefs
that the pipeline operator holds, and guide people in how these shall be realized.
11.3.3 Organisation and personnel
11.3.3.1 The roles and responsibilities of personnel involved with integrity management of the pipeline
system shall be clearly defined.
11.3.3.2 The interface between the responsibilities of the different organisational units is particularly
important. Such interfaces shall be managed and important areas that need to be handled are:
— battery limits
— government regulatory responsibilities and statutory regulations
— emergency response, including contingency planning and responding to emergencies.
11.3.3.3 Training needs shall be identified and training shall be provided for relevant personnel in relation to
management of pipeline integrity.
11.3.4 Management of change
11.3.4.1 Modifications of the pipeline system shall be subject to a management of change procedure
that shall address the continuing safe operation of the pipeline system. Documentation of changes and
communication to those who need to know is essential.
11.3.4.2 If the operating conditions are changed relative to the design premises, a re-qualification of the
pipeline system according to [11.5] shall be carried out.
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11.3.5 Operational controls and procedures
11.3.5.1 Relevant operational controls and procedures shall be established, implemented and maintained.
Typical operational controls and procedures are:
—
—
—
—
—
—
start-up, operating and shutdown procedures
procedures for handling non-conformances
instructions for cleaning and other maintenance activities
corrosion control activities
inspection and monitoring activities
procedures for operating safety equipment and pressure control systems.
11.3.5.2 Measures shall be in place to ensure that critical fluid parameters are kept within the specified
design limits. As a minimum, the following parameters should be controlled or monitored:
— pressure and temperature at the inlet and outlet of the pipeline
— dew point for gas lines
— fluid composition, water content, flow rate, density and viscosity.
11.3.5.3 All safety equipment in the pipeline system, including pressure control and over-pressure protection
devices, emergency shutdown systems and automatic showdown valves, shall be periodically tested and
inspected. The purpose it to verify the integrity of the safety equipment and that the equipment can perform
the safety function as specified.
11.3.5.4 Safety equipment in connecting piping systems shall be subject to regular testing and inspection.
11.3.5.5 For pressure control during normal operation, see [3.4.2].
11.3.5.6 Operational control shall ensure that design temperature limits are not exceeded. If the design is
based on a constant temperature along the whole route, control of the inlet temperature will be sufficient. If
the design is based on a temperature profile for the pipeline, additional measures may be required.
11.3.6 Contingency plans
11.3.6.1 Plans and procedures for emergency situations shall be established and maintained based on
a systematic evaluation of possible scenarios. Dependent upon the commercial criticality of the pipeline
system, plans and procedures for contingency repair of the pipeline should also be established.
11.3.7 Reporting and communication
11.3.7.1 A plan for reporting and communication to employees, management, authorities, customers,
public and others shall be established, implemented and maintained. This covers both regular reporting and
communication, and reporting in connection with changes, special findings, emergencies, etc.
11.3.8 Audit and review
11.3.8.1 Audits and reviews of the pipeline integrity management system shall be conducted regularly.
11.3.8.2 Typical focus in the reviews should be on:
— effectiveness and suitability of the system
— improvements to be implemented.
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11.3.8.3 Typical focus in the audits should be on:
— compliance with regulatory and pipeline operator requirements
— rectifications to be implemented.
11.3.9 Information management
11.3.9.1 A system for collection of historical data, an in-service file, shall be established and maintained for
the whole service life, see [12.1.1.3] and [12.6.2.1]. The in-service file will typically consist of documents,
data files and databases.
11.3.9.2 The in-service file, together with the DFI-resume, shall be the basis for future integrity
management planning.
11.3.9.3 The in-service file and the DFI-resume shall be easily retrievable in case of an emergency situation.
11.3.9.4 The documents, data and information shall be managed as described in [12.6] and [12.9].
11.4 Integrity management process
11.4.1 General
11.4.1.1 The integrity management process consists of the following steps (see Figure 11-1):
— Risk assessment and IM planning – includes threat identification, risk assessment, long term and short
term (annual) planning.
— Inspection, monitoring and testing – includes planning, conducting and documentation of such activities.
— Integrity assessment - carried out using recognized methods and based on design data, operational
experience and the results from inspection, monitoring and testing.
— Mitigation, intervention and repair - assess the need for, and the type of, intervention and repair activities
and other mitigating actions.
This process shall be performed regularly.
11.4.1.2 The requirements for corrosion inspection and monitoring, and the capability of optional
techniques, shall be evaluated at an early stage of the pipeline system design.
Guidance note:
Pipelines manufactured from corrosion resistant alloys (CRA) do not normally require inspection and monitoring of internal
corrosion.
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11.4.1.3 Preliminary development of strategies for inspection, monitoring, testing and repair should start
during the concept development phase. The strategies should be finalized after construction.
11.4.1.4 All the inspection, monitoring and testing requirements identified during the design phase that
affects the safety and reliability during operation shall be covered in the inspection, monitoring and testing
program, see [3.4.1] and [5.2.3].
11.4.1.5 A special investigation shall be performed in case of any event which impairs the safety, reliability,
strength or stability of the pipeline system. This investigation may initiate further inspections.
11.4.1.6 If mechanical damage or other abnormalities are detected during the periodic inspection, a proper
evaluation of the damage shall be performed. This may include additional inspections.
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11.4.2 Risk assessment and integrity management planning
11.4.2.1 Different risk assessment methods can be used. Risk can be evaluated using qualitative and/
or quantitative methods as most feasible. A levelled approach for assessing risk uses a combination of
qualitative and quantitative methods. This levelled approach is described in more detail in DNVGL-RP-F116.
The results from the risk assessment shall be used to develop a long term integrity management program.
Specific requirements related to the activities in the integrity management program can be found in [11.4.3]
to [11.4.5].
11.4.2.2 The risk assessment should be based on:
—
—
—
—
data from design and commissioning
previous risk assessments
condition assessment results
operational history (pressure, temperature, flow rate, fluid composition, etc.).
11.4.2.3 Threats shall be systematically identified, assessed and documented throughout the operational
lifetime. This shall be carried out for each section along the pipeline and for components. Examples of typical
threats are:
—
—
—
—
—
internal corrosion
external corrosion
free-spans
buckles
impact damage.
A more detailed list of threats and related damage/anomalies can be found in DNVGL-RP-F116.
11.4.2.4 A long term inspection program reflecting the overall safety objective for the pipeline shall be
established, and shall be maintained/updated on a regular basis. The long term inspection program shall be
based on the risk assessment. In addition the following should be taken into consideration:
—
—
—
—
consequence of failure
likelihood of failure
strategies for inspection, monitoring, testing and repair
available inspection, monitoring and testing methods.
11.4.2.5 The long term inspection program shall cover the entire pipeline system according to the operators'
equipment scope. This includes the pipeline, protective means ensuring the structural integrity of the pipeline
system and all the components according to the definitions [1.8.2], [D.2.1.5] and [5.6].
11.4.3 Inspection, monitoring and testing
11.4.3.1 A pipeline configuration survey is a survey to determine the position, configuration and condition of
the pipeline and its components.
11.4.3.2 The start-up external inspections should be completed within one year from start of production, see
[11.2.3]. In case of significant increase in temperature, pressure or flow rate after this first inspection, the
need for additional inspections should be considered.
11.4.3.3 A detailed external inspection plan including specifications for the inspections shall be prepared for
each survey. The detailed inspection plan should be updated based on previous inspections as required.
11.4.3.4 Pipeline systems that are temporarily out of service shall also be subject to periodical survey.
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11.4.3.5 External inspections shall be carried out to ensure that the design requirements remain fulfilled and
that no damage has occurred. The inspection program should, as a minimum, address:
— exposure and burial depth of buried or covered lines, if required by design, regulations or other specific
requirements
— free spans including mapping of length, height and end-support conditions
— condition of artificial supports installed to reduce free spans
— local seabed scour affecting the pipeline integrity or attached structures
— trawl or anchor scars in the seabed close to or, if the pipeline is buried, across the pipeline
— sand wave movements affecting the pipeline integrity
— excessive pipe movements including expansion effects
— identification of areas where upheaval buckling or excessive lateral buckling has taken place
— integrity of mechanical connections and flanges
— integrity of subsea valves including protective structures
— Y- and tee connections including protective structures
— settlement of exposed pipelines, particularly at the valve/tee locations
— the integrity of pipeline protection covers (e.g. mattresses, covers, sand bags, gravel slopes, etc.)
— mechanical damage to pipe, coating and anodes
— major debris on, or close to, the pipeline that may cause damage to the pipeline or the external corrosion
protection system
— leakage.
11.4.3.6 The frequency of future external inspections shall be determined based upon an assessment of:
—
—
—
—
—
—
—
—
authority and company requirements
degradation mechanisms and failure modes
likelihood and consequences of failure
results from previous inspections
changes in the operational parameters
re-qualification activities and results
repair and modifications
subsequent pipelay operation in the vicinity.
11.4.3.7 Critical sections of the pipeline system vulnerable to damage or subject to major changes in the
seabed conditions i.e. support and/or burial of the pipeline, shall be inspected externally at short intervals,
normally on an annual basis. The remaining sections should also be inspected, ensuring a full coverage of the
entire pipeline system within a suitable period determined based on the risk assessment.
11.4.3.8 In the splash zone and atmospheric zone damaged and/or dis-bonded coating can cause severe
corrosion damage.
11.4.3.9 In the splash and atmospheric zones, visual examination of the coating shall be performed in order
to assess the need for preventive maintenance. Besides visual indications of direct damage to the coating,
effects such as rust discoloration and bulging or cracking of the coating are indicative of rust underneath the
coating. Coating systems which prevent close inspection of corrosion underneath the coating shall require
special consideration.
11.4.3.10 In the submerged zone, coating damage is not critical with respect to external corrosion unless
it is combined with a deficiency in the cathodic protection system. For materials susceptible to HISC refer to
DNVGL-RP-F112.
11.4.3.11 To a large extent, inspection of external corrosion protection of pipelines with sacrificial anodes
can be limited to inspection of the condition of anodes. Excessive anode consumption is indicative of coating
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deficiencies, except close to platforms, templates and other structures where current drain may lead to
premature consumption of adjacent pipe anodes.
11.4.3.12 Potential measurements on anodes, and at any exposed bare pipe metal, may be carried out to
verify adequate protection. Electric field gradient measurements in the vicinity of anodes may be used for
semi-quantitative assessments of anode current outputs.
11.4.3.13 For pipelines with impressed current cathodic protection systems, measurements of protection
potentials shall, as a minimum, be carried out at the locations closest to, and most remote from, the
anode(s).
11.4.3.14 A survey of the external corrosion protection system should be carried out within one year of
installation.
11.4.3.15 In-line inspection is carried out in order to confirm the integrity of the pipeline system, primarily
by means of in situ wall thickness measurements.
Guidance note:
Un-piggable pipelines are subject to separate evaluations and alternative methods.
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11.4.3.16 An in-line inspection should be carried out with a carrier tool (inspection pig) capable of inspecting
the internal and external surface of the pipeline along its full circumference and length, or a critical part
thereof.
11.4.3.17 The technique for detection of internal and/or external corrosion shall be selected based on
considerations of fluid, linepipe material, diameter and wall thickness, expected form of damage, and
requirements to detection limits and defect sizing capability. The latter shall be determined based on pipeline
design and operational parameters.
11.4.3.18 Candidate operators of inspection tools should be required to document the capability of their
systems with respect to detection limits and sizing of relevant corrosion defects (including localised corrosion
at girth welds) for the pipe dimensions considered.
11.4.3.19 The frequency of in-line inspections shall be determined based on factors such as:
—
—
—
—
authority and pipeline operator requirements
likelihood and consequences of failure
potential corrosivity of fluid
potential for development of external corrosion at hot-spots such as riser(s) and landfall/onshore pipeline
sections
— detection limits and accuracy of inspection system
— results from previous surveys and monitoring
— changes in pipeline operational parameters, etc.
See also [11.2.3].
11.4.3.20 Inspection by special internal tools may be used to detect external corrosion of pipelines in all
three zones (atmospheric/splash/submerged).
11.4.3.21 The objective of monitoring internal corrosion is to confirm that the fluid remains non-corrosive
or, more often, to assess the efficiency of any corrosion preventive measures, and accordingly to identify
requirements for inspection of corrosion.
11.4.3.22 Corrosion monitoring as defined above does not normally give any quantitative information of
critical loss of wall thickness. Although monitoring may be carried out as actual wall thickness measurements
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in a selected area, it cannot replace pipeline inspection schemes that cover the pipeline system, or sections
thereof, in its full length and circumference. On the other hand, inspection techniques for internal corrosion
are not normally sensitive enough to replace monitoring.
11.4.3.23 The following major principles of corrosion monitoring may be applied:
— fluid analyses; i.e. monitoring of fluid physical parameters and sampling of fluid for chemical analysis of
corrosive components, corrosion retarding additions or corrosion products
— corrosion probes; i.e. weight loss coupons or other retrievable probes for periodic or on-line determination
of corrosion rates
— in-situ wall thickness measurements, i.e. repeated measurements of wall thickness at defined locations
using portable or permanently installed equipment.
11.4.3.24 Techniques and equipment for corrosion monitoring shall be selected based upon:
— monitoring objectives, including requirements for accuracy and sensitivity
— fluid corrosivity and the corrosion preventive measures to be applied
— potential corrosion mechanisms.
11.4.3.25 A typical major objective of corrosion monitoring is to detect changes in either intrinsic corrosivity
of the fluid, or in the efficiency of the corrosion prevention measures. For pipelines carrying dry (i.e. fully
processed) gas, inspection of internal corrosion may be postponed provided that monitoring demonstrates
that no corrosive liquids have entered the pipeline, or been formed by condensation downstream of the inlet.
Testing
11.4.3.26 Testing activities may be specified to be carried out during the operational phase. Such activities
shall be planned, executed, reviewed and documented. Testing activities may comprise:
—
—
—
—
system pressure testing
hydrostatic testing
gas or media testing
shut-in testing.
Recommended practice for testing during operation is given in DNVGL-RP-F116.
11.4.4 Integrity assessment
11.4.4.1 Pipeline systems with unacceptable damage/anomalies may be operated temporarily under the
design conditions or reduced operational conditions until the defect has been removed or repair has been
carried out. It shall, however, be documented that the pipeline integrity and the specified safety level is
maintained, which may include reduced operational conditions and/or temporary precautions.
11.4.4.2 When a potentially unacceptable damage or abnormality is detected, an evaluation shall be carried
out including:
— quantify details of the damage/abnormality
— identify the root cause
— evaluate accuracy and uncertainties in the inspection results.
If the damage/abnormality is not acceptable, then further evaluations can include:
— options for continued operation of the pipeline system
— repair methods.
11.4.4.3 In each case a thorough evaluation of the damage/abnormality and the impact on safety and
reliability for the operation of the pipeline shall be performed. The requirements given in the following
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sections regarding necessary actions, e.g. grinding or replacement, may be waived if it can be documented
that the specified safety level for the pipeline system is not impaired.
11.4.4.4 Damage or abnormalities that affect the safety or reliability of the pipeline shall either be removed
by replacing the damaged section of the pipe or repaired by local reinforcement. Alternatively, the pipeline
may be permanently re-qualified to lower operational conditions, see [11.5] and Sec.5, e.g. reduced
pressure, which may remove the requirement for repair.
11.4.4.5 Recommended practice for free spanning pipelines is given in DNVGL-RP-F105.
11.4.4.6 If the design is based on controlled global buckling including plastic strains, the pipeline should
be verified based on established design limits and conditions (curvatures, strains, bending moment). If
unexpected global buckling occurs, utilisation of the pipeline should be evaluated based on relevant failure
modes. Recommended practice for global buckling of submarine pipelines is given in DNVGL-RP-F110.
11.4.4.7 Sharp defects like grooves, gouges, and notches should preferably be removed by grinding or other
agreed repair methods. For a grinded defect where all the sharp edges are confirmed removed, the defect
can be regarded as a smooth metal loss defect, see [11.4.4.8].
11.4.4.8 Metal loss defects caused by e.g. corrosion, erosion, or grind repair shall be checked for capacity.
Recommended practice for corroded pipelines is given in DNVGL-RP-F101.
11.4.4.9 A dent is defined as a depression which produces a gross disturbance in the curvature of the pipe
wall. For dent acceptance criteria, see [5.4.11].
11.4.5 Mitigation, intervention and repairs
11.4.5.1 Examples of mitigation, intervention and repairs are:
— mitigation:
— restrictions in operational parameters (pressure, temperature, flow rate, fluid composition, etc.)
— use of chemical injections
— intervention:
— rock dumping
— installation of pipeline protection
— trenching
— repairs:
— local reinforcement (clamps, etc.)
— replacement of pipeline parts.
All mitigation, intervention and repairs shall be documented.
11.4.5.2 Repair and modification shall not reduce the safety level of the pipeline system below the specified
safety level.
11.4.5.3 All repairs shall be carried out by qualified personnel in accordance with agreed specifications and
procedures, and be up to the standard defined for the pipeline.
11.4.5.4 All repairs shall be tested and inspected by experienced and qualified personnel in accordance with
agreed procedures. NDT personnel, equipment, methods, and acceptance criteria shall be agreed upon in
accordance with App.D.
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11.4.5.5 Depending upon the condition of the damage, a temporary repair may be accepted until the
permanent repair can be carried out. If a temporary repair is carried out, it shall be documented that the
pipeline integrity and safety level are maintained either by the temporary repair itself or in combination with
other precautions.
11.4.5.6 Recommended practice for pipeline repair in general is given in DNVGL-RP-F113.
11.4.5.7 A dent affecting a weld can result in cracks, and removal of the damaged portion of the pipe should
be considered. The damaged part can be cut out as a cylinder and replaced. Alternatively it can be repaired
by installing a grouted repair clamp, a full encirclement welded split sleeve or bolted clamp which is designed
to take the full internal operating pressure.
11.4.5.8 Prior to carrying out a permanent repair of any leak, the cause of the leak shall be established.
11.4.5.9 The most suitable method for repairing a leak in the pipe depends upon e.g. the pipe material, pipe
dimensions, location of leak, load conditions, pressure and temperature. The following repair methods may
be used:
— The damaged section is cut out of the pipe as a cylinder and a new pipe spool is installed by welding or by
the use of a mechanical connector.
— Clamps are installed, and the required tightness is obtained by welding, filler material, friction or other
qualified mechanical means.
11.4.5.10 Leaking flanges and couplings may be sealed by installing a seal clamp covering the leaking flange
or coupling, increasing the bolt pre-load, or replacing gaskets and seals. Prior to increasing the pre-load in
bolts, it shall be documented by calculation that no over-stressing can occur in bolts, flange or gasket/seals.
If the pre-load in the bolts is removed, e.g. due to a gasket replacement, new bolts shall be used for the
flange connection.
11.4.5.11 All repair clamps, sleeves, pipe spools and mechanical connectors shall be qualified prior to
installation and leak tested after installation.
11.4.5.12 Procedures for repair welding, welding equipment and welders shall be qualified as described in
App.C.
11.4.5.13 Repair welding above water shall be carried out as described in App.C.
11.4.5.14 Underwater welding shall be carried out in a dry habitat, see App.C.
11.4.5.15 Repair welding may, in special cases, be carried out on pipelines during operation, dependent on
the pipe material, pipe wall thickness, fluid type, pressure and temperature. It shall be documented that the
safety for carrying out the repair is acceptable, and a safety procedure shall be established and implemented.
11.4.5.16 All repair welds shall be subject to visual inspection and non-destructive testing, see App.D.
Following the repair, pressure testing may be required for the repaired section.
11.5 Re-qualification
11.5.1 General
11.5.1.1 The purpose of this section is to define re-qualification and to give requirements for re-qualification
of pipeline systems.
11.5.1.2 Re-qualification is a re-assessment of the design under changed design conditions.
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11.5.1.3 A re-qualification may be triggered by a change in the original design basis, by not fulfilling the
design basis, or by mistakes or shortcomings discovered during normal or abnormal operation. Possible
causes may be:
— preference to use a more recent standard, e.g. due to requirements for higher utilisation for existing
pipelines
— change of the premises such as:
— environmental loads
— deformations
— scour
— change of operational parameters such as:
— pressure or temperature
— fluid composition, water content, H2S-content
— operating cycles
— change of flow direction of change of fluid
— deterioration mechanisms having exceeded the original assumptions such as:
— corrosion rate (internal or external)
— dynamic responses contributing to fatigue, e.g. VIV, start/stop cycles
— extended design life
— discovered damage such as:
—
—
—
—
—
—
dents
damage to pipeline protection
weld defects
corrosion related defects
cracks
consumption or damage to anodes.
11.5.2 Application
11.5.2.1 Within the original design life, and without essential changes in the manner of employment
(repair, etc.), the standard under which the pipeline was built may apply when considering incidents, minor
modifications or rectification of design parameters exceeded during operation. Alternatively, this standard
and associated DNV GL standards or recommended practices may be used.
11.5.2.2 For major modifications or other instances not covered by the above paragraph this standard shall
apply. For lifetime extensions, see also ISO 12747, NORSOK Y-002 and NORSOK U-009.
11.5.2.3 The same safety level shall apply for lifetime extensions of an existing pipeline as would apply for
the design of a new pipeline. The reason for requiring use of this standard is in case the original standard
used for design is less stringent than necessary to meet the target safety levels specified in this standard.
11.5.3 Safety level
11.5.3.1 A target safety level as defined in [2.3.5] shall apply for a re-qualification assessment.
11.5.3.2 Operational experience, e.g. change of operational conditions, inspection records and modifications,
shall be considered in a re-qualification assessment.
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11.5.4 System pressure test
11.5.4.1 System pressure testing may be required when:
— the original mill pressure test or system pressure test does not satisfy requirements according to this
standard at the new design pressure
— a significant part of the pipeline has not been system pressure tested, e.g. new pipeline section as part of
a modification or repair campaign (for omission of system pressure test, see [5.2.2.3]).
11.5.5 Deterioration
11.5.5.1 All relevant deterioration and damage mechanisms shall be evaluated. Typical mechanisms are:
— corrosion:
— external corrosion
— internal corrosion
— erosion
— accidental loads
— development of free spans
— fatigue
— settlement.
11.5.5.2 Sufficient reliability or safety measures shall be applied to account for the accuracy and
uncertainties in the inspection results.
11.5.5.3 Accumulated damage experienced prior to the re-qualification shall be included in the evaluation.
11.5.6 Design criteria
11.5.6.1 The parameters that trigger the re-qualification and the implication of changes in these parameters
on different design conditions shall be clearly identified and documented. For re-design based on these
design conditions, see Sec.5.
11.6 De-commissioning
11.6.1 General
11.6.1.1 De-commissioning is the set of activities associated with taking the pipeline temporarily out of
service.
11.6.1.2 Pipeline de-commissioning shall be planned and prepared.
11.6.1.3 De-commissioning shall be conducted and documented in such a way that the pipeline can be recommissioned and put into service again.
11.6.1.4 A de-commissioning evaluation shall at least include the following aspects:
— relevant national regulations
— environment, especially pollution
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— obstruction for ship traffic
— obstruction for fishing activities
— corrosion impact on other structures.
11.6.1.5 De-commissioned pipelines shall be preserved to reduce the effect of degradation mechanisms.
11.6.1.6 Sub-section [11.2] shall apply for pipeline re-commissioning.
11.7 Abandonment
11.7.1 General
11.7.1.1 Abandonment of a pipeline system comprises the activities associated with taking the system or
part of the system permanently out of operation.
11.7.1.2 An abandoned pipeline is not intended to be returned to operation.
11.7.1.3 Pipeline abandonment shall be planned and prepared.
11.7.1.4 A pipeline abandonment evaluation shall at least include the following aspects:
—
—
—
—
—
—
relevant national regulations
health and safety of personnel, if the pipeline shall be removed
environment, especially pollution
obstruction for ship traffic
obstruction for fishing activities
corrosion impact on other structures.
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SECTION 12 DOCUMENTATION
12.1 General
12.1.1 Objective
12.1.1.1 This section specifies the minimum requirements to documentation needed for design,
manufacturing/fabrication, installation, operation and abandonment of a pipeline system.
12.1.1.2 A design fabrication installation (DFI) resumé, as described in [12.8], shall be established with
the main objective being to provide the operations organisation with a concentrated summary of the most
relevant data from the design and construction (incl. pre-commissioning) phases (see [12.2], [12.3] and
[12.4]).
12.1.1.3 An in-service file containing all relevant data achieved during the operational phase of the
pipeline system and with the main objective to systemise information needed for integrity management
and assessment of the pipeline system shall be established and maintained for the whole service life (see
[12.6.2]).
12.1.1.4 For the design, fabrication and installation phase, all required documentation shall be reflected in a
master document register (MDR).
12.1.1.5 The required documentation for all phases of the pipeline system’s lifetime shall be submitted to
the relevant parties for acceptance or information as agreed.
12.1.1.6 Recommended practice for technical documentation required for assemblies, equipment,
components and materials that are delivered as part of a subsea (or pipeline) contract is given in DNVGL-RPO101.
12.2 Design
12.2.1 Structural
12.2.1.1 A design basis for the pipeline system shall be established, including, but not limited to:
—
—
—
—
—
—
—
—
—
—
—
—
—
safety objective
pipeline system description incl. location, general arrangements, battery limits, inlet and outlet conditions
functional requirements including field development restrictions, e.g. safety barriers and subsea valves
requirements to repair and replacement of pipeline sections, valves, actuators and fittings
project plans and schedule, including planned period of the year for installation
design life including specification of start of design life, e.g. installation, final commissioning, etc.
transport capacity and pipeline sizing data
attention to possible code breaks in the pipeline system
geometrical restrictions such as specifications of constant internal diameter, requirement for fittings,
valves, flanges and the use of flexible pipe
pigging requirements such as bend radius, pipe ovality and distances between various fittings affecting
design for pigging applications
relevant pigging scenarios (inspection and cleaning)
pigging fluids to be used and handling of pigging fluids in both end of pipeline including impact on process
systems
topographical and bathymetrical conditions along the intended pipeline route
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— geotechnical conditions
— environmental conditions
— operational conditions such as pressure, temperature, fluid composition, flow rate, sand production etc.
including possible changes during the pipeline system's design life
— principles for strength and in-place analysis
— corrosion control philosophy
— second and third party activities.
12.2.1.2 The purpose of the design documentation is to ensure a reliable pipeline system. The design shall
be adequately documented to enable second and/or third party verification. As a minimum, the following
items shall be addressed:
—
—
—
—
—
—
—
—
—
pipeline routing
physical and chemical characteristics of fluid
materials selection
temperature/pressure profile and pipeline expansion
strength analyses for riser and riser supports
all relevant strength and in-place stability analyses for pipeline
relevant pipeline installation analysis
risk analysis as applicable
systematic review of threats in order to identify and evaluate the consequences of single failures and
series of failures (see [2.2.3])
— corrosion control (internal and external)
— piggability
— installation and commissioning.
12.2.1.3 Drawings shall be provided for the fabrication and installation of the pipeline system, including but
not limited to:
— pipeline route drawings including information on, e.g. seabed properties and topology, existing and future
platforms, pipelines/cables, subsea well heads, ship lanes, etc.
— alignment sheets
— detailed pipeline crossing drawings
— platform layout drawings with risers, riser protection systems, loading zones, boat landing areas, rescue
areas, etc. as applicable
— spool fabrication drawing
— other components within the pipeline system (connectors, pigging loops etc.)
— pipeline protection drawings
— riser and riser clamp fabrication drawings
— land ownership details.
12.2.2 Material selection
12.2.2.1 The selection of materials during conceptual and/or detailed design shall be documented,
preferably in a materials selection report in accordance with ISO 21457, section 5.
The documentation shall refer to the requirements and recommendations of Sec.6, including
— use of CRAs,
— corrosion allowance and
— provisions for internal corrosion control.
The design premises for materials selection should be identified, making reference to the design basis and
any other relevant project documents, together with the applicable standards and recommended practices.
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12.2.2.2 Any requirements and conditions on pipeline fabrication and operational procedures used as the
basis for materials selection shall be duly high-lighted in the document to ensure that they are adequately
transferred into these phases of the pipeline.
Guidance note:
The internal corrosion control of pipelines carrying potentially corrosive fluids based on chemical treatment is much based on
conditions for periodic cleaning, corrosion monitoring and inspection of the integrity of the pipeline which are not always defined in
the project design basis and need to be verified by the operator of the pipeline.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
12.2.2.3 The following shall be prepared as separate documents in detailed design:
—
—
—
—
—
—
specification of line pipe material,
specification of pipeline components (including fasteners),
specification of pipe coatings (including line pipe coating, field joint coating and any concrete coating),
cathodic protection design report
anode manufacture specification and
anode installation specification.
12.2.3 Linepipe and pipeline components (including welding)
12.2.3.1 The following documentation shall be established:
— material manufacturing specifications
— welding and NDT specifications
— material take off/data sheets.
12.2.4 Corrosion control systems and weight coating
12.2.4.1 The following documentation shall be established, as applicable:
—
—
—
—
—
—
—
—
—
cathodic protection design report, see [6.4.5.8]
anode manufacturing and installation specifications, see. [9.4] and [9.5]
outline anode drawings
linepipe coating application specifications
field joint coating specification(s)
coating field repair specification(s)
concrete coating specification (if applicable)
corrosion monitoring system specification
material take off/data sheets.
The cathodic protection design report shall pay attention to the landfall section (if any) and possible
interaction with the relevant onshore CP-system.
12.2.5 Installation
12.2.5.1 The following documentation shall be established:
— failure mode effect analysis (FMEA) and HAZOP studies (see Sec.10)
— installation and testing specifications and drawings
— welding procedure qualification (WPQ) records.
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12.2.6 Operation
12.2.6.1 Decisions and parameters having an impact on the operational phase of the pipeline system such
as:
— operation envelope
— external and internal inspection strategies incl. piggability, ROV surveys
— measuring points for in-situ wall thickness measurements, ER-probes, weight loss coupons, fluid
monitoring etc.
shall be emphasised and documented in design.
12.2.6.2 As a minimum, the following documentation shall be established:
— pipeline integrity management strategy covering strategies for corrosion control, inspection and
maintenance
— emergency response strategy
— emergency repair contingency strategy.
12.2.7 DFI-resumé
12.2.7.1 The design part of the DFI-resumé shall be established and in accordance with the requirements
given in [12.8].
12.3 Construction - manufacturing and fabrication
12.3.1 Linepipe and pipeline component
12.3.1.1 The documentation to be submitted for review prior to start or during start-up of manufacturing
shall include, but not be limited to:
—
—
—
—
—
—
—
—
—
quality plan (QP)
manufacturing procedure specifications (MPS) including test requirements and acceptance criteria
manufacturing procedure qualification test (MPQT) results
manufacturing procedures (e.g. hydrostatic testing, dimensional measurements, mechanical and corrosion
testing etc.)
welding procedure specifications (WPS), including procedures for repair welding
welding procedure qualification (WPQ) records
non-destructive testing (NDT) procedures
personnel qualification records (e.g. for welders and NDT operators)
manufacturer's/fabricator's quality system manual.
12.3.1.2 The as built documentation to be submitted after manufacturing shall include, but not be limited to:
—
—
—
—
—
—
—
quality control (QC) procedures
inspection and test plan (ITP)
traceability procedure
material certificates
manufacturing procedure specifications (MPS) including test requirements and acceptance criteria
results from MPQT
test procedures (e.g. hydrostatic testing, dimensional measurements, mechanical and corrosion testing
etc.)
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—
—
—
—
—
—
—
—
—
—
—
—
—
—
mechanical test reports
hydrostatic testing report
weld log records
consumable batch numbers
welder certificates
heat treatment records
NDT procedures and records
NDT operator certificates
dimensional reports
equipment calibration certificates/reports
storage procedures
release certificates
pipe tally sheet
complete statistics of chemical composition, mechanical properties and dimensions for the quantity
delivered.
12.3.2 Corrosion control system and weight coating
12.3.2.1 The documentation to be submitted for review prior to start of manufacturing shall include, but not
be limited to:
— application/manufacturing procedure specification, including inspection/test requirements and acceptance
criteria, repairs, documentation, etc.
— documentation of materials and concrete mix design
— procedure qualification trial (PQT) results
— inspection and testing plan (ITP) with referenced procedures for inspection, testing and calibrations
— anode drawings.
12.3.2.2 The as built documentation to be submitted after manufacturing shall include, but not be limited to:
— application/manufacturing procedure specification, including test requirements and acceptance criteria,
repairs, personnel qualification records, etc.
— material data sheets and certificates
— daily logs including production test records
— complete statistics of coating dimensions, weight and negative buoyancy for the each joint delivered
— repair log
— electrical resistance test log.
12.3.3 DFI-resumé
12.3.3.1 The manufacturing/fabrication part of the DFI-resumé shall be established and in accordance with
the requirements given in [12.8].
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12.4 Construction - installation and pre-commissioning
12.4.1 General
12.4.1.1 The documentation to be submitted for review prior to start of installation shall include, but not be
limited to:
— installation procedures for pipelines, risers, spools and components including acceptance criteria, test
certificates for equipment, qualification records for personnel (e.g. welding, coating), etc.
— installation procedures for protective structures (as mattresses etc.) and pipeline anchoring structures
— installation manuals (IM) procedures
— trenching specification
— intervention procedure
— survey procedure
— hydrotest procedures
— pre-commissioning procedure, incl. procedures for dewatering, cleaning, drying, flooding, mothballing,
etc.
— filling of fluid procedures.
12.4.1.2 Documentation produced in connection with the pressure testing of the pipeline system shall
include:
—
—
—
—
—
—
pressure and temperature record charts
log of pressure and temperatures
calibration certificates for instruments and test equipment
calculation of air content
calculation of pressure and temperature relationship and justification for acceptance
endorsed test acceptance certificate.
12.4.1.3 The as built documentation to be submitted after installation and pre-commissioning shall include,
but not be limited to:
—
—
—
—
survey reports
updated drawings
intervention reports
pre-commissioning reports.
12.4.1.4 Records and documentations should include authorisations and permits to operate.
12.4.2 DFI-resumé
12.4.2.1 The Installation (incl. pre-commissioning) part of the DFI-resumé shall be established and in
accordance with the requirements given in [12.8].
12.5 Operation - commissioning
12.5.1 General
12.5.1.1 As a part of the commissioning (see [11.2]) the documentation made available shall include, but
not be limited to:
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— procedure and results from fluid filling operations with special emphasis on design parameters having an
impact on the integrity of the pipeline system such as temperature, pressure and dew points
— procedures and results from operational verification activities (i.e. start-up inspection). Important
parameters to document are typically:
—
—
—
—
expansion
movement
global buckling
wall thickness/metal loss
— inspection plans covering the future external and internal inspections of the pipeline system.
12.6 Operation
12.6.1 General
12.6.1.1 In order to maintain the integrity of the pipeline system, the documentation made available during
the operational phase shall include, but not be limited to:
— organisation chart showing the functions responsible for the operation of the pipeline system
— personnel training and qualifications records
— history of pipeline system operation with reference to events which may have significance to design and
safety
— installation condition data as necessary for understanding pipeline system design and configuration, e.g.
previous survey reports, as-laid/as-built installation drawings and test reports
— physical and chemical characteristics of transported media including sand data
— inspection and maintenance schedules and their records
— inspection procedure and results covering the inspection aspects described in Sec.11, including supporting
records.
12.6.1.2 In case of mechanical damage or other abnormalities that might impair the safety, reliability,
strength and stability of the pipeline system, the following documentation shall, but not be limited to, be
prepared prior to start-up of the pipeline:
— description of the damage to the pipeline, its systems or components with due reference to location, type,
extent of damage and temporary measures, if any
— plans and full particulars of repairs, modifications and replacements, including contingency measures
— further documentation with respect to particular repair, modification and replacement, as agreed upon in
line with those for the construction or installation phase.
12.6.1.3 In case of re-qualification of the pipeline system, see [11.5], all information related to the reassessment process of the original design shall be documented.
12.6.2 In-service file
12.6.2.1 The in-service file, as defined in [11.3.9] shall as a minimum contain documentation regarding:
—
—
—
—
results and conclusions from the in-service inspections
accidental events and damages to the pipeline system
intervention, repair, and modifications
operational data (fluid composition, flow rate, pressure, temperature etc.) affecting corrosion and other
deterioration mechanisms.
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12.7 Abandonment
12.7.1 General
12.7.1.1 Records of abandoned pipelines shall be available and shall include but not be limited to:
— details of abandoned pipelines on land including route maps, the size of the pipeline depth of burial and its
location relative to surface features
— details of abandoned offshore pipelines, including navigation charts showing the pipeline route.
12.8 DFI-resumé
12.8.1 General
12.8.1.1 A design fabrication installation (DFI) resumé shall be prepared to provide information for operation
of the pipeline system. The DFI resumé shall clearly show the limits of the submarine pipeline system.
12.8.1.2 The DFI-resumé shall reflect the as-built status of the pipeline system and shall provide information
for preparation of plans for inspection and maintenance planning.
12.8.1.3 The DFI-resumé shall specify design and operating premises and requirements.
12.8.1.4 The DFI-resumé shall contain all documentation required for normal operation, inspections
and maintenance and provide references to the documentation needed for any repair, modification or requalification of the pipeline system.
12.8.1.5 The preparation of the DFI-resumé shall be carried out in parallel, and as an integrated part, of the
design, fabrication and installation phase of the project.
12.8.2 DFI resumé content
As a minimum, the DFI-resumé shall contain the below listed items:
Table 12-1 DFI resumé content
Considered aspect
Remark
System description
Shall include a description of the pipeline system including:
— final dimensions
— final operational parameters
— a table, for planning of future pigging operations, listing all components in
the system from pigtrap to pigtrap. Key data like inner diameter (ID), bend
radius and wall thickness (WT) should be included, as well as references to
additional documentation/drawings.
Document filing system
Shall give an overview of as-built documentation including description of filing
system and method.
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Considered aspect
Remark
Design basis
Shall give a summary of the final design basis, on which engineering,
fabrication and installation is based. Design parameters of key importance
for the operation of the pipeline system should be emphasised. The following
parameters are considered important for the operation of the pipeline system:
— design life and limitations
— design standards
— environmental conditions
— tabulated geotechnical parameters as used in design
— design pressure and temperature
— flow rate
— fluid composition
— corrosion allowance
— depth of cover
— material specifications, covering pressure containing equipment and
structure
— CP-system (i.e. anode details)
— coating system
— fatigue design assumptions incl. free span criteria
— incidental pressure relief system
— flow control techniques and requirements.
Design
Shall include a design activity resumé, all engineering assumptions and
assessments not listed in the design basis in addition to applicable deviations
and non-conformances including a description of possible impact on the
operational phase.
Construction - fabrication
Shall include a manufacturing/fabrication activity resumé, reference to
specifications, drawings etc., discussion of problem areas and any deviations
from specifications and drawings of importance for the operational phase.
Construction - installation
Shall include an installation activity resumé, reference to specifications,
drawings etc., discussion of problem areas and any deviations from
specifications and drawings of importance for the operational phase.
Construction - pre-commissioning
Shall include a pre-commissioning activity resumé and any results from the
pre-commissioning phase. All applicable deviations and non-conformances
shall be listed including a description of possible impact on the operational
phase.
Certificate and authority approval
Shall include a hierarchical overview of issued certificates, release notes and
authority approvals with reference to items and nature of any conditional
approvals. The certificates, release notes and authority approvals shall
show unambiguous reference to applicable standards and documents,
items covered, accepted deviations, certification activities and condition for
certificates.
Surveys
Shall give all engineering assumptions and assessments drawn from the route
and site surveys in addition to all applicable as-installed route drawings.
Inspection, maintenance and repair
Shall include an overview of:
— identified areas deemed to require special attention during normal
operation of the pipeline system
— operational constraints.
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Considered aspect
Remark
Deviations and non-conformances
Shall include a complete list of waivers, deviations and non-conformances
with special emphasis on identified areas deemed to require special attention
during normal operation of the pipeline system.
Selected drawings
Shall include a complete as-built drawing list, including drawings from subvendors and contractors, with reference to the as-built filing system. Selected
drawings from the design, fabrication and installation phase, as:
— drawings of special components
— alignment sheets
— as-installed route drawings
shall be included.
12.9 Filing of documentation
12.9.1 General
12.9.1.1 Maintenance of complete files of all relevant documentation during the life of the pipeline system is
the responsibility of the pipeline operator.
12.9.1.2 The DFI-resumé (see [12.8.2]) and all documentation referred to in the DFI-resumé shall by filed
for the lifetime of the system. This includes also documentation from possible major repair or re-construction
of the pipeline system.
12.9.1.3 The engineering documentation not mentioned in [12.9.1.2] shall be filed by the pipeline operator
or by the engineering contractor for a minimum of 10 years.
12.9.1.4 Files to be kept from the operational phase of the pipeline system shall as a minimum include final
in-service ([12.6.2]) inspection reports from start-up, periodical and special inspections, condition monitoring
records, and final reports of maintenance and repair.
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SECTION 13 COMMENTARY (INFORMATIVE)
13.1 General
13.1.1 Objective
This section provides informative:
— background to the requirements in the standard
— guidance to reflecting good engineering practice.
The section is informative and some of the recommendations may be founded on engineering judgement
only.
13.2 Safety and design philosophy
13.2.1 Safety class discussion
Safety class shall be specified for each part of the pipeline and for each phase. The classification shall be
based on the requirements in Sec.2.
The safety class concept allows the owner some flexibility in terms of risk which is both a reasonable and
rational approach, e.g. this allows the owner to differentiate between the design conservatism for a flow line
with a 5 year design life and a trunk line with 40 years design life.
The main aspect when determining the safety class is the consequence, typically to people, environment and
cost. Note that this consequence not necessarily is limited to failure of the considered pipeline itself, but also
to its impact on the total exploration. One such example may be reduction in production if a water injection
line or a system for waste water fails which from an isolated point of view could be defined as safety class
low.
Another example is differentiation of temporary phases. A failure during installation, normally considered as
safety class low, will have a significantly smaller consequence than a failure during a shut-down period of the
pipeline, where both pollution and time for repair are significantly more expensive and time consuming. In
case a wet buckle occurs during installation and the vessel does not have the capacity to hold or eventually
retrieve the pipe, this may have large consequences as another vessel may have to retrieve the pipe, and
hence this may call for a higher safety class than low.
However, the total safety may not always be increased by specifying a higher safety class. This may be the
case when the most probable cause of failure would be draught of vessel, where the emphasis should be put
on operating procedures and back-up. During such circumstances, it may not be required with a higher safety
class.
The above clearly illustrates that Table 2-4 is for normal classification only, as stated.
13.2.2 Structural reliability analyses
Structural reliability methods consider structural analysis models in conjunction with available information
regarding the involved variables and their associated uncertainties. The reliability as assessed by reliability
methods is not an objective physical property of the pipeline itself in the given operational and environmental
condition, but rather a nominal measure of the reliability given a particular physical and probabilistic
modelling and analysis procedure applied.
Structural reliability analysis is only one part of a total safety concept as gross errors are not included. A
gross error is defined as a human mistake during the design, construction or operation of the pipeline that
may lead to a safety level far below what is normally aimed for by use of a partial safety factor design format
or specific reliability analysis. In the following only natural variability are discussed and the corresponding
probabilities are referred to as nominal throughout this standard.
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Nominal target reliabilities have to be met in design in order to ensure that certain safety levels are achieved.
A probabilistic design check can be performed using the following design format:
Pf,calculated < Pf,T
Pf,calculated is the calculated nominal probability of failure evaluated by a recognised (accepted) reliability
method and pf,T is a nominal target value that should be fulfilled for a design to be accepted.
Acceptable nominal failure probabilities depend in general on the consequence and nature of failure, the
risk of human injury, economic losses, social (political) inconvenience and the expense and effort required
to reduce the failure probability. The target values were proposed by Professor Torgeir Moan, see Sotberg
(1997) and were based on implied failure probability within different design equations representing different
risks as reflected by the safety class.
The target failure probability is express as annual failure probability which has been discussed in the industry.
It shall be interpret as probability that a failure occurs in the period of one year.
Failure statistics may be used as guidance on relative failure probability levels but only limited information
about specific failure probability for SLS, ULS and FLS can be deduced from failure statistics. Structural
(nominal) failure probability from a SRA is a nominal value and cannot be interpreted as an expected
frequency of failure.
13.2.3 Characteristic values
In a LRFD format, so called characteristic values are used. These are often lower fractiles for strength and
resistance, not always however, and upper fractiles for loads. Typical examples of these may be SMYS for the
yield stress and 100-year waves for loads.
The characteristic value in the resistance formulas is a lower fractile and the expected yield stress is typically
in the order of 8% higher. On commonly overlooked implication of this is that it is not allowed to replace the
fy based upon a certificate or test. Such a replacement requires a thorough reliability assessment.
13.3 Loads
13.3.1 Conversion of pressures
The pressure used in the design criteria is now the incidental pressure. The incidental pressure is normally
-2
defined as the pressure with an annual probability of exceedance of 10 .
The incidental pressure is reflected also in many other standards or recommended practices, referred to as
incidental pressure or maximum pressure and allows typically pressures 10% above the design pressure to
account for water hammer effect and other not permanent pressures.
The incidental pressure has been used as the characteristic pressure (for extreme functional loads) and is
therefore used in all the limit states of this standard. This is in contradiction with many other standards or
recommended practices that use the design pressure or the maximum allowable operating pressure. This
standard has selected the incidental pressure based on structural reliability arguments; it is a more likely
pressure in case of failure.
The ratio between the incidental pressure and design pressure shall be determined based on the pipeline
control and safety system tolerances and capabilities to ensure that the local incidental pressure meets the
given probability of being exceeded within a year. This will then include simulation of the hydraulics of the
medium.
If the pressure cannot exceed the incidental pressure, e.g. full shut-in pressure is used as incidental
pressure, the design pressure may be taken as equivalent to the incidental pressure, see Table 3-1.
Different systems may have different definitions of pressures, e.g. between topside and a pipeline system.
When converting the defined pressures in one system to pressure in another system, the conversion shall
-2
be based on pressure having an annual probability of exceedance less than 10 . This pressure shall then
be defined as the incidental pressure in the pipeline system. Determination of design pressure shall then be
made based on the above principles.
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For pipeline systems with a two peak annual extreme pressure distribution, special considerations are
required. See [13.4.6].
13.4 Design criteria
13.4.1 General
The basis for most of the given limit states have been published as papers or reports that can be ordered,
see e.g. Jiao (1996) and Mørk (1997).
The work was incorporated in DNV Rules for Submarine Pipeline Systems, 1996 (DNV'96) and modified in
order to allow for additional aspects, not necessarily to be considered in a research project. Hence, all limit
states may not have identical partial factors as in the above references.
In the 2000 revision of this standard, the LRFD format was modified on the resistance side as described
in Sec.5 and the limit states from 1996 version modified correspondingly. The local buckling formulation
included some results from the Hotpipe project, allowing a higher utilisation of pressurised pipes, see e.g.
Vitali (1999). In the 2007 revision, this was further improved to allow for higher utilisation for pressurised
pipes. The characteristic pressure is now incidental pressure for all limit states.
13.4.2 Condition load effect factors
The load condition factor γC = 1.07, pipeline resting on uneven seabed refers to the load effect uncertainty
due to variation in weight, stiffness, span length or heights. This implies that it is not applicable for the sag
bend evaluation during installation on uneven seabed.
A γC lower than unity is used in DNVGL-RP-F110 for expansion and global buckling design to represent the
degree of displacement control and uncertainties in, primarily, the pipe-soil properties.
13.4.3 Calculation of nominal thickness
The negative fabrication tolerance is normally given as a percentage of the nominal thickness for seamless
pipes, and as an absolute measure for welded pipes.
The pressure containment criterion gives a minimum required minimum wall thickness, t1. Depending on
the fabrication tolerance format, the implication of the corrosion allowance will be different. For a fabrication
tolerance given as a percentage, % tfab, Equation (13.1) applies.
(13.1)
Correspondingly, the nominal thickness based on an absolute fabrication tolerance, tfab, is given by Equation
(13.2).
(13.2)
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13.4.4 Pressure containment - equivalent format
The format of the pressure containment resistance in Sec.5 is given in a LRFD format. This corresponds to
the traditional format, which usually is expressed in terms of allowable hoop stress, is given in Equation
(13.3).
(13.3)
The differential pressure is here given as a function of the local incidental pressure. Introducing a load
factor, γinc, reflecting the ratio between the incidental pressure and the design pressure, the formula can be
rearranged for the reference point above water, as given in Equation (13.4).
(13.4)
Introducing a usage factor as given in Equation (13.5), the criteria can be given as in Equation (13.6) and
Equation (13.7).
(13.5)
(13.6)
(13.7)
The corresponding usage factors for γinc = 1.10 are given in Table 13-3.
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Table 13-1 Usage factors η for pressure containment
Utilisation factor,αU
1.00
Safety class
Low
0.847
Medium
3)
High
0.802
0.698
0.77
0.67
1)
Pressure test
0.96
(0.843)
0.96
0.813
3)
2)
0.96
(0.838)
1)
In location class 1, 0.802 may be used
2)
In location class 1, 0.77 may be used
3)
Effectively this factor since the pressure test is governing
13.4.5 Pressure containment criterion, design pressure less than 10%
below the incidental pressure
The characteristic pressure when determining the wall thickness is the local incidental pressure. The
submarine pipeline system shall have a pipeline control and safety system which ensures that there is a
-2
probability for exceeding the local incidental pressure at any point in the system less than 10 within a
year. If it can be documented that the ratio between incidental and design pressure, γinc, can be reduced,
a corresponding reduction in wall thickness can be achieved, alternatively a higher design pressure can be
used. For hydraulically softer systems like gas trunk lines, a γinc of 1.05 is often achieved.
13.4.6 High integrity pressure protection system and similar systems
A pipeline is designed for a static pressure without allowing for the pressure loss along the pipe unless
the pipeline is sectionised into parts with different design pressure. Hence, the pipeline will always have a
pressure during normal operation lower than the design pressure due to the pressure drop caused by the
flow of the fluid.
For high pressure wells, this downstream pressure may be reduced on purpose by a choke in order to enable
a lower pressure pipeline downstream. This reduced pressure is dependent on a constant flow and will
increase to the shut-in pressure in case of blockage downstream.
A high integrity pressure protection system (HIPPS) serve the purpose to protect the downstream pipeline
from the shut-in pressure by stopping the flow in case a pressure increase is experience (due to some
blocking down-stream). The closer this blockage is to the HIPPS, the faster will the pressure increase occur.
Hence, the speed of this HIPPS will determine how long part of the pipeline downstream that not can be
protected but designed for the full shut-in pressure. This part is referred to as the fortified zone.
In case of failure of this HIPP system, the downstream pipeline will experience the full shut-in pressure. In
-2
order to take advantage of a HIPP system, the annual probability of this to happen shall be less than 10 .
The resulting annual extreme pressure distribution will then be similar to Figure 13-1, a two peak distribution
where the right peak describes the pressure distribution in case of failure of the HIPPS.
From the example in the figure, it is evident that the over pressure scenario will burst the pipeline (a factor
2.5 times the incidental pressure).
-2
For a failure probability less than 10 this over-pressure may be considered as an accidental limit state
and the methodology in [5.4.10] may be used. The wall thickness will then be the larger of the pressure
containment criterion based:
— on the choke pressure and
— the accidental scenario of the shut-in pressure.
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With the example in Figure 13-1 the accidental scenario will govern the wall thickness design. If the over
pressure would have been less than 20-30% above the incidental pressure, the choke pressure may govern
the design.
The accidental criterion is:
(13.8)
where pf|Di is the failure probability given that the scenario happens and PDi is the probability of the scenario
(over pressure) to happen. In the following, it is assumed that the over pressure scenario will be the overall
contributing accidental scenario and the summation sign is neglected.
For the HIPPS scenario outlined above, the probability of the scenario, PDi, will be equal to the probability of a
blockage to happen times the on-demand-failure of the HIPPS.
PDi = Pblockage · Pfailure on demand(HIPPS)
(13.9)
The resulting wall thickness for the accidental scenario will then be the wall thickness giving the failure
probability required in accordance with Equation (13.8).
Note that the nominal target failure probability in accordance with Sec.2 primarily shall be equal to similar
limit states. The nominal failure probability of the pressure containment criterion is at least one order of
magnitude less than the other limit states target values in Table 2-5.
Figure 13-1 Pressure distribution
13.4.7 Local buckling - collapse
The collapse pressure, pc, is a function of the:
— elastic capacity
— plastic capacity
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— the ovality.
The formulation adopted in this standard is identical as in BS8010, apart from the safety margin. The formula
is given in Equation (13.10) with the defined elastic and plastic capacities in Equation (13.11) and Equation
(13.12).
(13.10)
(13.11)
(13.12)
This third degree polynomial has the following analytical solution:
(13.13)
where:
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13.4.8 Buckle arrestor
The buckle arrestor formula in Sec.5 is taken from Torselletti (2003).
13.4.9 Local buckling - moment
The given formula is valid for 15 < D/t2 < 60 for yielding and ovalisation failure modes. Up to D/t2 equal to
45, these failure modes will occur prior to other failure modes, e.g. elastic buckling, and hence do not need
to be checked.
For D/t2 above 45, elastic buckling has to be checked separately, typically through FE analysis, with D/t2
a sufficient safety margin above the actual D/t2 in order to account for both uncertainty as well as natural
thickness variations.
In addition to check for elastic buckling, a thinner pipe becomes more susceptible to imperfections. Special
considerations shall be made to
— girth welds and mismatch at girth welds, and
— point loads, e.g. point supports.
If both the elastic buckling has been documented to occur beyond the valid range and the implications
of imperfections has found to be acceptable, the criteria may be extended to D/t2 = 60. Derrivation and
comparison of the local buckling criterion see Collberg (2016) and Fyriliev (2016).
13.4.10 Local buckling - girth weld factor
Research on buckling of pipes including girth welds has shown that the girth weld has a significant impact on
the compressive strain capacity, see Ghodsi (1994). A reduction in the order of 40% was found for D/t2 = 60.
There are no other known experiments on the impact from girth welds for lower D/t2.
It is assumed that the detrimental effect is due to on-set of buckling due to imperfections at the weld on the
compressive side. If this is true, this effect will be more pronounced for higher D/t2's. The girth weld factor
should be established by test and/or FE-calculations.
If no other information exists and given that the reduction is due to the misalignment on the compressive
side, the reduction is expected to be negligible at D/t2 = 20. A linear interpolation is then proposed up to D/
t2 = 60.
If no other information exists then the girth weld factor in Figure 13-2 is proposed.
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Figure 13-2 Proposed girth weld factors
13.4.11 Ovalisation
Pipe ovalisation is mentioned in three different places within this standard:
[5.4.12], where the maximum allowable ovalisation O0 = 3%. This applies for the pipeline as installed
condition. This limitation is due to the given resistance formulations which not includes the ovality explicitly,
as well as other functional aspects as stated in the paragraph.
[5.4.4], where the minimum ovalisation O0 = 0.5% to be accounted for in the system collapse check; and
the combined loading. The collapse formula includes the ovality explicitly giving a lower resistance for a
larger ovality, hence a minimum ovality is prescribed.
Table 7-17, dimensional requirements, where the maximum allowable out of roundness to be delivered from
manufacturer is specified.
The ovality of a pipe exposed to bending strain may be estimated by Equation (13.14). This is a characteristic
formula without any safety factors.
(13.14)
For further information, see Murphey (1985).
13.5 API material grades
13.5.1 API material grades
The API requirements to the grades X42 through X80 are listed in Table 13-2. For full details see the API
Specification for Line Pipe (API Specification 5L). The SMYS and SMTS values given in MPa in the table below
are converted from the API specification (in ksi), and differ slightly from the mechanical properties in Table
7-5, which apply for this standard.
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Table 13-2 API material grades
API
Grade
SMYS
SMTS
ksi
MPa
ksi
MPa
X42
42
289
60
413
X46
46
317
63
434
X52
52
358
66
455
X56
56
386
71
489
X60
60
413
75
517
X65
65
448
77
530
X70
70
482
82
565
X80
80
551
90
620
ksi = 6.895 MPa; 1 MPa = 0.145 ksi; ksi = 1000 psi (lb f/in2)
13.6 Pipe-in-pipe
13.6.1 General
Objective
This informative section provides guidance on pipe-in-pipe design and integrity management based on the
criteria given in this standard. It focuses on the general aspects of PiP systems. As new ideas develop these
general aspects may have to be further developed and detailed on a project to project basis.
Pipe-in-pipe systems
Pipe-in-pipe systems are built up of an inner pipe (also called the flowline), carrying the fluid, inside a larger
outer pipe also called carrier, or jacket, pipe. The annulus is dry and normally not pressurised which allows
the use of high performance insulation. This may be a good alternative to expensive wet insulation for deep
water pipelines or for very high temperatures. The annulus can be fully or partially filled by the insulation
material. In case of being partially filled, centralizers spaced at regular predetermined intervals are provided
to protect the insulation from mechanical loading and damage during installation and operation, and to
prevent buckling of the inner pipe inside the outer pipe. PiP systems are increasingly considered as a robust
solution to combat these flow assurance challenges, ensuring that a very low OHTC can be achieved. In
addition, pipe-in-pipe systems are increasingly considered as an additional protective layer against loss of
containment or to withstand the impact force due to third party or trawl/fishing gear interaction. PiP systems
are also used in onshore arctic field developments to safeguard against spillage into the environment due
to mechanical failure of inner pipe. The primary objective for selecting a PiP system is the high thermal
insulation potential. This makes it the preferred solution for challenging flow assurance flowlines. In addition
to the good thermal insulation, secondary advantages are:
— High submerged weight. This may increase the on-set to global buckling due to the high lateral pipe-soil
resistance.
— Axial transfer of forces between the outer and inner pipe. This may reduce the overall expansion of high
pressure/high temperature pipelines.
— High resistance to external impacts. This may also be an advantage in arctic water where the outer pipe
constitutes a second barrier to containment.
— Dry annulus. This may allow different types of instrumentation (e.g. leakage) as well as heating systems
(e.g. water circulation).
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The pipe-in-pipe systems are often project specific and vary in design but can be differentiated by the load
transfer between inner and outer pipe and split into:
— Fully bonded systems, i.e. entire annulus is filled with insulation material.
— Sliding systems, i.e. insulation is achieved by wrapping standard size insulation pads onto the inner pipe.
— Regular multiple (double, quad, etc.) pipe-in-pipe joints with discrete bulkheads.
It is important that the load effect analyses reflect the actual load transfer between the outer and inner pipe.
At the ends of a PiP section, a transition is required from a double wall of a PiP system to a single wall of
the connection system (e.g. to a PLET, PLEM, tie-in spools). This is achieved by using end bulkheads which
act as stress distribution diaphragms within a PiP system. The end bulkheads are generally made of forged,
heat treated material and machined to the required tolerance. At the double wall end, they are welded to the
inner and outer pipes and at the single wall end to the hub flange or spool piece. Thus, end bulkheads have a
conical shape in order to seal the annulus, maintain the concentricity of the system and transfer installation
and operational (expansion) loads between the inner and outer pipes.
As the end bulkheads act as a permanent means of the load transfer between the two parts, they are classed
as pipeline components and are designed in accordance with recognized PVC. However, there are a number
of PVCs that can be used for design and their selection and implementation are at the discretion of the
pipeline operator and designer.
Other components are also included in pipe-in-pipe to achieve specific functionalities, most notably thermal
insulation but also spacers, water stops, heating wires, etc.
Typical elements in pipe-in-pipe systems, in addition to inner and outer pipe, and their purpose are:
— Insulation, as well as insulating the inner pipe, the mechanical strength of the insulation material may be
used for the design of the pipeline if its material properties can be documented. Typical examples of its
use for other properties than thermal are as a spacer to keep inner and outer pipes from contacting or as
a shock absorber against external impact loads.
— Spacers, with the purpose of centralising the inner pipe, preventing buckling of the same, and ensuring an
even space in the annulus. This may be done by the insulation itself or by specific centralisers.
— Water stops, with the purpose of avoiding ingress of water to move along the pipeline annulus, impacting
the insulation properties. This has limited axial structural capacity. Although not their intended purpose,
project experience suggest water stops can also serve as an installation aid in PiP fit-up.
— Bulkheads, with the objective to avoid ingress of water to move along the pipeline annulus and to transfer
the axial loads between the inner and outer pipes. Intermediate bulkheads can also be used during
installation (in deep water conditions) to reduce the compression forces locked-in in the inner pipe.
— Field joints connecting sections of PiP. Different field joint types can affect the behaviour of other elements
in the PiP system. Examples of different types of field joints include:
—
—
—
—
standard girth welds in sliding systems
welded half-shells with the objective to connect outer pipe sections after welding of inner pipe.
sliding sleeves
swaged ends, where the outer pipe is swaged to touch the inner pipe. These often have resin adhered
single- and double-sleeves elements over swaged outer pipe ends.
— Pipelay elements present in the system as an aide to installation. This include forgings such as J-Lay
collars and inner pipe pull-out collars, as well as stiffened pipe sections from ILTA and FTA structures if
they are part of the pipelay string.
The interactions of these elements with the pipes (inner and outer) and with each other should be carefully
assessed, in particular to assess stress and strain concentrations in the vicinity of the area where they
interact with the line pipes. Typical examples are strain concentrations in the vicinity of bulkheads,
waterstops and spacers. The distance between the bulkheads are typically governed by the structural
response, including the degree of sliding, and the installation method. Further, tie-ins and potential hot-taps
should be considered. The design of the bulkheads should also assess consequence assessments related to
damage of the bulkheads. Distance between water stops should be based upon consequence evaluations
Special attention shall be given to construction and welding details and different field joint types, buckle
arrestors etc. Field joint fit-up tolerances and strength variability between pipe joints, sleeves and half shells
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as potential sources of stress/strain concentration should be considered. PiP systems are inherently difficult
to fabricate, hence the manufacturing process (e.g. welding) is often chosen to minimize potential delays.
Likewise, NDT shall be planned and allowed for, requiring sufficient space. The different installation methods
for PiP systems impose different requirements to axial transfer between the pipes and continuity in bending
moment capacity and thereby guide the Pipe-in-Pipe concept selection. Installation methods introducing
plastic strain during installation will require special attention to straightening and residual straightness of the
pipe after installation. For pipe-in-pipe installed by reeling, functionality of the components after installation
need to be assessed including possible knockdown effects on thermal performance due to compression of
insulation and movement of spacers etc.
Design premises
The pipe-in-pipe concept selection process shall include formulation of design premises with primary and
secondary purpose of the different pipe-in-pipe system elements. This will constitute important input for
safety class selection, design including progressive failure evaluations and integrity management planning of
the pipeline system.
The data and description should include the following items specific to PiP systems, as applicable:
—
—
—
—
—
—
—
—
—
Safety class selection for inner and outer pipe.
Installation method and the consequences for the selection and design of the PiP concept.
Expected life history e.g. fabrication, installation, commissioning, operation etc.
Flow assurance – insulation requirements, average and maximum local OHTC, cool down time, bulkhead/
waterstop spacing, arrival temperature requirements, inner and outer pipe temperature profiles, expected
location of low temperature. An operating/shutdown philosophy should be developed as necessary to
safeguard the pipeline from wax and hydrate formations during cool-down below the wax appearance
temperature (WAT).
Attention to possible code breaks in the pipeline system.
Bulkhead design.
Details/properties of components (spacers/water stops).
Field joint system.
Axial and bending continuity.
13.6.2 Safety class
A pipe-in-pipe or bundle system is more complex than a conventional pipeline. Different design configurations
may result in the same probabilities of failure and satisfy the same overall safety class. The designer shall
decide how to satisfy the overall safety class through design of the different components. Safety class should
be determined with respect to the functions the inner/outer pipe is expected to perform. A risk assessment
or consequence analyses may be a helpful tool in this selection process that also shall include progressive
failures. The consequences shall not be limited to structural failures only but also functional failures. The
safety class is normally given by the location and contents of the pipeline. The safety class for a conventional
(single) pipeline is thereby the same for a pipe-in-pipe with the same location and contents. This could (for
example) be described as the nominal pipe-in-pipe safety class. In many loading cases, the resistance of
both pipes is needed to withstand the applied loading safely. In this case there is no redundancy and both
inner and outer pipes shall have the same (nominal) safety class. Most of the time, the outer pipe is used
for insulation purposes only, whereas the inner pipe acts as primary barrier to pressure containment and
hence has to be designed, manufactured and fabricated to suit more stringent requirements. For some
loading cases, the design may have evolved to give the system an element of redundancy. If there is some
redundancy, and this can be demonstrated by carefully considering each relevant failure mechanism, then
the safety class of one or both pipes (typically the outer pipe) may be reduced provided that the combined
safety class is equivalent to, or exceeds, the nominal safety class, and that the consequences of taking
advantage of such redundancy and related issues are fully understood. In most cases, if the thought process
is thoroughly gone through, the safety class of the inner pipe often remains unchanged. In general, it is
not recommended to reduce safety class for the inner pipe, even if there are apparent redundancies to take
advantage of, e.g. collapse in deep waters. That said, sometimes a thinner inner pipe can be attractive, e.g.
to reduce compressive force when designing against upheaval buckling. The challenge is to then consider all
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the failure modes in enough detail, ensure that the mechanisms, consequences and level of redundancy are
understood. Changing the safety class could also have implications further down the life cycle, e.g. during
operation.
Another example of progressive failure is bursting limit state close to a change in location class, e.g. when
entering the safe zone. A containment release of the inner pipe may then travel along the annulus. If the
outer pipe has the same wall thickness in both location class 1 and 2, containment release from the outer
pipe is equal likely in both location classes. Solutions to this could be either to have a thicker outer pipe in
the location class 2 or design a bulkhead that may resist containment release into the annulus.
13.6.3 Global system behaviour
Load effect
Load effect calculation requires knowledge about the actual layout of system, this is a main challenge
compared to a single pipe system. Load effect calculation may therefore have additional uncertainties
compared to single pipe systems, and examples may include:
— Initial condition following installation, such as axial loadings in the individual pipes and residual moment.
— A pipe-in-pipe system that expands (as axial or lateral motions) will influence the axial loads in both
inner- and outer pipe:
— Inner pipe in compression (equal or higher compared to single pipe)
— Outer pipe in tension (higher tension compared to single pipe).
— Axial friction and sliding in between the inner and outer pipe (note that there is no buoyancy on inner pipe
resulting in that even if the friction factor is lower compared to between outer pipe and soil, the friction
force could be large)
— Bending interaction between inner and outer pipe, plasticity in the different pipes, differences in curvature
of the two pipes and load transfer shall be taken into account, see Goplen (2011)
— Temperature difference and different sources of heating
— Influence of spacers, bulkhead and field joint design, position and tolerances
A load effect analysis is required to determine both the global system behaviour as well as the load effect of
each individual pipe for limit state design purposes. For pipe-in-pipe systems the following concerns apply:
— Installation by Reel-lay, J-lay or S-lay
— Holding of inner and outer pipe
— Potential residual curvature
— Residual axial forces
— Installation by reel lay method
— Straightening and residual curvature
— Global buckling
—
—
—
—
Global response and axial sliding
Degree of displacement control for buried pipes
Sources of localised stress/strain concentration and bending moments
Bending stiffness continuity, e.g. due to presence of field joint or bulkhead
System behaviour
The DNVGL-RP-F110 covering global buckling can be applied for a pipe-in-pipe in case the pipeline can be
considered to be fully bonded in the axial and radial direction. Bonding is here related to no movement,
including axial sliding, between the inner and outer pipe. Hence a bonded pipe will have equal displacement
pattern for both inner and outer pipe. An un- bonded pipe-in-pipe will face larger uncertainties and higher
degree of randomness in the initiation of global buckles and post buckling behaviour. This shall be reflected in
the design approach and in the applied safety factors. The friction between the pipes is related to mechanical
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properties of spacers, insulation, rollers etc. that is used in the annulus. The friction is influenced by
curvature in the pipe and the operational conditions of the pipe. The higher pressure and temperature, the
higher friction is obtained. Further, the bending strain capacity of the outer thinner pipe may be lower and
hence influence on the total bending strain capacity of the pipe-in-pipe system.
Restrained force
The effective axial restrained force of a bonded pipe-in-pipe system where there are no axial displacements
between the pipes is given by Equation (13.15).
(13.15)
Reeled pipe-in-pipe systems
A conventional reeled pipe-in-pipe (PiP) consists of the inner and outer pipes, insulation, and a number of
uniformly distributed spacers (or centralisers) which maintain the separation and transfer loads between the
two pipes and protect the insulation. Detailed knowledge of the response of the PiP system during reeling is
a key requirement for installation engineering purposes. The main objectives of the installation engineering
analyses are to check straightener settings, estimate loads on equipment, and to determine a suitable
spacer pitch which avoids crushing of the insulation in the annulus. The reeling installation method can have
an effect on the subsequent in-service behaviour, due to the residual stresses, strains and deformations
imparted on the pipe. Of particular interest are the self-equilibrating residual moments in the inner and outer
pipe and the residual deformation in the inner pipe. A representative moment-curvature plot of the outer
and inner pipes during installation are shown in Figure 13-3. The plot shows the moment and curvature
in the plane of reeling. The plot shows two strain cycles, corresponding to i) spooling on and off the reel,
and ii) passing over the aligner and through the straightener. The greatest curvature in the outer pipe, on
the reel and aligner, is geometrically defined by the reel and aligner radii and is independent of the spacer
location. In contrast, the inner pipe curvature on the reel and aligner depends on the discrete radial loads
transmitted through the spacers, and therefore varies with spacer location. There are two residual momentcurvature effects at the end of the reeling process. Firstly, the inner pipe has a residual curvature which
varies along the PiP axis at the spacer pitch. The residual curvature changes sign between the spacers, and
is greatest in magnitude at each spacer. (A similar but reversed effect occurs in the outer pipe but is smaller
because the equal and opposing spacer force has less influence on the bending of the outer pipe). Secondly,
the inner and outer pipes have residual moments which are equal in magnitude but of opposite sign, such
that the combined residual moment in the PiP is zero. These moments are constant and do not vary with
the spacer pitch. The reeling process also results in near-yield magnitude residual stresses in parts of the
cross-section. The axial stress distributions are complex and depend on the distance from the pipe neutral
axis and the cyclic elastic-plastic response of the pipe material. This elastic-plastic response is influenced by
strain-hardening and the Bauschinger effect, where the elastic limit is modified by the plastic strain history.
The same effects occur in a conventional reeled pipeline, but are much more complex in a PiP due to the
additional interaction between the inner and outer pipes. The full variation in moment as shown in Figure
13-3) and stress distribution are normally calculated by non-linear FE analysis. The overall effect is that
the response of a reeled PiP will depend on the direction of loading with respect to the plane of reeling,
and on the pitch and position of the spacers. The response of a reeled PiP under operational loads will be
different from that of a non-reeled PiP. The difference is relatively small, however, and is normally neglected
during conceptual design and FEED. However these effects may justify more detailed analysis during detailed
design.
Guidance on modelling
Screening of bonded pipe-in-pipe systems can be achieved by considering an equivalent single pipe with
the combined stiffness of the inner and outer pipe, provided plasticity is not predicted in either pipeline.
Movement of the inner pipe relative to the outer pipe mean that this approach is not necessarily conservative
for an unbonded pipe-in-pipe system. The issues associated with movement of the inner pipe relative to
outer pipe include
— Sliding between inner and outer pipes affecting effective force in system and leading to potential axial
localisation effects, e.g. axial load wrinkling
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— The friction between the pipes is related to mechanical properties of spacers, insulation, and rollers
etc. that are used in the annulus. The friction is also influenced by curvature in the pipe and the
operational conditions of the pipe. The higher pressure and temperature, the higher friction is
obtained.
— Bending stiffness of system is not the sum of the inner and outer pipes as they need not have the same
curvature.
— Potential for increased local radius in inner pipe leading to higher buckling resistance being needed than
predicted from the curvature of the outer pipe and hence greater likelihood of global buckling.
— Snaking/helical buckling of inner pipe in outer pipe and hence relief of axial load.
— Response to cyclic loading, potentially larger stress ranges in inner pipe than predicted from equivalent
single pipe.
Miscellaneous
Pipe-in-pipe has a high on-bottom stability level due to the high submerged weight, however, the potential
for sinking into soil, particular fluidized sand or soft clay can be high and should be considered for both the
installation and the operational phase. Anode design will normally be equal to a single pipe.
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Figure 13-3 Moment - curvature of the inner and outer pipe during installation (at spacer and
between spacer locations). Note that the finishing point in the figure not is in equilibrium, i.e. it
will spring back slightly when pipe is released.
13.6.4 Limit states
Most of the limit states listed in Sec.5 will apply to one or both pipes in the pipe-in-pipe system.
Failure modes and PiP specific limit states
A limit state is a state beyond which the structure no longer satisfies the requirements, this means failure
mode in some sense. The limit states are grouped into different limit states categories dependent on the how
severe that failure mode is and includes:
— Ultimate limit state (ULS) category failure is defined as a condition which, if exceeded, compromises the
integrity of the pipeline. Examples of such may be bursting, collapse, buckling and fatigue limit state
(FLS) category and accidental limit state (ALS) category are two sub-categories of the ULS. An ULS failure
often implies release of content.
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— Serviceability limit state (SLS) category failure is defined as a condition which, if exceeded, renders the
pipeline unsuitable for normal operations. Exceedance of a serviceability limit state category shall be
evaluated as an accidental limit state.
Re-assessment of a failure consequences shall be reflected in the safety class, not by changing limit
state category. It is difficult to summarize PiP limit states into clearly defined context due to complexity.
Some PiP system limit states are same as those for a single pipe, but many are associated with insulation
performances. Also, it is unclear whether an individual flooded section is acceptable, and whether dents are
acceptable as they may not affect insulation but can reduce fatigue life and structural performance. The
intention is to try and capture this complexity in the standards or recommended practices so that guidance is
provided to inexperienced engineers. It is important that the design premises sub-section reflects operational
aspects so that they feed into failure mode and limit state considerations. Failure modes for PiP systems may
be summarised as follows:
— Outer pipe collapse without breach: ULS (including FLS which requires caution in application, rigorous
engineering shall be demonstrated); failure modes include:
—
—
—
—
damaged cables/fibres
reduced resistance to bending (progressive failure may cause buckling of the complete PiP system)
reduced U value
ovalization of outer pipe (SLS).
— Outer pipe breach –ULS/SLS. Failure modes include:
—
—
—
—
flooded annulus
loss of U-value
inner pipe collapse
corrosion in annulus.
— Inner pipe breach/loss of inner pipe containment – ULS/SLS. Failure modes include:
— damaged insulation, cables, fibre optic cables (FOCs), etc.
— outer pipe burst - escape to environment
— corrosion of annulus.
— Loss of insulation due to failure of field joint or component – SLS, loss of insulation.
— Failures due to fatigue (FLS), e.g. installation fatigue damage, operational high cycle low stress (VIV or
slug flow pulsations) or low cycle high strain events (lateral buckles and local strain concentrations).
— Loss of flow assurance – SLS.
— Other failure modes:
—
—
—
—
—
local corrosion
local buckling of inner/outer pipe
crushed insulation
water stops for sliding PiP systems
gas permeation into the annulus.
Description of failure modes and limit states should account for project-specific considerations, e.g. for
pipelines in the arctic regions, the outer pipe need to perform pressure containment should the inner pipe
fails. Limit states of the inner pipe should be considered as a single pipe in the absence of more rigorous
engineering. Design of the PiP system should capture induced/progressive failure modes, interaction
between/amongst multiple limit states, and the possibility that combinations/interactions of SLSs may
lead to a more critical limit state for the PiP systems. Limit state criteria in Sec.5 are valid for each of the
pipes. The residual loading from installation should be considered in the analysis. Compared to a single
pipe solution the close to zero pressure in the annulus may imply higher wall thickness in the inner pipe
caused by the pressure containment requirement (burst). Collapse is an issue throughout life time of the
outer pipe as the pressure in the annulus often is close to zero and will be unchanged during lifetime. In
case beneficial combined effect of insulation, spacers etc. in annulus between inner pipe and outer pipe
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shall be considered, such as in collapse or propagating buckling, this shall be documented (e.g. collapse).
Progressive failure mechanisms need to be considered. During design for FLS of PiP systems, S-N curves
and Stress Concentration Factors (SCFs) shall be chosen appropriately. Relevant considerations include:
the inner and outer pipe fit-up, out of roundness, weak/strong inner and outer pipe strength mismatch,
offshore and on-shore field joint criteria in regard to double, quad or hex joints and field joint systems,
KDF, pipelay forgings, PUPs, connectors, collars, J-Lay forgings bulkhead interfaces, and stiffener pieces
to ITA/FTA structures. In addition, localised deformations and fatigue resulting from helical movements of
compressed inner pipe within the PiP annulus may be an additional consideration for certain PiP systems
without centraliser.
Local buckling – combined loading; displacement or load control
Local buckling - combined loading criteria differentiates between:
— load controlled condition (LC condition)
— displacement controlled condition (DC condition).
A load-controlled condition is one in which the structural response is primarily governed by the imposed
loads while a displacement-controlled condition is one in which the structural response is primarily
governed by imposed geometric displacements. The question on if a condition is load controlled or
displacement controlled is wrong. The question should be; how can one take partial benefit of that a
condition is partially displacement controlled? On a general basis this needs sensitivity analyses. In any
sensitivity study the system effect is also important to consider. A uniform moment/curvature cannot
be applied to the whole pipeline at once but will typically occur as a peak moment moving along the
pipeline. This applies to sag bend, stinger and reeling. Local buckling – combined loading will then be
governed by the maximum moment capacity variation along the pipe. This will occur a small distance
(typically in the order of a diameter) into the weak part, when the peak moment moves from strong to
weak section. For such applications, more detailed assessment can be based on a weak link evaluation,
where this weak link is the extreme variation from one joint to another. Pipe-in-pipe systems typically
have numerous stress/strain concentration sites within them capable of serving as weak links along the
production flowline system. Such sites usually associated with half shells, J-lay forgings, sliding single
or double sleeves all have strength, wall thickness and pipe-in-pipe fit-up variability within them. Loss
of integrity from at a critical field joint girth weld during pipelay or through-life operation may result in
progressive failure of the PiP system through water ingress, loss of insulation, movement of the high
P&T loaded inner pipe and a developing cold spot within the production system during operation. All this
can be aided by inadequate field joint welds, missing spacers or water stops. [5.4.6.4] states that a load
controlled design criterion can always be applied in place of a displacement controlled design criterion. For
a single pipe the requirements can be summarised as follows:
—
—
—
—
—
—
buried pipes – DCC
exposed pipe on seabed – LCC with adjusted safety factors
spans, including buckling at spans – LCC
sag bend during installation – LCC
over bend during installation – LCC
reeling during installation – (partially) DCC.
For a PiP system, the outer pipe may generally be treated to be the same as a single pipe. The inner
pipe may for some concepts have a similarity with pipe on stinger, as discussed in guidance note of
[5.4.6.4], where the moment is imposed by discrete spacer points. LCC would always be acceptable, but
it is permitted to go for DCC if demonstrated sufficiently, e.g. when inner pipe movement is restrained by
the outer pipe and the limiting strains can be documented and demonstrated as acceptable for both inner
and outer pipes. It is key that the correct loadings are applied. Loadings will be determined by nominal
or average properties. Resistance, and the highest expected strains, will be determined in sections
with minimum properties. For PiP systems, both system checks and inner/outer pipe checks need to be
performed. Inner and outer pipe should be modelled separately, and force distribution at components.
need to be considered carefully due to possible localization effects.
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Figure 13-4 Illustration of derivation of relevant limit states
13.6.5 In-line components
Pipe-in-pipe bulkheads
Pipe-in-pipe and bundles may include a number of structural load-bearing components, including
bulkhead(s), flanges, collars etc. For some of these components, such as flanges and collars, the design
considerations are the same as for the same component in a conventional pipeline. However bulkheads are
key components which are unique for pipe-in-pipe and bundles. The design of bulkheads for pipe-in-pipe is
discussed below. This also provides relevant guidance for the design of bundle bulkheads.
There are two generic types of bulkhead; end bulkheads and midline bulkheads.
End bulkheads are used in every pipe-in-pipe system. At the ends of a pipe-in-pipe section, a transition is
required from a double wall of a pipe-in-pipe system to a single wall of the connecting piping (to a PLET,
PLEM, tie-in spool etc.). At the double wall side, the bulkhead is connected to the inner and outer pipes. At
the single wall side, the bulkhead is typically connected to a hub flange or spool piece. The bulkhead seals
the annulus, maintains the concentricity of the system and transfers the axial loads between the inner and
outer pipes. The bulkhead design usually adopts a conical shape for effective transfer of high axial loads
between the different components.
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Midline bulkheads are used to connect one section of the pipe-in-pipe system to another section of the same
pipe-in-pipe system. The bulkhead isolates the different sections of the pipe-in-pipe and transfers axial forces
between the inner and outer pipes. The midline bulkhead may be used to transfer forces between the two
pipes during installation or operation, or to provide an annular seal to minimise the extent of damage in the
event of inner or outer pipe failure.
Examples of typical end and midline bulkheads are shown in Figure 13-5 and Figure 13-6. More complex (and
proprietary) designs have also been used, but satisfy the same generic functionality.
Figure 13-5 Example of end bulkhead
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Figure 13-6 Example of midline bulkhead
Design of bulkheads
Bulkhead design should follow the requirements set in [E.8.8.7]. The requirements of a recognised pressure
vessel code should be followed. The codes require FE analysis of the bulkhead. There are three methods of
FE analysis that can be adopted:
— Elastic stress analysis: The analysis is based on elastic material properties only, and can be used where
the bulkhead does not experience any form of plasticity. Stresses associated with different loadings are
categorised as primary and secondary stresses. Different stress limits should be satisfied. This method
requires stress linearization techniques.
— Elastic-perfectly plastic stress analysis. The analysis takes the elastic-perfectly plastic response of the
material (i.e. without any strain hardening) into consideration. The concept of load and resistance factor
design (LRFD) is used where factored loads are compared with the resistance of the component. A
global plastic collapse load is established in the FE model, equal to the load that causes overall structural
instability in the bulkhead. This method provides a more economic design than elastic analysis but it is not
suitable for reeled bulkheads for which an elastic-plastic stress analysis is required.
— Elastic-plastic stress analysis. The analysis follows the same approach as an elastic-perfectly plastic
stress analysis, but takes into consideration the actual post-yield response of the material (i.e. with strain
hardening). This method is used for the design of highly loaded components (with gross plasticity) such as
reeled bulkheads.
The pressure vessel codes identified in Table 5-13 generally adopt two or more of the three methods listed
above.
Pressure vessel codes classify the type of load into several categories and assign load factors for each
category. In the assessment of pipeline components, the loads should be classified carefully as the load
categories in pressure vessel codes are not necessarily representative of the loads experienced by subsea
pipelines.
In the development of FE models, geometrical variability between the different components, including
dimensional variation and misalignment, should be considered. Similarly, for the elastic-plastic analyses, the
effect of variation in material properties should be considered. Sensitivity studies should be performed to
investigate all possible combinations (lower bound, best estimate and upper bound) of material properties
and dimensions. The critical case is usually a combination of upper and lower bounds.
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The use of a pressure vessel code requires a specific code break between this standard and the Pressure
Vessel Code, e.g. ASME VIII Division 2. See [5.6.1]. The code break location has to ensure that the overall
level of safety is maintained.
The component is generally more rigid than the pipeline. The presence of the component may introduce
stress or strain concentrations in the adjacent linepipe and the intermediate girth weld. The selection of the
code break location should take into account the following:
— All possible limit states or failure modes;
— Differences in material properties, including the manufacturing process;
— The effect of the component on the overall integrity of the pipeline
The current guidance in [5.6.1.7] states that the standard or recommended practice for [the] pipeline
component shall include pipe sections affected by the presence of the component. The pipe sections affected
by the component are assessed using a pressure vessel code, and the remaining sections unaffected by the
presence of the component are assessed using the pipeline standard or recommended practice. Given that
the presence of the component extends into the adjacent linepipe, these linepipe sections shall be assessed
against the (generally more conservative) pressure vessel code. It can be difficult to identify a satisfactory
design. The designer may be forced to change the code break location for different loading condition, with
acknowledgement that this is in disagreement with the concept in this standard of code breaks at a fixed
location for all loading scenarios.
This guidance on the extent of the component has therefore been removed. The modified Figure 5-3 shows
the two main options for defining the code break location.
Figure 5-3 (a) illustrates a code break at the material transition between the parts manufactured in
accordance with this standard requirements (i.e. linepipe) and the component.
This material-based code break allows the designer to take credit for different material properties and
different partial safety factors between this standard and the pressure vessel codes. The designer may also
consider the differences in manufacture of forgings for pressure vessels and forgings for subsea applications.
The pressure vessel code often requires a greater wall thickness than the linepipe standard. This means that
a wall thickness transition is required. This generally requires the manufacture of a machined transition piece
and additional girth weld.
Figure 5-3 (b) illustrates a code break within the component. The code break is placed at a location on the
component side of the wall thickness transition. This geometry-based code break avoids the need for an
additional transition piece. However part of the component now comes under this standard. The designer
should ensure that material specification for this section also satisfies the material requirements of this
standard.
The geometry-based code break illustrates an example where the manufacturing process and material
specification should meet the appropriate material requirements for more than one standard or
recommended practice. The manufacturing process includes fabrication and installation. For example,
the swaging process used for some proprietary pipe-in-pipe bulkheads imposes a specific geometry by
deformation of the inner or outer pipes, and may modify the material properties. Similarly, large plastic
strains may modify the material properties of a reeled pipe-in-pipe. The material properties after all
manufacturing, fabrication and installation activities should remain within the requirements of the relevant
standard or recommended practicee.
Pressure vessel codes are based on limit states and are therefore conceptually compatible with design
standards or recommende practices for subsea pipelines, such as this standard. In practice, however, the
levels of safety in pressure vessel and pipeline standards or recommended practices are inconsistent. The
partial safety factors prescribed in the pressure vessel codes are not necessarily valid for components in
subsea pipelines. The load factors in pressure vessel codes are intended for any component under any
loading condition, but were not derived for the load conditions typically experienced within pipelines. In
particular, the displacement controlled condition commonly used in the design of subsea pipelines cannot be
fully considered in pressure vessel codes. Similarly, the factors on material properties do not account for the
more stringent methods used to manufacture components for subsea pipelines.
Within this standard, there is a clear provision to perform a problem specific reliability based analysis. This
route can be used to reduce the conservatism in the partial safety factors used in the pressure vessel codes.
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In the future, this approach could be developed further to derive generic partial safety factors for the design
of pipeline components. This may remove the need for artificial code breaks and achieve consistent levels of
safety across the pipeline and its components.
Reeled bulkheads
Bulkheads in reeled pipe-in-pipe have traditionally been welded into the pipeline on the lay vessel ramp
during installation. Welding the bulkhead into the pipeline at the spoolbase and reeling the bulkhead onto the
reel is more cost effective than offshore welding.
The reel lay method induces gross plastic deformation in the pipeline. Bulkheads are generally much stiffer
than the pipeline; the reeling of a bulkhead does not normally induce significant strains in the body of the
bulkhead, but can introduce very high strains in the bulkhead nibs and adjacent linepipe.
Design of reelable pipe-in-pipe bulkheads requires a design by analysis approach using non-linear FE analysis
to predict the strains during installation. The high strains mean that a full elastic-plastic stress analysis
(including the actual post-yield response of the material, with strain hardening) is required. The pressure
vessel code approach to the analysis may be adopted, but the absence of pressure during reeling, and
the very high level of strain, mean that the pressure vessel code criteria are not appropriate. In addition,
most pressure vessel codes (e.g. ASME VIII Division 2) have serviceability criteria which require that the
component (in this case the reeled bulkhead) to have satisfactory performance following application of a load
(in this case reeling). The implementation of this criterion is under the discretion of the designer. The analysis
determines the maximum strains that occur in the weaker nibs and linepipe. The designer uses the analysis
to develop a bulkhead design which provides an adequate margin of safety against collapse during reeling.
For a number of bulkheads in the pipeline, load combination a, Table 4-4 is appropriate with a functional load
effect factor of 1.2, and a condition load factor of 0.82 in Table 4-5. A reduction in condition load factor may
be allowed if demonstrated by FE analysis.
-2
A low safety class in Table 2-5 with annual probability of failure less than 10 (equivalent to a safety index,
β of 2.32) can be used to assess the serviceability limit state during the reeling and unreeling phase provided
that the repair of potential damage is feasible and may be performed during laying.
A lower probability of failure may be appropriate if the above criteria are not satisfied.
Geometric and material variability has a significant influence on the maximum strain during reeling. This
should be considered in the analysis. The most onerous combination of upper and lower bounds may govern
the design. In this case, load combination b in Table 4-4 may be used.
The probability of buckling may be reduced by placing pipe joints which closely match the actual bulkhead
dimensions and yield stress on either side of the bulkhead. Fracture assessment of the girth welds shall be
performed as per DNVGL-RP-F108.
13.6.6 Construction
Requirements to manufacture, testing and documentation of inner pipe and outer pipe should follow relevant
requirements given in Sec.7.
Relevant requirements to manufacture, testing and inspection of pipe-in-pipe bulkhead that typically is a
forged component are given in [8.3] through [8.5].
Applicable requirements to assembly welding of pipe-in-pipe are given in App.C.
For pipe-in-pipe and bundles the inner pipe and outer pipe should have equal requirements to manufacture of
linepipe, welding and connection. However, some differences to requirements may be considered depending
on project specific requirements, e.g. in case of H2S service, it could relevant only to specify Suppl. Req. S
for the inner pipe. Temperature should be monitored in the individual pipes during construction. Tolerances
related to distance keepers (spacers, foam etc.) to be established and documented. Measure sliding between
inner and outer pipe during construction of stalks
The installation process will impact in service pipe-in-pipe system design in terms of:
— acceptable stress/strain limits from ECA weld defect criteria
— presence of SCF and SnCF from installation fit up tolerances
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— strength mismatches between sleeve half shell and J-Lay forgings
—
—
—
—
residual reel lay moments
post installation inner and outer pipe tensions
possible presence of FTA/ILTA structures along the pipelay string
level of pipelay induced fatigue damage at key sites along the route.
The effect of the installation by reeling on the various parts of the pipe-in-pipe system should be accounted
for including straightening of inner and outer pipe during off-reeling, see Endal (1998). For installation by Slay or J-lay sliding of the inner pipe shall be evaluated.
Leak testing of the annulus can be carried out to increase confidence in the construction and installation of
the pipeline, e.g. pressure testing of the annulus.
During system pressure test there will be no external pressure on inner pipe, and this may affect the wall
thickness sizing of the inner pipe.
13.6.7 Operation
The principles of integrity management are described in Sec.11, and guidance is given in DNVGL-RPF116Integrity management of submarine pipeline systems. Specific considerations for PiP systems wrt
integrity management are given here. There are two main structural failure modes for pipelines:
— loss of containment – leakage or rupture
— gross deformation of the pipe cross-section.
Other known failure modes from past pipe-in-pipe project experience include:
—
—
—
—
—
corrosion
blockage of flow (loss of pipeline function) due to, e.g. insulation defects and hydrate formation
failure of carrier pipe and/or field joint, leading to fatigue failure of inner pipe
stuck PIG
anchor dragging.
As for single pipe, the premises for operations are set in the design phase and will be governing for the
operations phase. The design philosophy for a PiP system will include:
— function of pipe-in-pipe elements (incl. handling of progressive failure)
— inspection and monitoring
— contingency and repair.
This includes primary and (possibly) secondary functions for outer pipe, inner pipe, annulus and components,
e.g. inner pipe collapse, outer pipe burst, acceptability of limited outer pipe local damage. An example of
a progressive failure may be leak into annulus, followed by damaged insulation and blockage of flow. A PiP
system is more complex compared to a single pipe system, however, it may be regarded as a robust system
due to the double wall. Table 13-4 gives and overview of specific considerations for PiP systems with respect
to integrity management: A risk assessment scheme may be used to map this in more detail (see example
in Table 13-5). In the design phase, the purpose of having such a matrix is to increase awareness of Pipeline
Integrity Management (PIM). Documentation of the integrity in the operation phase may be limited for a
pipe-in-pipe compared to a single pipe. This will again affect the life-time extension and re-assessment of the
pipeline.
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Table 13-3 Integrity consideration for PiP systems
Aspect
Comment
Condition of annulus and insulation
Detection of leaks into annulus (from internal or external
fluids) may not be easily identified and the associated
environment in the annulus cannot be fully controlled or
reversed.
Inspection capabilities
Inspection possibilities are more limited for pipe-in-pipe,
and hence detection of corrosion in annulus and external
corrosion is challenging. As it stands, there is no single
inspection system or technique that is capable of inspecting
both the inner and the outer pipe simultaneously.
Repair and intervention methods
Limited opportunities and more complicated compared to
single pipe.
Table 13-4 Risk assessment scheme example
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13.7 Installation
13.7.1 Safety class definition
Installation of pipeline and pipeline components is normally defined as safety class low. However, if the
installation activity impose a higher risk to personnel, environment or the assets, a higher safety class should
be used. Such activities may typically be repair, where the system is shut down, but the production medium
is still within the system, modifications to existing system or installation operations where failure may lead to
extensive economic loss, see also [13.2.1].
13.7.2 Coating
In case no other data is available the following criterion should be used. The mean overbend strain:
(13.16)
should satisfy:
(13.17)
where:
D
R
εmean
εaxial
γcc
εcc
= outer steel diameter
= stinger radius
= calculated mean overbend strain
= axial strain contribution
= 1.05 safety factor for concrete crushing
= limit mean strain giving crushing of the concrete. Positive strain denotes tensile strain.
Note the sign convention is that compressive is negative in the above criterion.
The mean overbend strain at which concrete crushing first occurs depends on the pipe stiffness, the concrete
strength and thickness, the axial force and the shear resistance of the corrosion coating. Crushing occurs at
lower mean overbend strains for lower concrete strength, lower axial force, higher pipe stiffness and higher
shear resistance. If no other information is available, concrete crushing may be assumed to occur when the
strain in the concrete (at the compressive fibre in the middle of the concrete thickness) reaches (-)0.2%.
For concrete coating of 40 mm thickness or more, together with asphalt corrosion coating, a conservative
estimate of εcc is (-)0.22% for 42" pipelines and (-)0.24% for 16" pipelines, with linear interpolation in
between.
See Endal (1995) or Ness (1995).
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13.7.3 Simplified laying criteria
This simplified laying criteria may be used as a preliminary simplified criterion of the local buckling check
during early design stages. It does not supersede any of the failure mode checks as given in the normative
part of the standard.
In addition to the simplified stress criteria given below, the limit states for concrete crushing ([13.7.2]),
fatigue ([5.4.8]) and rotation ([5.8.3]) shall be satisfied. Reference is further made to Endal et. al. (1995) for
discussion on the rotation limit state.
For static loading at the overbend the calculated strain shall satisfy criterion I in Table 13-5. The strain shall
include effects of bending, axial force and local roller loads. Effects due to varying stiffness (e.g. strain
concentration at field joints or buckle arrestors) need not be included.
For static plus dynamic loading the calculated strain shall satisfy criterion II in Table 13-5. The strain shall
include all effects, including varying stiffness due to field joints or buckle arrestors.
For combined static and dynamic loads in the sagbend the equivalent stress in the sagbend and at the stinger
tip shall be less than
σeq < 0.87 times fy
(13.17)
with all load effect factors set to unity.
Effects due to varying stiffness or residual strain from the overbend may be ignored.
For the sagbend in deeper water, where collapse is a potential problem, the normative buckling criteria in the
standard shall also be satisfied.
The following calculation requirements to the lay analysis apply both when using Limit State Criteria and
Simplified Criteria:
— The analysis shall be conducted using a realistic non-linear stress-strain (or moment-curvature)
representation of the material (or cross-section).
— For calculation of strain concentration at field joints, non-linear material properties of the steel, the
concrete and the corrosion coating shall be considered.
— The characteristic environmental load during installation is to be taken as the most probable largest value
for the sea-state (Hs, Tp) considered with appropriate current and wind conditions. The sea-state duration
considered is not to be less than 3 hrs.
— If the dynamic lay analysis is based on regular waves, it shall be documented that the choice of wave
heights and periods conservatively represents the irregular sea-state (Hs, Tp).
Table 13-5 Simplified criteria, overbend
Criterion
X70
X65
X60
X52
I
0.270%
0.250%
0.230%
0.205%
II
0.325%
0.305%
0.290%
0.260%
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13.8 References
Banneyake, R., Sun, J., Jukes, P., & Chen, J. (2009). Analytical Estimation of Pretension Requirements to
Inner Pipe of Pipe-in-Pipe Flowline in Ultra Deep Water Using J-Lay Installation. Houston: OTC.
Chen, Q., & Chia, H. K. (2010). Pipe-In-Pipe walking – Understanding the mechanism, evaluating and
mitigating the phenomenon. Shanghai: ASME.
Collberg, L., and Levold, E., DNV-OS-F101 Combined Loading Criterion – Background and Derivation, 35th
International Conference on Offshore Mechanics and Arctic Engineering, OMAE 2016
Dixon et al., Deepwater Installation Techniques for Pipe-in-Pipe Systems Incorporating Plastic Strains,
OTC2003 15373
Fyrileiv, O., Marley, M., & Pettersen, S. (2011). Design methodology for axial force response of Pipe-In-Pipe –
A probabilistic approach. Rotterdam: ASME.
Fyrileiv, O., Collberg, L. (2016) DNV-OS-F101 Combined loading criterion - Range of application and
comparison with other criteria. 35th International Conference on Ocean, Offshore and Arctic Engineering,
OMAE 2016-54741
Ghodsi Nader Yoosef-, Kulak G. L. and Murray D. W.; Behaviour of Girth Welded Line-pipe, University of
Alberta department of Civil Engineering, Structural Engineering Report No. 23, 1994
Goplen S., Fyrileiv O., Grandal J. P., Børsheim L. Global buckling of pipe-in-pipe - Structural response and
design criteria, OMAE 2011-49960, OMAE 2011, Rotterdam
Harrison and McCarron, Potential Failure Scenario for High-Temperature, Deepwater Pipe-in-Pipe, OTC2006
18063
Jiao G., Sotberg T., Bruschi R., Verley R. and Mørk K; The SUPERB Project: Wall Thickness Design Guideline
for Pressure Containment of Offshore Pipelines, Proceedings of OMAE'96 conference, Florence, Italy
Jukes et al., 2008 The Sequential Reeling and Lateral Buckling Simulation of Pipe-in-Pipe Flowlines Using
Finite Element Analysis for Deepwater Applications, ISOPE 2008
Jukes, P., Eltaher, A., Sun, J., & Harison, G. (2009). Extra High-Pressure High-Temperature (XHPHT) Flowlines
– Design. Honolulu: ASME.
Murphey D.E. and Langner C. G. Ultimate pipe strength under bending collapse and fatigue, Offshore
Mechanics and Arctic Engineering symposium, New Orleans 1985.
Mørk. K, Spiten J., Torselletti E., Ness O. B., and Verley R.; The SUPERB Project and DNV'96: Buckling and
Collapse Limit State, Proceedings of OMAE'97 conference, Yokohama, Japan
Ness O. B. and Verley R.; Strain Concentrations in Pipelines with Concrete Coating: An Analytical Model,
Proceedings of OMAE'95 conference, Copenhagen, Denmark
Sotberg, T. ; Moan, T. ; Bruschi, R. and Jiao, G.; The SUPERB project: recommended target safety levels for
limit state based design of offshore pipelines. Yokohama : ASME, 1997. 1997 16th International Conference
on Offshore Mechanics and Arctic Engineering. ss. v 5, p 71-77
Sun, J., & Jukes, P. (2009). From installation to operation - a full-scale finite element modelling of deep-water
pipe-in-pipe system. Honolulu, Hawaii: ASME.
Torseletti E., Bruschi R., Marchesani F., Vitali L. Buckle Propagation and its Arrest: Buckle Arrestor Design
Versus Numerical Analyses and Experiments, OMAE2003-37220
Vitali L., Bruschi R., Mørk K., Verley R.(1999); Hotpipe project - Capacity of pipes subjected to internal
pressure, axial force and bending moment, Proc. 9th Int. Offshore and Polar Engineering Conference, Brest
1999.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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APPENDIX A FRACTURE LIMIT STATE OF GIRTH WELDS
This appendix is intentionally left empty.
Content of this appendix from previous editions has been implemented in DNVGL-RP-F108.
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APPENDIX B MECHANICAL TESTING AND CORROSION TESTING
B.1 General
B.1.1 Objective
B.1.1.1 This appendix addresses methods for mechanical testing, chemical analysis and corrosion testing of
materials and products.
B.1.2 Application
B.1.2.1 This appendix is applicable for the testing of all types of materials with testing requirements as
referred to in this standard.
B.1.2.2 Test laboratories shall meet the requirements of ISO 17025 or an accepted equivalent.
B.2 Mechanical testing and chemical analysis
B.2.1 General requirements to selection and preparation of samples and
test pieces
B.2.1.1 Selection of samples and preparation of test pieces shall as far as applicable be in accordance with
the general conditions of ISO 377. In addition the following requirements apply.
B.2.1.2 For any of the mechanical tests, any test piece that shows material imperfections unrelated to the
intent of the particular mechanical test, whether observed before or after testing, may be discarded and
replaced by another test piece from the same pipe. If the test results are influenced by improper sampling,
machining, preparation, treatment or testing, the test sample shall be replaced by a correctly prepared
sample from the same pipe and a new test performed.
B.2.1.3 For tensile tests, CVN impact tests, DWT tests, guided-bend tests, and flattening tests of linepipe,
the samples shall be taken, and the corresponding test pieces prepared, in accordance with the applicable
reference standard.
B.2.1.4 Samples and test pieces for the various test types for linepipe shall be taken from alternating pipe
ends in the locations as shown in Figure 5 and Figure 6 in ISO 3183 and as given in Table 7-9, and the details
stated below. Sampling from alternating pipe ends over the course of a reasonable time period (e.g. shift,
day, week) shall be reviewed, and during this period an approximately equal number of front and tail ends
shall be tested.
B.2.1.5 The location of samples and test pieces from components should be according to [8.5].
B.2.1.6 For induction bends and bolts the location of samples and test pieces shall be according to the
recognised standard or specification used for manufacture, as specified for the relevant component in Sec.8.
B.2.1.7 For welds not performed as part of linepipe fabrication, including girth welds, samples shall be taken
in accordance Figure C-1 and Figure C-2.
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B.2.2 Chemical analysis
B.2.2.1 Samples for heat and product analyses shall be taken and prepared in accordance with ISO 14284.
Methods and procedures for chemical analysis shall be according to recognised industry standards, of
acceptable uncertainty. Results from chemical analyses shall be given with the same number of digits (or
more) as given in the specification of the product and/or in this standard.
Guidance note:
ISO/TR 9769 gives a list of available international standards providing chemical analysis methods, with information on the
application and precision of the various methods.
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B.2.2.2 The chemical composition of the weld overlay shall be obtained at the surface of the overlay after
machining of the overlay such that the minimum distance from the surface to the fusion line is either 3 mm
or the minimum thickness specified for the finished component, whichever is the lesser.
B.2.3 Tensile testing
B.2.3.1 Tensile testing shall be carried out in accordance with the requirements in this appendix and ISO
6892 or ASTM A370. The test piece configuration and possible test piece flattening shall be the same for all
the delivered items. The extensometer shall be attached to a machined surface. Double sided extensometers
should be used.
Guidance note:
The elongation requirements in Table 7-5 are based on a formula identical with API 5L and ISO 3183. The formula is calibrated
for use with tensile test specimens prepared according to ASTM A370 (i.e. API test specimens). It should be noted that the same
material tested with specimens based on ASTM A370 and ISO 6892 can give different elongation results due to the different
specimen geometries.
In general it should be considered to use ASTM A370 specimens for normal tensile testing, since this would give the best
correspondence with the requirements in Table 7-5.
Tensile specimens based on ISO 6892 can be used, but then the acceptance criteria should be reviewed. Some options are (i)
use the values from Table 7-5, (ii) during qualification perform a number of tests on both types of specimens to establish an
empirical correspondence for the specific material or (iii) define elongation criteria based on relevant testing experience and
existing documentation.
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B.2.3.2 Base material tensile properties may be determined using rectangular or round test pieces at the
manufacturers discretion, see [B.2.3.3] and [B.2.3.4], respectively.
B.2.3.3 Rectangular test pieces shall represent the full wall thickness. Longitudinal/axial test pieces shall not
be flattened. Transverse/tangential test pieces shall be flattened. Test piece grip ends may be flattened or
machined to fit the test machine's grips. Weld beads may be ground flush and local imperfections may be
removed.
B.2.3.4 Round test pieces shall be obtained from non-flattened samples. For longitudinal/axial tensile tests
when t ≥ 19.0 mm, such test pieces shall be 12.7 mm in diameter, or largest obtainable diameter if 12.7 mm
is not possible. For transverse or tangential tensile tests the diameter of such test pieces shall be as given in
Table 21 in ISO 3183, except that the next larger diameter may be used at the option of the manufacturer.
B.2.3.5 For testing when D < 219.1 mm full-section longitudinal/axial test pieces may be used at the option
of the manufacturer.
B.2.3.6 If agreed, ring expansion test pieces may be used for the determination of transverse yield strength.
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B.2.3.7 All weld tensile tests shall be carried out using round test pieces.
Guidance note:
All-weld tensile specimens are not required to conform to the sizes in Table 21 in ISO 3183, see [B.2.3.4] above. The all-weld
tensile specimen shall be as large as possible when considering that the gauge length material shall be only weld metal.
Note that the grip area of the tensile specimens can contain material from the HAZ and also base metal. This will not influence the
results for the weld metal on the gauge length.
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B.2.3.8 For pipes to be tested according to supplementary requirement P and when ECA is to be performed,
specimens should be of proportional type with gauge length:
(B.1)
where S0 is the cross-section area of the specimen. If the test results shall be used as basis for ECA, the
whole stress-strain curve shall be reported.
Guidance note:
For supplementary requirement P additional tensile testing is required, and of particular interest is the elongation. The industry
experience and qualification testing is primarily based on proportional specimens according to ISO 6892. Consequently the criteria
have been established for such tensile specimens, and it is not relevant to use specimens based on ASTM A370 for supplementary
requirement P.
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B.2.3.9 Test pieces for transverse weld (cross weld) tensile shall be rectangular and in accordance with
[B.2.3.3]. The weld reinforcement shall be removed on the face and root sides by machining or grinding. The
tensile strength shall be determined (yield stress and elongation is not required).
B.2.3.10 Transverse weld tensile test pieces of clad or lined linepipe shall be performed on the full thickness
of the carbon steel, after removal of the CRA, taking care not to reduce the C-Mn steel wall thickness.
All-weld tensile testing of load bearing weld overlay
B.2.3.11 Test pieces shall be round with maximum obtainable diameter. The test pieces shall be machined
from the weld overlay transverse to the welding direction.
Tensile testing of girth welds relevant for ECA
B.2.3.12 Full stress-strain curves shall be established from the testing. If possible, the test specimens shall
either be all-weld specimens (recommended) or transverse all-weld specimens as follows:
— All-weld tensile specimens: The specimens shall be round and of proportional type
— Transverse all-weld specimens: The recommended geometry is as indicated in Figure B-13. If the weld
metal portion of the specimen is instrumented with strain gauges, three strain gauges are recommended
around the circumference. The width of the weld metal should be minimum 6mm. For narrow bevels,
it is recommended that the positioning of the test specimen is validated by polishing and etching to
ensure that the reduced section of the specimen contains 100% weld metal. Possible yield plateau may
be difficult to discover using this specimen type and the tensile stress-strain curve is typically 5% higher
compared with results using traditional round specimens. Hence, if this specimen is used as input to FE
analyses or for demonstrating weld metal strength, over-match the engineering stress shall be lowered
5%
If the weld and pipe geometry is such that it is difficult to establish stress-strain curves representing the weld
metal, one of the following solutions shall be followed:
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— Dedicated special specimens may be tested if possible, similar specimen geometry shall then be fabricated
also from the parent pipe material
— Weld strength over-match with sufficient confidence may be demonstrated by cross-weld tensile testing
— If none of the above is possible and an ECA is required full-scale testing of representative worst case girth
welds (i.e. geometry, material properties and weld defect) shall be tested to the worst case loading to
demonstrate the fracture integrity
B.2.4 Charpy V-notch impact testing
B.2.4.1 The test pieces shall be prepared in accordance with ASTM A370 without any prior flattening of the
material. Testing according to ISO 148-1 is acceptable if agreed and the required striking radius (2 or 8 mm)
is specified. Each set shall consist of three specimens taken from the same test coupon. Full size test pieces
shall be used whenever possible.
B.2.4.2 The size, orientation and source of the test pieces from linepipe shall be as given in Table 22 in
ISO 3183, except that the next smaller test piece size may be used if the absorbed energy is expected to
exceed 80% of the full-scale capacity of the impact testing machine. Additional sets of HAZ test pieces shall
be sampled compared to ISO 3183, see Table 7-7 and Table 7-8. The notch locations shall be according to
[B.2.4.8] - [D.2.1.5].
Guidance note:
It is not necessary to impact-test linepipe with combinations of specified outside diameter and specified wall thickness not covered
by Table 22 in ISO 3183.
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B.2.4.3 For seamless pipe with t > 25 mm and delivered in the quenched and tempered condition, one
additional set of transverse direction CNV test pieces shall be sampled 2 mm above the internal surface
during MPQT.
B.2.4.4 The locations of test pieces taken from components shall be according to [8.5].
B.2.4.5 The locations of test pieces taken from girth welds shall be according to Figure C-2.
B.2.4.6 Whenever possible, and apart for testing of the root of double sided welds, the test pieces shall be
sampled 2 mm below the external surface. A smaller distance than 2 mm shall be used if necessary (due to
the dimensions of the material) to make specimens with the largest possible cross section. The axis of the
notch shall be perpendicular to the surface.
B.2.4.7 For weld metal and HAZ tests, each test piece shall be etched prior to notching in order to enable
proper placement of the notch.
B.2.4.8 For production welds other than HFW pipe the axis of the notch of the weld metal sample shall be
located on, or as close as practical to, the centreline of the outside weld bead.
B.2.4.9 For test pieces taken in the weld of HFW pipe, the axis of the notch shall be located on, or as close
as practical to the weld line.
B.2.4.10 The HAZ notch positions comprise the fusion line (FL), the FL+2 mm and the FL+5 mm test pieces
shall be sampled in the positions given in Figure B-3 to Figure B-8, with the notch positions as applicable. FL
test pieces shall always be located such that 50% of weld metal and 50% of HAZ is sampled.
B.2.4.11 Impact testing of clad/lined pipes shall be performed in the carbon steel portion of the material.
B.2.4.12 When dissimilar materials are welded, both sides of the weld shall be tested.
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B.2.4.13 For weld overlay material contributing to the transfer of load across the base material/weld overlay
fusion line, impact testing of the weld overlay and HAZ shall be performed (i.e. when the overlay is a part of
a butt joint or acts as a transition between a corrosion resistant alloy and a carbon steel). The longitudinal
axis of the specimen shall be perpendicular to the fusion line and the notch parallel to the fusion line.
B.2.5 Bend testing
B.2.5.1 The test pieces for guided-bend testing of the seam weld of welded pipe shall be prepared in
accordance with ISO 7438 or ASTM A370, and Figure 8 in ISO 3183.
B.2.5.2 For pipe with t > 19.0 mm, the test pieces may be machined to provide a rectangular cross-section
having a thickness of 18.0 mm. For pipe with t ≤ 19.0 mm, the test pieces shall be full wall thickness curvedsection test pieces.
B.2.5.3 For SAW pipes, the weld reinforcement shall be removed from both faces.
B.2.5.4 The guided-bend test shall be carried out in accordance with ISO 7438. The mandrel dimension shall
not be larger than that determined using the following equation, with the result rounded to the nearest 1
mm:
(B.2)
where:
A gb
D
t
e
1.15
= the mandrel dimension, expressed in millimetres (inches)
= the specified outside diameter, expressed in millimetres (inches)
= the specified wall thickness, expressed in millimetres (inches
= the strain, as given in Table 23 of ISO 3183
= the peaking factor.
B.2.5.5 Both test pieces shall be bent 180° in a jig as shown in Figure 9 in ISO 3183. One test piece shall
have the root of the weld directly in contact with the mandrel; the other test piece shall have the face of the
weld directly in contact with the mandrel.
B.2.5.6 Clad pipes shall be subjected to bend testing (the longitudinal weldment shall not be included).
Specimens shall be of full thickness, including the full thickness of the clad layer. The width of the specimens
shall be approximately 25 mm. The edges may be rounded to a radius of 1/10 of the thickness.
The specimens shall be bent 180° around a former with a diameter 5x the pipe wall thickness.
B.2.5.7 Longitudinal weld root bend test shall include the corrosion resistant alloy.
— The longitudinal axis of the weld shall be parallel to the specimen, which is bent so that the root surface is
in tension.
— The width of the longitudinal root bend specimen shall be at least twice the width of the internal weld
reinforcement or maximum 25 mm. The edges may be rounded to a radius of 1/10 of the thickness.
— The internal and external weld reinforcement shall be removed flush with the original surfaces.
— The thickness of the specimen shall be equal to the base material thickness or a maximum of 10 mm, as
shown in Figure B-2.
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— The specimen shall be bent to an angle of 180° using a former with diameter 90 mm.
Bend testing for WPQT according to App.C
B.2.5.8 Bend testing shall be performed in accordance with ISO 5173. Bend test specimens shall have full
wall thickness. The width of root and face bend specimens shall be approximately 25 mm. The width of side
bend specimens shall be 10 mm. The edges may be rounded to a radius of 1/10 of the thickness.
B.2.5.9 Bend test of clad pipes shall be performed on full thickness of the pipe, including the corrosion
resistant alloy.
B.2.5.10 The weld reinforcement on both faces shall be removed flush with the original surfaces, as shown
in Figure B-1. The weld shall be located in the centre of each specimen.
B.2.5.11 The specimens shall be bent to an angle of 180° using a former with diameter depending on the
specified minimum yield stress SMYS for the parent material. For materials with SMYS up to 415 MPa, the
former diameter shall be 4x thickness of the test specimen. For materials with SMYS equal to or exceeding
415 MPa, the former diameter shall be 5× thickness of the test specimen.
B.2.5.12 If necessary, e.g. if one of the materials to be joined has a lower yield stress than the other,
guided bend testing in accordance with ISO 5173 may be applied, using the same roller diameter as for the
conventional bend testing.
B.2.5.13 After bending, the welded joint shall be completely within the tensioned region.
B.2.5.14 Side bend test specimens shall be used for bend testing of weld overlay. The test specimens shall
be sampled perpendicular to the welding direction.
— For pipes, the test specimens shall sample the full thickness of the weld overlay and the base material.
For heavy section components, the thickness of the base material in the specimen shall be at least equal
to 5x the thickness of the overlay.
— The thickness of side bend specimens shall be 10 mm. The edges may be rounded to a radius of 1/10 of
the thickness. The central portion of the bend test specimen shall include an overlap area.
— The specimens shall be bent to an angle of 180°. For base materials with SMYS up to 415 MPa the former
diameter shall be 4x thickness of the test specimen. For base materials with SMYS equal to or exceeding
415 MPa the former diameter shall be 5x thickness of the test specimen.
B.2.6 Flattening test
B.2.6.1 The test pieces shall be taken in accordance with ISO 8492, except that the length of each test piece
shall be ≥ 60 mm. Minor surface imperfections may be removed by grinding.
B.2.6.2 The flattening test shall be carried out in accordance with ISO 8492. As shown in Figure 6 in ISO
3183, one of the two test pieces taken from both end-of-coil locations shall be tested with the weld at the 6
or 12 o’clock position, whereas the remaining two test pieces shall be tested at the 3 or 9 o’clock position.
Test pieces taken from crop ends at weld stops shall be tested at the 3 or 9 o’clock position only.
B.2.7 Drop weight tear test
B.2.7.1 Drop weight tear test shall be carried out in accordance with API RP 5L3.
B.2.7.2 Full thickness specimens shall be used where possible. Reduced thickness specimens may be used
subject to purchaser agreement. The testing temperature reduction given in API RP 5L3 shall apply.
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The specimens shall be taken transverse to the rolling direction or pipe axis, with the notch perpendicular to
the surface.
For high toughness steels ductile crack initiation from the notch tip shall be acceptable (contrary to API RP
5L3, Clause 7.1).
B.2.8 Fracture toughness testing
B.2.8.1 For qualification testing of linepipe weld metal, see [B.2.8.4] and [B.2.8.13] to [B.2.8.15]:
— for qualification testing of girth welds, see [B.2.8.16] to [B.2.8.20].
B.2.8.2 The fracture toughness testing applicable to this standard is:
— Fracture toughness testing, J or CTOD (δ), a minimum of 3 specimens is required for each notch position.
— Fracture toughness resistance curve testing, J-Δa (J R-curve) or δ-Δa (δ R-curve), a minimum of 6
specimens is required for each notch position.
B.2.8.3 Fracture toughness testing should be performed using one of the following type of specimens:
— single edge notched tension (SENT), or
— single edge notched bend (SENB) specimen.
Pipeline walls are predominately loaded in tension independent of the loading mode. The specimen for such
conditions should be the SENT specimen, as shown in Figure B-12. See also to BS 8571 for further guidance.
Guidance note:
Commonly used testing standards describe methods for determining the fracture resistance from deeply notched SENB (Single
Edge Notched Bend) or CT (Compact Tension) specimens. These specimens, both predominantly loaded in bending, have high
crack tip constraint and will hence give lower bound estimates for the fracture resistance that can be used for conservative
fracture assessments for a large range of engineering structures. The SENB specimen can also be used but this is likely to result in
unnecessarily conservative fracture toughness.
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B.2.8.4 Fracture toughness testing as required in Sec.7 for weld metal shall be CTOD testing of SENB
specimens.
B.2.8.5 Other test specimen configurations may be used for deriving the fracture toughness for use in an
ECA provided that the fracture toughness can be derived from experimental measurement, e.g. load vs. clip
gauge displacement and that it is justified that the crack tip constraint of the test specimen is not smaller
than for the most severe pipeline weld defect assessed in the ECA.
B.2.8.6 Testing of SENB specimens shall be carried out in compliance with the latest revisions of ISO 12135
and ISO 15653 or an equivalent standard.
All SENT testing shall be performed in accordance with BS 8571.
B.2.8.7 Post-test metallography shall be applied to the specimens designated for FL/HAZ testing in order to
establish if the crack tip has been successfully located in the target microstructure.
The specimen is considered qualified if:
— the pre-crack tip is not more than 0.5 mm from fusion line
— grain coarsened heat affected zone (GCHAZ) micro-structure is present within a region confined by a
plane perpendicular to the crack plane through the crack tip and a parallel plane 0.5 mm ahead of the
crack tip.
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B.2.8.8 Testing of SENB specimens are acceptable, see [B.2.8.3], also with reduced notch length. However,
for use in an ECA the specimen notch length shall not be chosen shorter than the height of the most severe
weld defect assessed in the ECA.
The fracture toughness for SENB test specimens can be derived from the load vs. clip gauge displacement
record according to the following formulae:
(B.3)
where:
(B.4)
where Apl is the area under the load vs. crack mouth displacement (CMOD) curve. For definitions of the other
parameters it is referred to BS 7448, ISO 12135 and ASTM E1820 and Δa is the crack extension after testing.
B.2.8.9 If the total displacement, Vg, is measured at a distance z ≤ 0.2a from the physical crack mouth then
the CMOD can be calculated from:
(B.5)
B.2.8.10 The CTOD-value, δ, can be calculated from J according DNVGL-RP-F108.
B.2.8.11 The following information shall be reported from J/CTOD testing:
—
—
—
—
—
—
—
load vs. crack mouth opening displacement curves of all tests
crack measurements (a0)
j or δ results
test temperature
material condition (possible pre-straining and aging history)
welding procedure and weld metal designation
parent pipe designation.
B.2.8.12 The following information shall be reported from J R-curve or δ R- curve testing:
—
—
—
—
—
—
load vs. crack mouth opening displacement curves of all tests
crack measurements (a0 and Δa)
J-Δa or δ-Δa results
test temperature
material condition (possible pre-straining and aging history)
welding procedure and weld metal designation
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— parent pipe designation.
B.2.8.13 The following applies to fracture toughness testing of linepipe as required during MPQT:
δ fracture toughness testing of the weld metal shall be performed using SENB specimens.
B.2.8.14 Testing shall be conducted on through thickness notched specimens with the specimen orientated
transverse to the weld direction (the corresponding notation used by ISO 15653 is NP). The notch shall be
located in the weld metal centre line.
B.2.8.15 The number of valid CTOD or J tests for each location shall be minimum 3. The characteristic CTOD
or critical J value shall be taken as the lowest from 3 valid tests or selected in accordance with BS 7910. Only
specimens that are qualified with respect to crack tip location by post-test metallographic examination shall
be considered valid.
B.2.8.16 The specimen for fracture toughness testing of girth welds should be the SENT (single edge
notched tension) specimen. The calculation and performance of SENT testing shall be according to DNVGLRP-F108.
B.2.8.17 The SENT specimens shall be designed with a Surface Notch (SN), since this is the relevant
orientation for defects in the welds.
B.2.8.18 The notch positions and welding procedures to be tested shall be agreed. The notch may be
introduced either from the outer surface or from the inner surface. Typically the main line procedure(s), the
through thickness procedure(s) and the partial repair procedure(s) shall be tested as illustrated in Figure B-9
and specified in DNVGL-RP-F108.
Guidance note:
The FL/HAZ should be notched from the outer surface. Such notching is empirically more successful because the crack growth
tends to grow towards the base material. Hence, a crack tip at the FL boundary is typically growing through the HAZ if it is notched
from the outer surface.
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B.2.8.19 For situations involving plastic deformation and possibility of unstable fracture caused by tearing,
crack resistance curve testing (preferably J R-curve) shall be performed of the girth weld. If the SENT
specimen is tested, which is recommended, the testing shall be in accordance with DNVGL-RP-F108.
B.2.8.20 In case segment testing will be performed referece is given to DNVGL-RP-F108. The level of testing
and the test procedure shall be adjusted accoring to the loading considered.
B.2.9 Specific tests for clad and lined linepipe
B.2.9.1 Shear testing shall be performed in accordance with ASTM A264 (Standard Specification for Stainless
Chromium-Nickel Steel-Clad Plate, Sheet and Strip) or ASTM A265 (Standard Specification for Nickel and
Nickel-Base Alloy-Clad Steel Plate), whichever is relevant.
B.2.9.2 Gripping force of lined pipe shall be measured by the residual compressive stress test, in accordance
with Clause 7.3 b of API 5LD.
B.2.10 Metallographic examination and hardness testing
B.2.10.1 Macro examination shall be performed at 5× to 10× magnifications (for HFW the examination
shall be performed at minimum 40× and be documented at 10× to 20× magnification). Macro examination
shall be conducted on specimens given in Figure B-10 and Figure B-11, as applicable. The macro section
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shall include the whole weld deposit and in addition include at least 15 mm of base material on each side
measured from any point of the fusion line. The macro-section shall be prepared by grinding, polishing, and
etched on one side to clearly reveal the fusion line and HAZ.
The macro examination of weld overlay shall be sampled transverse to the welding direction. The width of
the macro section shall be minimum 40 mm. The face exposed by sectioning shall be prepared by grinding,
polishing and etched by a suitable etchant to clearly reveal the weld and heat affected zone.
B.2.10.2 Samples for optical metallography shall be prepared using standard procedures, and further etched
using a suitable etchant in order to reveal the microstructure.
Micro examination of duplex stainless steels shall be performed and documented at a minimum magnification
of 400X.
The ferrite content of the base material and weld metal shall be measured according to ASTM E562.
B.2.10.3 Hardness testing of base material and weld cross-section samples shall be carried out using the
Vickers HV10 method according to ISO 6507-1.
B.2.10.4 For pipe base material tests, individual hardness readings exceeding the applicable acceptance limit
may be considered acceptable if the average of a minimum of three and maximum of six additional readings
taken within close proximity does not exceed the applicable acceptance limit and if no such individual reading
exceeds the acceptance limit by more than 10 HV10 units.
B.2.10.5 Hardness test locations for SMLS pipe shall be as shown in Figure B-10 a), except that:
— when t < 4.0 mm, it is only necessary to carry out the mid-thickness traverse
— for pipe with 4.0 mm ≤ t < 6 mm, it is only necessary to carry out the inside and outside surface
traverses.
B.2.10.6 Hardness testing of welds shall be performed on the specimens used for macro examination, and
as shown in Figure B-10 b) and c), and Figure B-11. The hardness test indentations should be documented
on images of macro specimens and attached to the WPQR.
B.2.10.7 For SAW, HFW and MWP the following applies:
— for pipe with t < 4.0 mm, it is only necessary to carry out the mid-thickness traverse
— for pipe with 4.0 mm ≤ t < 6 mm, it is only necessary to carry out the inside and outside surface
traverses.
B.2.10.8 In the weld metal of SAW and MWP welds, a minimum of 3 indentations equally spaced along each
traverse shall be made. In the HAZ, indentations shall be made along the traverses for each 0.5 - 1.0 mm
(as close as possible but provided indentation is made into unaffected material). The first indentation in the
HAZ shall be placed as close to the fusion line as possible and with a maximum distance of 0.5 mm between
the centrepoint of the indentation and the fusion line, according to Figure B-10.
Guidance note:
Testing should be carried out to ensure that the highest and lowest level of hardness of both parent metal and weld metal is
determined.
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B.2.10.9 Hardness testing of clad/lined pipes shall have one additional hardness traverse located in the
thickness centre of the CRA material. See Figure B-11.
B.2.10.10 For hardness testing of weld overlay hardness testing shall be performed at a minimum of 3 test
locations: in the base material, in the HAZ and in each layer of overlay up to a maximum of 2 layers.
B.2.10.11 Surface hardness testing, e.g. of suspected hard spots detected by visual inspection, shall be
carried out in accordance with ISO 6506, ISO 6507, ISO 6508 or ASTM A370 using portable hardness test
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equipment. Depending on the method used the equipment shall comply with ASTM A956, ASTM A1038 or
ASTM E110.
B.2.11 Straining and ageing
B.2.11.1 Th strain ageing test is applicable if the cold forming during pipe manufacture of C-Mn and clad/
lined steels exceeds 5% strain and for Supplementary requirement F. This test does not apply to linepipe
delivered with a final heat treatment (e.g. normalising or quench and tempering).
A test coupon shall be machined from the pipe material and aged at 250°C for one hour. Thereafter, the
specified number of Charpy V-notch specimens shall be machined from the middle of the coupon. The
orientation of the specimens shall be longitudinal to the coupon centreline, with the notch perpendicular to
the surface of the test coupon.
B.2.11.2 Pre-straining is applicable to:
— Linepipe material to be qualified in accordance with supplementary requirement P.
— Girth welds to be qualified in accordance with DNVGL-RP-F108 (ECA) if subjected to plastic deformation.
B.2.11.3 Pre-straining can be carried out as full scale (reversed) bending of whole pipes sections or as
tension/compression straining of material cut from the pipe wall (segment specimens).
B.2.11.4 When full scale bending is applied whole pipes sections they shall be instrumented with strain
gauges on the outside of the pipe wall in the 12 and 6 o'clock positions, see Figure B-14 a). A sufficient
number of strain gauges shall be fitted along the length of the test section to ensure an efficient monitoring
of the strain along the whole test section. If reeling installation is simulated it is recommended to bend the
pipe against formers with the correct radiuses.
B.2.11.5 When pre-straining cut material such material shall be fitted with strain gauges on each of the
opposite sides with respect to the smallest measure on the cross-section, see Figure B-14. A sufficient
number of strain gauges shall be fitted along the length of the test section to ensure an efficient monitoring
of the strain along the whole test section. If the test machine is not sufficiently rigid, strain gauges shall also
be fitted either sides along the long cross-section.
B.2.11.6 The strain gauges shall be logged with sufficient frequency during the straining cycle to ensure
efficient monitoring of the cycle.
B.2.11.7 The pre-straining shall be carried out in such a way that the characteristic strain (see below)
reaches at least the strain levels to be simulated.
B.2.11.8 The characteristic strain shall for cut material (segments or strip specimens) be defined as the
mean value of the strains measured on the outside and inside of the pipe side with the highest strain. For full
scale bending of spool pieces/pipe sections the characteristic strain should be achieved by bending against
a former with the actual radius. If a former is not used the material which will be used for later material
testing shall at least reach the target strain (characteristic strain), where the strain is measured at the outer
curvature.
B.2.11.9 The differences between strain gauges may be large due to buckling of the segment/strip
specimens during compression. If fracture toughness testing of the FL shall be performed from a strained
specimen the FL against the parent pipe with strain level equal to the target strain shall be tested.
B.2.11.10 After straining for supplementary requirement P, the samples shall be artificially aged at 250°C for
one hour before testing. Regarding artificial ageing for ECA, see DNVGL-RP-F108.
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B.2.12 Testing of pin brazings and aluminothermic welds
B.2.12.1 2 test specimens shall the sectioned transverse to the anode lead and 2 test specimens
parallel with the anode lead for copper penetration test. The specimens shall be prepared and etched for
metallographic examination. The examination shall be performed at a magnification of 50X. The fusion line of
the weld/brazing shall at any point not be more than 1.0 mm below the base material surface. Intergranular
copper penetration of the base material shall not at any point extend beyond 0.5 mm from the fusion line.
B.2.12.2 HV10 hardness tests shall be made on each of the specimens for copper penetration
measurements. A traverse shall be made across the weld/brazing zone. The traverse shall consist of
minimum 10 indentations; two in the heat affected zone (HAZ) on each side of the weld/brazing, two in
the HAZ under the weld/brazing and two in the base material on each side of the weld/brazing. The HAZ
indentations shall be made as close to the fusion line as possible.
B.2.12.3 The maximum hardness shall not exceed the limits given in App.C as applicable for the intended
service and type of material.
B.2.12.4 The test specimen for the pull test shall be mounted in a tensile testing machine and secured in the
cable in one end and the base material in the other end. Force shall be applied until the specimen breaks.
The specimen shall break in the cable.
B.3 Corrosion testing
B.3.1 General
B.3.1.1 For certain material and fluid combinations where improper manufacture or fabrication can cause
susceptibility to corrosion related damage, the need for corrosion testing during qualification and/or
production of materials shall be assessed. Certain corrosion tests are further applicable to verify adequate
microstructure affecting toughness in addition to corrosion resistance. This subsection describes test
requirements and methods for corrosion testing.
B.3.2 Pitting corrosion test
B.3.2.1 This test is applicable to verify CRAs’ resistance to pitting and crevice corrosion by oxidising and
chloride containing fluids, e.g. raw seawater and other water containing fluids (including treated seawater)
with high residual contents of oxygen and/or active chlorine. For duplex stainless steels, this test is further
applicable to verify adequate microstructure after manufacturing or fabrication.
B.3.2.2 Testing shall be carried out according to ASTM G48, Method A.
B.3.2.3 Location of specimens is given in Figure C-1 and Figure C-2.
B.3.2.4 The minimum recommended size of test specimens is 25 mm wide by 50 mm long by full material
thickness (except as allowed by [B.3.2.5]). For welds, at least 15 mm of the base material on each side of
the weld shall be included in the test specimen.
B.3.2.5 Test specimens from clad/lined pipe shall be machined to remove the carbon steel portion and shall
contain the full weld and any heat affected zone in the corrosion resistant alloy. The specimen thickness shall
as a minimum be 1 mm where one of the surfaces is representing the inside of the pipe.
B.3.2.6 Rolled surfaces shall be tested as-received, i.e. without mechanical preparation. The root and the
cap side of the welds are only to be prepared with the intention of removing loose material that will interfere
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with weighing prior to and after testing. Cut faces shall be ground (500 grid) and sharp edges smoothed off.
The specimen shall subsequently be pickled to reduce the susceptibility of cut surfaces to end-grain attack.
For duplex stainless steels and austenitic grades with PRE > 30, 20% nitric acid + 5% hydrofluoric acid, 5
minutes at 60°C is adequate.
B.3.2.7 The test solution shall be prepared according to the referenced standard.
B.3.2.8 Specimens for corrosion testing of the weld overlay shall be machined from the base material
side. The remaining surface of the specimen shall be representative for the weld overlay at the minimum
distance from the fusion line (equal to 3 mm or the minimum weld overlay thickness specified for the finished
machined component, whichever is the lesser). The opposite surface of the specimen shall be machined such
that the thickness of the specimen is 2 mm. The size of the specimen shall be 25 × 25 mm in length and
width.
B.3.3 Hydrogen induced cracking test
B.3.3.1 Testing for Hydrogen Induced Cracking (HIC), also referred to as StepWise Cracking (SWC), as
defined in ISO 15156 is applicable to rolled C-Mn steel linepipe and pipeline components. Testing shall be
according to ISO 15156-2, B.5 (referring to NACE TM0284).
B.3.3.2 Tests should be conducted in a medium complying with NACE TM0284, Solution A.
If agreed, tests may be conducted:
— in 5% mass fraction NaCl + 0.4 mass fraction CH3COONa and pH adjusted to required value using HCl or
NaOH (see ISO 15156-2:2003, Table B.3)
— with a partial pressure of H2S appropriate to the intended application
— with acceptance criteria that are equal to or more stringent than those specified in [7.9.1.10].
Values of crack length ratio, crack thickness ratio, and crack sensitivity ratio shall be reported. If agreed,
photographs of any reportable crack shall be provided with the report.
B.3.4 Sulphide stress cracking test
B.3.4.1 For qualification of new materials (i.e. not listed for H2S service in ISO 15156-2/3), testing shall
be conducted on specimens from at least 3 heats of material. Qualification testing shall include testing of
simulated girth welds and for welded pipe also seam welds, in addition to longitudinal samples of the base
material. Specimen preparation, testing procedures and acceptance criteria shall comply with ISO 15156,
using triplicate specimens for each testing condition (i.e. heat of material and environment).
B.3.4.2 Materials listed for H2S service in ISO 15156 but not meeting the requirements in [7.9.1], (e.g.
maximum hardness or contents of alloying or impurity elements) may be qualified by testing for resistance to
Sulphide Stress Cracking (SSC) as specified in [B.3.4.1], except that testing shall be carried out on material
representing the worst case conditions to be qualified (e.g. max. hardness or max. sulphur content).
B.3.4.3 As an option to purchaser, SSC testing may be carried out for qualification of pipe manufacturing.
One longitudinal base material sample shall be taken from each test pipe.
B.3.4.4 For welded linepipe, testing shall include one additional sample transverse to the weld direction
(samples W or WS according to Figure 5 in ISO 3183) and shall contain a section of the longitudinal or helical
seam weld at its centre.
B.3.4.5 Three test pieces shall be taken from each sample. Test pieces for four-point bending SSC tests
should be ≥ 115 mm long × 15 mm wide × 5 mm thick. Samples may be flattened prior to machining test
pieces from the inside surface of the pipe.
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B.3.4.6 Tests should be performed in accordance with NACE TM0177, using Test Solution A. A four-point
bend test piece in accordance with ISO 7539-2 shall be used and the test duration shall be 720 h. The test
pieces shall be stressed to a fraction of AYS appropriate for the pipeline design, however minimum 80% of
the material AYS.
Figure B-1 Bend test specimens
Figure B-2 Longitudinal root bend test specimens
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— The FL specimen shall sample 50% WM and 50% HAZ.
— The FL+5 mm sample is applicable to WPQT only.
Figure B-3 Charpy V-notch impact testing specimen positions for single sided welds with t ≤ 25
mm
— The FL specimen shall sample 50% WM and 50% HAZ.
— The FL+ 5 mm sample is applicable to WPQT only.
Figure B-4 Charpy V-notch impact test specimen positions for single sided welds with t > 25 mm
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—
—
—
—
The specimens indicated in the root area are only applicable when t > 25 mm).
For t > 25 mm, sampling shall be from both ID and OD of longitudinal seam during pipe mill MPQT.
The FL specimen shall sample 50% WM and 50% HAZ.
The FL+5 mm samples are applicable to WPQT only (not at pipe mill).
Figure B-5 Charpy V-notch impact test specimen positions for double sided welds
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— The specimens indicated in the root area are only applicable when t > 25 mm).
Figure B-6 Charpy V-notch impact test specimen positions for HF welds
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— The FL specimen shall sample 50% WM and 50% HAZ.
— The FL+5 mm sample is applicable to WPQT only.
Figure B-7 Charpy V-notch impact test specimen positions for full thickness repair welding of
narrow gap welds
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— The FL specimen shall sample 50% WM and 50% HAZ.
— The FL+5 mm sample is applicable to WPQT only.
Figure B-8 Charpy V-notch impact test specimen positions for partial thickness repair welding
Figure B-9 Illustration of typical notch positions for fracture toughness testing of girth welds
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Figure B-10 Hardness locations in a) seamless pipes, b) HFW pipe, and c) fusion welded joints.
Figure B-11 Hardness locations clad materials
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Figure B-12 The clamped SENT (Single Edge Notched Tension) specimen
Figure B-13 Tensile specimen for determination of stress/strain curves of weld metals in the weld
transverse direction
Figure B-14 Instrumentation of pipe section of samples for pre-straining of materials
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APPENDIX C WELDING
C.1 General
C.1.1 Objective
C.1.1.1 This appendix gives requirements to all welding on submarine pipeline systems with exception of
longitudinal seam welding in pipe mills that is given in Sec.7.
C.1.2 Application
C.1.2.1 This appendix applies to all fabrication involving shop-, site- or field welding including post weld heat
treatment.
C.1.2.2 The base materials covered by this appendix are:
— C-Mn and low alloy steels
— corrosion resistant alloys (CRA) including ferritic austenitic (duplex) steel, austenitic stainless steels,
martensitic stainless steels (13Cr), other stainless steels and nickel based alloys
— clad and lined steels.
The base material requirements are specified in Sec.7 and Sec.8.
C.1.2.3 Welding may be performed with the following processes (see ISO 4063) unless otherwise specified:
—
—
—
—
—
—
—
—
Shielded Metal Arc Welding, SMAW (Process ISO 4063-111).
Flux Cored Arc Welding with active gas shield, G-FCAW (Process ISO 4063-136).
Flux Cored Arc Welding with inert gas shield, G-FCAW (Process ISO 4063-137).
Gas Metal Arc Welding with inert gas shield, GMAW (Process ISO 4063-131).
Gas Metal Arc Welding with active gas shield, GMAW (Process ISO 4063-135).
Tungsten Inert Gas Arc Welding, GTAW (Process ISO 4063-141).
Submerged Arc Welding, SAW (Process ISO 4063-12).
Plasma arc welding, PAW (Process ISO 4063-15) may be used for specific applications.
Guidance note:
GMAW and FCAW (downhill only) are regarded as methods with high potential for non-fusing type defects.
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C.1.2.4 The following processes (see ISO 4063) may be used for specific applications subject to agreement:
—
—
—
—
Laser beam welding, LBW (Process ISO 4063-52).
Electron beam welding, EBW (Process ISO 4063-51).
Electro slag welding.
Plasma transferred arc welding, PTA.
C.1.2.5 Mechanised and automatic welding systems where previous experience is limited, or where the
system will be used under new conditions, shall be subject to a more extensive pre-qualification programme
or documentation before they may be used. The extent and the contents of a pre-qualification programme for
such mechanised welding systems shall be agreed before start up. The contractor shall prove and document
that the welding systems are reliable and that the process can be continuously monitored and controlled.
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C.1.3 Definitions
C.1.3.1 The following definitions are used in this appendix:
Term
Description
welder
person who performs the welding
manual welder
welder who holds and manipulates the electrode holder, welding gun, torch or
blowpipe by hand
welding operator
welder who operates welding equipment with partly mechanised relative movement
between the electrode holder, welding gun, torch or blowpipe and the work piece.
manual welding
welding where the welding parameters and torch guidance are controlled by the
welder
partly-mechanised welding
welding where the welding parameters and torch guidance are controlled by the
welder, but where the equipment incorporates wire feeding
mechanised welding
welding where the welding parameters and torch guidance are fully controlled
mechanically or electronically but where minor manual adjustments can be performed
during welding to maintain the required welding conditions
automatic welding
welding where the welding parameters and torch guidance are fully controlled
mechanically or electronically and where manual adjustment of welding variables
during welding is not possible and where the task of the welding operator is limited to
preset, start and stop the welding operation
C.2 Welding equipment, tools and personnel
C.2.1 Welding equipment and tools
C.2.1.1 Inspection of the workshop, site or vessel prior to start of welding shall be required. This shall
include verification of calibration and testing of all tools and welding equipment used during qualification/
production welding.
Guidance note:
ISO 3834-2 gives quality requirements for welding both in workshops, sites or vessels that may be applicable for submarine
pipeline systems.
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C.2.1.2 Welding equipment shall be of a capacity and type suitable for the work. The equipment shall be
calibrated and maintained in good working condition.
C.2.1.3 The control software for mechanised and automatic welding systems shall be documented. The
name and unique version number of control software and the executable programme in use shall be clearly
visible, e.g. on displays and/or printouts. For mechanized welding, a welding system which displays the
instantaneous heat input on screen with outputs for recording various parameters should be used.
C.2.1.4 All welding equipment shall have a unique marking for identification.
C.2.1.5 Calibration status and the validity of welding, monitoring and inspection equipment shall be
summarised giving reference to the type of equipment, calibration certificate and expiry date.
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C.2.1.6 Welding return cables shall have sufficient cross-section area to prevent concentration of current and
shall be securely attached to prevent arc burns.
C.2.2 Personnel
C.2.2.1 All personnel involved in welding related tasks shall have adequate qualifications and understanding
of welding technology. The qualification level shall reflect the tasks and responsibilities of each person in
order to obtain the specified quality level.
Welding co-ordinator
C.2.2.2 The organisation responsible for welding shall nominate at least one authorised welding co-ordinator
in accordance with ISO 14731 to be present at the location where welding is performed. The welding coordinator shall have comprehensive technical knowledge according to ISO 14731, paragraph 6.2.a.
Welding operators and welders
C.2.2.3 Through training and practise prior to qualification testing, the welding personnel shall have an
understanding of (see Annex D of ISO 9606-1):
—
—
—
—
fundamental welding techniques
welding procedure specifications
relevant methods for non-destructive testing
acceptance criteria.
C.2.2.4 Welding operators performing automatic welding shall be qualified according to ISO 14732.
C.2.2.5 Welders performing manual, partly-mechanised welding and mechanised welding shall be qualified
for single side butt welds of pipes or plates in the required principal position in accordance with ISO 9606-1
or other relevant and recognised standards, for the respective positions, material grades and welding
processes. These requirements are also applicable for welders performing temporary welds and tack welds.
C.2.2.6 Welders shall be qualified for single side butt welding of pipes in the required principal position.
Welders may be qualified for part of the weld, root, fillers or cap by agreement. Repair welders will be
qualified for all types of repair after successfully being tested on full penetration repair providing the welding
processes are the same for the particular section. Minimum repair length shall be 300 mm, and the repair
shall be performed in the most difficult position expected (normally 6 o’clock position).
C.2.2.7 The qualification test shall be carried out with the same or equivalent equipment to be used during
production welding, and should be at the actual premises, i.e. work shop, yard, and vessel. Use of other
premises shall be specially agreed.
C.2.2.8 Qualification NDT shall be 100% visual examination, 100% radiographic or ultrasonic testing, and
100% magnetic particle or liquid penetrant testing. Test requirements and acceptance criteria shall be in
accordance with [D.2].
C.2.2.9 When using processes which have high potential for non-fusing type defects, including G-FCAW ,
bend testing shall be performed with the number of bend tests according to ISO 9606-1. Bend testing may
be omitted in situations where AUT is applied during welder qualification.
C.2.2.10 A welder or welding operator who has produced a complete and acceptable welding procedure
qualification is thereby qualified.
Retesting
C.2.2.11 A welder may produce additional test pieces if it is demonstrated that the failure of a test piece is
due to metallurgical or other causes outside the control of the welder/welding operator.
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C.2.2.12 If it is determined that the failure of a test is due to welder’s lack of skill, retesting shall only be
performed after the welder has received further training.
Period of validity
C.2.2.13 The period of validity of a welder qualification shall be in accordance with the standard used for
qualification. A qualification can be cancelled if the welder/welding operator show inadequate skill, knowledge
and performance.
C.2.2.14 When a qualification testing of recent date is transferred to a new project, the welding personnel
shall be informed about particular project requirements for which their welding performance will be especially
important.
Identification of welders
C.2.2.15 Each qualified welder shall be assigned an identifying number, letter or symbol to identify the work
of that welder.
C.2.2.16 Qualified welders shall be issued with and be carrying an ID card displaying the identifying number,
letter or symbol.
C.2.2.17 The Welding Coordinator shall maintain a list of welders ID stating the qualification range for each
welder.
Thermal cutters and air-arc gougers
C.2.2.18 Personnel to perform air-arc gouging shall be trained and experienced with the actual equipment.
Qualification testing may be required.
Operators for pin brazing and aluminothermic welding
C.2.2.19 Operators that have performed a qualified procedure test are thereby qualified.
C.2.2.20 Other operators shall each complete three test pieces made in accordance with the procedure
specification prior to carrying out operation work. Each test piece shall pass the test for electrical resistance
and mechanical strength according to Table C-6.
C.2.3 Qualification and testing of welding personnel for hyperbaric dry
welding
C.2.3.1 Requirements for qualification and testing of welding personnel for hyperbaric dry welding are given
in [C.9].
C.3 Welding consumables
C.3.1 General
C.3.1.1 Welding consumables shall be suitable for their intended application, giving a weld with the required
properties and corrosion resistance in the finally installed condition.
C.3.1.2 Welding consumables for arc welding shall be classified according to recognised classification
schemes.
C.3.1.3 Welding consumables and welding processes shall give a diffusible hydrogen content of maximum 5
ml/100g weld metal unless other requirements are given for specific applications in this appendix. Hydrogen
testing shall be performed in accordance with ISO 3690.
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C.3.1.4 For the FCAW welding processes it shall be documented that the hydrogen content of the deposited
weld metal will be below 5 ml diffusible hydrogen per 100 g weld metal under conditions that realistically can
be expected for production welding.
C.3.1.5 Welding consumables for processes other than manual or mechanised arc welding may require
special consideration with respect to certification, handling and storage.
C.3.1.6 Depletion of alloying elements during welding performed with shielding gases other than 99.99%
argon shall be considered.
C.3.1.7 All welding consumables shall be individually marked and supplied with an inspection certificate type
3.1 according to EN 10204 or equivalent. Certificate type 2.2 is sufficient for SAW flux.
Cellulose coated electrodes
C.3.1.8 Cellulose coated electrodes may be used only subject to agreement for welding of pipeline girth
welds in C-Mn linepipe with SMYS ≤ 450 MPa. If used, see additional requirements in [C.5.1.8].
C.3.1.9 Use of cellulose coated electrodes is not permitted for:
— repair welding of pipeline girth welds
— welding of pipeline girth welds in C-Mn linepipe with SMYS > 450 MPa.
Data Sheet
C.3.1.10 Each batch of welding consumables shall be delivered in accordance with a manufacturer’s data
sheet, which shall state:
— guaranteed maximum value for diffusible hydrogen in the deposited weld metal
— the guaranteed minimum and maximum levels of C, alloying elements and any other intentionally added
elements
— guaranteed mechanical properties (tensile and impact)
— determined under defined reference conditions. The data sheet shall, when relevant, also give
recommendations for handling/recycling of the welding consumables in order to meet the guaranteed
maximum value for diffusible hydrogen in the deposited weld metal.
Guidance note:
The contractor responsible for the welding and the welding consumable manufacturer should agree on the content and the
specified limits in the data sheets.
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C.3.2 Chemical composition
C.3.2.1 All welding consumables shall be delivered in accordance with manufacturer's data sheets, which
shall state the minimum and maximum levels of C, Mn, Si, P, S, micro-alloying elements and any other
intentionally added elements.
C.3.2.2 For solid wire and metal powders, the chemical analysis shall represent the product itself. The
analysis shall include all elements specified in the relevant classification standard and the relevant data
sheet.
C.3.2.3 For coated electrodes and cored wires, the analysis shall represent the weld metal, deposited
according to ISO 6847. The analysis shall include all elements specified in the relevant classification standard
and the relevant data sheet
C.3.2.4 When H2S service is specified, the chemical composition of the deposited weld metal shall comply
with ISO 15156. The Ni-content in welding consumables for girth welds in C-Mn steel may be increased up to
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2% Ni, provided that other requirements in ISO 15156 are fulfilled, and that the welding procedure has been
tested for resistance to SSC.
C.3.2.5 The chemical composition of the weld overlay materials shall comply with the material requirements
specified for the applicable type of overlay material or with a project specification.
C.3.3 Mechanical properties
Pipeline girth welds
C.3.3.1 Weld metal in pipeline girth welds shall, as a minimum have strength, ductility and toughness
meeting the requirements of the base material.
C.3.3.2 For girth welds exposed to strain εl,nom< 0.4%, the yield stress (Rt0.5) of the weld metal should be
minimum 80 MPa above SMYS of the base material. If two grades are joined, the requirement applies to the
SMYS of the lower strength base material.
C.3.3.3 For girth welds exposed to strain εl,nom ≥ 0.4%,the minimum required weld metalyield strength shall
be 20 MPa less than the specified max YS of base material.
ECA shall be conducted for all girth welds exposed to a strain εl,nom ≥ 0.4% (see DNVGL-RP-F108).
C.3.3.4 Whenever an ECA is performed, the tensile properties of the weld metal shall at least be equal to the
properties used as input to the ECA. If the properties of the weld metal do not meet these requirements, it
shall be validated that the assumptions made during design and/or the ECA have not been jeopardised.
C.3.3.5 Whenever an ECA is performed or for steels with SMYS ≥ 450 MPa, any batch intended for use in
production welding that was not qualified during welding procedure qualification, shall be qualified according
to [C.3.4].
C.3.3.6 For girth welds, all batches of consumables used in production including possible wire/flux
combinations should be qualified by testing during welding procedure qualification.
C.3.3.7 Batch testing is not required for steels with SMYS < 450 MPa and when ECA is not performed
providing the tensile and impact properties stated on the material/supplier certificates are above 90% of the
values on the material/supplier certificates for the batch used during welding procedure qualification.
Pipeline components
C.3.3.8 For welds in pipeline components the weld metal shall, as a minimum, have ductility and toughness
meeting the requirements of the base material and the actual yield stress (Rt0.5) of the deposited
weld metal should be minimum 80 MPa above SMYS of the base material. If two grades are joined, the
requirement applies to the SMYS of the lower strength base material.
C.3.4 Batch testing of welding consumables for pipeline girth welds
C.3.4.1 A consumable batch is defined as the volume of product identified by the supplier under one unique
batch/lot number, manufactured in one continuous run from batch/lot controlled raw materials. For solid wire
welding consumables, a batch may be defined as originating from the same heat of controlled raw materials,
and not necessarily manufactured in one continuous run.
C.3.4.2 Batch testing shall be conducted to verify that consumables not tested during qualification of the
welding procedure will give a deposited weld metal nominally equivalent to those batches used for welding
procedure qualification, with respect to chemistry and mechanical properties.
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C.3.4.3 The batch testing shall be performed for all welding consumables, including possible wire/flux
combinations. Consumable batches and combinations used during WPQ are considered tested.
C.3.4.4 Each individual product (brand name and dimensions) shall be tested once per batch/lot, except for
solid wire originating from the same heat, where one diameter may represent all. SAW fluxes do not require
individual testing but SAW wires shall be tested in combination with a selected, nominal batch of flux of the
same classification as used for the welding of the girth welds.
Mechanical testing
C.3.4.5 The testing shall be performed on samples taken from girth welds welded according to the welding
procedure to be used in production. Samples shall be removed from same clock positions as for the WPQT.
The testing shall be performed as required in App.B, and include:
— 1 all-weld metal tensile test.
— 1 macro section with hardness test of weld metal (HV10) as per Figure B-10, with only indentations
towards the centre line of the weld, spaced by 1 mm.
— 1 set of Charpy V-notch test at weld centre line. Test temperature shall be the same as for qualification of
the relevant welding procedure.
C.3.4.6 If an ECA is not performed, the mechanical properties shall meet the specified minimum
requirements.
C.3.4.7 If an ECA is used as basis for establishing acceptance criteria for pipeline girth welds (see DNVGLRP-F108), fracture toughness testing shall be performed with the same type of specimens and test conditions
as for qualification of the relevant welding procedure, whenever:
— average impact test values are not within 80% of the average value obtained during WPQT
— all weld metal yield stress is not within 90% of the value obtained during WPQT
In case of fracture toughness testing, the results shall as a minimum meet the values that have been used as
the basis for the ECA.
Chemical analysis
C.3.4.8 For solid wire and metal powders the analysis shall represent the product itself. For coated electrodes
and cored wires, the analysis shall represent the weld metal, deposited according to EN 26847 (ISO 6847).
The analysis, made by manufacturer or contractor, shall include:
— all elements specified in the relevant classification standard and the relevant data sheet, see [C.3.2.1]
— the N content.
C.3.4.9 The chemical analysis shall be in accordance with the composition ranges stated in the
manufacturer's data sheets, see [C.3.2.1].
C.3.5 Shielding, backing and plasma gases
C.3.5.1 The classification and designation and purity of shielding, backing and plasma gases shall be in
compliance with ISO 14175.
C.3.5.2 Gases shall be delivered with a certificate stating the classification, designation, purity and dewpoint
of the delivered gas.
C.3.5.3 The gas supply/distribution system shall be designed and maintained such that the purity and
dewpoint is maintained up to the point of use.
C.3.5.4 Shielding, backing and plasma gases shall be stored in the containers in which they are supplied.
Gases shall not be intermixed in their containers.
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C.3.5.5 If gas mixing unit systems are used, the delivered gas composition shall be verified and regularly
checked.
C.3.6 Handling and storage of welding consumables
C.3.6.1 A detailed procedure for storage, handling, recycling and re-baking of welding consumables to
ensure that the hydrogen diffusible content of weld metal is maintained at less than 5 ml per 100 g weld
metal shall be prepared. The procedure shall, as a minimum, be in accordance with the manufacturer's
recommendations. The procedure shall be reviewed and agreed prior to start of the production.
C.3.6.2 The manufacturer's recommendations may be adapted for conditions at the location of welding
provided the following requirements are met:
— solid and flux cored wire shall be treated with care in order to avoid contamination, moisture pick-up and
rusting, and shall be stored under controlled dry conditions. Ranges of temperature and relative humidity
for storage shall be stated
— if vacuum packed low hydrogen SMAW welding consumables are not used, low hydrogen SMAW
consumables shall be stored, baked, handled and re-baked in accordance with the manufacturer’s
recommendation. Re-baking more than once should not be permitted
— flux shall be delivered in moisture proof containers/bags. The moisture proof integrity of bags shall be
verified upon delivery and when retrieving bags for use. The flux shall only be taken from undamaged
containers/bags directly into a hopper or storage container
— the temperature ranges for heated hoppers, holding boxes and storage containers shall be in accordance
with the flux manufacturer’s recommendations
— whenever recycling of flux is applied, the recycling process shall ensure a near constant ratio of new/
recycled flux and the ratio of new/recycled flux shall be suitable to prevent any detrimental degradation of
the flux operating characteristics, e.g. moisture pick-up, excessive build-up of fines and change of grain
size balance.
C.4 Welding procedures
C.4.1 General
C.4.1.1 Detailed welding procedure specifications shall be prepared for all welding covered by this appendix.
C.4.1.2 All welding shall be based on welding consumables, welding processes and welding techniques
proven to be suitable for the type of material and type of fabrication in question.
C.4.2 Previously qualified welding procedures
General
C.4.2.1 A qualified welding procedure of a particular manufacturer is valid for welding only in workshops or
sites under the operational technical and quality control of that manufacturer.
C.4.2.2 For welding procedures developed, qualified and kept on file for contingency situations such as
hyperbaric welding procedures intended for pipeline repair and other contingency situations, the restrictions
below shall not apply.
Pipeline girth welds
C.4.2.3 Previously qualified welding procedures shall not be used for:
— welding of girth welds when the SMYS of C-Mn linepipe is > 450 MPa
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— welding of girth welds in clad or lined, duplex stainless steel or 13Cr martensitic stainless steel linepipe.
C.4.2.4 Except as limited by [C.4.2.3] above, a WPS for new production may be based on a previously
qualified WPQR. The type and extent of testing and test results for the previously qualified WPQR shall meet
the requirements of this appendix. A WPS for the new production shall be specified within the essential
variables of this appendix.
C.4.2.5 For WPQRs older than 5 years the validity shall be documented through production tests.
Pipeline components
C.4.2.6 Previously qualified welding procedures shall not be used for welding of steels with SMYS > 450 MPa.
A WPS for new production may otherwise be based on a previously qualified WPQR. The type and extent of
testing and test results for the previously qualified WPQR shall meet the requirements of this appendix and
a WPS for the new production shall, based the previously qualified WPQR, be specified within the essential
variables of this appendix.
C.4.2.7 For a WPQR where the actual qualification is more than 5 years old, it shall be documented through
production tests that a WPS based on the qualifying WPQR have been capable of producing welds of
acceptable quality over a period of time. Alternatively a limited confirmation welding may be performed to
demonstrate that the WPS is workable and producing welds of acceptable quality.
C.4.3 Preliminary welding procedure specification
C.4.3.1 A preliminary Welding Procedure Specification (pWPS) shall be prepared for each new welding
procedure qualification. The pWPS shall contain the relevant information required for making a weld for the
intended application when using the applicable welding processes, including tack welds.
C.4.4 Welding procedure qualification record
C.4.4.1 The Welding Procedure Qualification Record (WPQR) shall be a record of the materials, consumables,
parameters and any heat treatment used during qualification welding and the subsequent non-destructive,
destructive and corrosion test results. All essential variables used during qualification welding that are
relevant for the final application of the WPQR shall be documented and the welding parameters recorded in
relevant positions for each pass.
C.4.5 Welding procedure specification
C.4.5.1 A Welding Procedure Specification (WPS) is a specification based on one or more accepted WPQRs.
One or more WPSs may be prepared based on the data of one or more WPQRs provided the essential
variables are kept within the acceptable limits and other requirements of this appendix are met. A WPS may
include one or a combination of welding processes, consumables or other variables.
All limits and ranges for the applicable essential variables for the welding to be performed shall be stated in
the WPS. Grouping of passes, e.g. fill and cap passes, may be allowed subject to agreement.
C.4.5.2 The WPS shall be submitted together with the referenced supporting WPQR(s) for review and
acceptance prior to start of production.
C.4.6 Welding procedure specification for repair welding
C.4.6.1 Repair welding procedure specifications shall be prepared in line with the type of repair weld
qualifications required in [C.5.3.7].
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C.4.7 Contents of preliminary welding procedure specification
C.4.7.1 The preliminary welding procedure specification (pWPS) shall contain the relevant information
required for the applicable welding processes, including any tack welds. A pWPS for production welding shall
include the information given in Table C-1 and [C.4.7.2], as relevant for the welding to be performed.
Table C-1 Contents of preliminary welding procedure specification
Manufacturer
Identification of manufacturer
pWPS
Identification of the pWPS.
Welding process
Welding process and for multiple processes; the order of processes used.
Manual, partly-mechanised, mechanised and automatic welding.
Welding equipment
Type and model of welding equipment. Number of wires.
Base materials
Material grade(s), supply condition, chemical composition and manufacturing process.
For steels with SMYS > 450 MPa; Steel supplier and For CRAs; UNS and PRE numbers.
Material thickness and
diameter
Material thickness of test piece. Nominal ID of pipe.
Groove configuration
Groove design/configuration; dimensions and tolerances of angles, root face, root gap and
when applicable; diameters. Backing and backing material.
Alignment and tack
welding
Tack welding (removal of tack welds or integration of tack welds in the weld).
Welding consumables
Electrode or filler metal diameter or cross-section area. Type, classification and trade name.
Manufacturer consumable data sheet shall be attached.
Shielding, backing and
plasma gases
Designation, classification and purity according to ISO 14175. Nominal composition of other
gases and gas mixtures. Gas flow rate.
Electrical characteristics
and pulsing data
Polarity. Type of current (AC, DC or pulsed current). Pulse welding details (machine settings
and/or programme selection).
Arc Characteristics
Spray arc, globular arc, pulsating arc or short circuiting arc.
Welding techniques
Welding position according to ISO 6947. Welding direction. Stringer/weave beads. Sequence
of deposition of different consumables. Number of passes to be completed before cooling to
below preheat temperature. Accelerated weld cooling (method and medium).
Type of line-up clamp. Stage for removal of line-up clamp.
Time lapse between completion of root pass and start of hot pass and number of welders on
each side.
Time lapse between completion of root pass and start of hot pass.
For double sided welding: Sequence of sides welded first and last and number of passes
welded from each side.
Preheating
Method of preheat and minimum preheat temperature. Minimum initial temperature when
preheat is not used.
Interpass temperature
Maximum and minimum interpass temperature.
Heat input
Heat input range for each pass.
Post weld heat treatment
Method, time and temperature for post heating for hydrogen release
Method of post weld heat treatment (holding time and heating and cooling rates).
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Manufacturer
Identification of manufacturer
Specific for the SMAW
welding process
Run-out length of electrode or travel speed.
Specific for the SAW
welding process
Number and configuration of wire electrodes. Flux, designation, manufacturer and trade
name. Additional filler metal. Contact tip - work piece distance. Arc voltage range.
Specific for the FCAW
welding process
Mode of metal transfer (short circuiting, spray or globular transfer).
Specific for the GMAW
welding process
Shielding and backing gas flow rate. Additional filler metal. Contact tip - work piece distance.
Arc voltage range.
Specific for the GTAW
welding process
Shielding and backing gas flow rate. Nozzle diameter. Diameter and codification of tungsten
electrode (ISO 6848). Hot or cold wire.
Specific for the PAW
welding process
Shielding, backing and plasma gas flow rate. Nozzle diameter. Type of torch. Contact tip work piece distance. Hot or cold wire.
Specific for mechanized
welding processes
(general)
Control software (programme and/or software version. List of welding parameters that can
be adjusted by the welders. Minimum number of welders for each pass.
Specific for mechanized
GMAW welding process
Wire feed. Oscillation width and frequency. Side wall dwell time.
Specific for mechanized
GTAW/PAW welding
processes
Programmed arc voltage. Wire feed including pulsing pattern and timing diagram. Oscillation
width and frequency. Side wall dwell time. Shielding gas timing diagrams and pulse pattern.
C.4.7.2 A pWPS for repair welding shall in addition to the requirements applicable for a pWPS for production
welding include the following information:
—
—
—
—
—
type of repair (see Table C-7)
method of removal of the defect, preparation and design of the repair weld excavation
minimum repair depth and length
minimum ligament
visual examination and NDT to be performed of the excavated area according to [D.2] to confirm complete
removal of defect before welding as well as visual examination and NDT of the final repaired weld.
— In cases when through thickness or partial thickness repeated repairs are permitted or agreed (see Table
C-7) the location of additional Charpy V-notch tests, in addition to the tests required by Table C-4, shall
be shown on sketches in the pWPS.
C.4.8 Essential variables for welding procedures
C.4.8.1 A qualified welding procedure remains valid as long as the essential variables are kept within the
limits specified in Table C-2.
C.4.8.2 For special welding processes as stated in [C.1.2.4] and welding systems using these processes
other essential parameters and acceptable variations need to be applied and shall be subject to agreement.
C.4.8.3 The limits and ranges for essential variables for a WPS shall be based on the on documented records
in one or more WPQRs.
C.4.8.4 The essential variables given in Table C-2 shall, when applicable, be supplemented with the
requirements in [C.4.8.5] through [C.4.8.12] below.
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C.4.8.5 If two different materials are used in one test piece, the essential variables shall apply to each of
the materials joined. A WPQR qualified for a dissimilar material joint will also qualify each material welded to
itself, provided the applicable essential variables are complied with.
C.4.8.6 Multiple test pieces may be required to qualify a pWPS where the size of a single test piece will not
allow extraction of sufficient number of test specimens according to Figure C-2. In such cases the heat input
for the same weld regions and passes between the test pieces should be as similar as possible. Maximum
allowed heat input variations between the different test pieces are:
— 15% for mechanised and automated welding
— 30% for manual and partly-mechanised welding
An average heat input shall be calculated in line with [C.5.1.7].
Hardness and impact testing shall be taken as follows:
— hardness test specimens from the test piece and position welded with the lowest heat input
— impact test specimens from the test piece and position welded with the highest heat input.
C.4.8.7 When it is intended to qualify a pWPS with an extended heat input range (larger difference between
high and low heat input) , the maximum difference between lowest and highest average heat input shall not
exceed 30%. In the production WPS it is allowed to add the heat input tolerances as given in Table C-2. All
required mechanical testing shall be performed on test pieces welded with both high and low heat input.
C.4.8.8 The minimum preheat or work piece temperature to be stated in the WPS shall not be below that of
the test piece with the recorded highest preheat.
C.4.8.9 The maximum interpass temperature of any pass to be stated in the WPS shall not be higher than
the recorded highest interpass temperature during qualification of the procedure. It is not allowed to boost
the interpass temperature for one pass only. The maximum interpass temperature shall reflect the maximum
interpass temperature that is expected during production.
Guidance note:
The all weld tensile test sample should be taken as close as possible to the location were the highest interpass temperature to be
stated in the WPS is measured.
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C.4.8.10 When multiple filler metals are used in a test joint, the qualified thickness for each deposited filler
metal shall be between 0.75 to 1.5 times the deposited thickness of that filler material during qualification.
To document the properties of each filler material, the test sample should at least contain 30% of the
specimen cross-section for the filler material to be tested. If the mechanical properties of each filler material
will not be documented by the original welding procedure qualification, separate welds with each consumable
should be made to allow testing of AWT and WM/FL Charpy V-notch specimens.
C.4.8.11 If welders have been working on opposite sides of a test piece, the maximum difference in heat
input between the welders shall not exceed the following:
— 15% for mechanised and automated welding.
— 30% for manual and partly-mechanised welding.
The allowable variation in heat input shall be based on the average of the heat inputs used by the welders.
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Table C-2 Essential variables for welding of pipeline girth welds and component longitudinal
welds
Variable
Changes requiring re-qualification
1 Manufacturer
Manufacturer
a
Any change in responsibility for
operational, technical and quality control.
The process(es) used
a
Any change.
The order of processes used
b
Any change when multiple processes are
used.
Manual, partly-mechanised, mechanised
or automatic welding
c
Any change between manual, partlymechanised, mechanised and automatic
welding.
Welding
a
Any change in make, type and model
for partly-mechanised, mechanised and
automatic welding.
Welding equipment
b
Any change in type for manual welding.
Number of wires
c
Change from single wire to multiple wire
system and vice versa (e.g. going from
tandem/twin to single wire). This does not
apply to multiple torch systems where the
wires feed into separate weld pools.
Material grade
a
A change from a lower to a higher
strength grade but not vice versa.
Supply condition
b
A change in the supply condition (TMCP,
Q/T or normalised).
Steel supplier
c
For SMYS ≥ 450 MPa; a change in base
material origin (steel/plate/pipe mills)
(linepipe to linepipe girth welds only – e.g.
not for components).
Chemical composition
d
An increase in Pcm of more than 0.020,
CE of more than 0.030 and C content of
more than 0.02% for C-Mn and low alloy
steel.
Manufacturing process
e
A change in manufacturing process
(rolled, seamless, forged, cast).
UNS numbers.
f
A change in the UNS number for CRAs.
2 Welding process
3 Welding equipment
4 Base materials
5 Material thickness and diameter
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Variable
Material thickness (t = nominal thickness
of test joint.)
Changes requiring re-qualification
a
For non-H2S service:
— t ≤ 25 mm: A change outside 0.75 t to
1.5 t
— t > 25 mm: A change outside 0.75 t to
1.25 t
For H2S service:
— A change outside the thickness interval
0.75 t to 1.25 t.
Nominal ID of pipe
b
— t ≤ 25 mm: A change of pipe ID
outside the range 0.5 ID to 2 ID
— t > 25 mm: A change of pipe ID
outside the range 0.5 ID to ∞.
6 Groove configuration
Groove design/configuration.
a
Any change in groove dimensions outside
the tolerances specified in the agreed WPS
(all dimensions shall have tolerances).
Backing and backing material.
b
Addition or deletion of backing or change
of backing material (e.g. from copper to
ceramic).
Tack welding
a
Any change in removal of tack welds or
integration of tack welds in the weld.
Line-up clamp
b
Omission of a line-up clamp and a change
between external and internal line-up
clamp.
Removal of line-up clamp
c
Any reduction in length of each section of
root pass welded; the spacing of sections,
number of sections and percentage of
circumference welded for external line-up
clamp.
d
Any decrease in number of completed
passes and length of passes for internal
line-up clamp.
a
Any change of diameter or cross-section
area.
b
Any change of type classification and
brand (brand not applicable for bare wire).
c
Any use of a non tested welding
consumables batch when batch testing is
required.
7 Alignment and tack welding
8 Welding consumables
Electrode or filler metal
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Variable
Changes requiring re-qualification
d
Any use of a welding consumables batch
with a reduction in tensile or impact
properties of more than –10% (average
values) from the batch used for WPQR
when batch testing is not required.
e
Any change of type, classification and
brand.
f
Any increase in the ratio of recycled to
new flux.
Gases according to ISO 14175
a
Any change in designation, classification
and purity according to ISO 14175.
Other gases and gas mixtures
b
Any change in nominal composition, purity
and dew point.
Oxygen content of backing gas
c
Any increase.
Shielding gas flow rate
d
For processes 131, 135 136, 137 and 141
(see ISO 4063): Any change in flow rate
beyond ± 10%.
Polarity
a
Any change in polarity.
AC, DC or pulsed current
b
Any change in type of current and a
change from normal to pulsed current and
vice versa.
Pulse frequency range in pulsed manual
welding
c
Any change in: Pulse frequency for
background and peak current exceeding ±
10% and pulse duration range exceeding
± 10%.
a
A change from spray arc, globular arc or
pulsating arc to short circuiting arc and
vice versa.
Angle of pipe axis to the horizontal
a
A change of more than ± 15°from the
position welded. The L045 position
qualifies for all positions provided all other
essential variables are fulfilled.
Welding direction
b
A change from upwards to downwards
welding and vice versa.
Stringer/weave
c
A change from stringer to weave of more
than 3X electrode/wire diameter or vice
versa.
Flux
9 Shielding, backing and plasma gases
10 Electrical characteristics and pulsing data
11 Arc Characteristics
Mode of metal transfer
12 Welding techniques
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Variable
Changes requiring re-qualification
Sequence of deposition of different
consumables
d
Any change in the sequence.
Sequence of sides welded first and last
(double sided welds)
e
Any change in the sequence.
Passes welded from each side
f
Change from single to multi pass welding
and vice versa.
Number of welders
g
Any decrease in number of welders for
welding of root and hot pass for cellulose
coated electrodes.
Time lapse between completion of root
pass and start of hot pass
h
Any increase above maximum time
qualified.
Weld completion
i
Any reduction in the number of passes
completed before cooling to below preheat
temperature.
Accelerated weld cooling
j
Any change in method and medium and
any increase in maximum temperature of
the weld at start of cooling.
Preheat temperature
a
Any reduction.
Initial temperature when preheat is not
used
b
Any reduction.
a
Any increase for CRAs, C-Mn and low alloy
steel. Any reduction below the preheat
temperature.
a
For C-Mn and low alloy steels with SMYS
≤ 450 MPa in non-H2S service:
13 Preheating
14 Interpass temperature
Maximum and minimum interpass
temperature
15 Heat input
Heat input range for each pass
Any change exceeding ± 15%.
b
For C-Mn and low alloy steels with SMYS
> 450 MPa and C-Mn and low alloy steels
in H2S service: Any change exceeding ±
10%.
c
For CRAs: Any change exceeding ± 10%.
a
Any reduction in the time and temperature
and deletion but not addition of post
heating.
16 Post weld heat treatment
Post heating; hydrogen release
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Variable
Post weld heat treatment
Changes requiring re-qualification
b
Addition or deletion of post weld heat
treatment.
Any change in holding temperature
exceeding ± 20°C.
Any change in heating and cooling rates
outside ± 5%.
Holding time
c
Any change in holding time outside below
formula (± 5%):
holding time = (actual thickness/qualified
thickness) × qualified holding time.
17 Specific for the SAW welding process
Wire electrode configuration.
a
Each variant of process 12 (121 to 125)
shall be qualified separately.
Flux
b
Any change of type, classification and
brand.
Arc voltage range.
c
Any change beyond ± 10%.
a
A change from short circuiting transfer to
spray or globular transfer.
18 Specific for the FCAW welding process
Mode of metal transfer
Qualification with spray or globular
transfer qualifies both spray or globular
transfer.
19 Specific for the GMAW welding process
Arc voltage range
a
Any change beyond ± 10%.
Diameter and codification of tungsten
electrode (ISO 6848)
a
Any change.
Hot or cold wire.
b
A change from hot to cold wire and vice
versa.
a
A change from hot to cold wire and vice
versa.
20 Specific for the GTAW welding process
21 Specific for the PAW welding process
Hot or cold wire
22 Specific for automatic welding of pipeline girth welds
Control software
a
Any change.
Pre-set parameters
b
Any change (applies to parameters that
can not be adjusted by the welder).
23 Specific for mechanised welding of pipeline girth welds
Control software
a
Any change.
24 Specific for repair welding
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Variable
Welding techniques
Changes requiring re-qualification
a
A change from internal to external repairs
and vice versa for pipeline girth welds.
b
A change from single to multi pass repairs
and vice versa.
c
A change from cold to thermal method for
removal of the defect but not vice versa.
d
Any increase above 20% in the depth of
excavation for partial thickness repairs.
C.4.8.12 If CRA or clad welds are subject to solution annealing heat treatment after welding a slight
variation in welding parameters outside those in Table C-2, Items 10 through 15 may be agreed.
C.5 Qualification of welding procedures
C.5.1 General
C.5.1.1 Qualification welding shall be performed based upon the accepted pWPS, using the type of welding
equipment to be used during production welding, and under conditions that are representative of the actual
working environment for the work shop, site, or vessel where the production welding will be performed. The
configuration of the test joint shall be representative of the actual weld to be performed during production.
C.5.1.2 The number of test joints shall be sufficient to obtain the required number of specimens from the
required locations given in Figure C-1 and Figure C-2. Allowance for re-testing should be considered when
deciding the number of test joints to be welded.
C.5.1.3 The test joints for qualification welding shall be of sufficient size to give realistic restraint during
welding.
C.5.1.4 The base material selected for the qualification testing should be representative of the upper range
of the specified chemical composition for C-Mn and low alloy steels, and of the nominal range of the specified
chemical composition for corrosion resistant alloys.
C.5.1.5 The material thickness shall be the same for both pipes/components/plates to be welded, except to
qualify joining of two base materials with unequal thickness and for fillet end T-joint test pieces.
Qualification welding
C.5.1.6 Certificates for materials and consumables, including shielding, backing and plasma gases, shall be
verified, and validity and traceability to the actual materials shall be established prior to start of qualification
welding. The records from qualification welding shall include all information needed to establish a WPS for the
intended application within the essential variables and their allowable ranges.
C.5.1.7 The following requirements apply:
— the welding qualification test shall be representative for the production welding with respect to welding
positions, interpass temperature, application of preheat (propane will also qualify for induction coil
preheating), heat conduction, etc.
— if multiple welding arcs are combined in a single welding head the parameters for each welding arc shall
be recorded
— the direction of plate rolling (when relevant) and the 12 o’clock position (for fixed pipe positions) shall be
marked on the test piece
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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— when more than one welding process or filler metal is used to weld a test piece, the parameters used and
the approximate thickness of the weld metal deposited shall be recorded for each welding process and
filler metal
— if tack welds are to be fused into the final joint during production welding, they shall be included when
welding the test piece
— backing gas oxygen content and the duration of backing gas application before, during and after welding
shall be recorded
— each test piece shall be uniquely identified by hard stamping or indelible marking adjacent to the weld and
the records made during test welding, non-destructive testing and mechanical testing shall be traceable to
each test piece
— average heat input shall be calculated and should be based on averages of each parameter (V, A, travel
speed).
Pipeline girth welds
— the welding qualification test shall be representative for the production welding with respect to angle of
pipe axis., interpass temperature, application of preheat, heat conduction, etc.
— for girth welds in welded pipe in all positions, except 1G (PA) and 2G (PC), it is recommended that one of
the pipes used for the welding procedure qualification test be fixed with the longitudinal weld in the 6 or
12 o'clock position
— for welding of pipe with diameter ≥ 20” in fixed positions, the weld circumference shall be divided in
appropriate sectors around the circumference. The welding parameters shall be recorded for each pass in
each sector and for each welding arc. For each sector an average heat input shall be determined for each
pass. For manual welding, the heat input for a sector shall be recorded as average of all the average heat
inputs for the run-out lengths in each pass in that sector
— for welding of pipe with diameter < 20” the average heat input shall be recorded for each pass. For
manual welding, the heat input for each pass shall be recorded as average of all the average heat inputs
for the run-out lengths in each pass in the pipe circumference
— the heat input range to be stated on the WPS for the full circumference shall be based on the highest and
lowest circumferential or sectoral average heat input, as relevant, with tolerances as given in Table C-2.
Grouping of passes, e.g. fill and cap passes, may be allowed subject to agreement
— the release of external line-up clamps shall be simulated during qualification welding. Clamps should not
be released until the completed sections of the root pass covers a minimum of 50% of the circumference
with even spacing. The length of each section, the spacing of the sections, the number of sections welded
and the percentage of welded sections of the circumference shall be recorded
— if it is expected that the interpass temperature will drop below preheat temperature during installation
welding, this scenario shall be simulated during qualification welding. The number of passes completed
before cooling to below preheat temperature shall be recorded
— accelerated cooling of the weld shall be performed during qualification welding if accelerated weld cooling,
e.g. for AUT will be performed in production. The cooling method and the weld temperature at the start of
the cooling shall be recorded. A macro and hardness shall be taken at cooling start point.
C.5.1.8 If the use of cellulose covered electrodes has been agreed, the following additional requirements
shall apply:
— preheat shall be minimum 100°C
— delay between completion of the root pass and the start of depositing the hot pass shall be minimum 6
minutes
— immediately upon completion of welding during welding procedure qualification the test pieces shall be
water quenched as soon as the temperature of the test piece is below 300°C
— non destructive testing of the test piece shall be by Automated Ultrasonic Testing (AUT) or Radiographic
testing and Manual Ultrasonic Testing.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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C.5.2 Repair welding procedures
C.5.2.1 Repair welding shall be qualified by a separate weld repair qualification test.
C.5.2.2 Preheat for repair welding should be minimum 50°C above minimum specified preheat for production
welding.
C.5.2.3 When a heat treated pipe or component is repaired by welding, a new heat treatment may have to
be included in the qualification of the weld repair procedure, depending on the effect of the weld repair on
the properties and microstructure of the existing weld and base material.
C.5.2.4 Qualification of repair welding procedures shall be made by excavating a groove in an original weld
welded in accordance with a qualified welding procedure.
C.5.2.5 The excavated groove shall be of sufficient length to obtain the required number of test specimens +
50 mm at each end.
Repeated repairs
C.5.2.6 If repeated weld repairs are permitted or agreed, these shall be qualified separately.
C.5.2.7 In case of repeated repairs, the test piece shall contain a repair weld of a repaired original weld.
For repeated in-process root repair, single pass cap repair and/or single pass root sealing repairs the repair
weld shall be removed prior to re-repair. A repeated repair qualification may qualify a repair WPS providing
it is ensured that the HAZ has been exposed to two heat treatment cycles, i.e. the second excavation is
performed exactly on the same location as the first excavation.
C.5.2.8 The qualification test shall be made in a manner realistically simulating the repair situation to be
qualified.
C.5.2.9 Qualification welding shall be performed in accordance with [C.5.1.1] through [C.5.1.8].
C.5.2.10 For pipeline girth welds the repair qualification welding shall be performed in the overhead through
vertical positions.
C.5.2.11 For roll welding the length of the repair weld may be centred at the 12 o’clock location for external
repairs and at the 6 o’clock location for internal repairs, in which case repair welding is qualified for repair
welding in these locations only.
C.5.3 Qualification of girth butt welds and component longitudinal welds
welding procedures
C.5.3.1 Qualification of welding procedures for pipeline system girth welds and welds in pipeline components
may be performed by any of the arc welding processes specified in [C.1.2].
C.5.3.2 The WPS shall be qualified and approved by all parties prior to start of any production welding.
C.5.3.3 The type and number of destructive tests for welding procedure qualification are given in Table C-3,
with methods and acceptance criteria as specified in [C.6].
C.5.3.4 For pipeline girth welds exposed to strain ≥ 0.4%, testing should be performed to determine the
properties of weld metal in the strained and aged condition after deformation cycles and also at elevated
temperature. See DNVGL-RP-F108.
Qualification of repair welding procedures
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Table C-3 Qualification of welding procedures for girth butt welds including component
longitudinal welds
Test joint
Minimum number of each specified test
Wall
Transverse
D
thickness
weld
(mm)
(mm)
Tensile
≤ 25
> 25
Transverse
all-weld
1)
Tensile
All-weld
tensile
2
2
Root
bend
1)
≤
300
>
300
2
2
2
2
all
2
2
2
9)
2
2)
4
2)
0
Face
bend
9)
2
2)
4
2)
0
)
Charpy
V-notch
3,
sets
Macro and
hardness
0
4
2
11)
12)
12)
12, 13)
Side
bend
4,5,6,7)
10)
Other Fracture
tests toughness
0
4
2
11)
4
6
2
11)
Notes:
1)
The strength mismatch between the girth weld and the parent material shall be evaluated when ECA is required.
All-weld tensile specimens are recommended when ECA is performed, however, transverse all-weld specimens are
acceptable. In case of ECA, full stress-strain curves shall be established as far as possible, see also DNVGL-RP-F108.
If it is impossible to prepare test samples due to size limitations, weld metal properties shall be documented based
on the weld consumables material certificates provided by the supplier (i.e. to document that the yield and ultimate
tensile weld metal strength are above the base metal values).
2)
For welding processes GMAW, GTAW, FCAW and SMAW side bend tests shall be performed instead of root and face
bend tests. For t > 12 mm side bend test is an acceptable alternative to root and face bend tests.
3)
Impact testing is not required for t < 6 mm.
4)
Each Charpy V-notch set consists of 3 specimens.
5)
The notch shall be located in the weld metal, the fusion line (FL) sampling 50% of HAZ, FL+2 mm and FL+5 mm,
see App.B, Figure B-3 through Figure B-5.
6)
For double sided welds on C-Mn and low alloy steels, four additional sets of Charpy V-notch test specimens shall be
sampled from the weld metal, FL (sampling 50% of HAZ), FL+2 mm and FL+5 mm in the root area, see Figure B-5.
7)
If several welding processes or welding consumables are used, impact testing shall be carried out in the
corresponding weld regions, even if the region tested cannot be considered representative for the complete weld.
8)
When the wall thickness exceeds 25 mm for single sided welds, two additional sets of Charpy V-notch test
specimens shall be sampled from the weld metal root and FL in the root area.
9)
Bend tests on clad/lined pipes shall be performed as side bend tests. 4 side bend tests shall be performed (for all
wall thicknesses).
10) For girth welds in welded pipe, one macro and hardness shall include an intersection between a longitudinal/girth
weld.
11) Requirements for corrosion tests, chemical analysis and microstructure examination are specified in [C.6].
12) Fracture toughness testing is only required when a generic or full ECA is performed for pipeline girth butt welds.
Extent of testing shall be in accordance with DNVGL-RP-F108.
13) For nominal wall thickness above 50 mm in C-Mn and low alloy steels fracture toughness testing is required unless
PWHT is performed.
C.5.3.5 Qualification of repair welding procedures for pipeline system girth welds and welds in pipeline
components may be performed by any of the arc welding processes specified in [C.1.2].
C.5.3.6 The WPS for repair welding shall be qualified prior to start of any production repair welding.
C.5.3.7 The following types of repairs should be qualified to the extent that such repairs are feasible and
applicable for the repair situation considering the size of pipe or component:
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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—
—
—
—
—
through thickness repair
partial thickness repair
in-process root repair
single pass cap repair
single pass root sealing repair.
C.5.3.8 The type and number of destructive tests for qualification or repair welding procedure are given in
Table C-4, with methods and acceptance criteria as specified in [C.6] below.
Repeated repairs
C.5.3.9 If it has been agreed to permit through thickness or partial thickness repeated repairs (see Table
C-7), and a HAZ is introduced in the weld metal from the first repair, then additional Charpy V-notch sets (in
addition to the tests required by Table C-4) shall be located in the re-repair weld metal and in FL, FL+2 mm
and FL+5 mm of the weld metal from the first repair and/or the base material as applicable and as shown in
the accepted pWPS, see [C.4.7.2].
C.5.3.10 If it has been agreed to permit repeated in-process root repair, single pass cap repair and/or single
pass root sealing repair, see Table C-7, the extent of testing shall be as tests required by Table C-4.
Table C-4 Qualification of repair welding procedures for girth butt welds including components
longitudinal welds
Test joint
Type of repair
Minimum number of each specified test
Transverse Transverse All-weld
1)
weld
all-weld
tensile ,
1)
2)
tensile
tensile
Root
bend
Face
bend
Side
bend
Charpy
V-notch
sets
Through
thickness repair
1
1
1
1
2)
1
2)
2
3)
9
Partial thickness
repair
1
1
1
1
2)
1
2)
2
3)
7
In-process root
repair
1
Single pass cap
repair
Single pass root
sealing repair
1
1
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
Submarine pipeline systems
DNV GL AS
Macro and
hardness
Other Fracture
tests toughness
4, 5, 6)
1
7)
8, 9)
4, 5, 6)
1
7)
8, 9)
1
7)
1
7)
1
7)
Page 364
Notes:
1)
The strength mismatch between the girth weld and the parent material shall be evaluated when ECA for repair weld
is required. All-weld tensile specimens are recommended when ECA is performed, however, transverse all-weld
specimens are acceptable. In case of ECA, full stress-strain curves shall be established as far as possible, see also
DNVGL-RP-F108. If it is impossible to prepare test samples due to size limitations, weld metal properties shall be
documented based on the weld consumables material certificates provided by the supplier (i.e. to document that the
yield and ultimate tensile weld metal strength are above the base metal values).
2)
1 root and 1 face bend test for t ≤ 25 mm. For t > 12 mm side bend test is an acceptable alternative to root and
face bend tests.
3)
For welding processes GMAW, GTAW, FCAW and SMAW, for clad/lined pipes and for all pipes when t > 25 mm, side
bend tests shall be performed instead of root and face bend tests.
4)
For partial penetration and through thickness repairs where a new HAZ is introduced in the original weld metal,
Charpy V-notch sets of 3 specimens shall be located according to App.B, Figure B-7 and Figure B-8.
5)
The notch shall be located in the repair weld metal, the fusion line (FL) sampling 50% of HAZ, FL+2 mm and FL+5
mm of both the base material and the original weld.
6)
If several welding processes or welding consumables are used, impact testing shall be carried out in the
corresponding weld regions, even if the region tested cannot be considered representative for the complete weld.
7)
Requirements for corrosion tests, chemical analysis and microstructure examination are specified in [C.6].
8)
Fracture toughness testing of repairs is only required when a generic or full ECA is performed for the original
pipeline girth butt welds. Extent of testing shall be in accordance with DNVGL-RP-F108.
9)
For nominal wall thickness above 50 mm in C-Mn and low alloy steels fracture toughness testing is required unless
PWHT is performed
C.5.4 Qualification of welding procedures for corrosion resistant overlay
welding
Qualification of welding procedures
C.5.4.1 Qualification of welding procedures for corrosion resistant overlay welding shall be performed with
GMAW or pulsed GTAW. Other methods may be used subject to agreement.
C.5.4.2 The chemical composition of test pieces shall be representative for the production conditions.
C.5.4.3 Qualification of weld overlay shall be performed on a test sample which is representative for the
size and thickness of the production base material, e.g. tolerance ranges in ISO 15614-7 may be considered
acceptable. The minimum weld overlay thickness used for the production welding shall be used for the
welding procedure qualification test.
C.5.4.4 The dimensions of, or the number of test pieces shall be sufficient to obtain all required tests.
C.5.4.5 The test pieces used shall be relevant for the intended application of the weld overlay:
— forging or casting for overlay welding of ring grooves
— pipe with the overlay welding performed externally or internally, or
— plate or pipe with a prepared welding groove for qualification of buttering and when the weld overlay
strength is utilised in the design.
C.5.4.6 If a buffer layer will be used in production welding, it shall also be used in welding the test piece.
C.5.4.7 The WPS shall be qualified prior to start of any production welding.
C.5.4.8 The type and number of destructive tests for welding procedure qualification are given in Table C-5
with methods and acceptance criteria specified in [C.6].
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Qualification of repair welding procedures
Table C-5 Qualification of corrosion resistant overlay welding procedures
Test joint
Thickness of
base material
All
Minimum number of each specified test
Side
bend
4
1)
Macro and
hardness tests
Chemical
analysis
1
1
All-weld
tensile
2
2)
Charpy V-notch
Impact tests
Other tests
2,3,4,5)
6)
Notes:
1)
Side bend specimens shall be taken transverse to the welding direction.
2)
Only required when the weld overlay strength is utilised in the design of the welded joint (e.g. load bearing weld
overlay).
3)
Only required when the weld overlay is load bearing across the overlay/base material fusion line.
4)
Sets shall be tested with the notch in the overlay weld metal, Fl, and FL+2 mm and FL+5 mm in the base material.
5)
If several welding processes or welding consumables are used, impact testing shall be carried out in the
corresponding weld regions if the region otherwise required to be tested cannot be considered representative for the
complete weld.
6)
Requirements for corrosion tests and microstructure examination are specified in [C.6].
C.5.4.9 Unless the production welding procedure can be applied, the repair welding procedure shall be
qualified. Weld repair performed on weld overlay machined to the final thickness shall be separately qualified.
C.5.4.10 The type and number of destructive tests for qualification of repair welding procedure are given in
Table C-5. In cases when qualification is performed using a pipe, component or plate with a prepared welding
groove, and a new HAZ is introduced in the original weld metal, additional Charpy V-notch impact sets shall
be located according to Figure B-7 and Figure B-8.
C.5.5 Qualification of procedures for pin brazing and aluminothermic
welding of anode leads
Qualification of procedures
C.5.5.1 Attachment of anode leads shall be by pin brazing or aluminothermic welding methods. Other
methods may be used subject to agreement. Full details of the technique used and associated equipment
shall be available prior to qualification of procedures.
C.5.5.2 The chemical composition of test pieces shall be representative for the production conditions and be
selected in the upper range of the chemical composition.
C.5.5.3 Qualification for brazing/welding of anode leads shall be performed on test samples which is
representative for the size and thickness of the production base material and the number of test pieces shall
be minimum 4 and sufficient to obtain all required tests.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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C.5.5.4 The WPS shall be qualified prior to start of any production.
Table C-6 Qualification of pin brazing and aluminothermic welding procedures
Test joint
Minimum number of each specified test
Thickness of
base material
Electrical
resistance
Mechanical
strength
All
4
4
Copper
penetration
2)
4
1)
Hardness
4
3
)
Pull test
4
Notes
1)
The number of tests refers to the total number of tests from all pieces.
2)
2 test specimens shall the sectioned transverse to the anode lead and 2 test specimens parallel with the anode lead.
3)
The hardness tests shall be made on the specimens for copper penetration measurements.
C.5.5.5 The type and number of destructive tests for procedure qualification are given in Table C-6 with
methods and acceptance criteria specified in [C.6] below.
C.5.6 Qualification of welding procedures for temporary and permanent
attachments and branch welding fittings to linepipe
Qualification of welding procedures
C.5.6.1 Qualification of welding procedures for temporary and permanent attachments and branch welding
fittings to linepipe may be performed by any of the arc welding processes specified in [C.1.2], but use of
cellulose coated electrodes is not permitted.
C.5.6.2 The WPS shall be qualified prior to start of any production welding.
C.5.6.3 The type and number of destructive tests for welding procedure qualification are given in [C.5.6.4]
to [C.5.6.14] with methods and acceptance criteria as specified in [C.6].
Longitudinal welds in doubler sleeves
C.5.6.4 Longitudinal welds in doubler sleeves shall be made with backing strips and qualified as required in
[C.5.3] and Table C-3, but with the extent of testing limited to:
— transverse weld tensile
— Charpy V-notch impact testing
— macro and hardness testing.
Fillet welds in doubler sleeves and anode pads
C.5.6.5 The fillet weld qualification test shall comprise two test pieces welded in the PD and PF plate
positions to qualify the welding procedure for welding in all positions.
C.5.6.6 The extent of testing for each test piece shall be 3 macro and hardness specimens taken from the
start, end and middle of each test weld with methods and acceptance criteria as specified in [C.6].
Branch welding fittings
C.5.6.7 The branch fitting qualification test welds shall be welded in the PF and PD pipe positions to qualify
welding in all positions.
C.5.6.8 The extent of testing shall be 4 macro and hardness specimens taken from the 12, 3, 6 and 9 o’clock
locations of each test weld. A procedure qualified as a butt weld may be used.
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C.5.6.9 Charpy V-notch impact testing with the notch in the weld metal, FL, FL+2 mm and FL+5 mm using
full size or reduced size specimens shall always be performed whenever the material thickness allows. Charpy
V-notch specimens shall be taken from both test welds.
Qualification of repair welding procedures for longitudinal welds in doubler sleeves
C.5.6.10 Repair welding procedures for longitudinal welds in doubler sleeves shall be qualified as required in
[C.5.3] and Table C-4, but with the extent of testing modified according to [C.5.6.4].
Qualification of repair welding procedures for fillet welds
C.5.6.11 Qualification welding shall be performed in the PD and PF plate positions. The extent of qualification
of repair welding procedures shall at as a minimum consist of:
— through thickness repair
— single pass repair against the pipe material
— single pass repair against the sleeve material.
C.5.6.12 Methods of testing and acceptance criteria shall be as specified in [C.6].
Qualification of repair welding procedures for branch welding fittings
C.5.6.13 Qualification welding shall be performed in the PD and PF pipe positions. The extent of qualification
of repair welding procedures shall at as a minimum consist of:
— through thickness repair
— single pass cap repair against the fitting
— single pass cap repair against the pipe.
C.5.6.14 Methods of testing and acceptance criteria shall be as specified in [C.6].
C.5.7 Qualification of welding procedures for structural components
C.5.7.1 Welding procedures for structural components, supplied as a part of the pipeline systems, shall
be qualified in accordance with ISO 15614-1. The requirements shall be appropriate for the structural
categorisation of the members and stresses in the structure. The extent of tensile, hardness and impact
testing and the testing conditions should be in compliance with this appendix.
C.5.8 Qualification of welding procedures for hyperbaric dry welding
C.5.8.1 Requirements for qualification of welding procedures for hyperbaric dry welding are given in [C.9].
C.6 Examination and testing for welding procedure qualification
C.6.1 General
C.6.1.1 All visual examination, non-destructive testing, mechanical testing and corrosion testing of test
pieces shall be performed in the as welded or post weld heat treated condition, whatever is applicable for the
final product.
Visual examination and non-destructive testing
C.6.1.2 Visual examination and non-destructive testing shall be performed no earlier than 24 hours after
the completion of welding of each test piece. Original welds intended for repair welding qualification may be
examined and tested when temperature of test piece allows for it.
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C.6.1.3 If a test piece does not meet the acceptance criteria for visual examination and NDT, one further test
piece shall be welded and subjected to the same examination. If this additional test piece does not meet the
requirements, the WPQ is not acceptable.
Destructive testing
C.6.1.4 The type and number of mechanical tests and microstructure evaluations for qualification tests are
given in [C.5.3] to [C.5.7].
C.6.1.5 Test specimens shall be taken from the positions shown in Figure C-1 and Figure C-2 for longitudinal
welds and girth welds respectively.
Re-testing
C.6.1.6 A destructive test failing to meet the specified requirements may be re-tested. The reason for the
failure shall be investigated and reported preferably before any re-testing is performed. If the investigation
reveals that the test results are influenced by improper sampling, machining, preparation, treatment or
testing, the test sample and specimen (as relevant) shall be replaced by a correctly prepared sample or
specimen and a new test performed.
C.6.1.7 A destructive test failing to meet the specified requirements shall be rejected if the reason for failure
can not be related to improper sampling, machining, preparation, treatment or testing of specimens.
C.6.1.8 Re-testing of a test failing to meet the specified requirements should only be performed subject to
agreement. This re-testing shall consist of at least two further test specimens/sets of test specimens. If both
re-tests meet the requirements, the test may be regarded as acceptable. All test results, including the failed
tests, shall be reported.
C.6.1.9 If there are single hardness values in the different test zones (weld metal, HAZ, base material) that
do not meet the requirement, retesting shall be carried out on the reverse side of the tested specimen or
after grinding and re-preparation of the tested surface. None of these additional hardness values shall exceed
the maximum value.
C.6.1.10 For Charpy V-notch impact testing the following requirements shall apply:
— in order to consider a set as approved, the average requirement has to be met and only one test
specimen out of the three may have a value between the average and the single minimum requirement.
— subject to agreement, retest may be performed with two test specimen sets.
Note 1: For pipeline girth welds, if applicable, one macro and hardness specimen shall include a pipe
longitudinal seam weld.
Note 2: The indicated location of the test specimens are not required for qualification of welding in the PA
(1G rotated) where sampling positions are optional.
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Figure C-1 Welding procedure qualification test - sampling of test specimens for longitudinal butt
welds.
Note: The indicated location of the test specimens are not required for qualification of welding in the PA (1G)
and PC (2G) positions, where sampling positions are optional.
Figure C-2 Welding procedure qualification test - typical sampling of test specimens for girth butt
welds.
Note 1: For pipeline girth welds, if applicable, one macro and hardness specimen shall include a pipe
longitudinal seam weld.
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Note 2: The indicated location of the test specimens are not required for qualification of welding in the PA
(1G rotated) where sampling positions are optional.
C.6.2 Visual examination and non-destructive testing requirements
C.6.2.1 Each test weld shall undergo 100% visual examination and 100% ultrasonic and 100% radiographic
testing and 100% magnetic particle or liquid penetrant testing. Testing shall be in accordance with [D.2]. AUT
in line with production inspection as required in App.E may be used instead of manual UT + RT.
C.6.2.2 Acceptance criteria for visual examination and non-destructive testing shall be in accordance with
[D.2.9] for welds exposed to strains < 0.4%. For welds exposed to strains ≥ 0.4%, the acceptance criteria
shall be as for the production welding or according to [D.2.9], whichever is the more stringent.
Guidance note:
When results from ECA are not available, it is recommended to consider relevant historical data compared with workmanship
criteria [D.2.9] as basis for acceptance criteria.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
C.6.2.3 Weld overlay shall be non-destructively tested according to [D.3.3] with acceptance criteria
according to [D.3.6]. The surface and weld thickness shall be representative for the production welding, i.e.
after machining of the overlay thickness or the thickness representative for the thickness on the finished
component.
C.6.3 Testing of butt welds
C.6.3.1 All testing shall be performed in accordance with App.B.
Transverse weld tensile testing
C.6.3.2 For longitudinal welds and girth welds exposed to strain εl,nom ≥ 0.4% the fracture shall not be
located in the weld metal, while for longitudinal welds and girth welds exposed to strain εl,nom <0.4% and
where no ECA is performed the fracture should not be in the weld metal. The ultimate tensile strength shall
be at least equal to the SMTS for the base material. When different material grades are joined, the ultimate
tensile strength of the joint shall be at least equal to the SMTS for the lower grade.
All-weld tensile testing
C.6.3.3 For longitudinal welds and girth welds exposed to strain εl,nom <0.4% and where no ECA is
performed, the upper yield or the Rt0.5 of the deposited weld metal should be 80 MPa above SMYS of the
base material and the elongation not less than 18%. If two grades are joined the requirement applies to the
lower strength material.
Transverse all-weld tensile testing
C.6.3.4 For pipeline girth welds where generic ECA acceptance criteria (see DNVGL-RP-F108) are applied, the
upper yield or the Rt0.5 of the deposited weld metal shall as a minimum exceed or be equal to a value 20 MPa
below the specified maximum base material yield strength. The elongation shall as a minimum be 18%.When
different material grades are joined, the yield stress requirements applies to the lower grade.
C.6.3.5 For pipeline girth welds exposed to strain εl,nom ≥ 0.4% and where full ECA acceptance criteria shall
be applied, the upper yield or the Rt0.5 of the deposited weld metal shall as a minimum exceed or be equal to
a value 20 MPa below the specified maximum base material yield strength, or the assumptions made during
design and/or the ECA. The elongation shall as a minimum be 18%.
Bend testing
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C.6.3.6 The end tests shall not disclose any open defects in any direction exceeding 3 mm. Minor ductile
tears less than 6 mm, originating at the specimen edge may be disregarded if not associated with obvious
defects.
Charpy V-notch impact testing
C.6.3.7 The average and single Charpy V-notch toughness at each position shall not be less than specified
for the base material in the transverse direction (KVT values). Requirement for fracture arrest properties
does not apply.
— C-Mn and low alloy steels shall meet the requirements given in [7.2.4].
— Duplex and martensitic stainless steels shall meet the requirements given in [7.3.4].
— The C-Mn steel backing material in clad and lined linepipe shall meet the requirements given in [7.2.4].
C.6.3.8 When different steel grades are joined, the required impact tests shall be performed on both sides of
the weld. The weld metal shall meet the less stringent energy requirement.
Macro section
C.6.3.9 The macro section shall be documented by photographs (magnification of at least 5×).
C.6.3.10 The macro section shall show a sound weld merging smoothly into the base material and meeting
Quality level C of ISO 5817.
C.6.3.11 For girth welds in welded pipe, one macro section shall include a longitudinal weld.
Hardness testing
C.6.3.12 The maximum hardness in the HAZ and weld metal is:
— 325 HV10 for C-Mn and low alloy steels in non-H2S service (also applies to backing steel in clad or lined
material).
— 250 HV10 for C-Mn and low alloy steels in H2S service (for weld caps not exposed to the H2S media,
maximum hardness of 275 HV10 may be agreed for base material thickness >9 mm) unless a higher
hardness has been qualified according to [6.2.2.2] and [B.3.4].
— 350 HV10 for 13Cr martensitic stainless steels
— 350 HV10 for duplex stainless steels
— 345 HV10 for Ni-based alloys in clad or lined material in non-H2S service. For explosion welded clad
material the requirement of maximum 40 HRC in accordance with API 5LD applies.
— 300 HV10 for austenitic stainless steels in clad or lined material in non-H2S service
— 275 HV10 for anode pads.
For clad or lined materials in H2S service special considerations are required, see ISO 15156.
C.6.3.13 Subject to agreement, additional hardness measurements shall be taken in the start/stop area for
repair weld qualification.
C.6.3.14 For girth welds in welded pipe, one hardness test specimen shall include a longitudinal weld.
Corrosion testing
C.6.3.15 Sulphide stress cracking testing (SSC) is only required for C-Mn and low alloy steels with SMYS >
450 MPa, 13Cr martensitic stainless steels and other materials not listed for H2S service in ISO 15156.
Acceptance criteria shall be according to ISO 15156.
C.6.3.16 Pitting corrosion test according to ASTM G48 is only required for 25Cr duplex stainless steel (see
2
[6.2.3.2]). The maximum weight loss shall be 4.0 g/m when tested at 40°C for 24 hours and there shall be
no pitting at 20 X magnification.
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C.6.3.17 Welds in duplex stainless steel materials, CRA materials and clad/lined materials shall be subject
to microstructure examination. The material shall be essentially free from grain boundary carbides, nitrides
and intermetallic phases. Essentially free implies that occasional strings of detrimental phases along the
centreline of the base material is acceptable given that the phase content within one field of vision (at 400X
magnification) is < 1.0% (max. 0.5% intermetallic phases).
For duplex steel the ferrite content of the weld metal shall be within the range 35 to 65%.
The ferrite content of austenitic stainless steel weld deposit shall be within the range 5 to 13%.
Micro cracking at the fusion line is not permitted.
Chemical analysis
C.6.3.18 For welds in clad or lined materials, a chemical analysis shall be performed. The analysis shall
be representative of the CRA composition at a point at the centreline of the root pass 0.5 mm below the
surface. The chemical composition shall be within the specification limits according to the UNS number for
the specified cladding/lining material or, if the weld metal is of a different composition than the cladding/liner,
within the limits of chemical composition specified for the welding consumable.
Fracture toughness testing
C.6.3.19 Fracture toughness testing shall be performed for both girth welds and repair welds when
acceptance criteria for girth welds are established by an ECA. The extent of testing shall be in accordance
with DNVGL-RP-F108.
C.6.3.20 For nominal wall thickness above 50 mm in C-Mn and low alloy steels fracture toughness testing is
required unless PWHT is performed.
C-Mn and low alloy steels shall meet the requirements given in [7.2.4.15].
Duplex and martensitic stainless steels shall meet the requirements given in [7.3.4.3].
C.6.4 Testing of weld overlay
C.6.4.1 When the weld overlay is not contributing to strength (e.g. not load bearing), tensile testing and
Charpy V-notch testing of the weld overlay material are not required. When the weld overlay strength is
considered as a part of the design, such mechanical testing of the weld overlay material is required (see
[C.6.4.12] to [C.6.4.17]).
C.6.4.2 The base material shall retain the minimum specified mechanical properties after any post weld heat
treatment. The base material properties in the post weld heat treated condition shall then be documented by
additional testing and recorded as a part of the welding procedure qualification.
C.6.4.3 The testing in [C.6.4.4] through [C.6.4.11] shall, as a minimum, be performed when the overlay
material is not considered as part of the design and when the base material has not been affected by any
post weld heat treatment. When the overlay material is considered to be part of design, the testing in
[C.6.4.12] through [C.6.4.17] shall be performed in addition to the testing in [C.6.4.4] through [C.6.4.11].
Bend testing of weld overlay
C.6.4.4 The bend testing shall be performed in accordance with [B.2.5.14]. The bend tests shall disclose
no defects exceeding 1.6 mm. Minor ductile tears less than 3 mm, originating at the specimen edge may be
disregarded if not associated with obvious defects.
Macro examination of weld overlay
C.6.4.5 The macro sections shall be documented by photographs (magnification of at least 5X). The macro
section shall show a sound weld merging smoothly into the base material and meeting Quality level C of ISO
5817.
Hardness testing of weld overlay
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C.6.4.6 The maximum hardness for base material and HAZ shall not exceed the limits given in [C.6.3.12]
above as applicable for the intended service and type of material. The maximum hardness for the overlay
material should not exceed any limit given in ISO 15156 for H2S service.
Chemical analysis of weld overlay
C.6.4.7 The chemical composition shall be obtained in accordance with App.B. Specimens for chemical
analysis shall either be performed directly on the as welded or machined surface or by taking specimen or
filings/chips from:
— the as welded surface
— a machined surface
— from a horizontal drilled cavity.
The location for the chemical analysis shall be considered as the minimum qualified thickness to be left after
any machining of the corrosion resistant weld overlay.
C.6.4.8 The chemical composition of overlay shall be shall be within the specification limits according to the
UNS for the specified overlay material. The iron content of alloy UNS N06625 overlay shall be < 10%.
Microstructure examination of weld overlay
C.6.4.9 The surface to be used for microstructure examination shall be representative of a weld overlay
thickness of 3 mm or the minimum overlay thickness specified for the finished machined component,
whichever is less. Microstructure examination shall be performed after any final heat treatment.
C.6.4.10 Metallographic examination at a magnification of 400X of the CRA weld metal HAZ and the base
material shall be performed. Micro cracking at the CRA to the C-Mn/low alloy steel interface is not permitted.
The material shall be essentially free from grain boundary carbides, nitrides and inter-metallic phases in the
final condition (as-welded or heat treated as applicable).
C.6.4.11 The ferrite content of austenitic stainless steel weld overlay deposit shall be within the range
5-13%. The ferrite content of duplex stainless steel weld overlay in the weld metal and HAZ shall be within
the range 35-65%.
All-weld tensile testing of load bearing weld overlay
C.6.4.12 All-weld tensile testing shall be performed in accordance with [B.2.3].
C.6.4.13 The yield stress and ultimate tensile strength of the weld deposit shall be at least equal to the
material tensile properties used in the design.
Charpy V-notch impact testing of load bearing weld overlay
C.6.4.14 When the weld overlay material is designed to transfer the load across the base material/weld
overlay fusion line, impact testing of the weld overlay and HAZ shall be performed (i.e. when the overlay is a
part of a butt joint or acts as a transition between a corrosion resistant alloy and a C-Mn/low alloy steel).
C.6.4.15 Testing shall be with the notch in the overlay weld metal, FL, FL+2 mm and FL+5 mm in the base
material.
C.6.4.16 The average and single Charpy V-notch toughness at each position shall not be less than specified
for the base material. When different steel grades are joined, a series of impact tests shall be considered in
the HAZ on each side of the joint. The weld metal shall meet the more stringent energy requirement.
Corrosion testing of weld overlay
C.6.4.17 Corrosion testing and microstructure examination of stainless steel and nickel base weld overlay
materials shall be considered.
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C.6.5 Testing of pin brazing and aluminothermic welds
Electrical resistance
C.6.5.1 The electrical resistance of each test weld/brazing shall not exceed 0.1 Ohm.
Mechanical strength
C.6.5.2 Each test weld/brazing shall be securely fixed and tested with a sharp blow from a 1.0 kg hammer.
The weld/brazing shall withstand the hammer blow and remain firmly attached to the base material and show
no sign of tearing or cracking.
Copper penetration
C.6.5.3 2 test specimens shall the sectioned transverse to the anode lead and 2 test specimens parallel with
the anode lead. The fusion line of the weld/brazing shall at any point not be more than 1.0 mm below the
base material surface. Intergranular copper penetration of the base material shall not at any point extend
beyond 0.5 mm from the fusion line.
Hardness
C.6.5.4 HV10 hardness tests shall be made on each of the specimens for copper penetration measurements.
C.6.5.5 The maximum hardness shall not exceed the limits given in [C.6.3.12] as applicable for the intended
service and type of material.
Pull test
C.6.5.6 The specimen shall break in the cable.
C.6.6 Testing of welds for temporary and permanent attachments and
branch outlet fittings to linepipe
C.6.6.1 Welds shall be tested to the extent required in [C.5.6] and meet the relevant requirements given in
[C.6.3] above.
C.7 Welding and post weld heath treatment requirements
C.7.1 General
C.7.1.1 All welding shall be performed using the type of welding equipment and under the conditions that
are representative for the working environment during procedure qualification welding.
C.7.1.2 Pre-qualification testing shall be performed for welding systems where the contractor has limited
previous experience, or where the system will be used under new conditions. All welding equipment shall be
maintained in good condition in order to ensure the quality of the weldment.
C.7.1.3 All welding shall be performed under controlled conditions with adequate protection from detrimental
environmental influence such as humidity, dust, draught and large temperature variations.
C.7.1.4 All instruments shall have valid calibration certificates and the adequacy of any control software shall
be documented.
C.7.1.5 Welding and welding supervision shall be carried out by personnel qualified in accordance with the
requirements given in [C.2.2].
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C.7.2 Production welding, general requirements
C.7.2.1 All welding shall be carried out strictly in accordance with the accepted welding procedure
specification and the requirements in this subsection. If any parameter is changed outside the limits of the
essential variables, the welding procedure shall be re-specified and re-qualified. Essential variables and
variation limits are specified in [C.4.8].
C.7.2.2 The preparation of bevel faces shall be performed by agreed methods. The final groove configuration
shall be as specified in the WPS and within the tolerances in the WPS.
C.7.2.3 After cutting of pipe or plate material for new bevel preparation, a new lamination check by
ultrasonic and magnetic particle/dye penetrant testing should be performed. Procedures for ultrasonic and
magnetic particle/dye penetrant testing and acceptance criteria shall be in accordance with App.D.
C.7.2.4 For welding processes using shielding, backing and plasma gases, the gas classification moisture
content and dew point shall be checked prior to start of welding. Gases in damaged containers or of
questionable composition, purity and dew point shall not be used. All gas supply lines shall be inspected for
damage on a daily basis. All gas supply lines shall be purged before the welding is started.
C.7.2.5 The weld bevel shall be free from moisture, oil, grease, rust, carbonised material, coating etc., which
may affect the weld quality.
C.7.2.6 The alignment of the abutting ends shall be adjusted to minimise misalignment. Misalignment shall
not exceed the tolerances in the WPS.
C.7.2.7 The weld area shall be heated to the minimum preheat temperature specified in the WPS. Preheating shall also be performed whenever moisture is present or may condense in the weld area and/or
°
when the ambient temperature or material temperature is below 5 C. Welding below 20°C should not be
performed.
C.7.2.8 When pre-heating is applied prior to welding, including tack welding, the pre-heating temperature
shall be measured at a distance of minimum 75 mm from the edges of the groove at the opposite side of the
heating source when practically possible. If this is not possible, the adequacy of the performed measurement
shall be demonstrated.
C.7.2.9 Tack welding shall only be performed if qualified during welding procedure qualification. The
minimum tack weld length is 2t or 100 mm, whichever is larger. For small pipe diameters, shorter tack
lengths may be agreed. Temporary tack welds using bridging or bullets shall only be performed using
materials equivalent to the base material and using a WPS based on a qualified welding procedure. All such
tack welds and any spacer wedges shall be removed from the final weldment. Tack welds to be fused into the
weld shall be made in the weld groove only and the ends of the tack welds shall have their ends ground and
feathered and examined for cracks by an adequate NDT method. Defective tack welds shall be removed or
repaired prior to production welding.
C.7.2.10 Removal of tack welds shall be by grinding and cleaning followed by examination of the ground
area by visual inspection. Where temporary tack welds are removed, the bevel configuration and root gaps
specified in the WPS shall be maintained for the subsequent pass and the groove visually inspected prior to
resuming welding of the root pass.
C.7.2.11 The interpass temperature shall be measured at the edge of the groove immediately prior to
starting the following pass. For multi torch bugs, the interpass temperature is defined as the temperature in
front of the first wire on each bug.
C.7.2.12 Earth connections shall be securely attached to avoid arc burns and excessive resistance heating.
Welding of earth connections to the work piece is not permitted.
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C.7.2.13 The number of welders and the weld sequence shall be selected in order to cause minimum
distortion of the pipeline or the components.
C.7.2.14 Start and stop points shall be distributed over a length of weld and not stacked in the same area.
C.7.2.15 Welding arcs shall be struck on the fusion faces only. Weld repair of base material affected by stray
arcs is not permitted.
C.7.2.16 Arc burns shall be repaired by mechanical removal of affected base material followed by NDT to
verify absence of cracks and ultrasonic wall thickness measurements to verify that the remaining material
thickness is not below the minimum allowed.
C.7.2.17 Surface slag clusters, surface porosity and high points shall be removed by grinding and the weld
visually inspected prior to deposition of the next weld pass.
C.7.2.18 After weld completion, all spatter, scales, slag, porosity, irregularities and extraneous matter on the
weld and the adjacent area shall be removed. The cleaned area shall be sufficient for the subsequent NDT.
Peening is not permitted.
C.7.2.19 Welding shall not be interrupted before the joint has sufficient strength to avoid plastic yielding
and cracking during handling. Prior to restart after an interruption, preheating to the minimum interpass
temperature of the pass in question shall be applied.
C.7.2.20 Welds shall only be left un-completed if unavoidable. Welding of fittings shall always be completed
without interruption. If welding is interrupted due to production restraints, the minimum number of passes
specified in the WPS shall be completed before stopping welding. If the WPS does not specify a minimum
number of passes, at least 3 passes or half the thickness of the joint should be completed before the welding
is interrupted. When interruption of welding is imposed by production restraints, interrupted welds shall
be wrapped in dry insulating material and allowed to cool in a slow and uniform manner. Before restarting
welding of an interrupted weld, the joint shall be reheated to the interpass temperature recorded during
qualification of the welding procedure.
C.7.2.21 Maximum root gap for fillet welds should be 2 mm. Where the root gap is > 2 mm but ≤ 5 mm,
this shall be compensated by increasing the throat thickness on the fillet weld by 0.7 mm for each mm
beyond 2 mm gap. Welding of fillet welds with root gap > 5 mm is subject to repair based on an agreed
procedure.
C.7.3 Repair welding, general requirements
C.7.3.1 The allowable repairs and re-repairs are given in Table C-7 and are limited to one repair in the same
area. Repeated repairs shall be subject to agreement and are limited to one repeated repair of a previously
repaired area.
Table C-7 Types of weld repairs
Type of material
Type of repair
C-Mn and low
alloy steel
13Cr MSS
Clad/lined
CRA/Duplex SS 1)
Through thickness repair
Permitted
Permitted
If agreed
If agreed
Partial thickness repair
Permitted
Permitted
Permitted
Permitted
In-process root repair
Permitted
Permitted
Permitted
Permitted
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Single pass cap repair
Permitted
Permitted
Permitted
Permitted
Single pass root sealing repair
If agreed
If agreed
If agreed
If agreed
Through thickness repeated repair
If agreed
Not permitted
Not permitted
Not permitted
Partial thickness repeated repair
If agreed
Not permitted
Not permitted
Not permitted
In-process root repeated repair
Not permitted
Not permitted
Not permitted
Not permitted
Single pass cap repeated repair
Not permitted
Not permitted
Not permitted
Not permitted
Single pass root sealing repeated repair
Not permitted
Not permitted
Not permitted
Not permitted
Note
1)
Provided solution annealing is performed after welding, all repairs are allowed.
C.7.3.2 Repair welding procedures shall be qualified to the extent that such repairs are feasible and
applicable for the repair situation in question. Qualification of repair welding procedures denoted if agreed,
need only be done if performing such repairs is agreed and are feasible for the repair situation in question.
C.7.3.3 Cellulosic coated electrodes shall not be used for repair welding.
C.7.3.4 Repair welding of cracks is not permitted unless the cause of cracking by technical evaluation has
been established not to be a systematic welding error (cracks in the weld is cause for rejection).
C.7.3.5 Defects in the base material shall be repaired by grinding only.
C.7.3.6 Defective welds that cannot be repaired with grinding only may be repaired locally by welding.
Repair welding shall be performed in accordance with a qualified repair welding procedure. For welding
processes applying large weld pools, e.g. multi-arc welding systems, any unintended arc-stops shall be
considered as defects.
C.7.3.7 Weld seams may only be repaired twice in the same area, if agreed. Repeated repairs of the root
in single sided welds are not permitted, unless specifically qualified and accepted in each case. Weld repairs
shall be ground to merge smoothly into the original weld contour.
C.7.3.8 Repairs of the root pass in a single-sided joint for material meeting H2S service requirements shall
be carried out under constant supervision.
C.7.3.9 A local weld repair shall be at least 50 mm long or 4 times the excavation depth, whichever is
longest. The length of the excavation measured at the bottom of the groove shall be minimum 50 mm.
C.7.3.10 The excavated portion of the weld shall be large enough to ensure complete removal of the defect,
and the ends and sides of the excavation shall have a gradual taper from the bottom of the excavation to
the surface. Defects can be removed by grinding, machining or air-arc gouging. Air-arc gouging shall be
controlled by a documented procedure including the allowed variables according to AWS C5.3. If air-arc
gouging is used, the last 3 mm through the root of the weld shall be removed by mechanical means and the
whole excavated area shall be ground to remove any carbon enriched zones. The width and the profile of
the excavation shall be sufficient to ensure adequate access for re-welding. Complete removal of the defect
shall be confirmed by magnetic particle testing, or by dye penetrant testing for non ferromagnetic materials.
Residuals from the NDT shall be removed prior to re-welding.
C.7.3.11 Weld repairs shall be ground to merge smoothly into the original weld contour.
C.7.3.12 Repair by welding after final heat treatment is not permitted.
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C.7.3.13 For partial thickness repair the minimum ligament should be 6 mm. Subject to agreement, a lower
ligament may be qualified, but never smaller than 3 mm.
C.7.4 Post weld heat treatment
C.7.4.1 Welds shall be subjected to PWHT as specified in the pWPS or WPS and to a documented procedure.
C.7.4.2 Post weld heat treatment shall be performed for welded joints of C-Mn and low alloy steel having a
nominal wall thickness above 50 mm, unless fracture toughness testing shows acceptable values in the as
welded condition. In cases where the minimum design temperature is less than -10°C, the thickness limit
shall be specially determined.
C.7.4.3 If post weld heat treatment is used to obtain adequate resistance of welded joints against sulphide
stress cracking, this shall be performed for all thicknesses.
C.7.4.4 Whenever possible, PWHT shall be carried out by placing the welded assembly in an enclosed
furnace. Requirements to PWHT in an enclosed furnace are given in [8.4.5].
C.7.4.5 If PWHT in an enclosed furnace is not practical, local PWHT shall be performed by means of electric
resistance heating mats or other methods as agreed or specified. The PWHT shall cover a band over the
entire length of the weld. The band shall be centred on the weld and the width of the heated band shall not
be less than 5 times the thickness of the thicker component in the assembly.
C.7.4.6 Temperatures should be measured by thermocouples in effective contact with the material and at a
number of locations to monitor that the whole length of the weld is heated within the specified temperature
range. In addition temperature measurements shall be made to confirm that undesired temperature
gradients do not occur.
C.7.4.7 Insulation shall be provided if necessary to ensure that the temperature of the weld and the HAZ is
not less than the temperature specified in the pWPS or WPS. The width of the insulation shall be sufficient to
ensure that the material temperature at the edge of the insulation is less than 300°C.
1
C.7.4.8 The rate of heating for C-Mn and low alloy steels above 300°C shall not exceed 5500/t °C · h and
1
the rate of cooling while above 300°C shall not exceed 6875/t °C · h with t expressed in mm. During heating
°
and cooling at temperatures above 300°C the temperature variation shall not exceed 35 C in any weld length
of 1000 mm.
The holding time at temperature should be minimum 30 minutes +2.5 minutes per mm thickness. Below
300°C the cooling may take place in still air.
C.7.4.9 The holding temperature for C-Mn low alloy steels should be within 580°C to 620°C unless otherwise
specified or recommended by the material/welding consumable supplier. The maximum PWHT temperature
for quenched and tempered low alloy steels shall be 25°C less than the tempering temperature of the
material as stated in the material certificate.
C.7.4.10 The heat treatment temperature cycle charts shall be available for verification if requested.
C.7.4.11 For materials other than C-Mn and low alloy steels the PWHT heating and cooling rates,
temperature, and holding time shall be as recommended by the material manufacturer.
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C.7.5 Welding of pipeline girth welds
Production welding
C.7.5.1 These requirements apply to welding of girth welds in pipelines regardless of whether the welds are
made onboard a laying vessel or at other locations, onshore or offshore. Girth welds in expansion loops, pipe
strings for reeling or towing and tie-in welds are considered as pipeline girth welds.
C.7.5.2 The type of welding equipment and the welding procedure shall be qualified prior to installation
welding.
C.7.5.3 In addition to the requirements given in [C.7.1] and [C.7.2], the requirements below shall apply for
production welding of pipeline girth welds.
C.7.5.4 Bevels shall be prepared by machining. Bevelling by thermal cutting shall be performed only when
bevelling by machining is not feasible e.g. for tie-in and similar situations. Bevels prepared by thermal
cutting shall be dressed to obtain the final configuration. The bevelling operator shall check the bevel
configuration for compliance with suitable tools or gauges at regular intervals.
C.7.5.5 When welds are to be examined by manual or automated ultrasonic testing, reference marking shall
be made on both sides of the joint as a scribed line around the pipe circumference. The reference marking
shall be at a uniform and known distance from the root face of the bevel preparation. The distance from the
root face and the tolerances shall be established, See also [E.2.1.4] and [E.2.10].
C.7.5.6 All pipes shall be cleaned on the inside to remove any and all foreign matters and deposits in
accordance with a documented procedure.
C.7.5.7 The longitudinal welds shall be staggered at least 50 mm. This is primarily to avoid a running
fracture along the weldseam over several linepipe joints. If agreed with end-user, it may be accepted to line
up the longitudinal welds of two consecutive linepipes given that there are sufficient amount of girth welds
with staggered longitudinal weld seams between such instances. Girth welds should be separated at least
1.5 pipe diameters or 500 mm, whichever is larger. Whenever possible girth welds shall be separated by the
maximum possible distance.
Guidance note:
The location of longitudinal welds along the circumference of the pipeline has no influence for pipeline integrity, however, for S-lay
welding it could be considered to locate the longitudinal weld in the top quadrant for inspection purposes.
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C.7.5.8 Excessive misalignment may be corrected by hydraulic or screw type clamps. Hammering or heating
for correction of misalignment is not permitted. Root gaps shall be even around the circumference. The final
fit-up shall be checked with spacer tools prior to engaging line-up clamps or tack welding.
C.7.5.9 The use of mitre welds to correct angular misalignment of more than 2 degrees between the axis of
two adjoining pipes is not permitted and a series of purpose made misalignment are not allowed to constitute
a bend, see [5.2.1.9].
C.7.5.10 Power operated internal line-up clamps shall be used whenever possible.
Internal line-up clamps shall not be released unless the pipe is fully supported on each side of the joint.
External line-up clamps shall not be removed unless the pipe is fully supported on each side of the joint and
not before the completed parts of the root pass meet the requirements to length of each section, the spacing
of the sections, the number of sections and the percentage of circumference required by the WPS.
C.7.5.11 Line-up clamps should not be removed before the first two passes are completed. For spool base
welding the internal line up clamps may be removed after completing root pass when pipe is supported by
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rollers to ensure a smooth transfer from station to station. See [10.5.2.3] regarding moving of pipe during
installation welding.
C.7.5.12 If cables are present inside the pipeline, e.g. buckle detector cables, and radiographic testing is
used, the starts and stops shall be made away from the six o’clock position to avoid masking of starts and
stops on radiographs.
C.7.5.13 Copper contact tips and backing strips shall be checked on a regular basis for damage that could
introduce copper contamination in welds. Damaged contact tips and backing strips shall be replaced.
C.7.5.14 Procedures shall be established for pre-cleaning, in process cleaning and post cleaning of welds.
C.7.5.15 If a pipe is to be cut for any reason, the cut shall be at a minimum distance of 25 mm from the
weld toe. It is acceptable to cut less than 25 mm providing it can be documented by macrograph that the
entire HAZ has been removed.
C.7.5.16 The root and the first filler pass shall be completed at the first welding station before moving the
pipe. Moving the pipe at an earlier stage may be permitted if an analysis demonstrates that the pipe can be
moved without any risk of introducing damage to the deposited weld metal. For spool base welding the pipe
may be moved after completing root pass when pipe is supported by rollers to ensure a smooth transfer from
station to station. See [10.5.2.3].
Repair welding
C.7.5.17 In addition to the requirements given in [C.7.3] the below requirements shall apply for repair
welding of pipeline girth welds.
C.7.5.18 For through thickness repairs where the defects to be repaired are less than 100 mm apart, they
shall be considered and repaired as one continuous defect.
C.7.5.19 The location of repair of burn through and other in process root repairs shall be marked on the
outside of the pipe to inform NDT personnel that a root repair has been made.
C.7.5.20 If the pipe and the area of repair is not exposed to bending and/or axial stresses at the repair
location when performing a repair, the length of a repair excavation shall not exceed 30% of the pipe
circumference for partial penetration repairs and 20% of the pipe circumference for through thickness
repairs.
C.7.5.21 Long defects may require repair in several steps to avoid yielding and cracking. The maximum
length of allowable repair steps shall be calculated based on the maximum stresses present in the joint
during the repair operation, and shall not exceed 80% of SMYS.
C.7.5.22 If the repair is performed at a location where the pipe and the area of repair is exposed to bending
and axial stresses the allowable length of the repair excavation shall be determined by calculations, see
[10.5.2.2] and [10.5.2.3].
C.7.5.23 If repairs can not be executed according to the requirements above, or are not performed
successfully, the weld shall be cut out.
C.7.5.24 Full records of all repairs, including in-process root repairs, shall be maintained.
Production tests
C.7.5.25 Production tests shall be performed in a manner which, as far as possible, reproduces the actual
welding, and covers the welding of a sufficient large pipe section in the relevant position. All welding stations
on the production line shall be used to produce the production test weld. Production welds cut out due to NDT
failure may be used.
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C.7.5.26 Production tests should be performed for each welding procedure specification (WPS) used for
welding of the pipeline girth welds. All welding stations/productions lines shall be covered. Production tests
should be performed as early as possible in the construction phase, e.g. within the first 100 welds.
Guidance note:
Production tests also applies to welding onshore for e.g. installation by reeling. Production tests may also be performed on the
vessel prior to start installation welding, e.g. when the vessel is moving to the pipelaying start destination.
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C.7.5.27 Production tests should not be required for welding procedures qualified specifically for tie-in welds,
flange welds, Tee-piece welds etc.
C.7.5.28 The extent of production tests shall be expanded if:
—
—
—
—
—
the contractor has limited previous experience with the welding equipment and welding methods used
the welding inspection performed is found to be inadequate
severe defects occur repeatedly
any other incident indicates inadequate welding performance
the installed pipeline is not subjected to system pressure testing, see [5.2.2.3].
C.7.5.29 The extent of production testing shall be consistent with the inspection and test regime and
philosophy of the pipeline project.
C.7.5.30 Production tests shall be subject to the non-destructive, macro, hardness, all-weld tensile and
Charpy V-notch impact testing as required in this appendix for welding procedure qualification testing
(WPQT).
C.7.5.31 If production tests show unacceptable results, appropriate corrective and preventative actions shall
be initiated and the extent of production testing shall be increased.
C.7.6 Welding and post weld heath treatment of pipeline components
C.7.6.1 The manufacturer shall be capable of producing pipeline components of the required quality.
C.7.6.2 Welding and PWHT shall be performed in accordance with [C.7.1] through [C.7.4] above.
C.7.6.3 Production tests shall be performed in a manner which, as far as possible, reproduces the actual
welding, and covers the welding of a sufficient large test section in the relevant position. All welding stations
on the production line shall be used to produce the production test weld. Production welds cut out due to NDT
failure may be used.
C.8 Material and process specific requirements
C.8.1 Internally clad/lined carbon steel and duplex stainless steel
WPS
C.8.1.1 In addition to the applicable data given in Table C-1, the WPS shall specify the following, as recorded
during the welding procedure qualification:
—
—
—
—
the minimum time period of backing gas application prior to start of welding
the minimum time period of backing gas application during welding
the minimum time period of backing gas application after welding
description of the back-purge dam type and method.
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Essential variables
C.8.1.2 The following essential variables shall apply in addition to those in Table C-2:
— any reduction of the time of backing gas application prior to start of welding
— any reduction in the number of passes completed before stopping back-purging.
Welding consumables for clad/lined carbon steel
C.8.1.3 For single sided (field) joints, the same type of welding consumable should be used for all passes
needed to complete the joint. Alternative welding consumables may be considered for fill and capping passes
after depositing a weld thickness not less than 2 times thickness of the cladding/lining. The alternative
welding consumables shall be documented to be compatible with the welding consumables used for the root
area, the base material and the applicable service conditions. Welding consumables for clad/lining shall be
segregated from consumables for C-Mn steel.
Welding consumables for duplex steel
C.8.1.4 Welding consumables with enhanced nickel and nitrogen content shall be used unless full heat
treatment after welding is performed. Sufficient addition of material from the welding consumables is
essential for welding of the root pass and the two subsequent passes. Welding consumables shall be
segregated from consumables for C-Mn steel.
C.8.1.5 Backing and shielding gases shall not contain hydrogen and shall have a dew point not higher than
-30°C. Some particular cases may exempt from this requirement (i.e. plasma shielding gas used for welding
of austenitic materials). The oxygen content of the backing gas should be less than 0.1% during welding of
the root pass. Backing gas shall be used for welding of root and hot pass as a minimum to avoid oxidation of
the CRA. (Exception from this requirement may be tie-in welds when stick electrodes are used for root bead
welding, subject to agreement.)
Production
C.8.1.6 Welding of clad/lined carbon steel and duplex stainless steel may be performed by the welding
processes listed in [C.1.2]. The welding shall be double sided whenever possible. Welding of the root pass in
single sided joints will generally require welding with Gas Tungsten Arc Welding (GTAW/141) or Gas Metal Arc
Welding (GMAW/135).
C.8.1.7 Onshore fabrication of clad/lined carbon steel and duplex stainless steel shall be performed in
a workshop, or part thereof, which is reserved exclusively for this type of material. During all stages of
manufacturing, contamination of CRA and duplex steel with carbon steel and zinc shall be avoided. Direct
contact of the CRA with carbon steel or galvanised handling equipment (e.g. hooks, belts, rolls, etc.) shall be
avoided. Tools such as earthing clamps, brushes etc, shall be stainless steel suitable for working on type of
material in question and not previously used for carbon steel. Contamination of weld bevels and surrounding
areas with iron and low melting point metals such as copper, zinc, etc. is not acceptable. The grinding wheels
shall not have previously been used for carbon steel, unless it can be documented that no contamination will
occur. Parts of internal line-up clamps that come in contact with the material shall be non-metallic or of a
similar alloy as the internal pipe surface. Thermal cutting shall be limited to plasma arc cutting.
C.8.1.8 The weld bevel shall be prepared by milling or other agreed machining methods. The weld bevel and
the internal and external pipe surface up to a distance of at least 25 mm from the bevels shall be thoroughly
cleaned with an organic solvent.
C.8.1.9 Welding consumables shall be segregated from consumables for C-Mn/low alloy steels.
C.8.1.10 The backing gas composition shall be monitored using an oxygen analyser immediately prior
to starting or re-starting welding. The flow rate of the back purge gas shall be adjusted to prevent gas
turbulence and possible air entrainment through open weld seams.
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C.8.1.11 Inter-run cleaning shall be by grinding to bright, defect free material for all passes.
C.8.1.12 Welds shall be multipass and performed in a continuous operation.
C.8.1.13 The interpass temperature shall be measured directly where a weld run will start and terminate.
The weld zone shall be kept below the maximum interpass temperature before a welding run is started.
Unless post weld heat treatment is performed, the maximum interpass temperature shall not exceed 150°C
for welding of all solid CRA and in root and hot pass for lined/clad carbon steel.
C.8.1.14 When clad/lined C-Mn linepipe is cut and/or re-bevelled a lamination check by through thickness
ultrasonic testing and dye penetrant testing on the bevel face shall be performed. If a laminar discontinuity is
detected on the bevel face the cladding/liner shall be removed and a seal weld shall be overlay welded at the
pipe end.
Additional for welding of duplex steel
C.8.1.15 The heat input shall be controlled to avoid detrimental weld cooling rates. For optimum control
of the heat input faster welding speeds and associated higher welding current should be used. Stringer
beads shall be used to ensure a constant heat input, and any weaving of the weld bead should be limited to
maximum 3X filler wire/electrode diameter. For girth welds the heat input should be kept within the range
0.5 - 1.8 kJ/mm and avoiding the higher heat input for small wall thicknesses. For wall thickness > 25 mm
and provided post weld heat treatment (solution annealing) is performed a maximum heat input of 2.4 kJ/
mm is acceptable. For the root pass the heat input shall be higher than for second pass. For SAW welding
small diameter wire and modest welding parameters (high travel speed and low arc energy) shall be used.
The depth to width ratio of the weld deposit shall be less than 1.0.
C.8.1.16 Solution annealing post weld heat treatment shall be performed in accordance with qualified heat
treatment procedure.
C.8.1.17 Excavation of repair grooves shall be by chipping, grinding or machining. Air-arc gouging shall not
be used. Entire welds shall be removed by plasma cutting or machining. Repeated repairs are not permitted.
C.8.1.18 All operations during welding shall be carried out with adequate equipment and/or in a protected
environment to avoid carbon steel contamination of the corrosion resistant material. Procedures for
examination of surfaces and removal of any contamination shall be prepared.
C.8.2 13Cr Martensitic stainless steel
WPS and essential variables
C.8.2.1 The additional data for the WPS and the essential variables given in [C.8.1.1] and [C.8.1.2] also
applies to 13Cr martensitic stainless steels.
Welding consumables
C.8.2.2 The requirements to backing and shielding gases in [C.8.1.5] also apply to 13Cr MSS.
Production
C.8.2.3 Welding of 13Cr MSS may be performed by the welding processes listed in [C.1.2], except active gas
shielded methods. The welding shall be double sided whenever possible.
C.8.2.4 During all stages contamination of 13Cr MSS with carbon steel and zinc shall be avoided. Direct
contact with carbon steel or galvanised handling equipment (e.g. hooks, belts, rolls, etc.) shall be avoided.
Tools such as earthing clamps, brushes etc., shall be stainless steel suitable for working on type of material in
question and not previously used for carbon steel. Contamination of weld bevels and surrounding areas with
iron and low melting point metals such as copper, zinc, etc. is not acceptable. The grinding shall not have
previously been used for carbon steel. Parts of internal line-up clamps that come in contact with the material
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shall be non-metallic or of a similar alloy as the internal pipe surface. Thermal cutting shall be limited to
plasma arc cutting.
C.8.2.5 The weld bevel shall be prepared by milling or other agreed machining methods. The weld bevel and
the internal and external pipe surface up to a distance of at least 25 mm from the bevels shall be thoroughly
cleaned with an organic solvent.
C.8.2.6 Welding consumables shall be segregated from consumables for C-Mn steel.
C.8.2.7 The backing gas composition shall be monitored using an oxygen analyser immediately prior to
starting or re-starting welding. Care shall be taken to adjust the flow rate of the back purge gas to prevent
gas turbulence and possible air entrainment through open weld seams.
C.8.2.8 The interpass temperature shall be measured directly at the points where a welding run will start
and terminate. The weld zone shall be below the maximum interpass temperature before a welding run is
o
started. The maximum interpass temperature shall not exceed 150 C.
o
C.8.2.9 PWHT (e.g.≈ 5 minutes at≈ 630 C) should be performed in accordance with the PWHT procedure
qualified during welding qualification.
C.8.2.10 Excavation of repair grooves shall be by chipping, grinding or machining. Air-arc gouging shall not
be used. Entire welds shall be removed by plasma cutting or machining.
C.8.2.11 All operations during welding shall be carried out with adequate equipment and/or in a protected
environment to avoid carbon steel contamination of the corrosion resistant material. Procedures for
examination of surfaces and removal of any contamination shall be prepared.
C.8.3 Pin brazing and aluminothermic welding
C.8.3.1 Anode leads may be attached by pin brazing or aluminothermic welding according to qualified
procedures including full details of the technique used and associated equipment.
Qualification of operators
C.8.3.2 Operators that have performed a qualified procedure test are thereby qualified.
C.8.3.3 Other operators shall prior to carrying out operation work, each complete three test pieces made in
accordance with the procedure specification under realistic conditions. Each test piece shall pass the test for
electrical resistance and mechanical strength according to Table C-6 and [C.6.5].
Essential variables
C.8.3.4 Essential variables for pin brazing and aluminothermic welding shall be:
Base material grade and chemical composition:
— a change in grade
— a change in the supply condition (TMCP, Q/T or normalised)
— any increase in Pcm of more than 0.02, CE of more than 0.03 and C content of more than 0.02% for C-Mn
linepipe.
For both methods a change in:
—
—
—
—
cable dimension
process (brazing or aluminothermic welding)
make, type and model of equipment
method for cleaning and preparation of cable ends and cable attachment area.
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For aluminothermic welding a change in:
— type, classification and brand of start and welding powder
— type, make and model of other consumables
— volume (cartridge, packaging type) and type of start and welding powder that will change the heat input
by more than ± 15%.
For pin brazing a change in:
—
—
—
—
type, composition, make and model of pin for pin brazing
the minimum preheat or working temperature
range of equipment settings for pin brazing
the equipment earth connection area.
Production requirements for welding/brazing of anode leads
C.8.3.5 The anode cable attachments shall be located at least 150 mm away from any weld.
C.8.3.6 For cable preparation cable cutters shall be used. The insulation shall be stripped for the last 50 mm
of the cable to be attached. The conductor core shall be clean, bright and dry. Greasy and oily conductor
cores shall be cleaned with residue free solvent or dipped in molten solder. Corroded conductor cores shall
be cleaned to bright metal with brush or other means. Wet conductor cores shall be dried by rapid drying
residue free solvent, alcohol or hand torch.
C.8.3.7 The cable attachment area, and for pin brazing also the equipment earth connection area, shall
be cleaned for an area of minimum 50 mm × 550 mm. All mill scale, rust, grease, paint, primer, corrosion
coating, and dirt shall be removed and the surface prepared to finishing degree St 3 according to ISO
8501-1. The surface shall be bright, clean and dry when welding/brazing is started.
Production testing
C.8.3.8 Each welded/brazed anode lead shall be subjected to electrical resistance test and mechanical
strength test according to Table C-6 with acceptance criteria according to [C.6.5].
Repair of welded/brazed anode leads
C.8.3.9 Welded/brazed anode leads not meeting the requirements in [C.6.5] shall be removed and the
affected area shall be removed by grinding.
C.8.3.10 For welded/brazed anode leads that are attached directly onto pressure containing parts the ground
areas shall blend smoothly into the surrounding material. Complete removal of defects shall be verified by
local visual inspection and polishing and etching to confirm removal of copper penetration. The remaining
wall thickness in the ground area shall be checked by ultrasonic wall thickness measurements to verify that
the thickness of the remaining material is more than the specified minimum. Imperfections that encroach on
the minimum permissible wall thickness shall be classified as defects.
C.9 Hyperbaric dry welding
C.9.1 General
C.9.1.1 Underwater welding on pressure containing components for hydrocarbons shall be carried out
utilising a low hydrogen process, in a chamber (habitat) where the water has been displaced. Other methods
can be used on non-pressure containing components subject to special acceptance by purchaser.
C.9.1.2 All relevant welding parameters shall be monitored and recorded at the surface control station
under supervision by a welding co-ordinator. The welding area shall have continuous communication with the
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control station. All operations including welding shall be monitored by a video system that can be remotely
controlled from the control station.
C.9.2 Qualification and testing of welding personnel for hyperbaric dry
welding
Hyperbaric welding co-ordinator
C.9.2.1 The welding co-ordinator for hyperbaric dry welding shall have adequate experience with welding
procedure qualification and offshore operations for the hyperbaric welding and welding related system used.
C.9.2.2 The welding co-ordinator shall, when applicable, have completed the training programme required
for mechanised welding required in [C.9.2.4] to [C.9.2.6].
Welders for hyperbaric welding
C.9.2.3 Prior to qualification testing for underwater (hyperbaric) dry welding of girth welds, welders shall
have passed a welding test for pipeline girth welds as specified in [C.2.2].
Training programme
C.9.2.4 The hyperbaric welders shall be informed on all aspects of the work related to the welding operation,
the qualified welding procedures, the applicable technical specifications and layout of the welding and habitat
system.
C.9.2.5 Hyperbaric welders shall receive a training programme and pass an examination upon completion of
the programme. The training programme shall be structured according to Annex B of ISO 15618-2.
C.9.2.6 In addition, for mechanised welding the training programme shall include:
—
—
—
—
—
software structure of welding programme and loading of any welding programme prior to start of welding
perform a complete butt weld, from programming of the welding parameters to welding of the cap passes
repair welding
daily maintenance of the welding equipment
knowledge about the functions of the welding heads and how to replace consumables such as welding
wire, contact tubes, gas nozzles and tungsten electrodes.
Test welding
C.9.2.7 The hyperbaric welders shall perform a qualification test using welding equipment identical or equal
in function to the hyperbaric welding equipment used for production welding.
C.9.2.8 The qualification welding for hyperbaric welding shall be performed in accordance with ISO 15618-2.
Qualification testing of welders
C.9.2.9 For welder qualification for dry hyperbaric welding of girth welds and other butt weld configurations
the test pieces shall be subject to same the testing and acceptance criteria as for pipeline girth welds in
[C.2.2].
C.9.2.10 A welder is deemed qualified for the applicable ranges of approval stated in Clause 6 of ISO
15618-2 when the following requirements for inspection and testing of test pieces, as applicable, are met:
— 100% visual examination and 100% ultrasonic testing with test requirements and acceptance criteria in
accordance with App.D
— macro-examination according to App.B. The specimen shall meet the requirements of ISO 15618-2,
Chapter 8
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— if 100% radiographic testing with test requirements and acceptance criteria in accordance with App.D is
performed in lieu of 100% ultrasonic testing, bend testing as required in ISO 9606 shall be performed for
all welding processes.
Retesting
C.9.2.11 See ISO 15618-2, Chapter 9.
Period of validity and prolongation
C.9.2.12 The period of validity shall be 6 months, and the prolongation in accordance with ISO 15618-2,
paragraph 10.2.
C.9.3 Welding processes for hyperbaric dry welding
C.9.3.1 The allowable welding processes are (see ISO 4063):
—
—
—
—
SMAW (Process ISO 4063-111)
G-FCAW (Process ISO 4063-137)
GMAW (Process ISO 4063-131)
GTAW (Process ISO 4063-141).
C.9.4 Welding consumables for hyperbaric dry welding
C.9.4.1 In addition to the requirements given in [C.3.1] to [C.3.4] the following shall apply:
— consumables should be of a type that is tested or developed for dry hyperbaric welding with respect to arc
stability and metal transfer behaviour and mechanical properties
— procedures for transfer of consumables to the hyperbaric chamber and for consumable handling in the
chamber, including disposal of unused exposed consumables. The procedure shall particularly consider the
maximum humidity expected during production welding
— all consumables for qualification of the welding procedure shall be from the same batch, a consumable
batch being defined as the volume of product identified by the supplier under one unique batch/lot
number, manufactured in one continuous run from batch/lot controlled raw materials.
C.9.5 Shielding and backing gases for hyperbaric dry welding
C.9.5.1 In addition to the requirements given in [C.3.5] the following shall apply:
— the purity of shielding and backing gases shall be 99.995 for Ar and 99.997% for He. The maximum
allowable moisture content in the gas used in the actual welding is governed by the moisture content of
the gas used during the qualification welding.
Guidance note:
The dew point temperature at atmospheric pressure (1 bar) is often used to specify the upper level acceptance criteria for the
moisture content in shielding gases. However, for hyperbaric conditions, even a low dew-point temperature (e.g. -30°C for an
Argon gas) can result in condensation of water at the relevant working depth/pressure and temperature (e.g. at 165 m at 5°C).
This means that the gas is saturated with water when used at this depth and condensed water will be present at greater depths.
In general the acceptance level for the water content in the shield gas should be specified precisely. The use of “ppm” alone is not
sufficient. It should be related either to volume or weight of the gas.
It is the water concentration in the gas at the working depth/pressure which is essential. This can be specified as weight of the
water per volume unit (mg H2O/m3) or partial pressure of the H2O (millibar H2O).
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C.9.6 Welding equipment and systems for hyperbaric dry welding
C.9.6.1 In addition to the requirements given in [C.2.1] the following shall apply unless the voltage is
measured at the arc during both qualification and production welding:
— Welding cables shall have the same dimension and approximately the same resistance during the welding
procedure qualification and production welding. If necessary artificial resistance to simulate the full cable
length used in production should be used during qualification welding.
C.9.7 Welding procedures for hyperbaric dry welding
Contents of pWPS
C.9.7.1 A pWPS shall be prepared for each welding and repair welding procedure that will be qualified for use
during welding of pipeline girth welds.
C.9.7.2 The pWPS shall contain the information required for the applicable welding processes, including any
tack welds and shall be prepared in accordance with Table C-1 and shall propose limits and ranges for the
applicable essential variables for welding and repair welding procedures given in Table C-2 and Table C-8.
C.9.7.3 In addition the pWPS shall address the following:
— vent hole, number of runs to be deposited before closing the root and methods for closing the root
— conditions for release of external line-up clamps including the percentage of the circumference for the
welded root sections, the length of each section and spacing of the sections
— water depth (minimum/maximum)
— pressure inside the chamber
— gas composition inside the chamber
— humidity, maximum level
— temperature inside the chamber (minimum/maximum)
— length, type and size of the welding umbilical
— position for voltage measurements
— welding equipment.
C.9.7.4 The welding procedures for closing possible vent holes shall also be qualified. This qualification test
should as a minimum include impact testing of weld metal, FL, FL+2, FL+5,macro/hardness testing and
for CRA also metallographic examination. The qualification may be performed as a buttering test providing
considerations are made to start/stop and that access limitations for the actual production welding is
simulated.
Essential variables
C.9.7.5 The essential variables for hyperbaric dry welding shall be according to Table C-2 with additional
requirements according to Table C-8 below.
Table C-8 Additional essential variables for hyperbaric dry welding
A qualified water depth for SMAW and GTAW
Water depth (WD) in metres:
1)
1
WD ≤ 200 m: Any increase in excess of + 20% or 10 m or whichever is greater.
2
200 m < WD ≤ 300 m: ± 10%
3
300 m < WD ≤ 500 m: ± 10%
B Habitat environment
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Gas composition (argon, heliox,
air or nitrox), and humidity
1
For water depth ≤ 200 m: A change from argon or heliox to air or nitrox but not
vice versa
2
For water depth > 200 m: Any change in gas composition
3
Any increase in relative humidity for SMAW and G-FCAW flux based welding
processes otherwise any increase in excess of + 10%
C Monitoring of electrical parameters
Method and point of monitoring
1
Any change
Note
1)
For other processes the depth of qualification shall be agreed.
C.9.8 Qualification welding for hyperbaric dry welding
C.9.8.1 Qualification welding shall be performed in the habitat at a water depth selected in accordance
with the intended range of qualification, or under appropriately simulated conditions. The qualification test
program shall consist of a minimum of one completed joint for manual welding, and a minimum of three
joints for mechanised welding systems.
C.9.8.2 Qualification welding shall comply with [C.5.1] and the following additions:
— for SMAW welding shall be performed at the maximum expected humidity in the chamber during
production welding
— the power source and the technical specification for the welding system shall be equivalent to the
production system
— the pipes shall be rigidly fixed to simulate restraint during welding
— method and position/point for monitoring of electrical parameters shall be as for production welding
— with increasing pressure the voltage gradient will increase. Accordingly may small changes in arc length
and or operating depth result in considerable changes in the monitored values of arc voltage. For
calculations of the heat input, the arc voltage shall be recorded at the position/point of welding during
qualification of the welding procedure and the difference between these values and remote monitored
values recorded for use during production welding.
Repair welding procedures
C.9.8.3 Qualification welding shall be performed in compliance with the requirements given in [C.5.2].
C.9.9 Qualification of welding procedures for hyperbaric dry welding
C.9.9.1 The requirements given in [C.5.3] shall apply.
C.9.10 Examination and testing
C.9.10.1 Examination and testing shall be in accordance with [C.6.1], [C.6.2] and [C.6.3].
C.9.11 Production welding requirements for dry hyperbaric welding
C.9.11.1 In addition to the applicable requirements given in [C.7], [C.8.1] and [C.8.2], the requirements
below shall apply for dry hyperbaric production welding:
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C.9.11.2 The habitat shall be of adequate size to allow access for welding and for all necessary welding,
safety and life support equipment. Further the habitat shall be lighted and be fitted with remote cameras for
surveillance. Welding fumes shall not prevent the use of the remote cameras in the welding area.
C.9.11.3 A function test of the habitat, habitat equipment and the monitoring and communication equipment
shall be performed to a written and agreed procedure, and accepted before lowering the habitat to the
working position. The function test shall also include verification of that the welding parameters are applied
correctly on the actual equipment.
C.9.11.4 If used, shielding and/or backing gas shall be of qualified purity including moisture limit. Gas purity
and composition in all containers shall be certified and traceable to the gas storage containers. The gas purity
and moisture content shall be verified after purging the gas supply system prior to start of welding. The
moisture content of the shielding gas shall be monitored at/near the torch during welding operation.
C.9.11.5 Pup pieces shall be bevelled, checked for correct length, laminations at cut ends and the bevel
profile.
C.9.11.6 At completion of positioning of the two pipe sections to be welded, the following information, as a
minimum, shall be reported to the surface:
— pipe sections to be connected (pipe number, heat number if possible)
— approximate distance from the girth weld to the pipe extremity
— position of the longitudinal welds.
C.9.11.7 If the requirement for staggering of longitudinal welds can not be met, any reduction in the
separation of welds shall be limited to two pipe lengths.
C.9.11.8 All operations including welding shall be monitored by a video system that can be remotely
controlled from the control station and the welding area shall have continuous communication with the
control station. All relevant data shall be monitored and recorded at the surface control station under
supervision by the welding co-ordinator, including:
—
—
—
—
—
environmental conditions (humidity, temperature, atmosphere composition)
welding parameters (mechanised and automatic welding)
gas moisture content
preheat and interpass temperature
information transmitted by the welders.
C.9.11.9 The following records shall be presented as part of the documentation:
— chart recordings of welding current, arc voltage, filler wire speed, welding speed
— video recording from the weld observation cameras.
Weld repair
C.9.11.10 The applicable requirements given Table C-7 shall apply. In addition repairs exceeding 30% of
pipe D shall be performed only if agreed.
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APPENDIX D NON-DESTRUCTIVE TESTING (NDT)
D.1 General
D.1.1 Objective
D.1.1.1 This appendix specifies the requirements for methods, equipment, procedures, acceptance criteria
and the qualification and certification of personnel for visual examination and non-destructive testing (NDT)
of C-Mn steels, low alloy steels, duplex steels, other stainless steels and clad steel materials and weldments
for use in pipeline systems.
D.1.1.2 This appendix does not cover automated ultrasonic testing (AUT) of girth welds. Specific
requirements pertaining to AUT of girth welds are given in App.E.
D.1.1.3 Requirements for NDT and visual examination of other materials shall be specified and be in general
agreement with the requirements of this appendix.
D.1.2 Application
D.1.2.1 The requirements in this appendix are given in several subsections with each subsection dealing with
the non-destructive testing of specific objects.
D.1.2.2 The requirements given in [D.1] are applicable for the whole of this appendix.
D.1.2.3 The requirements given within the other subsections are applicable only to the scope of the
subsection as indicated in the title of the subsection, unless specific references to other subsections are
made.
D.1.3 Quality assurance
D.1.3.1 In addition to the general requirements to quality assurance of Sec.2, NDT contractors and
organisations shall as a minimum supplement this with the requirements given in ASTM E1212.
D.1.4 Non-destructive testing methods
D.1.4.1 Methods of NDT shall be chosen with due regard to the conditions influencing the sensitivity of the
methods. The ability to detect imperfections shall be considered for the material, joint geometry and welding
process used.
D.1.4.2 As the NDT methods differ in their limitations and/or sensitivities, combination of two or more
methods shall be considered since this is often required in order to ensure optimum probability of detection
of harmful defects.
D.1.4.3 Magnetic particle, eddy current or magnetic flux leakage testing is preferred for detection of surface
imperfections in ferromagnetic materials. For detection of surface imperfections in non-magnetic materials,
either liquid penetrant testing or eddy current testing shall be preferred.
D.1.4.4 Ultrasonic and/or radiographic testing shall be used for detection of internal imperfections. It may
be necessary to supplement ultrasonic testing by radiographic testing or vice versa, in order to enhance the
probability of detection or characterisation/sizing of the type of flaws that can be expected, as specified in
[10.5.3].
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Radiographic testing is preferred for detection of volumetric imperfections. For material thicknesses above 25
mm radiographic testing should always be supplemented by ultrasonic testing.
Ultrasonic testing shall be preferred for detection of planar imperfections: Whenever determination of the
imperfection height and depth is necessary, e.g. as a result of an ECA, automated ultrasonic testing is
required. The sizing accuracy and POD has to be documented to be adequate for use with the applicable ECA
derived acceptance criteria.
Guidance note:
The detectability of cracks with radiographic testing depends on the crack height, the presence of branching parts of the crack, the
direction if the X-ray beam to the orientation of the crack and radiographic technique parameters. Reliable detection of cracks is
therefore limited.
Lack of sidewall fusion will probably not be detected unless it is associated with volumetric imperfections or if X-ray beam is in the
direction of the side-wall.
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D.1.4.5 When manual non-destructive testing in special cases is used as a substitute for automated
ultrasonic testing for pipeline girth welds, both radiographic and ultrasonic testing of the girth weld shall be
performed.
D.1.4.6 Alternative methods or combination of methods for detection of imperfections may be used if the
methods are demonstrated as capable of detecting imperfections with an acceptable equivalence to the
preferred methods.
D.1.5 Personnel qualifications
Manual or semi-automatic NDT
D.1.5.1 Personnel performing manual or semi-automated NDT and interpretation of test results shall be
certified to Level 2 by a Certification Body or Authorised Qualifying Body in accordance with ISO 9712 or
the ASNT Central Certification Program (ACCP). Personnel qualification to an employer based qualification
scheme as SNT-TC-1A may be accepted if the employer’s written practice is reviewed and found acceptable
and the Level 3 is ASNT Level III or ACCP Professional or ISO 9712 Level III and certified in the applicable
method. Company appointed Level 3 is not accepted.
Personnel performing testing of welds with duplex, other stainless steels and nickel alloy steel weld deposits
shall have documented adequate experience or having sustained a documented dedicated training for this
type of ultrasonic testing.
Automated NDT, general
D.1.5.2 Personnel calibrating equipment and interpreting results from automated equipment for NDT shall be
certified to an appropriate level according to a certification scheme meeting the requirements of [D.1.5.1]. In
addition, they shall be able to document adequate training and experience with the equipment in question,
and shall be able to demonstrate their capabilities with regard to calibrating the equipment, performing an
operational test under production/site/field conditions, and evaluating size and location of imperfections.
Automated NDT, linepipe manufacture
D.1.5.3 Personnel operating automated equipment for NDT during manufacture of linepipe shall be certified
according to ISO 11484 or equivalent certification scheme.
Preparation of NDT procedures
D.1.5.4 Preparation of NDT procedures and execution of all NDT shall be carried out under the responsibility
of Level 3 personnel. Any tasks involving calibration of the equipment, data acquisition and interpretation of
the results, shall include personnel qualified to at least Level 2 of applicable NDT method.
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Visual examination
D.1.5.5 Personnel performing visual examination of the whole welding process shall have documented
training and qualifications according to NS 477, minimum CSWIP3.1 (Level 2) or minimum IWI-S or
equivalent certification scheme. Personnel performing visual examination of other objects shall have training
and examination according to a documented in-house standard. Personnel performing visual testing of
finished, welded joints shall be qualified according to an independent certification scheme as NS 477,
minimum CSWIP3.1 (Level 2) or minimum IWI-S or equivalent or in accordance with ISO 9712, VT level 2, or
equivalent.
Visual acuity
D.1.5.6 Personnel interpreting radiographs, performing ultrasonic testing, interpreting results of magnetic
particle and liquid penetrant testing and performing visual examination shall have passed a visual acuity test
such as required by ISO 9712 or a Jaeger J-w test at 300 mm, within the previous 12 months.
D.1.6 Timing of non-desctructive testing
D.1.6.1 Whenever possible, NDT of welds shall not be performed until 24 hours has elapsed since completion
of welding.
D.1.6.2 If welding processes ensuring a diffusible hydrogen content of maximum 5 ml/100 g of weld metal
are used, adequate handling of welding consumables is verified, shielding gas content of H2 is controlled, or
measures (such as post heating of the weldment) are taken to reduce the contents of hydrogen, the time in
[D.1.6.1] above can be reduced, subject to agreement.
D.1.6.3 NDT of pipeline installation girth welds and longitudinal welds in linepipe can be performed as soon
as the welds have cooled sufficiently to allow the NDT to be performed.
D.2 Manual non-destructive testing and visual examination of welds
D.2.1 General
D.2.1.1 Non-destructive testing shall be performed in accordance with written procedures that, as a
minimum, give information on the following aspects:
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
applicable standards or recommended practices
welding method (when relevant)
joint geometries and dimensions
material(s)
method
technique
equipment main and auxiliary
consumables (including brand name)
sensitivity
calibration techniques and calibration references
testing parameters and variables
assessment of imperfections
reporting and documentation of results
reference to applicable welding procedure(s)
example of reporting forms
acceptance criteria.
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— testing parameters and variables.
D.2.1.2 If alternative methods or combinations of methods are used for detection of imperfections, the
procedures shall be prepared in accordance with an agreed standard or recommended practice. The need for
procedure qualification shall be considered in each case based on the method's sensitivity in detecting and
characterising imperfections and the size and type of defects to be detected.
D.2.1.3 All non-destructive testing procedures shall be signed by the responsible Level III person.
Reporting
D.2.1.4 All NDT shall be documented such that the tested areas may be easily identified and such that the
performed testing can be duplicated. The reports shall identify the defects present in the weld area and state
if the weld satisfies the acceptance criteria or not.
D.2.1.5 The report shall include the reporting requirements of the applicable standard, NDT procedure and
acceptance criteria.
At least the following minimum information shall be given:
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
name of the company and operator carrying out the testing including certification level of the operator
object and drawing references
place and date of testing
material type and dimensions
post weld heat treatment, if required
location of examined areas, type of joint
welding process used
surface conditions
temperature of the object
number of repairs if specific area repaired twice or more
contract requirements e.g. order no., specifications, special agreements etc.
example of reporting forms
sketch showing location and information regarding detected defects
extent of testing
test equipment used
description of the parameters used for each method
description and location of all recordable indications
testing results with reference to acceptance level
other information related to the specific method may be listed under each method.
D.2.2 Radiographic testing of welds
D.2.2.1 Radiographic testing shall be performed in compliance with ISO 17636-1 and as required below.
Digital radiographic testing shall be in accordance with ISO 17636-2 and as required below, and if relevant:
EN 13068 and EN14784. Digital radiographic testing of weld seam of welded steel tubes shall be according to
ISO 10893-7.
D.2.2.2 Radiographic testing shall be performed by use of X-ray according to accepted procedures. Use of
radiographic isotopes (gamma rays) may be required in some situations and is subject to agreement in each
case.
Radiographic testing procedures
D.2.2.3 Radiographic testing procedures shall be according to [D.2.1.1] through [D.2.1.3] and include:
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—
—
—
—
—
—
—
—
—
—
—
—
—
—
radiographic technique class
radiation source
technique
geometric relationships
film type
intensifying screens
exposure conditions
processing
image quality indicator sensitivities in percent of the wall thickness, based on source and film side
indicators respectively
backscatter detection method
density
film side image quality indicator (IQI) identification method
film coverage
weld identification system.
Classification of radiographic techniques
D.2.2.4 The radiographic techniques used shall be according to class B and the requirements below.
D.2.2.5 Class B techniques should also be used when using gamma ray sources.
If, for technical reasons, it is not possible to meet one of the conditions specified for class B, the note to
Chapter 5 of ISO 17636-1 shall apply.
Image quality indicators
D.2.2.6 Image quality indicators (IQIs) shall meet the requirements given in ISO 19232.
The wire material shall have a coefficient of absorption as close as possible to the material tested. If the
absorption coefficients of the IQI material and the material tested differ by more than 20%, an experimental
evaluation according to ISO 19232-4 shall be performed to establish the acceptable image quality values, or
IQIs according to ASTM E 747 having material characteristics similar to the item to be tested can be used.
For the latter option, absorption coefficient difference between IQI and material has to be less than 20% and
it shall be documented that the IQI ensures at least the same sensitivity as with ISO 19232.
Sensitivity
D.2.2.7 The sensitivities obtained during production radiography shall at least meet the requirements of ISO
17636-1, Annex A except for double wall techniques with the IQI on the film side. For this technique, the
sensitivity of the film side IQI from the procedure qualification shall be used as acceptance criterion for film
sensitivity.
Radiographic procedure qualification
D.2.2.8 Each radiographic procedure and the consumables used shall be qualified by making radiographic
exposures of a welded joint or base material with the same or typical configuration and dimensions, and of
material equivalent to that which shall be used in production radiography.
For procedures using source side IQIs, the sensitivity shall meet the applicable criterion in ISO 17636-1,
Annex A and the average density at the sound weld metal image shall be minimum 2.0. The maximum
density allowed shall be according to the capabilities of the available viewing equipment, but not more than
4.0.
D.2.2.9 For procedures using film side IQIs, the IQIs shall for radiographic procedure qualification purposes
be placed on both the film side and the source side.
The sensitivity of the source and film side IQIs shall both satisfy the applicable criteria in ISO 17636-1,
Annex A and the density shall meet the requirements of [D.2.2.8].
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If the sensitivity of the film side IQI is better than required by the applicable criterion in ISO 17636-1,
Annex A the film side sensitivity obtained during procedure qualification shall be recorded and be acceptance
criterion for the sensitivity of the film side IQI during production radiography.
Processing and storage
D.2.2.10 Processing of radiographs shall conform to ISO 17636-1. Storage shall be such that the
radiographs maintain their quality for a minimum of 5 years without deterioration. Thiosulphate tests shall be
performed at regular intervals.
If radiograph storage time in excess of 5 years is required, the radiographs should be digitised using methods
giving adequate resolution and stored in electronic media in an agreed manner.
Reporting
D.2.2.11 Reports shall be in accordance with [D.2.1.4] and [D.2.1.5]. In addition to the items listed in ISO
17636-1 the following shall be included in the radiographic testing report:
— radiographic procedure reference
— geometric unsharpness, at minimum all information required for calculation of it.
Specific requirements to radiography of installation girth welds
D.2.2.12 For radiography the following additional requirements shall apply for installation girth welds:
— Panoramic (single wall single image) exposures shall be used whenever possible
— Fluormetallic screens may be used in combination with X-ray based on a satisfactory procedure
qualification test where all requirements to sensitivity are met. Films used with fluormetallic screens shall
be designed for use with this screen type
— For pipe with internal diameter < 250 mm gamma ray and panoramic (single wall single image)
exposures may be used. The gamma ray source should be Se 75 used with a film system class better
than C4 according to ISO 17636, Table 3. Other types of radiation sources may be used for small wall
thicknesses in combination with other film types. The use of gamma ray sources shall always be based on
a satisfactory procedure qualification test where all requirements to sensitivity are met
— Where no internal access is possible, a double wall technique shall be applied
— For the double wall double image technique x-ray shall be used. Fluormetallic screens may be used based
on a satisfactory procedure qualification test where all requirements to sensitivity are met. Films for use
with fluormetallic screens shall be suitable for this screen type
— For the double wall single image technique both X-ray and gamma ray may be used. The choice of
radiation source, film and screen types shall be based on a satisfactory procedure qualification test where
all requirements to sensitivity are met.
D.2.3 Manual ultrasonic testing of welds in C-Mn/low alloy steel with C-Mn/
low alloy steel weld deposits
D.2.3.1 Ultrasonic testing shall be performed in compliance with ISO 17640 and as required below.
D.2.3.2 Ultrasonic testing shall be performed according to accepted procedures and DNVGL-CG-0051.
Ultrasonic testing procedures
D.2.3.3 Ultrasonic testing procedures shall be according to [D.2.1.1] through [D.2.1.5], and include:
—
—
—
—
—
type of instrument
type and dimensions of probes
range of probe frequencies
description of reference block
calibration details, range and sensitivity
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—
—
—
—
surface requirements, including maximum temperature
type of coupling medium
scanning techniques supplemented with sketches, showing the probes used and area covered
recording details.
D.2.3.4 Typical applications, which require specific UT procedures, are:
—
—
—
—
—
—
—
ultrasonic examination of welds in austenitic stainless steel
ferritic-austenitic (duplex) stainless steels
detection of corrosion and/or thickness measurement
phased array ultrasonic testing
automated ultrasonic testing, AUT
for special application during in-service inspection
estimation of defect size (height) using conventional beam spread diagram (20 dB drop), time-of-flightdiffraction (TOFD) technique or the back diffraction technique
— testing of objects with temperature outside the range 0°C to 40°C.
The ultrasonic testing procedure shall be submitted for acceptance.
D.2.3.5 No special procedure qualification test should be required when manual methods are used.
Ultrasonic testing techniques
D.2.3.6 Ultrasonic testing techniques shall be in accordance with ISO 17640, and the requirements below.
Guidance note:
Manual or semi- automated ultrasonic phased array systems may be used provided it is qualified that such systems will give the
same sensitivity, resolution and detection ability as conventional ultrasonic testing performed according to the requirements given
in [D.2.3] and that specific ultrasonic testing procedures are developed and accepted.
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Manual ultrasonic testing equipment
D.2.3.7 Manual ultrasonic testing equipment shall:
—
—
—
—
be applicable for the pulse echo technique and for the double probe technique
cover as a minimum the frequency range from 1 to 6 MHz
have a calibrated gain regulator with maximum 2 dB per step over a range of at least 60 dB
have a flat screen accessible from the front for direct plotting of reference curves or be equipped with
digital DAC- display presentation of user-defined curves
— allow echoes with amplitudes of 5% of full screen height to be clearly detectable under test conditions.
D.2.3.8 Calibration of ultrasonic equipment shall be undertaken yearly according to procedures established
according to a recognised standard or recommended practice, e.g. EN 12668-1-2-3 or ASME V. Verification
of Screen Height Linearity and Amplitude Linearity shall be performed at the beginning of each period of
extended use (or every 3 months, whichever is less). Calibration records shall be made available upon
request.
Semi-automated ultrasonic testing equipment
D.2.3.9 Semi-automated ultrasonic testing equipment shall follow the examination requirements of ASME V,
Article 4, Mandatory Appendix VI.
Time-of-flight-diffraction
D.2.3.10 Time-of-flight diffraction inspection shall be according to ISO 10863, testing level C.
Phased array ultrasonic testing
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D.2.3.11 Phased array based inspection techniques shall be according to ISO 13588, testing level C, as far
as applicable for manual UT.
Probes
D.2.3.12 Probes used for testing of welds with C-Mn steel weld deposits shall be characterised as required by
ISO 10375 and ISO 12715.
Angle beam shear-wave probes shall be available in angles allowing effective testing of the actual weld
connections. For testing of girth welds or welds in plate probe angles of 45°, 60° and 70° will normally be
sufficient but additional probes of 35° and 55° are recommended. Other applications may require probes
covering the range of 35° to 80° to allow effective testing.
Straight beam probes shall be single or twin crystal probes. Twin crystal probes shall be used when testing is
performed on material with nominal thickness t < 60 mm. Single crystal probes may be used when testing is
performed on material with nominal thickness t ≥ 60 mm.
Probes shall, if necessary, be suitable for use on hot surfaces (100 to 150°C).
D.2.3.13 Additional probes for time-of-flight diffraction (ToFD) and double probe techniques are
recommended.
D.2.3.14 Probe frequencies shall be selected according to ISO 17640.
Guidance note:
The nominal angle of probes used are normally valid for C-Mn steels with compression wave velocity of approximately 5900 m/s
o
and shear wave velocity of approximately 3200 m/s at 20 C.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
Coupling medium
D.2.3.15 The same coupling medium as used for calibration and setting of gains and amplification shall be
used during testing.
Calibration of range scale and angle determination
D.2.3.16 The IIW or ISO calibration blocks (K1 – K2) according to ISO 2400 or ISO 7963 respectively, shall
be used for calibration of range scale and for angle determination. These calibration blocks shall, as near as
practicable, have the same acoustic properties as the material to be tested.
Reference blocks for setting of reference levels
D.2.3.17 For testing of welds reference blocks shall be used for gain calibration and construction of the
reference curves. The reference block shall be manufactured from the actual material to be examined.
Reference blocks manufactured from other materials may be acceptable provided that the material is
documented to have acoustic properties similar to the actual material to be examined or, alternatively,
a transfer correction to accommodate for attenuation differences shall be performed, considering the
requirements in [D.2.3.19] and [D.2.3.25]. The reference block shall have length and width dimensions
suitable for the sound beam path for all probe types and the material dimension(s) to be tested.
For testing of welds in plate and similar geometries a reference block with side drilled holes shall be used.
The thickness of the reference block, diameter and position of the drilled holes shall be as shown in Figure
D-1 and Table D-1.
For testing of welds in pipe when testing can be performed from one side only, and the DAC reference signals
can only be obtained from the side where the inspection shall be performed, i.e. the D side, the reference
blocks shall have side drilled holes at T/4, T/2 and 3/4T.
When ultrasonic testing is to be performed on TMCP steel reference blocks shall, when required, be produced
perpendicular to and/or parallel to the direction of rolling. The rolling direction shall be clearly identified.
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D.2.3.18 For testing of longitudinal welds in pipe and similar geometries the reference block shall in addition
to the features required above, have a curvature equal to the pipe to be tested.
Figure D-1 Reference block dimensions
Table D-1 Reference block dimensions
Material thickness (t)
Thickness
of reference
block (T)
Diameter of
side drilled
hole (mm)
T < 15 mm
15 mm or t
2.4 ± 0.2
15 mm ≤ t < 35 mm
20 mm or t
35 mm ≤ t < 50 mm
38 mm or t
50 mm ≤ t < 100 mm
75 mm or t
100 mm ≤ t < 150 mm
125 mm or t
Position of side
drilled hole
3.0 ± 0.2
3.0 ± 0.2
T/2
T/4
Note
Additional holes are required for
testing of pipe when the DAC can
be constructed from one side only.
Additional holes are generally
allowed and recommended
D.2.3.19 All reference blocks shall be marked with an identification that relates to the specific application of
each block
Gain calibration
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D.2.3.20 The DAC- curve shall be constructed using reference blocks with side-drilled holes as described in
[D.2.3.16].
D.2.3.21 Reference blocks not made from the actual material to be tested shall be checked for variation in
acoustic properties between the reference block and the actual material. The variation can be checked by
calibrating the range scale on the ISO 2400 block with a normal probe and subsequently measure a known
material thickness with this calibration.
D.2.3.22 Whenever ultrasonic testing of welds in TMCP steel is performed, the difference in attenuation
between transverse and longitudinal rolling direction shall be checked when the scanning direction changes
between transverse and parallel to the rolling direction. This requires DAC constructed by use of calibration
blocks taken from transverse and parallel to the rolling direction. Difference in gain setting shall be noted and
taken into consideration when evaluation of indications is performed.
D.2.3.23 When testing is carried out of welds in TMCP steel the actual beam angle shall be determined. The
angle can be calculated using trigonometric functions as long as the distance and depth to the reflectors in
the TMCP steel reference block is known. Alternatively the method described in [E.11] can be used.
Construction of the reference curves (DAC)
D.2.3.24 The echo reflected from the drilled hole in the calibration block shall be maximised and the
amplitude set at 80% of full screen height.
D.2.3.25 The first point of DAC shall be selected such that the distance in sound path from the probe index
to the drilled hole is not less than 0.6 N where N is the near field length of the relevant probe. The DAC shall
be constructed by obtaining at least 3 points on the curve. The gain setting shall be recorded and comprises
the primary gain.
The recorded gain following all corrections for surface condition and attenuation is the corrected primary
gain. Alternatively, a Time Corrected Gain calibration can be used if the ultrasonic apparatus is fitted with a
time corrected gain (TCG) correction. The echo amplitude reflected from the drilled hole in the calibration can
be adjusted to 80% of full screen height over the whole range in question. DAC will thus be a horizontal line.
Periodical checks of equipment, re-calibration and re-examination
D.2.3.26 At approximately four-hourly intervals and at the end of testing, the range scale, probe angle and
primary gain shall be checked and confirmed.
If deviation is found to be larger than 2% of range scale, or 4 dB of primary gain setting or 2° of nominal
probe angle, the equipment shall be re-calibrated and the testing carried out with the equipment over the
previous period shall be repeated.
Re-calibration shall be performed whenever the equipment has been out function for any reason including onoff and whenever there is any doubt concerning proper function of the equipment.
Contact surface
D.2.3.27 For ultrasonic testing the contact surface shall be clean and smooth, i.e. free from dirt, scale,
rust, welding spatter, etc. which may influence the result of the testing. Correction for differences in surface
conditions and attenuation between the reference block and the actual work piece shall be performed
according to the following:
—if the difference is less than 2 dB, correction is not required
—if the difference is greater than 2 dB but smaller than 6 dB for flat surfaces and 12 dB for curved surfaces,
it shall be compensated for
— if transfer loss exceeds the limits above, the reason shall be determined and further preparation of the
scanning surfaces shall be carried out.
Transfer correction
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D.2.3.28 Transfer correction from reference block to the weld piece shall be evaluated on a portion of the
item to be tested without any discontinuity.
Transfer correction shall be performed using two of the same angle beam probes on the calibration block
that shall be used to construct a specific transfer DAC curve with 2 points, i.e. full skip or more, on the item
to be examined. One of the probes shall work as transmitter while the other as receiver. For the item to
be examined, the orientation of the probe pair upon transfer correction shall be the same as the scanning
direction. The difference in dB required to achieve an 80% FSH level on the calibration block and item to be
examined for the same pair of angle beam probes shall be recorded.
In case of difference in thickness between the reference block and the item to be inspected a specific transfer
correction to account for the different sound path shall be performed.
Testing levels
D.2.3.29 The testing level shall be in accordance with ISO 17640, chapter 11, testing level B and the
requirements below.
Probe selection
D.2.3.30 In addition to straight beam probe minimum number of angle probes to be applied shall be in
accordance with ISO 17640, see the guidance given in Table D-2. It is emphasised that this table is for
guidance and that the actual choice of angle probes shall be made carefully and depending on material
thickness, weld bevel and type of defects likely to occur with the welding method used.
Table D-2 Parent material thickness and related Probe angle
Parent material thickness, T
Probe angle
<15 mm
60° and 70°
15 to 40 mm
45°, 60° and 70°
T > 40 mm
45°, 60° and 70° (70° when ½ V or K groove)
D.2.3.31 The choice of optimum probe angle for initial full scanning of the weld shall be chosen such that
incident angle of the sound beam centre is perpendicular to the side of the weld bevel. If this angle does not
comply with any standard probe angle, the nearest larger probe angle shall be selected.
D.2.3.32 These additional probes shall have a larger and smaller angle than the probe used for initial
o
scanning. The differences in angle shall be more than 10 .
D.2.3.33 If only one additional probe can be used the angle for this probe should be:
— ≥ 10° different
— Larger than the initial probe if the sound beam centre of the initial probe is perpendicular to the side of
the weld bevel
— Smaller than the initial probe if the nearest larger probe angle was selected for the initial probe
Testing of welds
D.2.3.34 When scanning, the gain shall be increased by a minimum of 6 dB above the corrected primary
gain. Testing of welds shall be performed in accordance with ISO 17640.
D.2.3.35 The scanning zone for angle probes in the base material shall be examined with straight beam
(normal) probes for features that might influence the angle beam testing. The scanning zone is defined as
1.5 × full skip distance. Features interfering with the scanning shall be reported.
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D.2.3.36 The welds shall whenever feasible be tested from both sides on the same surface and include
scanning for both transverse and longitudinal indications. For T-joints and plate thickness above 70 mm,
scanning from both surfaces and all accessible sides shall be performed.
Evaluation of indications
D.2.3.37 For evaluation of indications the gain shall be reduced by the increased dB level used during
scanning.
D.2.3.38 All indications equal to or exceeding 20% of the reference curve (evaluation level) shall be
evaluated. The indications shall be investigated by maximising the echoes by rotating the probes and by
using different angle probes with DAC established according to [D.2.3.23] and [D.2.3.24].
D.2.3.39 The length of an indication shall be determined by the 6 dB drop method.
D.2.3.40 The final evaluation against the acceptance criteria shall be based on the echo amplitude and
length measured with the probe angle giving the maximum response.
Reporting
D.2.3.41 Reports shall be in accordance with [D.2.1.4] and [D.2.1.5]. In addition to the items listed in ISO
17640 the following shall be included in the ultrasonic testing report:
— identification of the ultrasonic testing procedure used
— the length of acceptable indications with amplitude exceeding 50% of the reference curve.
D.2.4 Manual ultrasonic testing of welds with corrosion resistance alloy
(duplex, other stainless steels and nickel alloy steel) weld deposits
General
D.2.4.1 Ultrasonic testing shall be performed in compliance with [D.2.3], ISO 22825, ISO 17640, and as
required below.
D.2.4.2 Weld deposits in duplex, austenitic stainless steels and nickel alloys have a coarse grain structure
with variations in grain size and structure resulting in unpredictable fluctuations in attenuation and ultrasonic
beam patterns. Duplex and austenitic stainless steel base materials, in particular forgings and castings, will
have the same characteristics.
Ultrasonic testing of welds with CRA (duplex, other stainless steels and nickel alloy steel) weld deposits will
in order to achieve an adequate detection of imperfections require that special calibration blocks and probes
are used for testing of welds in these materials. Angle probes generating compression waves shall be used,
but alternative waveforms may be employed providing procedure techniques have been demonstrated and
provide equivalent detection capabilities.
Ultrasonic testing procedures
D.2.4.3 Specific ultrasonic testing procedures shall be developed for this testing in compliance with this
chapter and including the information required in [D.2.1.1] and [D.2.3.3]. The procedure shall be submitted
for acceptance prior to start of testing.
Personnel qualifications
D.2.4.4 In addition to the requirements given in [D.1.5] personnel performing testing of welds with duplex,
other stainless steels and nickel alloy steel weld deposits shall be qualified for or document adequate
experience and training for this type of ultrasonic testing.
Manual ultrasonic testing equipment
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D.2.4.5 The requirements given in [D.2.3.7] and [D.2.3.8] shall apply
Probes
D.2.4.6 In addition to the requirements given in [D.2.3.9], [D.2.3.10], [D.2.3.11] and [D.2.3.12], the
requirements below shall apply.
D.2.4.7 Probes used for testing should be straight beam transducers and twin crystal (transmitter/receiver)
compression wave probes of 45°, 60° and 70°. In addition shear-wave angle probes shall be used, if found
suitable through demonstration of adequate signal to noise ratio for inspection at the area of interest.
D.2.4.8 In general, a combination of shear and compression wave angle probes should be used since the
detection of open to surface imperfections on the opposite surface of the scanning surface, e.g. incomplete
penetration or lack of fusion, may increase by using shear wave probes. It shall, however, be verified by
using calibration blocks with actual weld connections, see [D.2.4.18] below, that angle shear wave probes are
suitable.
D.2.4.9 Creep wave probes shall be used for inspection of surface area, unless testing can be performed
from opposite sides.
Reference blocks for setting of reference levels
D.2.4.10 In addition to the reference blocks as described in [D.2.3.17], [D.2.3.18] and [D.2.3.19], reference
blocks prepared from the actual test material and containing welds produced in accordance with the actual
WPS shall be used for establishing the DAC. These reference blocks shall have the weld ground flush and the
surface condition of the calibration blocks shall be typical of the condition of the parent material(s) in the
scanning areas.
D.2.4.11 The reference block for construction of DAC shall have side drilled holes with dimensions according
to Table D-3 and located as shown in Figure D-2. The length and width of the reference blocks shall be
sufficient to allow the scanning needed for construction of the DAC.
Figure D-2 Reference block for construction of DAC, dimensions
Notes:
1)
2)
3)
Side drilled holes shall be drilled in the fusion line and in the base material. Holes in the base material
shall be in the same relative position as the fusion line holes.
Holes shall be drilled in both fusion lines and base material when two dissimilar materials are welded to
each other.
For double sided welds, side drilled holes shall be located in the fusion line for the full thickness of the
weld.
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4)
For hole positions when t ≥ 50 mm, see Table D-3.
Table D-3 Reference block dimensions
Thickness of
reference block (T) in
Diameter of side
drilled hole in mm
T < 15 mm
15 mm or t
2.4 ± 0.2
15 mm ≤ t < 35 mm
25 mm or t
35 mm ≤ t < 50 mm
45 mm or t
50 mm ≤ t < 100 mm
75 mm or t
Material thickness (t)
100 mm ≤ t < 150
mm
125 mm or t
3.0 ± 0.2
3.0 ± 0.2
Position of side drilled holes
T/4, T/2 and T3/4
The distance between the two
outer holes and the nearest
surface shall not exceed 12 mm.
D.2.4.12 The reference block for sensitivity setting for creep wave probes shall have 0.5, 1.0 and 2.0 mm
spark eroded notches with a minimum length of 20 mm as shown in Figure D-3. The location of notches shall
allow setting against each individual notch.
Construction of the reference curves (DAC) for angle compression wave probes
Figure D-3 Reference block for sensitivity setting for creep wave probes, dimensions
D.2.4.13 Angle compression wave probes shall and can only be used for scanning without skipping. The
construction of the DAC curves using angle compression wave probe shall be performed according to:
— when the ultrasonic beam is passing through the parent metal only
— when ultrasonic beam is passing through the weld metal.
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D.2.4.14 When the ultrasonic beam is passing through the parent metal only the DAC curve shall be
constructed from the drilled holes in the parent material of the calibration blocks, see Figure D-2. Next, a
maximum response shall be obtained from the holes in the weld fusion line and if necessary, the gain setting
shall be adjusted such that this response reach the DAC constructed against drilled holes in the parent
material. This shall be the primary gain to be used when locating indications on the fusion line on the side of
the weld nearest to the scanning side.
D.2.4.15 When the ultrasonic beam is passing through the weld metal, the DAC curve shall be constructed
from the holes drilled in the fusion line on the side of the weld opposite to the scanning side. See Figure D-2.
This DAC shall be verified against the holes drilled in the base material. Any variations shall be noted so that
echoes reflected from indications within the weld zone can be evaluated for amplitude response.
Transfer correction
D.2.4.16 Since compression wave angle probes can only be used without skipping, transfer correction
can not be performed. The calibration blocks shall therefore have a surface finish similar to the production
material.
Sensitivity setting for creep wave probes
D.2.4.17 The reference block shown in Figure D-3 shall be used for sensitivity setting for creep wave probes.
The echo response from the 1.0 mm notch shall be set to 75% of FSH.
Shear wave angle probes
D.2.4.18 If shear wave angle probes are considered for skipped scanning or in the root area of single sided
welds, it shall be verified on the reference blocks with welds, see Figure D-2, if it is possible to obtain a DAC
with a shear wave angle probe that is comparable to the DAC obtained with an angle compression wave
probe.
Preparation of weld and scanning surfaces for testing
D.2.4.19 Prior to starting the testing the external weld cap shall be ground flush with the adjacent base
material. The surface finish of the weld and the scanning areas shall be as that on the reference blocks to be
used or better.
Probe selection
D.2.4.20 In addition to the straight beam probe minimum two angle probes shall be used for the testing, see
the guidance given in Table D-2 and [D.2.3.20] through [D.2.3.34].
D.2.4.21 Where the weld configuration or adjacent parts of the object are such that scanning from both
sides is not possible, two additional probes shall always be used.
D.2.5 Manual magnetic particle testing of welds
General
D.2.5.1 Magnetic particle testing shall be performed in compliance with ISO 17638 and as required below.
D.2.5.2 Magnetic particle testing shall be performed according to accepted procedures.
Magnetic particle testing procedures
D.2.5.3 Magnetic particle testing procedures shall be according to [D.2.1.1] through [D.2.1.3] and include:
— type of magnetisation
— type of equipment
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—
—
—
—
—
—
surface preparation
wet or dry method
make and type of magnetic particles and contrast paint
magnetising current (for prod magnetising, the prod type and spacing shall be stated)
demagnetisation
description of the testing technique.
D.2.5.4 No special procedure qualification tests is required.
Magnetising equipment
D.2.5.5 The equipment shall be tested at maximum 6 months interval to verify that the required field
strength is established at the maximum pole distance/prod spacing to be used. The results shall be recorded.
D.2.5.6 Prods shall be soft tipped with lead or similar. Sparks between the prods and the material tested
shall be avoided.
D.2.5.7 Electromagnetic AC yokes shall develop a minimum lifting force of 4.5 kg at maximum pole distance
on a block with equivalent magnetic properties as the object to be tested. The lifting force shall be checked
prior to start of any testing and at regular intervals during testing.
D.2.5.8 Use of permanent magnets and DC yokes may only be used for specific applications if required by
national regulations and subject to agreement.
Application techniques
D.2.5.9 Magnetic particle testing shall not be performed on parts with surface temperatures exceeding
300°C. Between 60°C and 300°C, only dry magnetic particle testing shall be used.
Detection media
D.2.5.10 For both wet or dry particles, they shall provide adequate contrast with the background or the
surface being tested.
Viewing conditions
D.2.5.11 Testing with fluorescent magnetic particles shall be conducted in a darkened area with maximum
20 lux background light, using filtered ultraviolet light with wave lengths in the range of 3200 to 3900 Å.
2
The minimum UV light intensity shall be 1000 μW/cm . Operators/interpreters shall allow sufficient time for
eyesight to adjust to the dark surroundings. Interpreters shall not wear photo-chromatic viewing aids.
For color contrast technique, the minimum viewing conditions shall be 1000 lx white light at the area of
interest.
Reporting
D.2.5.12 Reports shall be in accordance with [D.2.1.4] and [D.2.1.5]. In addition to the items listed in ISO
17638 the following shall be included in the testing report:
— Identification of the testing procedure used.
D.2.6 Manual liquid penetrant testing of welds
General
D.2.6.1 Liquid penetrant testing shall be performed in compliance with ISO 3452 and as required below
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D.2.6.2 Liquid penetrant testing should only be used on non-ferromagnetic materials or materials with great
variation in magnetic permeability.
D.2.6.3 Liquid penetrant testing shall be performed according to accepted procedures. Viewing conditions
shall be minimum 1000 lx at the area of interest.
Procedures
D.2.6.4 Liquid penetrant testing procedures shall be according to [D.2.1.1] through [D.2.1.3] and include:
—
—
—
—
surface preparation
make and type of penetrant, remover, emulsifier and developer
details of pre-testing cleaning and drying, including materials used and time allowed for drying
details of penetrant application: the time the penetrant remains on the surface, the temperature of the
surface and penetrant during the testing (if not within the 15°C to 35°C range)
— details of developer application, and developing time before evaluation
— method for post-test cleaning.
Application techniques
D.2.6.5 The penetration and developing times shall be long enough to allow effective detection of the
smallest indications allowed. The penetration time shall comply with the manufacturers recommendation,
minimum 15 minutes. Development time should be at least equal to the penetration time. The inspection
area shall be monitored during developing time. Demonstration of adequate detection shall be performed for
short penetration times.
D.2.6.6 When the temperature of the surface and the penetrant is within the range 10°C to 50°C, no special
procedure qualification tests should be required.
Outside the temperature range 10°C to 50°C, the procedure shall be qualified and a suitable comparator
block shall be used to compare indications from surface defects tested within and outside the range during
the procedure qualification.
Reporting
D.2.6.7 Reports shall be in accordance with [D.2.1.4] and [D.2.1.5].
D.2.7 Manual eddy current testing of welds
General
D.2.7.1 Eddy current testing shall be performed in compliance with ISO 17643. The limitations given in ISO
17643, paragraph 6.3, notes 1 and 2 shall apply.
D.2.7.2 Eddy current testing shall be performed according to accepted procedures.
Procedure
D.2.7.3 Eddy current testing procedures shall contain the information in [D.2.1.1] and:
—
—
—
—
—
—
—
type of instrument
type of probe
frequency setting
calibration blocks and calibration details
surface condition requirements
scanning details
recording details.
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Equipment
D.2.7.4 Eddy current equipment, including probes and cables, shall be calibrated at maximum 6 months
intervals and shall have calibration certification pertaining to the characteristics of the equipment.
D.2.7.5 Functional checks of the eddy current equipment shall be carried out whenever it has been out of
function for any reason including on/off, and whenever there is any doubt concerning proper functioning of
the equipment.
D.2.7.6 All calibration blocks shall be marked with an identification that relates to the specific application of
each block.
Surface conditions
D.2.7.7 Excess weld spatter, scale, rust and loose paint shall be removed before the inspection.
Application techniques
D.2.7.8 ISO 17643 shall apply.
Reporting
D.2.7.9 Reports shall be in accordance with [D.2.1.4] and [D.2.1.5]. In addition to the items listed in ISO
17643 the following shall be included in the testing report:
— Identification of the testing procedure used.
D.2.8 Visual examination of welds
General
D.2.8.1 Visual examination of welds shall be performed in accordance with ISO 17637 and accepted
procedures.
D.2.8.2 Reports shall be in accordance with ISO 17637. In addition to the items listed in ISO 17637 the
following shall be included in the testing report:
— Identification of the testing procedure used.
D.2.9 Acceptance criteria for manual non-destructive testing of welds not
considered to be fatigue sensitive and with εl,nom < 0.4%
General
D.2.9.1 The acceptance criteria given in Table D-4, Table D-5, Table D-6 and Table D-7 are applicable for
non-destructive testing of welds exposed to nominal strains < 0.4%.
D.2.9.2 The acceptance criteria use the term defect to define an imperfection/indication that has exceeded
given dimensions and thus is deemed unacceptable.
D.2.9.3 The acceptance criteria given in Table D-5 assume that multi-pass welds are used and that the
height of defects will not exceed 0.25 t or the height of a welding pass. The height of the welding pass shall
be assumed not to be more than 3 mm.
Pipeline girth welds
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D.2.9.4 The acceptance criteria given in Table D-4, Table D-5 and Table D-6 are generally applicable for
manual non-destructive testing of pipeline girth welds exposed to total nominal strains < 0.4%.
D.2.9.5 Acceptance criteria applicable for automated ultrasonic testing (AUT) of pipeline girth welds exposed
to total nominal strains < 0.4% are given in Table E-1 and Table E-2.
D.2.9.6 If the allowable defect sizes are established by an ECA for pipeline girth welds exposed to total
nominal strains ≥ 0.4%, the provisions according to [D.2.10] shall apply.
Welds in pipeline components
D.2.9.7 The acceptance criteria given in Table D-4, Table D-5 and Table D-6 are generally applicable for
manual non-destructive testing of welds in pipeline components. For girth welds connecting a component
to the pipeline or for pup-pieces welded to the component, the acceptance criteria for pipeline girth welds
shall apply, unless other acceptance criteria are given in the design, manufacture and testing data for the
component.
D.2.9.8 For welds exposed to total nominal strains ≥ 0.4%, the allowable defect sizes shall be established by
an ECA and the provisions according to [D.2.10] shall apply.
D.2.9.9 Automated NDT-procedures to be used with the acceptance criteria provided in Table D-4, Table D-5,
Table D-6 and Table D-7 shall be qualified in accordance with [D.6] in order to document the function of the
equipment. It should be noted that the acceptance criteria in this section in principle assumes manual NDT in
accordance with the respective requirements in this section. The qualification shall therefore document that
the required sensitivity for manual techniques, in addition to inspection coverage of the areas of interest are
maintained for the automated procedure.
D.2.10 ECA based non-destructive testing acceptance criteria for pipeline
girth welds
General
D.2.10.1 Acceptance criteria for pipeline girth welds can be based on an Engineering Critical Assessment
(ECA).
D.2.10.2 Whenever acceptance criteria for NDT are established by an ECA, the ECA shall be performed in
accordance with the requirements given in [5.4.8].
D.2.10.3 If acceptance criteria for weld defects are based on an ECA and hence involves sizing of indication
height and lengths, manual ultrasonic testing or automated ultrasonic testing shall be performed.
D.2.10.4 Sizing of indication height and length by manual or automated ultrasonic testing will have inherent
inaccuracies. The allowable defect sizes derived from an ECA shall accordingly be corrected for the ultrasonic
testing uncertainty (sizing error) as follows:
— If the ECA gives the allowable defect size the sizing error shall be subtracted from the calculated allowable
defect height and length to establish the acceptance criteria for non-destructive testing.
— If the ECA gives the material properties and stresses/strains allowed to tolerate a given defect size the
sizing error shall be added to the defect height and length used as input into the ECA to establish the
acceptance criteria for non-destructive testing.
D.2.10.5 If an embedded defect is located close to a surface, such that the ligament height is less than half
the defect height, the ligament height between the defect and the surface shall be included in the defect
height.
Automated ultrasonic testing uncertainty data
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Page 410
D.2.10.6 If automated ultrasonic testing (AUT) is used for testing of pipeline girth welds, the uncertainty
data used shall be obtained from the qualification testing of the automated ultrasonic testing system required
in App.E.
Manual ultrasonic testing uncertainty data
D.2.10.7 For manual ultrasonic testing the data used for quantitative estimates of uncertainty performance
and reliability in the sizing of indication length and height, shall preferably be of the measured response
versus actual flaw size type. The estimates shall be based on published results from comprehensive studies
into the reliability of manual ultrasonic testing. It has to be documented that the critical defect sizes of the
relevant types, i.e. with regards to orientation, location and shape, can be detected with a response above
the evaluation level.
D.2.10.8 If adequate data for manual ultrasonic testing are not available, the sizing error shall not be taken
as less than 2.5 mm.
Acceptance criteria based on ECA assessment
D.2.10.9 [5.4.8] gives requirements for establishing allowable flaw sizes based on an ECA assessment.
D.2.10.10
Acceptance criteria shall be established by correcting the allowable defect sizes derived from the ECA with
the ultrasonic testing uncertainty in accordance with [D.2.10.5] or [D.2.10.6] and [D.2.10.7].
Guidance note:
Acceptance criteria based on ECA will frequently allow significantly larger indications than workmanship based acceptance criteria.
In order to maintain a high standard of welding ECA based allowable defect sizes may be used as a weld repair criterion rather
than as acceptance criterion. Criteria that are more restrictive are then used as a measure of the welding standard obtained. If
these more restrictive criteria are exceeded, it should be required that preventative or corrective actions are performed to maintain
the required welding standard.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
D.2.10.11 Alternative NDT methods to AUT in accordance with requirements in this appendix should
be regarded as acceptable for pipes with wall thickness < 8.0 mm if it is considered that efficient AUT is
prevented by the pipe configurations. The alternative NDT process shall be technically justified to provide
sufficient inspection performance for the expected imperfections for the applied welding procedure.
Alternative NDT process can be inspection by one NDT method or consist of a combination of several NDT
methods. In case radiographic testing is used, acceptance criteria shall be in accordance with Table D-5,
except that linear indications shall not be acceptable.
Guidance note:
Girth welds of small diameter and/or thin wall thickness pipes can provide limitations for efficient inspection with AUT, and UT
inspection in general. In particular, low wall thickness configurations with corresponding acceptance criteria can be challenging for
AUT with regards to accurate height sizing and depth positioning.
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Table D-4 Acceptance criteria for visual examination and surface method testing of welds 1) 2)
Visual examination
External profile (not relevant for SAWL in pipe
mills)
Welds shall have a regular finish and merge smoothly into the base
material and shall not extend beyond the original joint preparation by
more than 5 mm (8 mm for SAW welds).
Fillet welds shall be of specified dimensions and regular in form.
Cap and root reinforcement height (Longitudinal
welds)
External welds: For t < 13
mm: max. 3.0 mm.
For t ≥ 13 mm: max. 4.0
mm
Internal welds: max. 3.5
mm
The radial offset of HFW and SAWL
linepipe shall not reduce the thickness to
weld to less than tmin.
For ground areas at pipe
ends: max. 0.5 mm.
Weld flash (HFW pipe longitudinal welds only)
The external flash shall be trimmed essentially flush with the pipe
surface, with no noticeable radial step.
The internal flash shall not extend above the contour of the pipe by
more than 0.3 mm + 0.05 t). The trimming shall not reduce the wall
thickness to below tmin, and the groove resulting from the trimming
shall have a smooth transition to the base material without notches
and the depth shall be max. 0.05 t. (see ISO 3183 Table 15)
Cap and root reinforcement height(Double sided
girth welds)
Height < 0.2 t, but max. 4.0 mm
Cap reinforcement (Single sided welds)
Height < 0.2 t, but max. 4.0 mm
Root penetration (Single sided welds)
Height < 0.2 t, but max. 3.0 mm. Length of excess penetration: max
25 mm
Weld interpenetration (double-sided SAW in pipe
mills)
Option 1) minimum 1.0 mm overlap in the radial direction Option 2)
Width of overlap to be measured with a straight line perpendicular to
the radial direction. The length shall be minimum 20% of nominal WT
or 5 mm, whichever is less.
Cap concavity
Not permitted.
Root concavity
At no point shall the weld thickness be less than tmin
Offset of strip/plate edges(Longitudinal welds)
For t ≤ 15 mm max. 1.3
mm
For 15 mm < t ≤ 25 mm
max. 0.1 t
For t > 25 mm max. 2.0
mm
High/low on root side of single sided girth welds
3)
For t ≤ 13 mm max. 1.3
mm
For 13 mm < t ≤ 20 mm
max. 0.1 t
For t > 20 mm max. 2.0
mm
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Additional requirements for clad/lined
pipes: The offset shall not reduce the
thickness of the CRA below the specified
thickness.
Additional requirements for clad/lined
pipes: Max. internal high/low shall
not exceed 1.0 mm unless otherwise
qualified or if the applied high/low does
not reduce the thickness of the CRA
barrier below the specified thickness.
Page 412
Visual examination
Transverse misalignment of weld beads for double max. 3.0 mm for t ≤ 20 mm max. 4.0 mm for t > 20 mm
sided welds
Deviation of weld toe from a straight line (double- The weld toe shall run parallel to the weld longitudinal axis. The
sided SAW in pipe mills)
maximum deviation within any section of 300 mm length is 0.20 t,
but not more than 4.0 mm.
A straight line shall be oriented parallel to the longitudinal axis of the
weld (e.g. the longitudinal axis of the pipe). The distance from this
line to the weld toe shall be determined, and the difference between
the point closest and farthest from the line shall not exceed the
acceptance criteria.
(COMMENT: the intention is to determine the presence of both
waving bead/dog-leg and widening/narrowing of the weld cap both of which indicates unstable welding process. This should not
be a reason to reject the pipe, since the cap can be ground. But an
inspector shall be informed before any grinding, and measures to
improve the welding practice shall be implemented)
Undercut
Individual undercuts
Depth d
Permitted length
d > 1.0 mm
Not permitted
1.0 mm ≥ d > 0.5 mm
50 mm
0.5 mm ≥ d > 0.2 mm
100 mm
d < 0.2 mm
unlimited
Accumulated
length of
undercuts in any
300 mm length of
weld:
None
< 4 t, max. 100
mm.
unlimited
Cracks, Arc burns, Start/stop craters/ poor
restart, Surface porosity
Not permitted.
Lack of penetration/lack of fusion
Not permitted in the root of welds in CRAs and clad/lined steel.
Individual acceptable length: t, max. 25 mm. Accumulated length in
any 300 mm length of weld: t, max. 50 mm.
Systematic imperfections
Imperfections that are distributed at regular distances over the
length of the weld are not permitted even if the size of any single
imperfection meets the requirements above
Burn through
Not permitted for welds in duplex stainless steel, CRAs and clad/lined
steel. Acceptable for welds in C-Mn and low alloy steels provided that
weld thickness at no point is less than t and:
— Individual length/width: t/4, max. 4 mm in any dimension.
— Accumulated length in any 300 mm length of weld: t/2, max. 8
mm.
Surface testing (MT, PT and ET)
Linear indication
Type of indication
Number
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Dimension
Page 413
Visual examination
Number of indications in any part of inspection
area
2
2.0 mm
Linear indication evaluated as incomplete fusion
2
25 mm
Rounded indication
2
4.0 mm
Notes:
1)
Any two imperfections separated by a distance smaller than the major dimension of the smaller imperfection shall
be considered as a single imperfection.
2)
Detectable imperfections are not permitted in any intersection of welds.
3)
For t > 25 mm an increased high/low could be accepted based on an engineering judgment including as a minimum
SCF calculations and AUT validation.
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Table D-5 Acceptance criteria for radiographic testing of welds
Type of defect
Acceptance criteria
1) 2) 3)10)11)
Individual discontinuities
Maximum accumulated size of in any
300 mm weld length for each type of
discontinuity
Diameter: < t/4, but max. 3 mm
Individual pore: <2 mm, cluster
diameter max. 12 mm Length: t/2, but
max. 12 mm, Width: t/10, but max.
3 mm Length: t, but max. 25 mm,
Width: max. 1.5 mm Diameter: < t/4,
max 3 mm Diameter: <2 mm group
length: 2t, but max. 50 mm, Clad/
lined steel: Individual pore <2 mm
See note 4. One cluster or total length
< 12 mm 2 wormholes or total length
< 12 mm Length 2 t, but max. 50 mm
-Length 2 t, but max. 50 mm
Width < 3 mm Width: max 1.5
Individual width: max 1.5
Length 12 mm, but max. 4 off
separated by min 50 mm Length 2 t,
but max. 50 mm Length 2 t, but max.
25 mm
Diameter < 0.5 t, but max. 3 mm Not
permitted
Max 2 off separated by min 50 mm -
Not permitted for welds with CRA weld
overlay and/or for clad/lined steel
-
Length: t, but max. 25 mm Length: 2t,
but max. 50 mm
Length t, but max. 25 mm Length 2 t,
but max. 50 mm
Not permitted in CRA layer of weld
overlay and/or for clad/lined steel
-
Length: t, but max. 25 mm Length: 2
t, but max. 50 mm
Length t, but max. 25 mm Length 2 t,
but max. 50 mm
Cracks
Not permitted
-
Shrinkage cavities and crater pipes
Not permitted
-
Root concavity
Length: 2t, but max. 50 mm
Length: 2 t, but max. 50 mm
Root undercut Excess penetration Burn
through
See Table D-4
See Table D-4
Porosity
1) 2)
Scattered Cluster
5)
Wormhole Hollow bead Isolated
On-line
Slag
6)
7)
1) 2) 3) 8)
Isolated Single lines Parallel lines
Inclusions Tungsten
Copper, wire
Lack of penetration
Root Embedded
1) 2) 3) 8)
9)
1) 2) 3) 8)
Lack of fusion
Surface Embedded
Total accumulation of discontinuities (excluding porosity)
— Maximum accumulation of discontinuities in any 300 mm weld length 3 t, max 100 mm.
— Maximum accumulation of discontinuities: 12% of total weld length.
— Any accumulation of discontinuities in any cross sections of weld that may constitute a leak path or may reduce the
effective weld thickness with more than t/3 is not acceptable.
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Type of defect
Acceptance criteria
1) 2) 3)10)11)
Individual discontinuities
Maximum accumulated size of in any
300 mm weld length for each type of
discontinuity
Notes:
1)
Refer to the additional requirements in [D.2.9.3] for welding methods that produce welding passes exceeding 0.25 t.
2)
Volumetric imperfections separated by less than the length of the smallest defect or defect group shall be considered
as one imperfection.
3)
Elongated imperfection situated in a line and separated by less than the length of the shortest defect shall be
considered as one imperfection.
4)
For single layer welds: 1.5% of projected area, for multi layer welds with t < 15 mm 2% of projected area, for multi
layer welds with t ≥ 15 mm 3% of projected area.
5)
Maximum 10% porosity in cluster area.
6)
Isolated pores are separated by more than 5 times the diameter of the largest pore.
7)
Pores are in a line if not isolated and if 4 or more pores are touched by a line drawn through the outer pores and
parallel to the weld. On-line pores shall be checked by ultrasonic testing. If ultrasonic testing indicates a continuous
defect, the criteria for lack of fusion defect shall apply.
8)
Detectable imperfections are not permitted in any intersection of welds.
9)
Applicable to double sided welding where the root is within the middle t/3 only.
10) Acceptance criteria of Table D-4 shall also be satisfied.
11) Systematic imperfections that are distributed at regular distances over the length of the weld are not permitted even
if the size of any single imperfection meets the requirements above.
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Table D-6 Acceptance criteria for manual ultrasonic testing of welds 1) 2) 3) 4) 5) 6) 7)
Base material thickness 8 mm ≤ t < 15 mm
Base material thickness 15 mm ≤ t ≤ 150 mm
Max. echo amplitude
Corresponding acceptable
indication length, L (mm)
Max. echo amplitude
Corresponding acceptable
indication length, L (mm)
Reference level (DAC)
L ≤ t (but max. 8 mm)
DAC + 4 dB
L ≤ 0.5t (but max. 12.5
mm)
DAC – 6 dB
L > t (but max. 8 mm)
DAC – 2 dB
0.5 t < L ≤ t (but max. 25
mm)
-
-
DAC – 6 dB
L > t (but max. 25 mm in
both outer t/3)
-
-
DAC – 6 dB
L > t (but max. 50 mm in
middle t/3)
Cracks are not permitted.
For welds in duplex stainless steel, CRAs and clad/lined steel: Lack of fusion and lack of penetration are not permitted in
the root of the weld.
Transverse indications: Indications shall be considered as transverse if the echo amplitude transversely exceeds the echo
amplitude from the same indication longitudinally with more than 2 dB. Transverse indications are unacceptable unless
proven not to be planar, in which case the acceptance criteria for longitudinal indications apply.
If an embedded defect is located close to a surface, such that the ligament height is less than half the defect height, the
ligament height between the defect and the surface shall be included in the defect height.
Total accumulation of discontinuities: The total length of acceptable indications with echo amplitude of reference level –
6 dB and above shall not exceed 3 t, maximum 100 mm in any weld length of 300 mm nor more than 12% of total weld
length. Any accumulation of defects in any cross-section of weld that may constitute a leak path or reduce the effective
thickness of weld more than t/3 is not acceptable.
If only one side of the weld is accessible for testing 6 dB shall be subtracted from the maximum echo permitted above.
Notes:
1)
Reference level is defined as the echo amplitude corresponding to the echo from the reflector in the reference blocks
described in Figure D-1, Figure D-2 and Figure D-3 of this appendix, or equivalent reflector.
2)
All indications exceeding 20% of the reference level shall be investigated to the extent that the operator determines
the shape, length and location of the imperfection.
3)
Indications that cannot be established with certainty shall whenever possible be tested with radiography. Indications
that are type determined in this way shall meet the acceptance criteria in Table D-5.
4)
Longitudinal imperfections where the echo height intermittently is below and above the acceptance level shall if
possible be investigated with radiography. Indications that are determined in this way shall meet the acceptance
criteria in Table D-5. If radiography cannot be performed, the length shall not exceed 3 t, maximum 100 mm in any
weld length of 300 mm.
5)
Length and depth shall be determined by an appropriate method, see [D.2.3.35] and [D.2.3.36].
6)
Detectable imperfections are not permitted in any intersection of welds.
7)
Systematic imperfections that are distributed at regular distances over the length of the weld are not permitted even
if the size of any single imperfection meets the requirements above.
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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D.2.11 Repair of welds
D.2.11.1 A repaired weld should be subject to the same testing requirements and acceptance criteria as the
original weld.
D.2.11.2 In cases when the acceptance criteria are based on an ECA, specific acceptance criteria for repair
welds shall be established by an ECA based on the fracture toughness properties obtained during qualification
of the repair welding procedure.
D.2.11.3 Repair welding of cracks is not permitted unless the cause of cracking has been established not to
be a systematic welding error. (If there is a crack in the weld, the weld is per definition considered rejected.
This means a technical evaluation of the cause of cracking shall be performed. If it can be demonstrated that
the crack is a one off situation, then repair welding may be performed subject to agreement).
D.3 Manual non-destructive testing and visual examination of plate,
pipe and weld overlay
D.3.1 General
D.3.1.1 All non-destructive testing, visual inspection of plate, pipe and weld overlay shall be according to
accepted procedures. Note that the requirements of [D.3.2] are not applicable to plate or pipe mills, see
[D.3.2.1].
D.3.1.2 Manual non-destructive testing and visual examination procedures shall be prepared as required in
[D.2.1.1] through [D.2.1.3] to reflect the requirements of the applied standard.
D.3.1.3 Acceptance criteria for manual non-destructive testing and visual examination of plate, pipe and
weld overlay are given in [D.3.6].
D.3.2 Plate and pipe
General
D.3.2.1 These requirements are not applicable for plate and coil examined at the plate/coil mill as covered
by [D.7], or for linepipe examined at the pipe mill as covered by [D.8].
General requirements for ultrasonic testing
D.3.2.2 Ultrasonic equipment shall meet the requirements given in [D.2.3.7] and [D.2.3.8].
D.3.2.3 Probes used for testing of pipe and plate shall be characterised as required by ISO 10375 and ISO
12715.
Angle shear-wave probes of 45° and 60° shall be used for C-Mn and low alloy steels. Angle probes for duplex
stainless steel and austenitic steels shall be twin crystal (transmitter/receiver) compression-wave probes of
45° and 60°. Angle compression wave probes shall and can only be used for scanning without skipping.
Straight beam probes shall be single or twin crystal. Twin crystal probes shall be used when testing is
performed on material with nominal thickness t < 60 mm. The focusing zone of the twin crystal probes shall
be adapted to the material thickness to be examined.
Single or twin crystal probes can be used when testing is performed on material with nominal thickness t
≥ 60 mm. The single crystal probes shall have a dead zone as small as possible, e.g. 10% of the material
thickness or 15 mm whichever is the smaller. Selected probes shall have a nominal frequency in the range of
2 MHz to 5 MHz and dimensions Ø 10 mm to Ø 25 mm.
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D.3.2.4 The IIW or ISO calibration blocks (K1 – K2) according to ISO 2400 or ISO 7963 shall be used for
calibration of range scale and for angle determination. These calibration blocks shall, as near as practicable,
have the same acoustic properties as the material to be tested.
Manual ultrasonic thickness measurements
D.3.2.5 Manual ultrasonic thickness measurements shall be done in accordance with ASTM E797 or
equivalent standard.
Ultrasonic testing for detection of laminar flaws
D.3.2.6 Manual ultrasonic testing for detection of laminar flaws in steel other than clad/lined steel shall be
performed according to ISO 10893-8 App.A, ISO 10893-9 App.A or equivalent standard.
D.3.2.7 Manual ultrasonic testing for detection of laminar flaws in clad/lined steel shall be done in
accordance with ASTM A578/578M or equivalent standard.
D.3.2.8 The surface condition of the material shall permit at least two successive back-wall echoes to be
distinguished when the probe is placed on any area free from internal imperfections.
D.3.2.9 The range scale shall be selected such that there are always at least two back-wall echoes
(reflections) on the screen.
D.3.2.10 The sensitivity shall be based on echoes reflected from Ø 6 mm flat bottom holes in reference
blocks of the material used or of a material with similar with acoustic properties.
D.3.2.11 DGS diagram or DGS- scales can be used provided they are developed for the probe used and can
be correlated to a Ø 6 mm flat bottom hole.
D.3.2.12 The pitch of the scanning grid shall be small enough to ensure detection of the smallest defect
allowed according to the applicable acceptance criteria.
D.3.2.13 Sizing of indications shall be performed according to ISO 10893-9, App.A.
Manual ultrasonic testing for detection of transverse and longitudinal flaws
D.3.2.14 Manual ultrasonic testing for detection of transverse and longitudinal flaws in plate and pipe shall
be done in general accordance with ASTM A577 or equivalent standard.
D.3.2.15 Probes shall meet the requirements of [D.3.2.3]. Additional angle probes will be required for
testing of pipe.
D.3.2.16 Sensitivity for C-Mn and low alloy steel shall be a DAC curve based on reference blocks with a
rectangular notch with depth 3% of the material thickness on both sides.
D.3.2.17 Reference blocks for duplex stainless steel and austenitic steels shall have one Ø 3 mm flat bottom
hole perpendicular to the angle of incidence of the probe and at the largest possible depth from the scanning
surface of the block. Reference blocks shall be of the actual material tested or of a material with similar with
acoustic properties.
D.3.2.18 Low frequency shear wave angle probes may be used for duplex stainless steel and austenitic
steels instead of twin crystal (transmitter/receiver) compression-wave probes. For acceptance, it shall be
verified on the reference blocks that it is possible to obtain a DAC with a shear wave angle probe that is
comparable to the DAC obtained with an angle compression wave probe.
D.3.2.19 The pitch of the scanning grid shall be small enough to ensure detection of the smallest defect
allowed according to the applicable acceptance criteria.
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D.3.2.20 All reference blocks shall be marked with an identification that relates to the specific application of
each block.
Magnetic particle testing
D.3.2.21 Manual magnetic particle testing of:
—
—
—
—
plate
pipe
edges
bevels.
shall be done in accordance with ISO 9934 or equivalent standard.
Liquid penetrant testing
D.3.2.22 Manual liquid penetrant testing of:
—
—
—
—
plate
pipe
edges
bevels.
shall be done in accordance with ISO 3452 or equivalent standard. The penetration and developing times
shall be long enough to allow effective detection of the smallest indications allowed.
Eddy current testing
D.3.2.23 Manual eddy current testing of C-Mn steel Pipe shall be done in accordance with ASTM E309 or
equivalent standard.
Manual eddy current testing of duplex stainless steels and austenitic stainless steels shall be done in
accordance with ASTM E426 or equivalent standard.
D.3.3 Weld overlay
D.3.3.1 Manual magnetic particle testing of ferromagnetic weld overlay deposits shall be performed in
accordance with ISO 9934 or equivalent standard.
D.3.3.2 Manual liquid penetrant testing of non-magnetic weld overlay deposits shall be performed in
accordance with ISO 3452 or equivalent standard.
D.3.3.3 Manual eddy current testing of weld overlay deposits shall be performed in accordance with ASTM
E309 or equivalent standard.
D.3.3.4 Manual ultrasonic testing of weld overlay shall be performed according to ISO 10893-9, App.A or
equivalent standard and:
— Straight beam probes shall be twin crystal. The focusing zone of the twin crystal probes shall be adapted
to the material thickness to be examined.
— The surface condition of the material shall permit at least two successive back-wall echoes to be
distinguished when the probe is placed on any area free from internal imperfections.
— The calibration of range scale shall be carried out using an IIW calibration block, a V2 calibration block or
on a defect free area of known thickness in the material to be examined. The range scale is to be selected
such that there are always at least 2 back-wall echoes (reflections) on the screen.
— The sensitivity shall be based on echoes reflected from a Ø 3 mm flat bottom hole in reference blocks
made from a base material with similar acoustic properties of the actual base material with overlay
deposited according to the same WPS as the actual overlay. The Ø 3 mm flat bottom hole shall be placed
Standard — DNVGL-ST-F101. Edition October 2017, amended December 2017
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Page 420
approximately at the fusion line between overlay and base material. If the testing shall be performed
of machined overlay, the scanning surface shall be machined to the same surface requirements as the
overlay.
— All reference blocks shall be marked with an identification that relates to the specific application of each
block.
Reporting
D.3.3.5 Reports shall be in accordance with [D.2.1.4] and [D.2.1.5].
D.3.4 Visual examination
D.3.4.1 Visual examination shall be carried out in a sufficiently illuminated area; minimum 1000 lx. If
required to obtain good contrast and relief effect between imperfections and background additional light
sources shall be used.
D.3.4.2 For direct examination the access shall generally permit placing the eye within 600 mm of the
surface to be examined and at an angle of not less than approximately 30°. If this is not possible then the
use of mirrors, boroscopes, fibre optics or cameras shall be considered.
D.3.4.3 A sufficient amount of tools, gauges, measuring equipment and other devices shall be available at
the place of examination.
D.3.4.4 The objects to be examined shall be cleaned to remove all scale and processing compounds prior to
examination. The cleaning process shall not injure the surface finish or mask possible imperfections.
D.3.4.5 Reporting of visual examination shall include:
—
—
—
—
—
—
—
Name of manufacturer
Name of examining company
Identification of examined object(s)
Material
Imperfections exceeding the acceptance criteria and their location
Extent of examination
Supplementary sketches/drawings.
D.3.5 Residual magnetism
D.3.5.1 Residual magnetism shall be measured with a calibrated Hall effect gauss meter or equivalent
equipment. Four readings shall be taken 90° apart around the circumference of each end of the pipe,
and at equal spacing for plate ends. The residual magnetism shall not exceed an average value (out of 4
measurements) of 2.0 mT (20 Gauss), with a maximum single value of 2.5 mT (25 Gauss). Some welding
methods may require a more stringent acceptance criterion.
D.3.5.2 Any product that does not meet the requirements of [D.3.5.1] shall be considered defective.
D.3.5.3 All defective products shall be de-magnetized full length, and then their magnetism shall be remeasured until at least three consecutive pipes meet the requirements of [D.3.5.1].
D.3.5.4 The requirements for residual magnetism shall apply only to testing at the specific location since
the residual magnetism in products may be affected by procedures and conditions imposed during and after
handling and shipment.
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D.3.6 Acceptance criteria for manual non-destructive testing of plate, pipe
and weld overlay
D.3.6.1 For manual ultrasonic thickness measurements acceptance criteria shall be according to applicable
specification or product standard.
D.3.6.2 Acceptance criteria for manual ultrasonic testing for laminar flaws in C-Mn, low alloy, duplex, other
stainless steels and nickel based corrosion resistant alloys (CRA) are given in Table D-12.
D.3.6.3 Acceptance criterion for manual ultrasonic testing for detection of laminar flaws in clad steel is given
in ASTM A263, A264 or A265 and shall correspond to the class 1 quality level. In addition, no areas with
laminations or lack of bonding are allowed over a width extending at least 50 mm inside the location of future
weld preparations.
D.3.6.4 For manual ultrasonic testing for detection of transverse and longitudinal flaws in C-Mn and low
alloy steel, the acceptance criterion shall be that no indications exceed the DAC curve established against the
rectangular notch with depth 3% of the thickness.
For manual ultrasonic testing for detection of transverse and longitudinal flaws in duplex stainless steel, the
acceptance criterion shall be that no indications exceed the DAC curve established against the Ø 3 mm flat
bottom hole.
D.3.6.5 Acceptance criterion for manual magnetic particle testing of plate/pipe bevels and edges shall be:
— No indications longer than 6 mm are permitted.
D.3.6.6 Acceptance criterion for manual liquid penetrant testing of plate/pipe bevels and edges shall be:
— no indications longer than 6 mm are permitted.
Guidance note:
For clad pipes made from explosion welded clad plates; indications from process related melt pockets within the bond zone of
explosion welded material are acceptable. It is acknowledged that these indications do not indicate lamination or a degrade
bond between backing and clad material. Lamination and disbonding imperfections shall be assessed according to the
acceptance criteria above.
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D.3.6.7 Acceptance criterion for manual eddy current testing of pipe/pipe bevels and edges shall be:
— no indications longer than 6 mm are permitted.
D.3.6.8 Defects at pipe bevels and edges shall be examined ultrasonically as required in this subsection and
the pipes cut back until no defects are present in the tested area.
D.3.6.9 Acceptance criteria for as-welded surfaces of magnetic and non magnetic weld overlay for visual
examination, magnetic particle testing, liquid penetrant and eddy current testing are:
— no round indications with diameter above 2 mm and no elongated indications
— indications separated by a distance less than the diameter or length of the smallest indication, shall be
considered as one indication
— accumulated diameters of round indications in any 100 × 100 mm shall not exceed 10 mm.
D.3.6.10 Acceptance criteria for ultrasonic testing of as-welded surfaces of magnetic and non-magnetic
weld overlay shall be no loss of back wall echo and no echo from an indication shall exceed 66% of the echo
reflected from Ø 3 mm flat bottom holes in reference blocks.
D.3.6.11 For machined surfaces, acceptance criteria shall be especially agreed upon.
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D.3.6.12 Defects shall be ground out, re-welded and re-tested to meet the acceptance criteria above.
D.3.6.13 When any subsequent process requires homogenous material, i.e. ultrasonic examination, other
acceptance criteria shall apply.
D.4 Non-destructive testing and visual examination of forgings
D.4.1 General
D.4.1.1 All non-destructive testing of forgings shall be performed according to accepted procedures.
D.4.1.2 Manual non-destructive testing and visual examination procedures shall be prepared as required in
[D.2.1.1] through [D.2.1.3] to reflect the requirements of the applied standard.
D.4.1.3 Acceptance criteria for manual non-destructive testing and visual examination forgings are given in
[D.4.5].
D.4.2 Ultrasonic and magnetic particle testing of C-Mn and low alloy steel
forgings
Ultrasonic testing
D.4.2.1 Ultrasonic testing of forgings shall be performed in accordance with ASTM A388 and the
requirements below.
Ultrasonic testing procedures
D.4.2.2 Ultrasonic testing procedures shall contain the information in [D.2.1.1] and:
—
—
—
—
—
—
—
—
type of instrument
type and dimensions of probes
range of probe frequencies
description of reference blocks
calibration details, range and sensitivity
surface requirements, including maximum temperature
type of coupling medium
scanning techniques supplemented with sketches, showing the probes used and area covered by each
probe
— description of methods for recheck of areas with reduction or loss of back reflection
— recording details.
Ultrasonic apparatus
D.4.2.3 Verification of screen height linearity and amplitude linearity shall be performed at the beginning of
each period of extended use (or every 3 months, whichever is less). Records shall be made available upon
request.
Probes
D.4.2.4 Straight beam probes with frequency 2 to 5 MHz and dimension Ø 10 to 30 mm shall be used. The
probes shall be single or twin crystal. Twin crystal probes shall be used when testing is performed on material
with nominal thickness t < 60 mm. The focusing zone of the twin crystal probes shall be adapted to the
material thickness to be examined.
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Single or twin crystal probes can be used when testing is performed on material with nominal thickness t
≥ 60 mm. The single crystal probes shall have a dead zone as small as possible, e.g. 10% of the material
thickness or 15 mm whichever is the smaller.
D.4.2.5 Angle beam probes shall be used for testing on rings, hollow and cylindrical sections. Angle beam
probes shall be available in angles, or be provided with wedges or shoes, ranging from 30° to 75°, measured
to the perpendicular of the entire surface of the forging being tested.
Reference blocks for straight beam testing
D.4.2.6 Supplementary requirement S1 of ASTM A388 shall apply, but with the following additional
requirements:
— For material thickness t ≤ 38 mm the flat bottom holes shall be Ø 1.6 mm
— For material thickness 38 mm < t < 60 mm the flat bottom holes shall be Ø 3 mm
— For material thickness t ≥ 60 mm the flat bottom holes shall be Ø 6 mm.
Reference blocks for angle beam testing
D.4.2.7 The reference notches shall be rectangular D and ID notches with a depth of:
— For material thickness t ≤ 38 mm, 3% of the thickness
— For material thickness 38 mm < t < 100 mm, 5% of the thickness
— For material thickness t ≥ 100 mm, 10% of the thickness.
D.4.2.8 A separate reference block shall have the same configuration, nominal composition, forging ratio,
heat treatment and thickness as the forgings it represents.
D.4.2.9 Where a group of identical forgings is made, one of the forgings may be used as the separate
reference block.
D.4.2.10 All reference blocks shall be marked with an identification that relates to the specific application of
each block.
Preparation of forgings for ultrasonic testing
D.4.2.11 For forgings of uncomplicated geometry, the requirements of ASTM A388, chapter 6 shall apply.
Forgings of complex geometry
D.4.2.12 Forgings are required to be forged and/or to be rough machined to near final dimensions prior
to heat treatment in order to obtain the required properties. This machining of forgings shall consider that
cylindrical shapes and faces that are flat and parallel to one another shall be obtained in order to provide
adequate conditions for ultrasonic testing. In the case of forgings with complex geometry, machining shall
provide intersecting
cylindrical and/or flat faces. The machining shall be such that areas where adequate ultrasonic testing is not
possible will be removed during the final machining. A sketch shall be provided for acceptance showing the
areas of the forging where adequate ultrasonic testing will not be achieved.
Acceptance criteria shall be according to component final dimensions.
Calibration of amplification and testing procedure
D.4.2.13 The IIW or ISO calibration blocks (K1 – K2) according to ISO 2400 or ISO 7963 shall be used for
calibration of range scale and for angle determination. These calibration blocks shall, as near as practicable,
have the same acoustic properties as the material to be tested. Calibration of range scale can alternatively
be done on a defect free area of known thickness in the material to be examined. The range scale is to be
selected such that there are always at least 2 back-wall echoes (reflections) on the screen.
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D.4.2.14 The calibration of the required amplification shall be performed according to ASTM A388, chapter 9.
The probe size and frequency that provides optimum response shall be used for the testing.
D.4.2.15 Notes 2 and 3 of, chapter 9 in ASTM A388 shall be adhered to.
D.4.2.16 When scanning, the gain shall increased by minimum 6 dB above the corrected primary gain. For
evaluation of indications the gain shall be reduced by the increased dB level used during scanning.
D.4.2.17 The method for re-check of areas with reduction or loss of back reflection, ASTM A 388, paragraph
9.2.4, shall be described.
D.4.2.18 Different frequencies, types, angles and diameter of probes shall be employed to obtain additional
information about detected indication.
Sizing of indications
D.4.2.19 In general, the area containing imperfections shall be sized (area and length) using the 6 dB drop
technique. The area refers to the surface area on the forgings over which a continuous indication exceeds the
acceptance criteria. This area will be approximately equal to the area of the real defect provided the defect
size is larger than the 6 dB beam profile of the probe.
D.4.2.20 If the real imperfection size is smaller than the 6 dB beam profile, the 6 dB drop technique is not
suited for sizing. The area measured on the surface will be measured too large and not represent the real
indication size. A guide to classify if the revealed indications are greater or smaller than the 6 dB drop profile
is given in EN 10228-3, part 13.
D.4.2.21 If the size of the indication is evaluated to be smaller than the 6 dB drop profile at the depth of
discontinuity a graphic plot, that incorporates a consideration of beam spread should be used for realistic size
estimation.
Periodical checks of equipment
D.4.2.22 At approximately four-hourly intervals and at the end of testing, the range scale, probe angle
and primary gain shall be checked and if necessary, corrected. Checks shall also be carried out whenever a
system parameter is changed or changes in the equivalent settings are suspected. If deviation is found to
be larger than 2% of range scale, or 3 dB of primary gain setting or 2° of nominal angle probe, the testing
carried out with the equipment over the previous period shall be repeated.
Reporting
D.4.2.23 Reports shall be in accordance with [D.2.1.4] and [D.2.1.5] and ASTM A388, chapter 9.
Manual magnetic particle testing of C-Mn steel forgings
D.4.2.24 Manual magnetic particle testing of C-Mn steel forgings shall be performed in accordance with ISO
9934 or equivalent standard.
D.4.3 Ultrasonic and liquid penetrant testing of duplex stainless steel
forgings
Ultrasonic testing
D.4.3.1 Ultrasonic testing of duplex stainless steel forgings shall be performed in accordance with [D.4.2],
but with the following additions to the requirements to:
— probes
— reference blocks for angle beam testing
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— preparation of forgings for ultrasonic testing
— testing procedure.
Angle probes
D.4.3.2 Angle probes for duplex stainless steel shall be twin crystal (transmitter/receiver) compression-wave
probes. Angle compression wave probes shall and can only be used without skipping.
D.4.3.3 Low frequency shear wave angle probes may be used for duplex stainless steel instead of twin
crystal (transmitter/receiver) compression-wave probes, provided it is verified on the reference blocks that
it is possible to obtain a DAC with a shear wave angle probe that is comparable to the DAC obtained with an
angle compression wave probe.
D.4.3.4 Creep wave probes shall be used for detection of sub surface defects close to the scanning surface,
unless testing can be performed from both sides.
Reference blocks for angle beam testing
D.4.3.5 Reference blocks for angle beam testing of duplex stainless steel with angle compression wave
probes shall have side drilled holes and a 1 mm deep and 20 mm wide spark eroded notch according to
Figure D-4 and Table D-7.
Preparation of forgings for ultrasonic testing
Figure D-4 Reference block for construction of DAC, duplex stainless steel
Table D-7 Reference block dimensions
Thickness of
reference block (T)
Diameter of side
drilled hole mm
T < 20 mm
15 mm or t
2.4 ± 0.2
20 mm ≤ t < 35 mm
20 mm or t
35 mm ≤ t < 75 mm
50 mm or t
75 mm ≤ t < 100 mm
90 mm or t
Material thickness (t)
100 mm ≤ t < 150 mm
125 mm or t
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3.0 ± 0.2
6.0 ± 0.2
Position of side drilled holes
T/4, T/2 and T3/4
The distance between the two
outer holes and the nearest
surface shall not exceed 12 mm
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D.4.3.6 The machining of duplex stainless steel forgings for ultrasonic testing shall take into account that
angle compression wave probes shall and can only be used without skipping.
Testing procedure
D.4.3.7 The testing procedure for duplex stainless steel forgings shall take into account that angle
compression wave probes shall and can only be used without skipping. The testing shall hence be performed
from as many faces that access permits.
Manual liquid penetrant testing of duplex stainless steel forgings
D.4.3.8 Manual liquid penetrant testing of duplex stainless steel forgings shall be performed in accordance
with ISO 3452 or equivalent standard. The penetration and developing times shall be long enough to allow
effective detection of the smallest indications allowed.
D.4.3.9 Reports shall be in accordance with [D.2.1.4] and [D.2.1.5] and ASTM A388, chapter 9.
D.4.4 Visual examination of forgings
D.4.4.1 Visual examination of forgings shall be performed in accordance with [D.3.4], with acceptance
criteria according to [D.4.5].
D.4.5 Acceptance criteria for forgings
D.4.5.1 Acceptance criteria for manual ultrasonic testing of forgings shall be:
Straight beam testing
— No single indication shall be larger than the indication received from the flat bottom holes in the reference
block required in [D.4.2].
Angle beam testing of C-Mn and low alloy steel forgings
— No single indication shall exceed a DAC curve established using the notches in the reference block
required in [D.4.2].
Angle beam testing of duplex stainless steel forgings
— No single indication shall exceed a DAC curve established using the side drilled holes in the reference
Multiple indications
— No indications within 13 mm of each other in any direction shall exceed 50% of the reference curve.
Acceptance criteria for manual magnetic particle testing of C-Mn and low alloy steel forgings
D.4.5.2 Acceptance criteria for manual magnetic particle testing of C-Mn and low alloy steel forgings shall be
according to Table D-8.
Acceptance criteria for manual liquid penetrant testing of duplex stainless steel forgings
D.4.5.3 Acceptance criteria for manual liquid penetrant testing of duplex stainless steel forgings done in
accordance with ISO 3452 or equivalent standard shall be according to Table D-8.
Acceptance criteria for visual examination
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Table D-8 Acceptance criteria for manual magnetic particle and liquid penetrant testing of
forgings
A
Crack-like indications: not permitted
B
Linear indications with length more than 2 mm or three times the width: not permitted. Linear indications
with length < 1.5 mm may be deemed irrelevant
C
Rounded indications: Diameter < 3 mm, accumulated diameters in any 100 × 150 mm area < 8 mm.
D.4.5.4 Acceptance criteria for visual examination of forgings shall be in accordance with ASTM A 961,
Chapter 15. If the surface imperfections acceptable under 15.5 are not scattered, i.e. more than 3 off in any
100 × 150 mm area, such imperfections shall be considered injurious.
D.5 Non-destructive testing and visual examination of castings
D.5.1 General
D.5.1.1 All non-destructive testing of castings shall be done according to accepted procedures.
D.5.1.2 Manual non-destructive testing and visual examination procedures shall be prepared as required in
[D.2.1.1] through [D.2.1.3] to reflect the requirements of the applied standard.
D.5.1.3 Acceptance criteria for manual non-destructive testing and visual examination of castings are given
in [D.5.6].
D.5.2 Ultrasonic and magnetic particle testing of C-Mn and low alloy steel
castings
D.5.2.1 Manual ultrasonic testing of castings shall be done according to ASTM A609, procedure A, and
Supplementary requirement S1. In addition the requirements below apply.
Ultrasonic testing procedures
D.5.2.2 Ultrasonic testing procedures shall contain the information in [D.2.1.1] and:
—
—
—
—
—
—
—
—
type of instrument
type and dimensions of probes
range of probe frequencies
description of reference blocks
calibration details, range and sensitivity
surface requirements, including maximum temperature
type of coupling medium
scanning techniques supplemented with sketches, showing the probes used and area covered by each
probe
— description of methods for re-check of areas with reduction or loss of back reflection
— recording details.
Ultrasonic apparatus
D.5.2.3 Verification of screen height linearity and amplitude linearity shall be performed at the beginning of
each period of extended use (or every 3 months, whichever is less). Records shall be made available upon
request.
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Probes
D.5.2.4 Straight beam (normal) probes with frequency 1-5 MHz and dimension Ø 10-30 mm shall be used.
Straight beam, normal probes shall be single or twin crystal. Twin crystal probes shall be used when testing
is performed on material with nominal thickness t < 25 mm. The focusing zone of the twin crystal probes
shall be adapted to the material thickness to be examined.
D.5.2.5 Single or twin crystal probes can be used when testing is performed on material with nominal
thickness t ≥ 60 mm. The single crystal probes shall have a dead zone as small as possible, e.g. 10% of the
material thickness or 15 mm whichever is the smaller.
Reference blocks
D.5.2.6 All reference blocks shall be marked with an identification that relates to the specific application of
each block.
Casting conditions for ultrasonic testing
D.5.2.7 Castings shall as far as possible be machined according to [D.4.2.11] and [D.4.2.12].
Calibration of amplification and testing procedure
D.5.2.8 The IIW or ISO calibration blocks (K1 – K2) according to ISO 2400 or ISO 7963 shall be used for
calibration of range scale and for angle determination. These calibration blocks shall, as near as practicable,
have the same acoustic properties as the material to be tested. Calibration of range scale can alternatively
be done on a defect free area of known thickness in the material to be examined. The range scale is to be
selected such that there are always at least 2 back-wall echoes (reflections) on the screen.
D.5.2.9 The calibration of the required amplification shall be performed according to ASTM A609, chapter 8
and S1. The probe size and frequency that provides optimum response shall be used for the testing.
D.5.2.10 Note 3 of ASTM A609, chapter 8: When scanning, the gain shall be increased by minimum 6 dB
above the corrected primary gain. For evaluation of indications the gain shall be reduced by the increased dB
level used during scanning.
D.5.2.11 Rechecks shall be performed if the loss of back reflection is 50% or greater. The method for further
investigation of areas with reduction or loss of back reflection, ASTM A 609 paragraph 8.5, shall be described.
D.5.2.12 Different frequencies, types, angles and diameter of probes shall be employed to obtain additional
information about detected indication
Sizing of indications
D.5.2.13 In general, the area containing imperfections, shall be sized (area and length) using the 6 dB drop
technique. The area refers to the surface area on the castings over which a continuous indication exceeds the
acceptance criteria. This area will be approximately equal to the area of the real defect provided the defect
size is larger than the 6 dB beam profile of the probe.
D.5.2.14 If the real imperfection size is smaller than the 6 dB beam profile, the 6 dB drop technique is not
suited for sizing. The area measured on the surface will be measured too large and not represent the real
indication size. A guide to classify if the revealed indications are greater or smaller than the 6 dB drop profile
is given in EN 10228-3, part 13.
D.5.2.15 If the size of the indication is evaluated to be smaller than the 6 dB drop profile at the depth of
discontinuity, a graphic plot that incorporates a consideration of beam spread should be used for realistic size
estimation.
Periodical checks of equipment
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D.5.2.16 At approximately four-hourly intervals and at the end of testing, the range scale, probe angle and
primary gain shall be checked and corrected. Checks shall also be carried out whenever a system parameter
is changed or changes in the equivalent settings are suspected. If deviation is found to be larger than 2%
of range scale, or 3 dB of primary gain setting or 2° of nominal angle probe, the testing carried out with the
equipment over the previous period shall be repeated.
Reporting
D.5.2.17 Reports shall be in accordance with [D.2.1.4], [D.2.1.5], and ASTM A609, chapters 9 and 19. All
indications exceeding 50% of the DAC shall be reported.
Manual magnetic particle testing of C-Mn and low alloy steel castings
D.5.2.18 Manual magnetic particle testing of C-Mn steel castings shall be performed in accordance with ISO
9934 or equivalent standard.
D.5.2.19 Reports shall be in accordance with [D.2.1.4] and [D.2.1.5].
D.5.3 Ultrasonic and liquid penetrant testing of duplex stainless steel
castings
Ultrasonic testing
D.5.3.1 Ultrasonic testing of duplex stainless steel castings shall be performed in accordance with [D.5.2],
but with the following additions to the requirements to:
—
—
—
—
probes
reference blocks for angle beam testing
casting conditions for ultrasonic testing
testing procedure.
Angle probes
D.5.3.2 Angle probes for duplex stainless steel shall be twin crystal (transmitter/receiver) compression-wave
probes. Angle compression wave probes shall and can only be used without skipping.
D.5.3.3 Low frequency shear wave angle probes may be used for duplex stainless steel instead of twin
crystal (transmitter/receiver) compression-wave probes, provided it is verified on the reference blocks that
it is possible to obtain a DAC with a shear wave angle probe that is comparable to the DAC obtained with an
angle compression wave probe.
D.5.3.4 Creep wave probes shall be used for detection of sub surface defects close to the scanning surface,
unless testing can be performed from both sides.
Reference blocks for angle beam testing
D.5.3.5 Reference blocks for angle beam testing of duplex stainless steel with angle compression wave
probes shall have side drilled holes and a 1 mm deep and 20 mm wide spark eroded notch according to
Figure D-4 and Table D-7.
Casting conditions for ultrasonic testing
D.5.3.6 Duplex steel stainless castings shall be machined according to [D.4.2.11] and [D.4.2.12].
D.5.3.7 The machining of duplex stainless steel castings for ultrasonic testing shall take into account that
angle compression wave probes shall and can only be used without skipping.
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Testing procedure
D.5.3.8 The testing procedure for duplex stainless steel castings shall take into account that angle
compression wave probes shall and can only be used without skipping. The testing shall hence be performed
from as many faces that access permits.
Manual liquid penetrant testing of duplex stainless steel castings
D.5.3.9 Manual liquid penetrant testing of duplex stainless steel castings shall be performed in accordance
with ISO 3452 or equivalent standard. Post-emulsified penetrants should be used on precision castings
only. The penetration and developing times shall be long enough to allow effective detection of the smallest
indications allowed.
D.5.3.10 Reports shall be in accordance with [D.2.1.4] and [D.2.1.5].
D.5.4 Radiographic testing of castings
General
D.5.4.1 Radiographic testing of castings shall be done according to ASME Boiler and Pressure Vessel Code,
Sec.5, article 2, mandatory appendix VII or equivalent standard. In addition, the applicable requirements of
[D.2.2] and the requirements below shall apply.
Procedures
D.5.4.2 Radiographic procedures shall in addition to the requirements of [D.2.2.3], give the following
information:
—
—
—
—
—
shooting sketches
coverage
source location
location of IQI
acceptance criteria.
D.5.5 Visual examination of castings
D.5.5.1 Visual examination of castings shall be performed in accordance with [D.3.4] and MSS SP-55.
D.5.5.2 Reports shall be in accordance with [D.3.4.5].
D.5.6 Acceptance criteria for castings
General
D.5.6.1 Acceptance criteria shall apply for the entire casting or portions of the casting. If different
acceptance criteria shall apply for different portions of the casting, the critical areas of the casting shall be
defined.
Guidance note:
Critical areas shall include abrupt changes of sections and at the junctions of risers, feeders and gates to the casting. Highly
stressed areas such as weld necks shall be considered as critical areas.
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D.5.6.2 Acceptance criteria for manual ultrasonic straight beam testing of castings shall be:
— No crack-like indications are acceptable, and
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— According to Table D-9.
Table D-9 Ultrasonic testing acceptance criteria for castings
Straight beam testing
ASTM A609, 10.2.1, 10.2.2 and 10.2.3
Critical areas
Other areas
Table 2, quality level 1
Table 2, quality level 3
Angle beam testing
ASTM A609 S1.4.1 and Table 2
Critical areas
Other areas
Table 2, quality level 1
Table 2, quality level 3
D.5.6.3 Acceptance criteria for manual radiographic testing of critical areas of castings shall be according to
Table D-10.
Table D-10 Radiographic acceptance criteria for castings
Type of defect
Acceptance criteria
Standard
Maximum severity level
Gas porosity
2
Inclusions
2
Shrinkage
Cracks
ASTM E280
2
0
Hot tears
0
Inserts
0
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D.5.6.4 Acceptance criteria for manual magnetic particle testing and manual liquid penetrant testing of
castings shall be according to Table D-11.
Table D-11 Acceptance criteria for manual magnetic particle and liquid penetrant testing of
castings
A
Crack-like defects: not permitted
B
Linear indications with length more than three times the width: not permitted. Linear indications with length <
1.5 mm may be deemed irrelevant.
C
Rounded indications: Diameter < 3 mm, accumulated diameters in any 100 × 150 mm area < 8 mm.
D.5.6.5 Acceptance criteria for visual inspection of castings shall be in accordance with MSS SP-055:
— Type 1: Not acceptable.
— Types 2 to 12: A and B.
Repairs by welding
D.5.6.6 Complete removal of the defect shall be confirmed by magnetic particle testing, or liquid penetrant
testing for non-ferromagnetic materials, before re-welding.
D.5.6.7 Repair welds of castings shall meet the acceptance criteria designated for the particular portion of
the casting.
D.6 Automated non-destructive testing
D.6.1 General
D.6.1.1 These requirements are applicable to all automated NDT processes except automated ultrasonic
testing of girth welds where specific requirements are given in App.E. The requirements given in this
subsection are additional to the requirements of any standard or recommended practice where automated
NDT methods are prescribed or optional.
D.6.1.2 Automated non-destructive testing can replace manual non-destructive testing or one automated
non-destructive testing method/system can replace another automated non-destructive testing method/
system provided the equivalence of systems is documented with regard to function, operation, ability in
detection and sizing and performance.
D.6.1.3 Documentation of capability/performance and qualification of automated NDT systems in pipe mills
should not be required for systems meeting the documentation requirements given in [D.8.4.4].
D.6.2 Documentation of function and operation
The automated NDT equipment shall be documented with regard to function and operation. Items subject to
documentation include:
—
—
—
—
—
brief functional description of the equipment
detailed equipment description
operation manual including type and frequency of functional checks
calibration
limitations of the equipment with regard to material or weld features including size, geometry, type of
flaws, surface finish, material composition etc.
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— repeatability.
D.6.3 Documentation of performance
D.6.3.1 The capability and performance of automated NDT equipment shall be documented by statistical
records covering, as relevant:
—
—
—
—
—
accuracy in indication sizing (random and systematic deviation)
accuracy in positioning/location
defect characterisation abilities compared to the results of other NDT performed
repeatability, and
probability of detection values or data for different threshold settings to determine the threshold to be
used for required detection during testing.
Guidance note:
Automated non-destructive testing equipment can generally be divided into two groups. One group consists of equipment intended
for detection, sizing and positioning of indications (typically real time radiography) and one group consisting of equipment intended
for detection only and where sizing and positioning of indications is performed by other means (typically ultrasonic testing of
the weld seam according to ISO 10893-11). For the latter types of equipment, documentation of performance may be limited
to demonstration of adequate detection of defects typical for the manufacturing process, threshold setting parameters and
repeatability.
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D.6.4 Qualification
D.6.4.1 A full qualification programme for automated NDT equipment will in general comprise the following
stages:
—
—
—
—
initial evaluation and conclusions based on available information
identification and evaluation of significant parameters and their variability
planning and execution of a performance test programme
reference investigations.
D.6.5 Evaluation of performance documentation
D.6.5.1 As a minimum a qualification will involve an assessment of the automated NDT equipment technical
documentation, including the quality assurance system, and available information on equipment capability
and performance. Limited practical tests shall be performed in many cases.
D.7 Non-destructive testing of pipe body of welded pipes
D.7.1 General
D.7.1.1 The pipe body material of welded pipes shall be tested with an ultrasonic inspection method. The
non-destructive testing of this material should be performed during manufacture of plate and coil, but can be
performed on the final pipe.
In addition, plate and coil shall be visually inspected. The testing shall be performed according to
documented procedures.
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Guidance note:
The pipe body is inspected for defects oriented parallel to the surface of plate and coil (e.g. laminations). Pipe manufacture (e.g.
forming, expansion, heat treatment) does not have a significant influence on such defects; consequently it is not required to
perform this inspection in the final delivery condition of the pipe.
Pipe body inspection does typically not look for defects oriented in the through-thickness direction (either transversely or parallel
to the pipe axis). The probability of such defects occurring and not detected by visual inspection is considered negligible for wall
thicknesses used for pipelines.
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D.7.1.2 The inspection shall be carried out in a manner that ensures detection of the minimum imperfection
size to be considered.
The scanning velocity shall be set low enough so that the distance the probe travels while inactive is
significantly less than the maximum length of allowable imperfections. There should be at least one
inspection point per millimeter of movement.
The inspection should ensure 100% coverage of the material perpendicularly to the movement of equipment,
with some overlap between inspection channels/tracks.
D.7.1.3 Lack of acoustic coupling shall be treated as an imperfection. An alarm for lack of acoustic coupling
shall be incorporated in the inspection equipment for every probe/channel. This alarm shall give a visual
signal, and should give an additional audio signal. The principle of detecting lack of acoustic coupling shall
be described in the procedure. The trigger level for the lack of acoustic coupling alarm shall be stated in
the procedure. The lack of acoustic coupling alarm shall be tested at least once per month (for instance by
closing the water supply for a probe).
D.7.1.4 The inspected material shall have a surface condition and geometry that ensures the validity of the
test. A reduction of 6-8 dB in back wall echo shall be detected and reported. When such variations in signal
occur, the manufacturer shall, based on review of plate condition and inspection result, conclude whether the
test is valid. An invalid test shall be repeated, or the plate shall be rejected.
D.7.1.5 Material that contains unacceptable imperfections or surface defects shall be rejected or cut until no
unacceptable imperfections or defects are present in the material.
D.7.2 Requirements to automated ultrasonic inspection for pipe body
D.7.2.1 When automated inspection systems are used, documentation and qualification records meeting the
requirements of [D.6] or [D.8.4.4] shall be available. Such documentation and records are not required to be
project-specific, but the qualified parameters and relevant intervals shall be stated and justified. In addition,
a full system calibration shall be done with intervals not exceeding 12 months.
D.7.2.2 The reference standard shall be a plate or pipe with the reflectors required for checking sensitivity,
coverage, sizing (if used) and evaluation (if used). In addition, the reference standard shall have:
— Similar wall thickness to the inspected product, unless the inspection equipment can take into account
variations in wall thickness (for instance by use of Distance-Gain-Signal curves).
— Similar acoustic properties.
— Width/diameter and length determined by the manufacturer.
— Identification and marking determined by the manufacturer.
D.7.2.3 The coverage of the inspection equipment shall be demonstrated by reflectors in the reference
standard. The reflectors shall be of same type and size as reflectors used for sensitivity setting. The location
shall be determined by the manufacturer. The following scenarios shall as a minimum be considered;
— For pipe; non-inspected area along longitudinal weld, measured in circumferential direction.
— For pipe and cut plate; non-inspected area at start and end of inspection.
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— For cut plate; non-inspected area at edges parallel to movement of inspection equipment (inspection of
cut plate is at least relevant when re-inspection is required due to failed dynamic calibration check).
D.7.2.4 The equipment shall be set up, optimized and calibrated in static mode. Subsequently the reference
standard shall be run at least once through the inspection system in normal production conditions – this
is the dynamic calibration check. If all relevant reflectors or artificial imperfections are detected above the
registration level, the equipment is ready for production. The scanning velocity during dynamic calibration
check is the maximum allowed velocity during production.
D.7.2.5 A dynamic calibration check shall be performed;
—
—
—
—
every four hours or once every 10 items inspected (whichever is longer),
at the start and end of each shift,
at any change of equipment operator,
whenever a malfunction of the equipment is suspected.
If a dynamic calibration check is unacceptable, all items inspected since last acceptable dynamic calibration
check shall be re-inspected. Re-inspection and continued production is allowed only after the inspection
equipment has been set up again and passed a new dynamic calibration check.
If a dynamic calibration check is unacceptable, it is allowed to do a double re-test with the reference
standard. If both re-tests are acceptable, the calibration check can be considered passed. It is also allowed
to visually inspect the reference standard and clean the surface. No change to any system settings shall be
made.
D.7.2.6 When a function for determination of dimensions and size of imperfections is used, this shall be
stated in the procedure. The function can determine the width, length or area, depending on requirements.
The reference standard shall contain reflectors with the following dimensions and location;
—
—
—
—
—
—
—
—
—
—
—
—
Area equal to maximum allowed for body. Located in body, mid-wall.
Area equal to maximum allowed for body. Located in body, 3-6 mm from back wall.
Area equal to maximum allowed for body. Located in body, 3-6 mm from front wall.
Area equal to maximum allowed for edge. Located in edge, mid-wall.
Area equal to maximum allowed for edge. Located in edge, 3-6 mm from back wall.
Area equal to maximum allowed for edge. Located in edge, 3-6 mm from front wall.
Width ≤ 8 mm. Located in body, mid-wall.
Width ≤ 8 mm. Located in body, 3-6 mm from back wall.
Width ≤ 8 mm. Located in body, 3-6 mm from front wall.
Length ≤ 10 mm. Located in edge or body, mid-wall.
Length ≤ 10 mm. Located in edge or body, 3-6 mm from back wall.
Length ≤ 10 mm. Located in edge or body, 3-6 mm from front wall.
The type and shape of reflectors shall be determined by the manufacturer. These reflectors shall be detected
and registered during each dynamic calibration check.At least once per week the result from the function for
these reflectors shall be compared with their actual dimensions. The procedure shall contain a table that lists
all reflectors, their actual dimensions and location in the test plate.Any under-sizing is unacceptable. In case
of under-sizing all items inspected since last acceptable check are suspect and shall be evaluated again, after
correction of the sizing algorithm.Variation in sizing and over-sizing is acceptable.
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Guidance note:
The dimension and location of the required reflectors are intended to demonstrate that small and large reflectors are adequately
sized. Imperfections with intermediary areas are expected to also be adequately sized. Consequently the area of the reflectors is
selected with a view to the relevant acceptance criteria.
Width and length are also criteria. It is considered that the smallest width and length are most difficult for the function to
determine. This is because the critical dimensions will typically be smaller than the size of the probe or channel. Consequently any
larger width and length should be adequately determined.
It is required to have reflector or artificial imperfections at different depths, in order to confirm that the algorithm correctly takes
into account the location in the wall thickness.
It is assumed that the inspection data for both edge and body are fed into one computer and handled by one sizing algorithm.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e--Guidance note:
If the sizing algorithm is found to give under-size results, the suspect plates/pipes shall be evaluated again. This can be done by (i)
re-inspecting the items with a full inspection routine or (ii) recalculating the sizes using the existing data.
As long as the sensitivity of the equipment is acceptable, the data produced by the system should be considered representative of
the inspected items.
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D.7.2.7 When a function for evaluation of imperfections is used, this shall be stated in the procedure. The
evaluation function requires as input dimensional data of imperfections, consequently the requirements to
a sizing function shall be implemented. In addition, the reference standard shall contain reflectors with the
following size, number and location;
— A group in plate body with a population density of one more that maximum allowed density within a given
reference area. This group shall be evaluated as unacceptable. Location in plate body and depth to be
decided by the manufacturer.
— A group in plate edge with a population density of one more that maximum allowed density within a given
reference area. This group shall be evaluated as unacceptable. Location in plate edge and depth to be
decided by the manufacturer.
— Two adjacent imperfections of such size and proximity that they shall be considered as one imperfection.
Location and depth to be decided by the manufacturer.
These reflectors shall be detected and registered during each dynamic calibration check.At least once per
week the result of the evaluation function for all reflectors in the reference standard shall be reviewed.
The procedure shall contain a table that lists all reflectors, their location in the test plate and the expected
evaluation result for each reflector.In case the evaluation result is incorrect and unacceptable, all items
inspected since last acceptable check are suspect and shall be evaluated again, after correction of the
evaluation function.
D.7.2.8 When functions for sizing of imperfections and/or evaluation of imperfections are used, a baseline for
the system shall be established before start of production. The reference standard shall be tested ten times
in conditions equal to production conditions. A report shall be issued, with the following information;
—
—
—
—
—
Reference to inspection procedure and date of baseline inspections.
Normal production reports for each dynamic calibration check.
Dimensions for each reflector; average, minimum and maximum result.
Evaluation result for each reflector or artificial imperfection.
Conclusion on the readiness and stability of the system.
D.7.2.9 Each channel and each probe shall be checked at least once per month. This check shall have
identical conditions for all channels and probes, so that the results may be compared and analyzed. The
procedure shall state how this check is performed, and the manufacturer shall established quantitative
criteria for the test. As a minimum, the back wall echo and the noise level shall be evaluated.
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Guidance note:
There are several approaches to a full system check of individual probes and channels. The below list of examples is not
exhaustive.
—
Static calibration check, one probe/channel at a time. This should be possible to automate by the equipment supplier.
—
Use of full wall in an area without any imperfections, either in the reference plate or a normal production plate.
—
Include a transverse notch in the reference standard, typically with a width of somewhere between 4-8 mm.
The check should include a test of the sensitivity.
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D.7.3 Ultrasonic testing of C-Mn steel and corrosion resistance alloy
D.7.3.1 When performed, ultrasonic testing for laminar imperfections shall be in accordance with ISO
10893-9, and with additional requirements as stated in this section. If the testing is done on the final pipe, it
shall be done in accordance with ISO 10893-8.
D.7.3.2 The inspection shall detect laminar imperfections in the material, and the material shall meet the
acceptance criteria in Table D-12. The edge criteria shall be applied as follows:
— Transverse edge; 150 mm inside the location of future bevel for girth weld.
— Longitudinal edge for HFW pipe; 15 mm inside location of future bevel for longitudinal weld.
— Longitudinal edge for other pipe; 50 mm inside location of future bevel for longitudinal weld
Guidance note:
The edge criteria on transverse edge are intended to avoid having signals from base metal to interfere with AUT of girth weld. 150
mm should be sufficient for normal welding and inspection practice. However, the pipe purchaser should consider extending the
edge criteria to take into account other factors, such as weld cut out and rebevelling.
If the pipe body material is inspected on the final pipe, it can be possible to waive the edge criteria for the longitudinal weld.
However, the risk of pipe body imperfections that mask weld defects cannot be neglected, and should be considered when planning
and performing pipe body inspection on the final pipe.
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D.7.3.3 A maximum inspection temperature shall be stated in the procedure. If water is used as couplant,
the maximum inspection temperature shall be 80°C. A higher inspection temperature can be agreed, if it is
demonstrated with practical tests in production conditions that the equipment provides reliable inspection
and acceptable sensitivity. Relevant parameters shall be determined (e.g. water pressure).
If another liquid is used as couplant, the maximum inspection temperature shall be sufficiently below the
boiling temperature of the substance.
Non-contact inspection equipment (e.g. electromagnetic acoustic transducer, EMAT) is allowed, provided the
sensitivity and stability of the equipment has been documented.
D.7.3.4 The inspection coverage in the wall thickness direction shall be stated in the procedure. A noninspected near-surface zone shall be maximum 3.0 mm. Reflectors of size and type required by ISO 10893-9
for sensitivity check shall be incorporated in the calibration standard at the relevant depths.
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Guidance note:
Many UT systems have a near-surface zone where the inspection is less reliable. This goes for both front wall and back wall. The
reason is that signals from imperfections may not be distinguished from the large signals from front wall and back wall. In other
words, it is a question of system resolution, and how well the different signals can be identified and differentiated.
Inspection in the near-surface zone is less reliable, and in principle should be considered as not controlled. The near surface zone
may have imperfections and defects. Still, a non-inspected surface zone may be acceptable;
—
Imperfections at the surface or immediately close to the surface should be identified by visual inspection. Such imperfections
would be associated with surface breaking defects in the slab or other types of defects introduced during rolling.
—
Imperfections in the plate volume can occur, but it is unlikely that they are limited to a zone of only 2-3 mm close to the
surface without being surface-breaking. Defects in the plate volume originate in the slab volume, and most slab defects are
close to the centreline – which will become plate mid-wall and fully inspected by plate AUT. Slab defects not associated with
the centreline should be distributed widely in the slab (e.g. pores, slag, inclusions) and consequently should be distributed also
throughout the plate thickness.
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Table D-12 Ultrasonic testing, acceptance criteria for laminar imperfections
Service
Maximum allowed
imperfection
Non-sour
Area: 1000 mm
2
Minimum
imperfection size to
be considered
Size of reference area
Maximum population
density
2
1000 mm x 1000 mm
10 within reference
area
2
500 mm x 500 mm
5 within reference area
Minimum
imperfection size to
be considered
Size of reference area
Maximum population
density
Length: 10 mm
1000 mm length
3 within reference area
Area: 300 mm
Length: 35 mm
Width: 8 mm
Sour
Area: 500 mm
2
Area: 150 mm
Length: 15 mm
Width: 8 mm
Acceptance criteria for edges
Service
All
Maximum allowed
imperfection
Area: 100 mm2 Length: 20
mm
Notes:
1) Two or more adjacent imperfections shall be considered as one imperfection if they are separated by less than the
smaller dimension of either indication.
2) The population density shall be the number of imperfections smaller than the maximum allowed and larger than the
minimum imperfection size to be considered
3) The reference area when the plate/coil width is less than one side of the square reference area shall be 1.00 m2 for
non-sour and 0.25 m2 for sour service.
4) The width of an imperfection is the dimension transverse to the rolling direction.
D.7.4 Ultrasonic testing of bonding in corrosion resistance alloy clad plate
D.7.4.1 When performed, ultrasonic testing for lack of bonding shall be in accordance with ISO 10893-9, and
with additional requirements as stated in this section.
D.7.4.2 The reference standard reflector shall be located within ±0.5 mm of the bonding interface.
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The inspection report from lamination control of both CRA and C-Mn steel shall be available. If there are
acceptable laminations in the plates, they can mask unacceptable lack of bonding. The manufacturer shall
have alternative inspection methods to inspect such areas.
D.7.4.3 During calibration check in production conditions the signal from the reference reflector shall be at
least 6 dB stronger than the signal from the interface between CRA and C-Mn steel material.
D.7.4.4 The acceptance criteria for plate body are:
— No single unbonded area shall exceed 25 mm in its longest dimension.
— Total unbonded area shall not exceed 1% of the total cladded surface area.
D.7.4.5 The acceptance criteria for plate edge are:
— No area with lack of bonding is allowed (i.e. no signal larger than the reference reflector).
The edge is the material extending 50 mm from the location of future weld preparations (both longitudinal
and transverse welds).
Guidance note:
For plate edge, no lack of bonding is allowed. According to ISO 10893-9, the system sensitivity is defined by 6 mm flat-bottom
hole. In practice, this means that lack of bonding smaller than 6 mm may be accepted.
When welding clad material, it is important to ensure the integrity of the CRA layer – both for longitudinal weld and girth weld. The
weld inspection may have very strict requirements. Consequently imperfections that are acceptable based on 6 mm FBH sensitivity
level may be large compared to allowable weld defects – and could mask weld inspection. In such cases it should be considered to
introduce stricter requirements to plate inspection.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
D.7.5 Alternative test methods
D.7.5.1 If agreed alternative methods of testing may be acceptable, if the alternative test method is
documented as required in [D.8.4.2] and the alternative test method is demonstrated to give at least the
same sensitivity and capability in detection of imperfections.
D.7.5.2 The demonstration of the alternative test method shall be based on the principles given in [D.6] and
using samples of plate similar to those ordered. The plates shall contain a representative and agreed size
range of natural and/or artificial defects of types that are typical for the manufacturing process in question.
D.7.6 Visual examination of plate and coil
D.7.6.1 Visual examination shall be carried out in a sufficiently illuminated area, minimum 350 lux on the
area of interest is recommended. If required to obtain good contrast and relief effect between imperfections
and background additional light sources shall be used.
D.7.6.2 For direct examination the access should permit placing the eye within 600 mm of the surface to be
examined and at an angle of not less than approximately 30°.
Guidance note:
The production process of coil can make it difficult or impossible to perform visual inspection. The coil can be too hot, moving too
fast and not be sufficiently clean to be able to visually inspect. In such cases the visual inspection, if required, shall be performed
at a later stage of the pipe production process.
The final visual inspection for pipe is after completion of all pipe production activities. The visual inspection at the plate/coil stage
is preliminary, however still important to ensure the integrity of the final pipes.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
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D.7.6.3 Relevant tools, gauges, measuring equipment and other devices shall be available at the place of
examination.
D.7.6.4 The material to be examined shall be cleaned to remove all scale and processing compounds prior to
examination. The cleaning process shall not injure the surface finish or mask possible imperfections.
D.7.7 Acceptance criteria and disposition of surface imperfections
D.7.7.1 Plate/coil shall meet the acceptance criteria specified by the pipe mill. The acceptance criteria shall
under no circumstance be less stringent than the applicable requirements for pipe, as specified in [D.8.5].
D.7.7.2 Imperfections shall be dressed out by grinding. Ground areas shall blend smoothly into the
surrounding material. Complete removal of defects shall be verified by local visual inspection and shall be
supplemented with a suitable surface inspection method. The remaining wall thickness in the ground area
shall be checked by ultrasonic wall thickness measurements to verify that the thickness of the remaining
material is more than the specified minimum. Imperfections that encroach on the minimum permissible wall
thickness after grinding shall be classified as defects.
D.8 Non-destructive testing of linepipe at pipe mills
D.8.1 General
D.8.1.1 The extent of non-destructive testing during manufacture of linepipe shall be as required in [7.6].
D.8.1.2 The types of testing required are defined as:
— ultrasonic testing
— surface imperfection testing
— radiographic testing.
Whenever the choice of non-destructive testing methods is optional, this is indicated in this subsection.
D.8.1.3 All NDT shall be performed according to documented procedures that, as a minimum, give
information on the following aspects:
—
—
—
—
—
—
—
—
—
—
—
—
—
applicable standard(s) or recommended practice(s)
welding method (when relevant)
joint geometry and dimensions (when relevant)
material
NDT method
technique
equipment, main and auxiliary
consumables when relevant (including brand name)
coverage calculation supplemented with sketches
sensitivity
calibration references and technique
trigger or alarm settings
for ultrasonic testing equipment the procedure shall describe the method for setting and checking the lack
of coupling alarm
— assessment of imperfections
— method for demonstrating compliance of equipment with the assumptions in the procedure
— reporting and documentation of results
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— assessment of imperfections, including decision tree corresponding with internal organization.
D.8.1.4 Personnel performing NDT shall be qualified according to [D.1.5].
D.8.1.5 All NDT for final acceptance of pipe shall be performed after completion of any cold expansion and
heat treatment operations.
For seamless pipe, the NDT for final acceptance may be performed prior to cropping, bevelling and end
sizing. Cold straightening and cold sizing of seamless pipe ends imposing a maximum strain of 1.5% may be
performed after surface testing of the pipe body but prior to testing of pipe ends.
All NDT for in-house purposes may be performed at any time at the manufacturer's discretion.
D.8.1.6 If NDT of plate in accordance with [D.7] is performed at the plate mill, ultrasonic testing for laminar
imperfections may be omitted at the pipe mill.
D.8.1.7 Reporting of NDT shall be according to the requirements of the applicable ISO standard unless
otherwise agreed.
D.8.2 Suspect pipe
D.8.2.1 In all cases when pipe inspection results in the automated NDT system is giving signals equal to or
greater than the threshold level or when surface imperfections are disclosed by visual examination, the pipe
shall be deemed suspect.
Suspect pipe can be dealt with according to one of the following options:
— the suspect pipe can be re-inspected using the automated NDT equipment in the static mode. Pipes
passing these tests are deemed acceptable
— the suspect area of the pipe can be re-tested by manual NDT using the same NDT method and sensitivity
as the automated NDT, and using appropriate techniques. Pipes passing these tests are deemed
acceptable
— the suspect area of welds, except HFW welds, can be radiographed to determine if the indication is caused
by slag or porosity type indications. Pipes meeting the requirements of ISO 10893-6 or respectively ISO
10893-7 are deemed acceptable
— defective welds, except HFW welds, can be repaired by welding according to [D.8.3.1] through [D.8.3.7]
— defects can be removed by grinding according to [D.8.3.8]
— the suspect area can be cut off if the minimum specified length is met after cutting
— the pipe can be scrapped.
If the suspect area is cut off, then all NDT requirements pertaining to pipe ends shall be performed on the
new pipe end.
D.8.3 Repair of suspect pipe
Repair welding
D.8.3.1 Repair welding of pipe body or repair welding of welds in HFW pipe is not permitted.
D.8.3.2 Repair welding of cracks is not permitted unless the cause of cracking has been established not to be
a systematic welding error. (If there is a crack in the weld the pipe is per definition considered rejected.) This
means a technical evaluation of the cause of cracking shall be performed. If it can be demonstrated that the
crack is a one off situation, repair welding may be performed subject to agreement)
D.8.3.3 Repair welding shall be performed according to qualified repair welding procedures. Each repair shall
be performed with a minimum of two passes over a length not less than 50 mm.
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D.8.3.4 The total length of weld repair in any single pipe shall not exceed 5% of the weld length.
D.8.3.5 Weld defects separated by less than 100 mm shall be repaired as a single continuous repair.
D.8.3.6 Re-inspection of repair welds shall be 100% visual examination and 100% ultrasonic and/or 100%
radiographic testing as required for the original weld.
D.8.3.7 Acceptance criteria for weld repairs shall be as for the original weld.
Repair of welds by grinding
D.8.3.8 Surface defects may be dressed out by cosmetic grinding. Ground areas shall blend smoothly into
the surrounding material. Complete removal of defects shall be verified by local visual inspection and shall
be supplemented with a suitable surface inspection method. The remaining wall thickness in the ground area
shall be checked by ultrasonic wall thickness measurements to verify that the thickness of the remaining
material is more than the specified minimum. Imperfections that encroach on the minimum permissible wall
thickness and/or weld thickness shall be classified as defects.
Repair of pipe body by grinding
D.8.3.9 Repair of pipe body by grinding shall be performed according to [D.8.5.25] through [D.8.5.27].
Disposition of pipe containing defects
D.8.3.10 Disposition of pipe containing defects after repair shall be according to [D.8.5.28].
D.8.4 General requirements for automated non-destructive testing systems
Alternative methods of testing
D.8.4.1 Subject to agreement, alternative methods of testing may be accepted if the alternative test method
is documented as required in [D.8.4.2] and the alternative test method is demonstrated to give at least the
same sensitivity and capability in detection of imperfections.
D.8.4.2 The demonstration of the alternative test method shall be based upon the principles given in [D.6]
and using sample lengths of pipe similar to those ordered. The pipes shall contain a representative and
agreed size range of natural and/or artificial defects of types that are typical for the manufacturing process in
question.
System calibration
D.8.4.3 All automated NDT systems shall have a full system calibration with intervals not exceeding 12
months. Documentation shall be available.
Documentation of system capabilities
D.8.4.4 Documentation of automated NDT systems shall be available to demonstrate that the systems
are capable of detecting the reference indicators used to establish the specified test sensitivity. The
documentation shall, as a minimum cover:
—
—
—
—
—
—
—
NDT system operating procedures
capability for the intended wall thickness
capability for the intended material
repeatability
detection of defects typical for the manufacturing process with the equipment in question
threshold level setting parameters
dynamic test data demonstrating the systems capability under production test conditions.
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Reference standards for ultrasonic and electromagnetic inspection
D.8.4.5 Reference standards shall meet the requirements of the applicable ISO standard and the
requirements given in this appendix.
D.8.4.6 The reference standard shall be a length of pipe with the same outside diameter and wall thickness
tolerances and with similar acoustic properties as the pipe tested during production. For welded pipe the
reference standard shall contain a weld typical for the production weld to be tested.
D.8.4.7 Reference standards may be of any convenient length as decided by the manufacturer.
D.8.4.8 Reference standards shall contain reference indicators as required by this appendix for the pipe to be
tested.
D.8.4.9 Verification of the dimensions and shape of all reference indicators shall be performed according to
a documented procedure. Documentation shall be available. All reference standards shall be marked with an
identification that relates to the specific application of each reference standard.
Validation of length of pipe tested
D.8.4.10 When automated non-destructive testing equipment is used, a short area at both pipe ends will
normally not be tested. A sample pipe shall be fitted with one ᴓ 3.0 mm through drilled hole at the weld
centerline at each end. The distance from the pipe end to the hole shall be equal to the length not covered
by the automated testing equipment during production testing. Prior to start of production the pipe shall
be passed through the ultrasonic testing equipment at the operational scanning velocity. For acceptance of
the equipment, both holes shall be detected by all probes/focal law. These holes can be introduced in the
reference block. If ᴓ 3.0 mm through drilled hole at the weld centerline at each end is unsuitable to register
at scanning sensitivity for the technique introduced to the inspection Set Up, alternative reference reflectors
shall be proposed and agreed on. For inspection of seamless pipes, a similar test shall be performed with
adequate reflectors included at pipe ends.
Scanning velocity
D.8.4.11 The scanning velocity shall be selectable. The scanning velocity shall be set low enough so that
the length between the activation of each probe (spatial resolution) is sufficiently short, i.e. the distance the
probe travels while inactive, shall be significantly less than the maximum length of allowable imperfections.
D.8.4.12 The scanning velocity VC for inspection of longitudinal welds shall be determined according to:
Where WC is the narrowest - 6 dB effective beam width at the appropriate distance of all probes within the
array and PRF is the effective pulse repetition frequency per probe.
D.8.4.13 The circumferential scanning velocity for inspection of seamless pipe and helical welds shall be
decided depending on effective pulse spacing (pulse density) and on circumferential scanning speed and
helical pitch. The effective pulse spacing (EPS) is specified as follows:
— EPS = circumferential scanning speed/PRF
— EPS shall not exceed 1 mm/pulse.
— The helical pitch (mm/revolution) shall not exceed the narrowest - 6 dB effective beam width of all probes
within the array.
Lack of coupling
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D.8.4.14 Automated ultrasonic testing systems shall incorporate a system for detection of lack of coupling.
The settings for lack of coupling alarm and check of the settings shall be described in the manufacturer’s
written procedure.
Initial sensitivity and threshold settings (calibration)
D.8.4.15 The sensitivity and threshold settings shall be established according to a documented procedure.
The system shall be optimised in the static mode. When the settings are optimised, the relevant parameters
shall be recorded and the reference standard shall be passed 3 times through the equipment at the
operational velocity. Any change in settings required to maintain the static mode settings shall be recorded
as an average of the 3 runs. For acceptance of the settings, all reference reflectors need to be detected at or
above the threshold.
D.8.4.16 During production testing the relative speed of movement between the pipe and the test assembly
shall not exceed that used for the sensitivity and/or alarm settings during dynamic calibration.
Verification of sensitivity and threshold settings (calibration)
D.8.4.17 The sensitivity and/or alarm settings shall be verified every fourth hour or once every 10 pipes
tested, whichever is the longer period, and:
— at the start and end of each shift
— at any change of equipment operator (for continuous shifts the end and start verification can be
combined)
— whenever a malfunction of the equipment is suspected.
The verification frequency when manufacturing HFW pipe from coil shall be agreed upon. As a minimum the
frequency shall be at the beginning and end of an inspection and at any stops in production.
Resetting of sensitivity and threshold settings (recalibration)
D.8.4.18 Resetting of sensitivity and threshold settings shall be performed whenever:
— the standard reflectors do not trigger the alarm during verification of sensitivity and threshold settings
— a change of component affecting the sensitivity and/or alarm setting is made in the system
— the verification of sensitivity and/or alarm settings fails to meet the requirements for the particular
equipment.
For re-setting of sensitivity and threshold settings during production the settings shall be optimised in the
static mode. When the settings have been optimised, the reference standard shall be passed once through
the equipment at the operational velocity. Any change in settings required to maintain the static mode
settings shall be recorded. For acceptance of the settings, all reference reflectors need to be detected at or
above the threshold.
Retesting of pipes
D.8.4.19 If the verification of sensitivity and threshold settings fails to meet the requirements for the
particular equipment, all pipes inspected since the previous successful verification shall be retested.
Specific requirements for ultrasonic testing equipment for welds
D.8.4.20 The equipment shall be capable of inspecting the entire thickness of the weld seam.
D.8.4.21 Before starting production testing, the range scale and angle of all probes shall be demonstrated to
comply with the documented procedure.
D.8.4.22 Equipment for testing of welds shall have a weld tracking system. The system should be capable of
tracking the weld centreline with an accuracy of ± 2 mm or better. For systems not meeting this requirement
it shall be documented that:
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— the sensitivity during production testing will not be affected by the lower accuracy of the tracking system
— that the lower accuracy is compensated by system sensitivity and gate settings.
D.8.4.23 The gates shall be set wide enough to cover 3 mm of the base material outside the fusion line and
to compensate for:
— the tolerances of weld tracking system
— variations in the width of external and internal caps
— offsets between the external and internal weld bead.
Ultrasonic testing of CRA pipes and welds with CRA weld deposits
D.8.4.24 Ultrasonic testing of welds with CRA (duplex, other stainless steels and nickel alloy steel) weld
deposits will in order to achieve an adequate detection of imperfections, normally require that special
reference blocks and probes are used for testing of these materials.
D.8.4.25 Angle probes for duplex stainless steel and austenitic steels shall be twin crystal (transmitter/
receiver) compression-wave probes. Angle compression wave probes shall and can only be used for scanning
without skipping and creep wave probes shall therefore be used for detection of sub-surface defects close to
the scanning surface.
D.8.4.26 Reference blocks for duplex stainless steel and austenitic steels materials and the weld deposits
shall have a specific location and type of reference reflectors in general compliance with [D.2.4]. Surface
notches will not be suitable due to the mode conversions at base material and a surface notch. This will result
in multiple echoes with different arrival time appearing from the same notch. The actual reflection from the
reflector will be weak and distinguishing this echo from other signals will often not be possible.
D.8.4.27 Specific ultrasonic testing procedures shall be developed for this testing. The procedures shall be
developed considering the requirements [D.2.4] and addressing the specific features and characteristics of
the equipment to be used.
D.8.4.28 It is recognised that not all equipment will be adaptable to meet the requirements above.
D.8.4.29 Low frequency shear wave angle probes may be used for duplex stainless steel and austenitic
steels instead of the angle compression wave probes, provided it is verified on reference blocks made in
accordance with [D.2.4] that it is possible to obtain a DAC with shear wave angle probe(s) that is comparable
to a DAC obtained from angle compression-wave probes. The shear wave angle probes used for this
verification shall be identical to the probes used in the production testing equipment.
D.8.4.30 If it is not possible to demonstrate adequate performance of low frequency shear wave angle
probes for ultrasonic testing of duplex stainless steel and austenitic steels, other methods or combination of
methods shall be used and the adequacy of the method(s) demonstrated.
D.8.4.31 Notches and through drilled holes are not considered a suitable reflector for compression wave
angle probes due to the mode conversion and unpredictable arrival times of mode converted signals. When
compression wave angle probes are used, other types of reflectors shall be used and the acceptance criteria
specified accordingly.
Specific requirements for radiographic testing
D.8.4.32 Radiographic testing shall be performed in accordance with ISO 10893-6, image class B using wire
type image quality indicators (IQI) in accordance with ISO 19232-1 or step/hole type on ISO 19232-2.
D.8.4.33 Digital radiographic testing techniques in accordance with ISO 10893-7 can be used provided the
equipment has been demonstrated, in accordance with [D.6], to give sensitivity and detection equivalent to
conventional x-ray according to ISO 10893-6.
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D.8.4.34 If radioscopic testing techniques are used, the quality of the ray image has to be verified as
required in [D.8.4.17].
D.8.5 Visual examination and residual magnetism
General
D.8.5.1 Visual examination shall be carried out in a sufficiently illuminated area; minimum 1000 lx, If
required additional light sources shall be used to obtain good contrast and relief effect between imperfections
and background.
D.8.5.2 In accordance with Table 7-16, each linepipe shall be subject to 100% visual inspection. This implies
100% visual inspection of the outside of the pipe body. The interior of the pipe shall be inspected from both
ends as far as access permits. The interior of duplex stainless steel and clad/lined material should be 100%
visually inspected.
D.8.5.3 A sufficient amount of tools, gauges, measuring equipment and other devices shall be available at
the place of examination.
D.8.5.4 The pipes to be examined shall be cleaned to remove loose scale and processing compounds that
may interfere with the examination. The cleaning process shall not affect the surface finish or mask possible
imperfections.
D.8.5.5 Subject to agreement, alternative methods of testing may be accepted. It shall be demonstrated
that the alternative test method give at least the same sensitivity and capability in detection of
imperfections. The demonstration of the alternative test method shall be based upon the principles given in
[D.6] on similar pipes to those ordered. The pipes shall contain a representative and agreed size range of
natural and/or artificial defects of types that are typical for the manufacturing process in question.
Visual examination of all linepipe
D.8.5.6 End preparation such as bevelling shall meet the specified requirements.
D.8.5.7 The internal weld bead shall be removed by grinding for a distance of at least 100 mm from each
pipe end. The transition between base material and weld metal shall be smooth and the height of the
remaining weld bead shall not extend above the adjacent pipe surface by more than 0.5 mm.
D.8.5.8 If specified, the external weld bead shall be removed by grinding for a distance of at least 250 mm
from each pipe end. The transition between base material and weld metal shall be smooth and the height of
the remaining weld beads shall not extend above the adjacent pipe surface by more than 0.5 mm.
Visual examination of welds in linepipe
D.8.5.9 Each linepipe weld shall be subject to 100% visual examination in accordance with ISO 17637. For
C-Mn steel linepipe with internal diameter (ID) ≥ 610, the internal weld shall be 100% visually inspected.
The internal weld of C-Mn linepipe with ID < 610 mm shall be inspected from both ends as far as access
permits.
D.8.5.10 The internal weld and adjacent surfaces in duplex stainless steel, CRA and clad linepipe shall be
inspected full length. If necessary, the inspection of the internal weld shall be assisted by a boroscope, video
endoscope or similar equipment.
D.8.5.11 Welds shall meet the requirements of Table D-4.
D.8.5.12 Line pipe containing welds not meeting the requirements above shall be classified as suspect pipe
according to [D.8.2], and treated according to [D.8.3].
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Surface conditions, imperfections and defects
D.8.5.13 The surface finish produced by the manufacturing process shall be such that surface defects can be
detected by visual inspection.
D.8.5.14 All pipes shall be free from defects in the finished condition. The manufacturer shall take adequate
precautions to prevent pipe damage and minimise the presence of imperfections.
D.8.5.15 Cracks, sweats or leaks are not acceptable and shall be classified as defects.
D.8.5.16 Surface imperfections evident by visual inspection shall be investigated, classified and treated as
according to [D.8.5.17] to [D.8.5.22]. [D.8.5.19] applies to surface imperfections at the internal surface of
clad or lined pipes.
D.8.5.17 Imperfections with depth ≤ 5% of the specified wall thickness, or 0.5 mm, whichever is greater,
but maximum 0.7 mm for t ≤ 25 mm, and maximum 1.0 mm for t > 25 mm, and which do not encroach
upon the specified minimum wall thickness, shall be classified as acceptable imperfections. The imperfections
may remain in the pipe or be dressed out by cosmetic grinding.
D.8.5.18 Imperfections with depth larger than stated in [D.8.5.17], and which do not encroach upon the
specified minimum wall thickness, shall be classified as dressable defects and shall either be removed by
grinding in accordance with [D.8.5.25] or treated in accordance with [D.8.5.28], as appropriate.
D.8.5.19 For the internal surface of clad or lined pipes the following applies: Imperfections with depth
≤ 0.5 mm, and which do not encroach upon the specified minimum wall thickness, shall be classified as
acceptable imperfections. The imperfections may remain in the pipe or be dressed out by cosmetic grinding.
Imperfections with larger depth, and which do not encroach upon the specified minimum wall thickness, shall
be classified as dressable defects and shall either be removed by grinding in accordance with [D.8.5.25] or
treated in accordance with [D.8.5.28], as appropriate.
D.8.5.20 Imperfections which encroach upon the specified minimum wall thickness shall be classified as
defects.
D.8.5.21 Two or more adjacent imperfections shall be considered as one imperfection if they are separated
by less than the smaller dimension of either indication.
D.8.5.22 Imperfections with depth according to [D.8.5.17] or [D.8.5.19] of which the depth can not be
assessed by suitable gauges or alternative means, shall either be removed by grinding in accordance with
[D.8.5.25] or treated in accordance with [D.8.5.28], as appropriate.
Dents
D.8.5.23 For dents without any cold formed notches and sharp bottom gouges, the length in any direction
shall be ≤ 0.5 D and the depth, measured as the gap between the extreme point of the dent and the
prolongation of the normal contour of the pipe, shall not exceed 6.4 mm.
— For dents with cold-formed notches and sharp bottom gouges with depth according to [D.8.5.17] the
depth of dents shall not exceed 3.2 mm.
— Dents > 1 mm are not acceptable at the pipe ends, i.e. within a length of 100 mm at each of the pipe
extremities.
— Dents exceeding these dimensions shall be classified as defects.
Hard spots
D.8.5.24 Hard spots, as identified e.g. due to irregularities in the pipe curvature of cold-formed welded
linepipe, shall be investigated to determine the hardness and dimensions of the area.
For linepipe intended for non sour service the hardness shall not exceed:
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— 300 HV10 for C-Mn steels
— the values given in Table 7-11, for the material in question.
For linepipe intended for sour service (Supplementary requirement S) the hardness shall not exceed:
— 250 HV10 C-Mn steel unless a higher hardness has been qualified according to [6.2.2.2] and [B.3.4].
— for other steels, maximum allowable hardness according to ISO 15156-3.
Hard spots outside the hardness requirements for the applicable material larger than 50 mm in any direction
and within 100 mm of the pipe ends regardless of size shall be classified as defects.
Grinding
D.8.5.25 Imperfections or defects according to [D.8.5.18] or [D.8.5.19] may be dressed-out by grinding.
Ground areas shall blend smoothly into the surrounding material. Complete removal of defects shall be
verified by local visual inspection and shall be supplemented with a suitable surface inspection method. The
remaining wall thickness in the ground area shall be checked by ultrasonic wall thickness measurements to
verify that the thickness of the remaining material is more than the specified minimum. If the defect was
identified by automated equipment, re-inspection of repaired pipe shall be performed by the same automated
equipment.
D.8.5.26 The sum of the ground area shall not exceed 10% of the sum of the external and internal surface
area of each pipe. Ground areas which have been smoothly blended into the surrounding material and
classified as cosmetic grinding shall not be counted in the calculation.
D.8.5.27 Full length machining of pipes is acceptable if machining is performed according to a qualified
procedure that ensures freedom from circumferential grooves or other defects with depth > 0.5 mm.
[D.8.5.26] does not apply to pipe that are machined full length.
Disposition of pipe containing defects
D.8.5.28 Linepipe containing defects shall be rejected or the area containing defects can be cut off. If pipes
are cut, the minimum specified length shall be met after cutting and all NDT pertaining to pipe ends shall be
performed on the new pipe end.
Residual magnetism
D.8.5.29 The longitudinal magnetic field shall be measured on pipe with D ≥ 168.3 mm and all smaller pipes
that are inspected full length by magnetic methods or are handled by magnetic equipment prior to loading.
— The measurements shall be taken on the root face or square cut face of finished pipe. Measurements
made on pipe in stacks are not considered valid.
— Measurements shall be made on each end of a pipe, for 5% of the pipes produced but at least once per
4 hr per operating shift using a Hall-effect gauss-meter or other type of calibrated instrument. In case of
dispute, measurements made with a Hall-effect gauss-meter shall govern. Measurements shall be made in
accordance with a written procedure demonstrated to produce accurate results.
— Pipe magnetism shall be measured subsequent to any inspection that uses a magnetic field, prior to
loading for shipment from the pipe mill.
— Four readings shall be taken 90° apart around the circumference of each end of the pipe.
D.8.5.30 The average of the four readings shall be less or equal to 2.0 mT (20 Gauss), and no single reading
shall exceed 2.5 mT (25 Gauss). Any pipe that does not meet this requirement shall be considered defective.
D.8.5.31 All pipes produced between the defective pipe and the last acceptable pipe shall be individually
measured unless the provisions of [D.8.5.30] can be applied.
D.8.5.32 If the pipe production sequence is documented, pipe may be measured in reverse sequence,
beginning with the pipe produced immediately prior to the defective pipe, until at least three consecutively
produced pipes meet the requirements.
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— Pipe produced prior to these three acceptable pipes need not be measured
— Pipe produced after the defective pipe shall be measured individually until at least three consecutive pipes
meet the requirements.
D.8.5.33 All defective pipe shall be de-magnetized full length, and then their magnetism shall be remeasured until at least three consecutive pipes meet the requirements of [D.8.5.30].
D.8.5.34 For pipe handled with electromagnetic equipment after measurement of magnetism, such handling
shall be performed in a manner demonstrated not to cause residual magnetism exceeding the acceptance
criteria in [D.8.5.30].
D.8.5.35 The requirements for residual magnetism shall apply only to testing within the pipe mill since the
residual magnetism in pipe may be affected by procedures and conditions imposed on the pipe during and
after shipment.
D.8.6 Non-destructive testing of pipe ends not tested by automated NDT
equipment
Untested pipe ends
D.8.6.1 When automated non-destructive testing equipment is used, a short area at both pipe ends will
normally not be tested (see [D.8.4.10]). Either the untested area of the pipe shall be cut off or the ends
subjected to manual or automated NDT to the same extent as required for the full length of pipe
D.8.6.2 The methods, sensitivity and acceptance criteria for testing of untested ends shall be the same as
used for retesting of pipes having signals equal to or greater than the threshold level from the automated
non-destructive testing equipment.
D.8.6.3 The manufacturer shall prior to start of production present for acceptance the proposed extent,
methods, sensitivity and acceptance criteria for testing of untested ends with reference to applicable
procedures. Otherwise the manufacturer shall demonstrate by using suitable reference indicators, that the
examination system is suitable for an automated testing up to the pipe end
D.8.7 Non-destructive testing of pipe ends
D.8.7.1 These requirements apply to both seamless and welded pipe. Pipes not meeting the acceptance
criteria below shall be deemed as suspect pipe according to [D.8.2] and shall be treated according to [D.8.3].
D.8.7.2 Both ends of each pipe shall be tested for laminar imperfections in accordance with ISO 10893-8
and the additional requirements in [D.8.4] over a band at least 50 mm inside the location of future welding
preparations for girth welds.
D.8.7.3 If additional non-destructive testing is specified by the purchaser, the width of the band should be:
— at least 150 mm inside the location of future welding preparations for girth welds if automated ultrasonic
testing of girth welds during installation will be performed
— at least 100 mm inside the location of future welding preparations for girth welds if allowance for rebevelling of pipe shall be included.
D.8.7.4 Acceptance criteria are:
— according to Table D-12
— [D.7.4.4] and [D.7.4.5] for clad pipe.
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D.8.7.5 Magnetic particle testing or eddy current testing, manual or automated, of both end faces or
bevels of each pipe in ferromagnetic steel for the detection of laminar imperfections shall be performed in
accordance with the requirements in [D.8.4] and:
— ISO 10893-5 for magnetic particle testing
— ISO 10893-2 for eddy current testing.
D.8.7.6 Liquid penetrant or eddy current testing, manual or automated, of the end face or bevel of each pipe
in non-ferromagnetic steel for the detection of laminar imperfections shall be performed in accordance with
the requirements in [D.8.4] and:
— ISO 10893-4 for liquid penetrant testing
— ISO 10893-2 for eddy current testing.
D.8.7.7 The acceptance criterion is:
— Imperfections longer than 6 mm in the circumferential direction are not permitted.
Guidance note:
For clad pipes made from explosion welded clad plates; indications from process related melt pockets within the bond zone of
explosion welded material are acceptable. It is acknowledged that these indications do not indicate lamination or a degrade
bond between backing and clad material. Lamination and disbonding imperfections shall be assessed according to the
acceptance criteria above.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
D.8.8 Non-destructive testing of seamless pipe
Pipe ends
D.8.8.1 Pipe ends shall be tested as required by [D.8.6] and [D.8.7].
Ultrasonic inspection for laminar imperfections in the pipe body
D.8.8.2 Ultrasonic inspection of the pipe body shall be performed in accordance with the requirements in
[D.8.4] and ISO 10893-8 amended as follows:
— the distance between adjacent scanning tracks shall be sufficiently small to ensure detection of the
minimum allowed imperfection size.
D.8.8.3 The acceptance criteria are:
— according to Table D-12
Ultrasonic inspection for longitudinal imperfections in the pipe body
D.8.8.4 Ultrasonic inspection of the pipe body shall be performed in accordance with the requirements
in [D.8.4] and ISO 10893-10. The probe angles shall be chosen to obtain the best test result for the wall
thickness/diameter ratio of the pipe to be tested.For pipes in CRA materials it shall be verified that the
presence of any possible coarse, anisotropic zones will not impede the testing, see [D.8.4.24] through
[D.8.4.31].
D.8.8.5 The acceptance criterion is:
— Acceptance level U2/C according to ISO 10893-10.
Ultrasonic inspection for transverse imperfections in the pipe body
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D.8.8.6 Ultrasonic inspection of the pipe body shall be performed in accordance with the requirements
in [D.8.4] and ISO 10893-10. The probe angles shall be chosen to obtain the best test result for the wall
thickness/diameter ratio of the pipe to be tested.
For pipes in CRA materials it shall be verified that the presence of any possible coarse, anisotropic zones will
not impede the testing, see [D.8.4.24] through [D.8.4.31].
D.8.8.7 The acceptance criterion is:
— Acceptance level U2/C according to ISO 10893-10.
Ultrasonic thickness testing of the pipe body
D.8.8.8 Ultrasonic thickness testing of the pipe body shall be performed in accordance with the requirements
in [D.8.4] and ISO 10893-12.
D.8.8.9 The acceptance criterion is:
— The specified maximum and minimum wall thickness shall be met.
Surface testing for longitudinal and transverse imperfections in the pipe body of ferromagnetic pipe
D.8.8.10 Testing of ferromagnetic seamless pipe for the detection of longitudinal and transverse surface
imperfections shall be performed in accordance with the requirements in [D.8.4] and one of the following
standards:
— ISO 10893-2 (eddy current testing)
— ISO 10893-3 (flux leakage testing)
— ISO 10893-5 (magnetic particle testing).
D.8.8.11 For detection of internal indications ISO 10893-2 or ISO 10893-3 shall be preferred provided
adequate signal amplitudes from the internal surface reflector are documented and used for sensitivity
setting.
D.8.8.12 The acceptance criteria are:
— ISO 10893-2: Alarm level/acceptance level E2
— ISO 10893-3: Alarm level/acceptance level F2
— ISO 10893-5: Alarm level/acceptance level Table 2, M2.
Surface testing for longitudinal and transverse indications in pipe body of non-magnetic pipe
D.8.8.13 Testing of non-magnetic seamless pipe for the detection of longitudinal and transverse surface
imperfections shall be performed in accordance with the requirements in [D.8.4] and one of the following
standards:
— ISO 10893-2 (eddy current testing)
— ISO 10893-4 (liquid penetrant testing).
D.8.8.14 For detection of internal indications ISO 10893-2 shall be preferred provided adequate signal
amplitudes from the internal surface reflector are documented and used for sensitivity setting.
D.8.8.15 The acceptance criteria are:
— ISO 10893-2: Alarm level/acceptance level E2
— ISO 10893-4: Alarm level/acceptance level P2.
Suspect pipe
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D.8.8.16 Pipes not meeting the acceptance criteria above shall be deemed as suspect pipe according to
[D.8.2] and shall be treated according to [D.8.3].
D.8.9 Non-destructive testing of high frequency welding pipe
Pipe ends
D.8.9.1 Pipe ends shall be tested as required by [D.8.6] and [D.8.7]
Ultrasonic testing of the pipe body for detection of laminar imperfections
D.8.9.2 Ultrasonic testing of the pipe body for detection of laminar imperfections need not be performed at
the pipe mill if testing of the coil edges was performed at the coil mill according to [D.7].
D.8.9.3 If performed at the pipe mill, ultrasonic testing of the pipe body for detection of laminar
imperfections shall be performed in accordance with the requirements in [D.8.4] and ISO 10893-8 amended
as follows:
— the distance between adjacent scanning tracks shall be sufficiently small to ensure detection of the
minimum allowed imperfection size.
D.8.9.4 Acceptance criteria are:
— according to Table D-12.
Ultrasonic testing of the area adjacent to the weld seam for detection of laminar imperfections
D.8.9.5 Ultrasonic testing of the area adjacent to the weld seam body for detection of laminar imperfections
shall be performed at the pipe mill if the strip is made by splitting of coil. If the strip is not made by splitting
of coil and is tested for laminar imperfections at the coil mill according to [D.7], no testing for detection of
laminar imperfections need to be performed at the pipe mill
D.8.9.6 If performed at the pipe mill, the testing shall be performed according to the requirements in [D.8.4]
and ISO 10893-8.
D.8.9.7 Acceptance criteria are:
— according to Table D-12.
Ultrasonic testing for longitudinal imperfections in the weld seam
D.8.9.8 Ultrasonic testing of the full length of the weld seam of HFW pipe for the detection of longitudinal
imperfections shall be performed in accordance with the requirements in [D.8.4] and ISO 10893-11 with
modifications as described in [D.8.9.9] through [D.8.9.18].
D.8.9.9 Accurate weld tracking with a tolerance ± 2 mm with respect to the centreline of the weld is
essential due to the width of the weld.
D.8.9.10 The reference standard shall contain a typical weld, with the external flash removed and including
tracks resulting from removal of the internal flash.
The reference reflectors shall be:
— external and internal reference notches located parallel to and in the centre of the weld. The notches
shall be “N” type with a depth of 5% of the wall thickness notches with a depth of minimum 0.3 mm and
maximum 1.2 mm.
D.8.9.11 One or more of the following probe configurations shall be used:
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— Single pulse echo probes shall be selected such as the angle of incidence is as perpendicular to the radial
centreline of the weld as possible.
— Tandem probes on each side of the weld with the angle of incidence as perpendicular to the radial
centreline of the weld as possible.
— Probes alternating as transmitter-receiver with the angle of incidence as perpendicular to the radial
centreline of the weld as possible.
The probe configuration shall provide a sufficient number of probes to cover the entire wall thickness from
both sides of the weld.
D.8.9.12 The equipment shall include devices for weld tracking/centering and provide checking of adequate
coupling for all probes.
D.8.9.13 Each probe shall be calibrated against the reference reflector located in the area of the weld to be
covered by that probe.
D.8.9.14 For single pulse echo probes and tandem probes the threshold settings shall be as follows:
— If the testing is performed with one probe pair covering the entire wall thickness, the response from the
intersections between the reference notches and the external and internal pipe surface shall optimised
and the threshold level set at 80% of full screen height of the lowest of the obtained responses.
— If the testing is performed with probe pairs each covering a part of the wall thickness, the threshold level
shall be set at 80% of full screen height.
D.8.9.15 For probes alternating as transmitter-receiver the threshold level shall be set corresponding to a
loss of 75% of the transmitted signal.
D.8.9.16 For each probe, the following shall be recorded:
—
—
—
—
type, frequency, angle and dimension
the distance from the index point to the weld centreline
the angle between the ultrasound direction and the major pipe axis.
amplitudes and gain settings.
D.8.9.17 Gates shall be set such that reflections from the tracks resulting from removal of the internal
flash are avoided but sufficiently wide to ensure that the tolerances in the weld tracking system will result in
responses from indications inside the weld and the HAZ.
D.8.9.18 The settings for lack of coupling alarm shall be set and checked.
D.8.9.19 The acceptance criterion is:
— Pipes producing signals below the threshold shall be deemed to have passed the test.
Plate/strip end welds
D.8.9.20 Testing of plate/strip end welds (when such welds are allowed) shall, unless otherwise agreed be
performed by ultrasonic testing according to this standard. The testing shall comply with the requirements of
this standard and methods and a set-up suitable for the applied welding method shall be used.
Suspect pipe
D.8.9.21 Pipes not meeting the acceptance criteria above shall be deemed as suspect pipe according to
[D.8.2] and shall be treated according to [D.8.3].
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D.8.10 Non-destructive testing of corrosion resistance alloy liner pipe
D.8.10.1 Testing of CRA pipe for the detection of longitudinal and transverse surface imperfections and the
longitudinal weld shall be performed in accordance with the requirements in [D.8.4] and ISO 10893-2 (eddy
current testing).
— The acceptance criterion for eddy current testing is:
— The response shall not exceed half the response of alarm level/acceptance level E2 according to ISO
10893-2.
D.8.10.2 Testing of the weld seam can alternatively be performed in accordance with the requirements in
[D.8.4] and ISO 10893-6 (radiographic testing). Digital radiography testing, if applicable, shall be performed
in accordance with ISO 10893-7, class B.
D.8.10.3 The acceptance criteria for radiographic testing are:
— No cracks, lack of fusion, lack of penetration or pore clusters. Individual circular imperfections shall not
exceed 1.5 mm or ¼ t, whichever is smaller. Accumulated diameters of permitted imperfections shall not
exceed 3 mm or ½ t, whichever is smaller. No other discernable indications are allowed.
Untested pipe ends
D.8.10.4 Untested pipe ends shall be tested as required by [D.8.6].
Suspect pipe
D.8.10.5 Pipes not meeting the acceptance criteria above shall be deemed as suspect pipe according to
[D.8.2] and shall be treated according to [D.8.3].
D.8.11 Non-destructive testing of lined pipe
Non-destructive testing of the backing pipe
D.8.11.1 Non-destructive testing of the outer C-Mn steel backing pipe shall be performed prior to insertion of
the CRA liner pipe. The backing pipe shall be subjected to the same testing with the same acceptance criteria
that are required in this appendix for the type of backing pipe used.
Pipe ends
D.8.11.2 After insertion of the liner pipe and performing seal and/or clad welding the ends of lined pipe shall
be tested for laminar imperfections in accordance with the requirements in [D.8.4] and ISO 10893-8 or ASTM
A578 S7 in a band at each pipe end. For clad welded pipe ends this includes testing for bonding defects. The
band shall be sufficiently wide to cover the width of the seal/clad weld between the C-Mn steel backing pipe
and the CRA liner pipe. Manual or automated methods may be used.
D.8.11.3 The acceptance criterion is:
— No indications are allowed within the tested areas.
Seal and clad welds
D.8.11.4 The seal and/or clad welds at pipe ends shall be subject to manual liquid penetrant testing
according to [D.2.6] or eddy current testing according to [D.2.7].
D.8.11.5 The acceptance criteria are:
— No round indications with diameter above 1 mm and no elongated indications.
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— Indications separated by a distance less than the diameter or length of the smallest indication, shall be
considered as one indication.
— Accumulated diameters of round indications in any 100 mm length of weld shall not exceed 6 mm.
D.8.12 Non-destructive testing of clad pipe
Pipe ends
D.8.12.1 Pipe ends shall be tested as required by [D.8.6] and [D.8.7].
Ultrasonic testing of the pipe body for detection of laminar imperfections
D.8.12.2 Ultrasonic testing of the pipe body for detection of laminar imperfections in the backing pipe need
not be performed at the pipe mill if testing of the plate was performed at the plate mill according to [D.7].
D.8.12.3 If performed at the pipe mill, ultrasonic testing of the pipe body for detection of laminar
imperfections shall be performed in accordance with the requirements in [D.8.4] and ISO 10893-8 amended
as follows:
— The distance between adjacent scanning tracks shall be sufficiently small to ensure detection of the
minimum allowed imperfection size.
D.8.12.4 Acceptance criteria are:
— according to Table D-12.
D.8.12.5 Ultrasonic testing of the pipe body for detection of lack of bond between the cladding and backing
pipe shall be performed in accordance with the requirements in [D.8.4] and ASTM 578 S7 amended as
follows:
— The distance between adjacent scanning tracks shall be sufficiently small to ensure detection of the
minimum allowed imperfection size.
D.8.12.6 The acceptance criterion is:
— ASTM A578 - S7. In addition, no areas with laminations or lack of bond are allowed in the plate edge
areas.
Ultrasonic testing for longitudinal and transverse imperfections in the weld seam
D.8.12.7 For ultrasonic testing of the CRA part of the weld seam it shall be demonstrated that low frequency
shear wave angle probes are adequate for detection as required in [D.8.4.24] through [D.8.4.31]. If it is not
possible to demonstrate adequate performance of low frequency shear wave angle probes other methods or
combination of methods shall used and the adequacy of the methodology demonstrated.
Ultrasonic testing of the weld seam of clad pipe for the detection of longitudinal and transverse imperfections,
when demonstrated to give acceptable results, shall be in accordance with the requirements in [D.8.4] and
ISO 10893-11 with modifications as described in [D.8.12.8] through [D.8.12.19].
D.8.12.8 The reference standard shall contain a typical production weld. The weld surface shall be ground
flush with the original pipe contour in an area around each reference reflector sufficient to obtain signals
without interference from un-ground weld reinforcements.
D.8.12.9 The reference reflectors shall be:
— One 1.6 mm diameter through-drilled hole at the weld centreline for detection of transverse indications.
— Longitudinal external and internal notches on both sides, parallel and adjacent to the weld seam for
detection of longitudinal imperfections outside the root area. The notch shall be the “N” type with 5% of
the wall thickness, but not more than 1.5 mm or less than 0.3 mm.
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— One notch on each side of the internal weld cap located immediately adjacent to and parallel with the weld
for detection of longitudinal imperfections in the root area. The notch shall be the “N” type with 3% of the
wall thickness, but not more than 1.2 mm or less than 0.3 mm.
— If agreed, the reference reflectors for detection of transverse imperfections can be internal and external
notches, “N” type with 3% of the wall thickness, positioned at right angles to, and centred over, the weld
seam.
— Additional reflectors may be used to define the weld extremities and aiding in the gate settings. The use,
type and numbers of such reflectors shall be at the manufacturer’s option.
The length of the notches shall be 1.5 times the probe (crystal) element size or 20 mm, whichever is shorter.
The length does not include any rounded corners. The width of the notches shall not exceed 1 mm.
D.8.12.10 The probe angles shall be chosen to obtain the best possible test result for wall thickness and
diameter of the pipe to be tested. The probe angle shall be chosen such that the angle of incidence is as
perpendicular as possible to the weld bevel in the area covered by the probe.
D.8.12.11 The frequency of the probes used in the root area shall be as low as possible and not above 2
MHz.
D.8.12.12 The probe configuration for detection of the longitudinal indications shall provide a sufficient
number of opposing probe pairs to cover the entire wall thickness. E.g. one pair of probes for the external
and internal N5 notches and one pair for the internal N3 notches in the root area.
D.8.12.13 The probe configuration for detection of transverse indications shall be two wide beam, opposing
probes travelling on bead. An X type configuration of the probes for detection of transverse indications may
be used, subject to agreement.
D.8.12.14 The gates shall be set wide enough to compensate for:
— The tolerances of weld tracking system
— Variations in the width of external and internal caps
— Offsets between the external and internal weld bead.
D.8.12.15 Each probe shall be calibrated against the reference reflector located in the area of the weld to
be covered by that probe. The response from the reference reflectors shall be optimised for each probe and
probe pair:
— For detection of longitudinal imperfections in the root area the optimised response for each probe shall
be obtained from the internal notch. The threshold level for each of the internal notches shall be set no
higher than 50% of full screen height from the maximised response.
— For detection of longitudinal imperfections outside the root area the response from the external and
internal notches shall optimised and the threshold level set to 80% of full screen height for each of the
maximised responses.
— For detection of transverse imperfections the threshold level for the 1.6 mm through drilled hole or
transverse notches shall be set no higher than 80% of full screen height.
— If the use of transverse notches is agreed for detection of transverse indications, the response from the
external and internal notches shall optimised and the threshold level set to 80% of full screen height for
each of the maximised responses.
— The additional reflectors allowed in [D.8.12.9] shall not be used for threshold settings.
D.8.12.16 For each probe, the following shall be recorded:
—
—
—
—
type, frequency, angle and dimension
the distance from the index point to the weld centreline
the angle between the ultrasound direction and the major pipe axis
amplitudes and gain settings.
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D.8.12.17 Gates shall be set such that reflections from the weld caps are avoided but sufficiently wide to
ensure full weld coverage and that, with the given tolerances of the weld tracking system, responses are
obtained from indications located inside the weld and the HAZ.
D.8.12.18 The settings for lack of coupling alarm shall be set and checked.
D.8.12.19 The acceptance criterion when using shear wave probes is:
— Pipes producing signals below the threshold shall be deemed to have passed the test.
When compression wave angle probes are used, other reflectors may be used and in this case the acceptance
criteria shall be specified and agreed accordingly.
Ultrasonic testing of the area adjacent to the weld seam for detection of laminar imperfections
D.8.12.20 Ultrasonic testing of the area adjacent to the weld seam body for detection of laminar
imperfections need not be performed at the pipe mill if testing of the plate edges was performed at the plate
mill according to [D.7].
D.8.12.21 If performed at the pipe mill, the testing shall be performed according to the requirements in
[D.8.4] and ISO 10893-8.
D.8.12.22 Acceptance criteria are:
— according to Table D-12.
Testing for the detection of surface imperfections in the weld area
D.8.12.23 Testing for the detection of longitudinal and transverse surface imperfections in the weld area
shall be performed in accordance with the requirements in [D.8.4] and one of the following standards:
— ISO 10893-2 (eddy current testing)
— ISO 10893-3 (flux leakage testing)
— ISO 10893-5 (magnetic particle testing).
D.8.12.24 The acceptance criteria are:
— ISO 10893-2: Alarm level/acceptance level E2
— ISO 10893-3: Alarm level/acceptance level F2
— ISO 10893-5: Alarm level/acceptance level Table 3, M2.
Radiographic testing of welds
D.8.12.25 Full length radiographic testing of the weld shall be performed in accordance with the
requirements in [D.8.4] and ISO 10893-6.
D.8.12.26 For pipe subject to full length ultrasonic testing of the weld, radiographic testing of the weld at
each pipe end shall include the area not covered by the automated ultrasonic testing and shall at least cover
a weld length of 300 mm. The testing shall be performed in accordance with the requirements in [D.8.4] and
ISO 10893-6. For digital radiographic systems, reference is made to clause [D.8.4.33].
D.8.12.27 The acceptance criteria are:
— according to ISO 10893-6 or ISO 10893-7.
Suspect pipe
D.8.12.28 Pipes not meeting the acceptance criteria above shall be deemed as suspect pipe according to
[D.8.2] and shall be treated according to [D.8.3].
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D.8.13 Non-destructive testing of submerged arc-welding longitudinal and
submerged arc-welding helical pipe
Pipe ends
D.8.13.1 Pipe ends shall be tested as required by [D.8.6] and [D.8.7].
Ultrasonic testing of the pipe body for detection of laminar imperfections
D.8.13.2 Ultrasonic testing of the pipe body for detection of laminar imperfections need not be performed at
the pipe mill if testing of the plate/coil edges was performed at the plate/coil mill according to [D.7].
D.8.13.3 If performed at the pipe mill, ultrasonic testing of the pipe body for detection of laminar
imperfections shall be performed in accordance with the requirements in [D.8.4] and ISO 10893-8 amended
as follows:
— the distance between adjacent scanning tracks shall be sufficiently small to ensure detection of the
minimum allowed imperfection size.
D.8.13.4 Acceptance criteria are:
— according to Table D-12.
Ultrasonic testing of the area adjacent to the weld seam for detection of laminar imperfections
D.8.13.5 Ultrasonic testing of the area adjacent to the weld seam body for detection of laminar
imperfections need not be performed at the pipe mill if testing of the plate/coil edges was performed at the
plate/coil mill according to [D.7].
D.8.13.6 If performed at the pipe mill, the testing shall be performed according to the requirements in
[D.8.4] and ISO 10893-8.
D.8.13.7 Acceptance criteria are:
— according to Table D-12.
Ultrasonic testing for longitudinal and transverse imperfections in the weld seam
D.8.13.8 Ultrasonic testing of the weld seam of SAW pipe for the detection of longitudinal and transverse
imperfections shall be in accordance with the requirements in [D.8.4] and ISO 10893-11 with modifications
as given in [D.8.13.9] through [D.8.13.20].
The equipment shall allow for the complete examination of the weld and its adjacent area for both
longitudinal and transverse defects. The equipment shall be fitted with an automatic paint spray system (or
alternative system, e.g. recording) for marking the areas giving ultrasonic indications and areas where a loss
of ultrasonic coupling with the pipe has occurred.
To verify that no defects originating from hydrogen is present, a minimum of 2% of the pipes shall be
examined by an optimized manual UT procedure for cracks. This investigation shall be done minimum 48
hours after welding. If an inspected pipe contains such defects, then production shall be stopped and all
pipes put in quarantine. The root cause shall be determined. Based on the root cause, all pipes shall be
considered for possible risk of hydrogen cracks based on production records. It may be necessary to inspect
some or all of the pipes in quarantine.
D.8.13.9 The reference standard shall contain a typical production weld, including representative weld
reinforcements.
D.8.13.10 The reference reflectors shall be in accordance with Table D-13.
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Additional reflectors may be used to define the weld extremities and aiding in the gate settings. The use,
type and numbers of such reflectors shall be at the manufacturer’s option and shall be described in the
documented procedure. The response from the reference reflectors shall define the reporting threshold.
Table D-13 Required reflectors in SAWL/SAWH pipe weld AUT reference standard
A
1.6 mm TDH, weld centreline
B
1
3.0 mm TDH at weld toe edge at both sides of the weld
C
2
N5 notch parallel and adjacent to weld seam at OD surface at both sides of the weld
D
2
N5 notch parallel and adjacent to weld seam at ID surface at both sides of the weld
E
Maximum 3.0 mm side-drilled hole located at the weld centreline at ½ WT depth (mid thickness),
and parallel to the weld.
F
3.0 mm TDH, weld centreline
G
N5 notch transverse to and over the weld seam at OD surface
H
N5 notch transverse to and over the weld seam at ID surface
I
3
To confirm area of coverage at the pipe ends: Maximum 3.0 mm through drilled hole (TDH) located
at the weld centreline. The position of the TDHs will define the untested area at the ends, and
should not exceed 250 mm from each pipe end.
1)
The weld toe of the widest weld cap should be used. (i.e. the reflector should be the farthest away from weld
centerline). As an alternative, separate reflectors may be made for OD and ID weld cap.
2)
The notch shall be the “N” type with 5% of the wall thickness, but not more than 1.5 mm or less than 0.3 mm. The
length of the notches shall be 1.5 times the probe (crystal) element size or 20 mm, whichever is shorter. The length
does not include any rounded corners. The width of the notches shall not exceed 1 mm.
3)
To confirm coverage at the pipe ends. Location to be determined by the manufacture, but should be maximum 250
mm from pipe ned. The reflector to be decided by the manufacturer, but shall not be larger than a 3 mm diameter
hole. Both pipe ends to have this reflector. The reflector should be a 3 mm through-drilled hole at weld centerline.
D.8.13.11 The inspection angles shall be chosen to obtain the best possible test result for wall thickness and
diameter of the pipe to be tested.
D.8.13.12 The probe configuration for detection of the longitudinal indications shall provide a sufficient
number of opposing probe pairs on both sides of the weld or focal laws to cover the entire wall thickness.
Both ID and OD surface area shall be inspected by minimum 2 angles each, of these 2 angles one of them
shall be not lower than 65°.
Dedicated channels set up on the mid wall SDH to cover the embedded parts of the weld is required if this is
not possible to achieve. The sensitivity shall then be set at 80% FSH for the mid wall SDH. Additional buried
SDHs might be included at different depths of the weld to demonstrate full coverage
Guidance note:
The reflectors required for detecting longitudinal defects may not detect lack-of-fusion in mid-wall. The risk is considered negligible
for normal two-pass SAW process because the high heat input and large quantity of weld deposit. It is expected that consistent
lack-of-fusion is unlikely, and will be detected in macro specimens. This would indicate an incorrect welding process, and a
new qualification should be required. Single-event lack-of-fusion may occur, but would be associated with other gross process
disturbances or weld defects that the pipe in question would be suspicious in any case. For multiple-pass SAW, or in cases where
lack-of-fusion is considered a risk, additional requirements to reflectors or system setup may be needed.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
D.8.13.13 The probe configuration for detection of transverse indications shall be two wide beam, opposing
probes travelling on bead. An X type configuration of the probes for detection of transverse indications may
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be used instead of wide beam probes on bead, subject to agreement. N5 transverse notches (reflectors G
and H) shall be used to confirm correct beam orientation and for gate setting of transverse channels.
D.8.13.14 Each probe or focal law shall be calibrated against the reference reflector located in the area of
the weld to be covered by that probe. The response from the reference reflector(s) shall be optimised for
each probe and probe pair as described in Table D-14. All relevant reference reflectors shall be above the
recording threshold during dynamic inspection.
Table D-14 contains a set of correspondances between channels and reflectors to ensure reasonable coverage
of the weld. Table D-14 should be used, but alternative channels and reflectors may be used, provided they
ensure similar coverage and inspection level. For each probe or focal law, the following shall be recorded:
—
—
—
—
type, frequency, angle and dimension
the distance from the index point to the weld centreline
the angle between the ultrasound direction and the major pipe axis
amplitudes and gain settings.
The following parameters shall be reported and a print out shall be made available at the AUT station:
— A comprehensive detailed list of probes/channels, longitudinal/transverse, ID/OD/Mid, flaw detection/
coupling.
— A matrix showing all channels including coupling channels, with response from the different reflectors
including calibration reflectors shall be made with dB levels, gain, signal height, trigger threshold. The
table channels/reflectors (C/R), shall be included in the AUT procedure/working instructions and submitted
to COMPANY for approval.
— Date, time, operator name and signature, inspector name and signature.
Table D-14 Requirements for channels and reference reflectors, AUT
Channel type
Reference reflector
Refelctors to confirm
coverage static calibration
Comment
Longitudinal OD
C
E, F, I
Minimum 2 angles
Longitudinal ID
D
E, F, I
Minimum 2 angles
Longitudinal Buried SDH
E
Transverse
A
B, G
Transverse, X-scheme
A
B, G
1)
1
Reflector types are described in Table D-13
D.8.13.15 The gates shall be set wide enough to compensate for, and include as a minimum:
— the tolerances of weld tracking system
— variations in the width of external and internal caps
— offsets between the external and internal weld bead.
For longitudinal channels, the gate shall not include the notch C or D at the opposite side of the weld.
D.8.13.16 The settings for lack of coupling alarm shall be set and checked. The alarm level for lack of
coupling should be set at maximum 14 dB loss of signal or reference echo.
D.8.13.17 Sensitivity/gain shall be set for each channel such that the reflectors in Table D-14 are
consistently reported upon repeated dynamic scans. When the settings are optimised, the relevant
parameters shall be recorded and the reference standard shall be passed 3 times through the equipment at
the operational velocity. In case the equipment settings need to be corrected to maintain required sensitivity,
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the change in settings should be based on an average from three runs. For acceptance of the settings for
a given probe/channel, the deviation in response from each reference reflector shall not be more than 3
dB over the three dynamic calibration checks. Gate settings shall not deviate more than 2.5 mm from the
reference position.
One dynamic calibration verification scan of the reference standard shall be carried out at the start of each
shift, whenever there is an equipment change over, whenever there is an operator change or every 4 hours,
whichever is the first event met.
D.8.13.18 The acceptance criterion is:
Pipes producing signals below the reporting threshold shall be deemed to have passed the test.
Additional requirements for SAWH pipe strip/plate end welds
D.8.13.19 For SAWH pipe the full length of strip/plate end welds (when such welds are allowed) shall
be ultrasonically tested as required above for the helical seam. Alternatively manual ultrasonic testing in
accordance with [D.8.14] may be used for testing of test strip/plate end welds.
In addition, the joints where the extremities of the helical and strip/plate end welds meet shall be subject to
radiographic testing in accordance with the requirements in [D.8.4] and ISO ISO 10893-6. For use of digital
radiographic equipment, see [D.8.4.33].
D.8.13.20 Acceptance criteria for these tests are:
— For automated ultrasonic testing: according to [D.8.13.19] above
— For manual ultrasonic testing: according to [D.8.14]
— For radiographic testing: According to ISO 10893-6.
Additional requirements for testing of SAW CRA pipes and welds with CRA weld deposits
D.8.13.21 Ultrasonic testing of welds in CRA materials with CRA (duplex, other stainless steels and nickel
alloy steel) weld deposits will, in order to achieve an adequate detection of imperfections, normally require
that special reference blocks and probes are used.
D.8.13.22 The requirements given in [D.8.4.24] through [D.8.4.31] shall be fulfilled and special reference is
made to [D.8.4.30] and [D.8.4.31].
D.8.13.23 When compression wave angle probes are used, other reflectors may be used and in this case the
acceptance criteria shall be specified and agreed accordingly.
Testing of ferromagnetic pipe for the detection of surface imperfections in the weld area
D.8.13.24 Testing of ferromagnetic pipe for the detection of longitudinal and transverse surface
imperfections shall be performed in accordance with the requirements in [D.8.4] and one of the following
standards:
— ISO 10893-2 (eddy current testing)
— ISO 10893-3 (flux leakage testing)
— ISO 10893-5 (magnetic particle testing).
The acceptance criteria are:
— ISO 10893-2: Alarm level/acceptance level E2
— ISO 10893-3: Alarm level/acceptance level F2
— ISO 10893-5: Alarm level/acceptance level Table 3, M2.
Testing of non magnetic pipe for the detection of surface imperfections in the weld area
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D.8.13.25 Testing of non-magnetic SAW pipe for the detection of longitudinal and transverse surface
imperfections shall be performed in accordance with the requirements in [D.8.4] and one of the following
standards:
— ISO 10893-2 (eddy current testing)
— ISO 10893-4 (liquid penetrant testing).
The acceptance criteria are:
— ISO 10893-2: Acceptance level E2
— ISO 10893-4: Acceptance level P2.
Radiographic testing
D.8.13.26 Radiographic testing of the weld at each pipe end shall include the area not covered by the
automated ultrasonic testing and shall at least cover a weld length of 300 mm. The testing shall be
performed in accordance with the requirements in [D.8.4], ISO 10893-6 and ISO 10893-7.
The acceptance criteria are:
— according to ISO 10893-6 for conventional RT and ISO 10893-7 for digital RT.
Suspect pipe
D.8.13.27 Pipes not meeting the acceptance criteria above shall be deemed as suspect pipe according to
[D.8.2] and shall be treated according to [D.8.3].
D.8.14 Manual non-destructive testing at pipe mills
General
D.8.14.1 In all cases when the automated NDT system give signals equal to or greater than the threshold
level, or surface imperfections are disclosed by visual examination, manual NDT may be performed in
order to confirm the presence or absence of a defect. Automated or semi-automated NDT may be used as
substitution of the manual NDT required in this sub-section provided the method is demonstrated to provide
the same or better sensitivity in detection of imperfections.
D.8.14.2 In addition, manual NDT may be performed on pipe ends that are not tested by the automated
equipment. See [D.8.6].
Radiographic testing
D.8.14.3 Radiographic testing shall be performed in accordance with the requirements in [D.8.4] and ISO
10893-6 or ISO 10893-7 to cover the full weld length or to supplement other NDT methods when the type of
or severity of an indication in weld can not be determined with certainty.
The acceptance criteria are:
— according to ISO 10893-6 for conventional RT and ISO 10893-7 for digital RT.
All pipe; manual ultrasonic testing for laminar imperfections and thickness testing
D.8.14.4 Manual ultrasonic thickness testing and testing for laminar imperfections shall be performed on
untested pipe ends and to confirm the presence or absence of a defect when automated NDT systems gives
signals equal to or greater than the threshold level.
Manual ultrasonic testing of pipe ends, laminar imperfections
D.8.14.5 Any additional non-destructive testing shall be as specified by the purchaser.
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D.8.14.6 If automated ultrasonic testing of girth welds during installation will be performed the width of the
band should extend at least 150 mm inside the location of future welding preparations for girth welds.
D.8.14.7 If allowance for re-bevelling of pipe shall be included, the width of the band should extend at least
100 mm inside the location of future welding preparations for girth welds.
D.8.14.8 Acceptance criteria are:
— according to Table D-12.
Manual ultrasonic testing of pipe ends, radial cracks
D.8.14.9 If required, for detection of cracks angle probes shall be used to supplement the straight beam
probes. Testing shall be in general accordance with ASTM A577 or equivalent standard and:
— Probes shall meet the requirements of [D.3.2.3].
— Sensitivity for C-Mn steel shall be a DAC curve based on reference blocks with a rectangular notch with
depth 3% of the material thickness on both sides.
— Reference blocks for duplex stainless steel and austenitic steels shall have one Ø 3 mm flat bottom hole
perpendicular to the angle of incidence of the probe and at the largest possible depth from the scanning
surface of the block. Reference blocks shall be of the actual material tested or of a material with similar
with acoustic properties.
— Low frequency shear wave angle probes may be used for CRA material instead of twin crystal
(transmitter/receiver) compression-wave probes. For acceptance, it shall be verified on the reference
blocks that it is possible to obtain a DAC with a shear wave angle probe that is comparable to the DAC
obtained with an angle compression wave probe.
D.8.14.10 The acceptance criterion is:
— no indications shall exceed the DAC.
Manual ultrasonic testing of the pipe body for detection of laminar imperfections
D.8.14.11 Manual ultrasonic testing of the pipe body for detection of laminar imperfections need not be
performed at the pipe mill if testing of the plate/coil edges was performed at the plate/coil mill according to
[D.7].
D.8.14.12 If performed at the pipe mill, manual ultrasonic testing of the pipe body for detection of laminar
imperfections shall be performed in accordance ISO 10893-8, App.A amended as follows:
— the distance between adjacent scanning tracks shall be sufficiently small to ensure detection of the
minimum allowed imperfection size.
D.8.14.13 Acceptance criteria are:
— according to Table D-12.
Manual ultrasonic testing of the area adjacent to the weld seam for detection of laminar imperfections
D.8.14.14 Manual ultrasonic testing of the area adjacent to the weld seam body for detection of laminar
imperfections need not be performed at the pipe mill if testing of the plate/coil edges was performed at the
plate/coil mill according to [D.7].
D.8.14.15 If performed at the pipe mill, the manual NDT shall be performed according to ISO 10893-8,
App.A.
D.8.14.16 Acceptance criteria are:
— according to Table D-12.
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Manual ultrasonic thickness testing of the pipe body
D.8.14.17 Manual ultrasonic thickness testing of the pipe body shall be performed in accordance with the
requirements ISO 10893-12.
D.8.14.18 The acceptance criterion is:
— the specified maximum and minimum wall thickness shall be met.
Seamless pipe; manual ultrasonic testing for longitudinal and transverse imperfections
D.8.14.19 Manual ultrasonic testing and testing of seamless pipe for longitudinal and transverse
imperfections shall performed on untested pipe ends and to confirm the presence or absence of a defect
when automated NDT systems gives signals equal to or greater than the threshold level.
D.8.14.20 For pipes in CRA materials it shall be verified that the presence of any possible coarse, anisotropic
zones will not impede the testing, see [D.8.4.24] through [D.8.4.31].
D.8.14.21 Manual ultrasonic testing of the pipe body for longitudinal imperfections shall be performed in
accordance with ISO 10893-10. The probe angles shall be chosen to obtain the best test result for the wall
thickness/diameter ratio of the pipe to be tested.
The acceptance criterion is:
— acceptance level U2/C according to ISO 10893-10.
D.8.14.22 Manual ultrasonic inspection of the pipe body for transverse imperfections shall be performed in
accordance with the requirements in ISO 10893-10. The probe angles shall be chosen to obtain the best test
result for the wall thickness/diameter ratio of the pipe to be tested.
The acceptance criterion is:
— acceptance level U2/C according to ISO 10893-10.
Welded pipe; manual ultrasonic testing of welds
D.8.14.23 Manual ultrasonic testing and testing of welds in welded pipe for longitudinal and transverse
imperfections shall be performed on untested pipe ends and to confirm the presence or absence of a defect
when automated NDT systems gives signals equal to or greater than the threshold level.
D.8.14.24 Manual ultrasonic testing of welds in C-Mn steel material with C-Mn steel weld deposits shall
be performed in accordance with [D.2.3] except that [D.2.3.16], [D.2.3.17], [D.2.3.23], [D.2.3.24] and
[D.2.3.41] shall not apply.
Manual ultrasonic testing of welds in HFW pipe
D.8.14.25 The reference block shall be according to [D.8.9.10].
D.8.14.26 One or more of the following probe configurations shall be used:
— Single pulse echo probes with the angle of incidence as perpendicular to the radial centreline of the weld
as possible.
— Tandem probes with the angle of incidence as perpendicular to the radial centreline of the weld as
possible.
D.8.14.27 The probe angle for the initial scanning shall be chosen to obtain the best possible test result for
wall thickness and diameter of the pipe to be tested and such that the angle of incidence is as perpendicular
as possible to the weld bevel.
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D.8.14.28 The DAC shall be constructed using the notches in the reference block. A 2-point DAC shall only
be used if scanning is limited to one full skip or less. If scanning is performed using more than one full skip, a
3-point DAC shall be established as a minimum.
D.8.14.29 The acceptance criterion is:
— no maximised echo from any probe shall exceed the DAC.
Manual ultrasonic testing of welds in CRA materials and in clad pipe
D.8.14.30 Ultrasonic testing of welds in CRA materials with CRA (duplex, other stainless steels and
nickel alloy steel) weld deposits will in order to achieve an adequate detection of imperfections normally
require that special reference blocks and probes are used for testing of these materials. Unless it can be
demonstrated as required in [D.2.4.18] and [D.8.4.29] that use of low frequency shear wave angle probes
gives acceptable detection, manual ultrasonic testing of the CRA weld deposit in the root shall be performed
as required in [D.2.4]
D.8.14.31 Angle beam probes shall be available in angles, or be provided with wedges or shoes, ranging
from 30° to 75°, measured to the perpendicular of the surface of the pipe being tested. Probe angles shall be
selected as required in [D.2.3]. The probe angles shall be chosen to obtain the best possible test result for
wall thickness and diameter of the pipe to be tested and such that the angle of incidence is as perpendicular
as possible to the weld bevel in the area covered by the probe. If shear wave angle probes are used for
testing of the root the frequency shall be 2 MHz or lower.
D.8.14.32 The reference standard for testing with shear angle probes shall be according to [D.8.12.8] and
[D.8.12.9].
Testing sensitivities shall be established as follows:
— For testing of longitudinal imperfections in the weld volume outside the root area, the DAC shall be
constructed using the longitudinal external and internal notches. A 2-point DAC shall only be used if
scanning is limited to one full skip or less. If scanning is performed using more than one full skip, a 3point DAC shall be established as a minimum.
— For testing of the root area longitudinal imperfections sensitivity setting shall be against the notch in the
root area on the opposite side of the weld and the response set to 50% of full screen height.
— For testing of transverse imperfections, the DAC shall be constructed using the 1.6 mm diameter through
drilled holes at the weld centreline with 2 points (e.g. ½ and full skip).
D.8.14.33 Scanning for transverse indications shall be performed on bead. Probes with beam angles of 45°
and 60° shall be available.
D.8.14.34 The acceptance criteria are:
— No maximised indications exceeding DAC for longitudinal and transverse indications.
— No maximised indications in the root area exceeding 50% of full screen height.
When compression wave angle probes are used, other types of reflectors are used and the acceptance
criteria shall be specified and agreed accordingly.
Manual ultrasonic testing of welds in SAWL and SAWH pipe
D.8.14.35 The reference standard shall be according to [D.8.13.9] and [D.8.13.10].
D.8.14.36 Angle beam probes shall be available in angles, or be provided with wedges or shoes, ranging
from 30° to 75°, measured to the perpendicular of the surface of the pipe being tested. Probe angles shall be
selected as required in [D.2.3].
D.8.14.37 Testing sensitivities shall be established as follows:
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— For testing of longitudinal imperfections in the weld volume, the DAC shall be constructed using the
longitudinal external and internal notches. A 2-point DAC shall only be used if scanning is limited to one
full skip or less. If scanning is performed using more than one full skip, a 3-point DAC shall be established
as a minimum
— For testing of transverse imperfections, the DAC shall be constructed using the 1.6 mm diameter through
drilled holes at the weld centreline with 2 points (e.g. ½ and full skip).
D.8.14.38 Scanning for transverse indications shall be performed on bead. Probes with beam angles of 45°
and 60° shall be available. Use of 4 MHz probes shall be preferred.
D.8.14.39 Acceptance criterion is:
— no maximised indications exceeding DAC
Manual ultrasonic testing of welds in CRA materials and CRA weld deposits/materials.
D.8.14.40 Refer to [D.8.4.24] through [D.8.4.31]. Ultrasonic testing of CRA materials and welds with CRA
(duplex, other stainless steels and nickel alloy steel) weld deposits will in order to achieve an adequate
detection of imperfections require that special calibration blocks and probes are used for testing of welds in
these materials. Angle probes generating compression waves should be used in addition to straight beam
probes, angle shear wave probes and creep wave probes.
D.8.14.41 Unless it can be demonstrated as required in [D.2.4.18] and [D.8.4.29] that use of low frequency
shear wave angle probes only gives acceptable detection, manual ultrasonic testing of CRA materials and
welds with CRA weld deposits shall be performed as required in B400.
D.8.14.42 Acceptance criteria manual ultrasonic testing of CRA materials and welds with CRA weld deposits
performed with angle compression wave probes are:
— according to Table D-6.
Manual magnetic particle testing
D.8.14.43 Manual magnetic particle surface testing shall be performed in accordance with [D.2.5] and ISO
10893-5.
D.8.14.44 Manual magnetic particle testing of pipe ends shall be performed in accordance with [D.2.5] and
ISO 10893-5.
D.8.14.45 Manual magnetic particle testing of welds shall be performed as required by [D.2.5].
D.8.14.46 Acceptance criteria shall be according to the relevant requirements of this subsection.
Manual liquid penetrant testing
D.8.14.47 Manual liquid penetrant surface testing and testing of pipe ends shall be performed in accordance
with ISO 10893-4.
D.8.14.48 Manual liquid penetrant testing of welds shall be performed in accordance with [D.2.6],
paragraphs [D.2.6.2] through [D.2.6.5].
D.8.14.49 Acceptance criteria shall be according to the relevant requirements of this subsection.
Manual eddy current testing
D.8.14.50 Manual eddy current surface testing and testing of pipe ends shall be performed in accordance
with ISO 10893-2.
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D.8.14.51 Manual eddy current testing of welds shall be performed in accordance with [D.2.7], paragraphs
[D.2.7.2] through [D.2.7.8] and ISO 10893-2 (eddy current testing)
D.8.14.52 Acceptance criteria shall be according to the relevant requirements of this subsection.
D.8.15 Non-destructive testing of weld repair in pipe
D.8.15.1 Weld repair of the body of any pipe and of the weld in HFW pipe is not permitted.
D.8.15.2 A repaired weld shall be completely re-tested using applicable NDT methods in accordance with
[D.8.8] through [D.8.13].
Alternatively, manual NDT may be performed in accordance with [D.8.14] and with acceptance criteria in
accordance with the requirements in [D.8.14]. In this case, manual ultrasonic testing shall be governing for
embedded defects.
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APPENDIX E AUTOMATED ULTRASONIC GIRTH WELD TESTING
E.1 General
E.1.1 Objective
E.1.1.1 This appendix details the examination requirements for the automated ultrasonic testing of pipeline
girth welds.
E.1.2 Applicability
E.1.2.1 The appendix applies when automated ultrasonic testing (AUT) is performed on pipeline girth welds.
E.1.2.2
Automated ultrasonic testing (AUT) is a general term that includes several approaches and techniques,
which are all acceptable for use as long as the general requirements of [E.2] can be fulfilled. This includes
zonal discrimination technique, phased array scan group based setups (e.g. sectorial and/or linear scan
groups) and ultrasonic imaging (e.g. total focusing method (TFM) or full matrix capture (FMC)). In addition,
application of inspection can put limitations and change approaches within the techniques used, for instance
due to differences between carbon steel and CRA materials.
E.2 Basic requirements
E.2.1 General
E.2.1.1 The primary requirement to any AUT system is that its performance is documented in terms
of adequate detection and sizing, or rejection abilities, in relation to specified/determined acceptable
imperfections. The performance of the AUT system has through the qualification to be demonstrated to meet
or exceed the requirements in terms of detection or rejection set by the applicable acceptance criteria for any
project.
E.2.1.2 The ultrasonic system to be used shall be accepted through qualification, see [E.8].
E.2.1.3 The ultrasonic system shall demonstrate 100% coverage of the weld and heat affect zone (HAZ) with
adequate beam coverage overlap and signal strength for relevant imperfection sizes.
It shall have a fully automatic recording system to indicate the location of imperfections and the integrity of
acoustic coupling. Different concepts of automated ultrasonic testing are acceptable, provided that [E.2.1.1]
is fulfilled. This includes zonal discrimination, phased array techniques (for instance sectorial and/or linear
scan groups) and ultraonic imaging techniques (for instance total focusing method (TFM), full matrix capture
(FMC))
E.2.1.4 The information provided by all AUT channel types shall be actively used in order to ensure adequate
imperfection detection and sizing.
E.2.1.5 The ultrasonic system may include scanner heads and system set-up specifically configured for
testing of repairs where the primary function is to confirm the complete removal of rejected defect. As a
minimum the AUT system with its normal set-up, but with gates wide enough to encompass the repair area
and confirm that the AUT defects have been removed. During this special attention shall also be made to
TOFD channel indications, and indications outside the normal gate settings.
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Due to the wide variation in repair weld groove shapes that may limit the detection capabilities of the
system, manual UT, or a dedicated semi-automatic UT system, shall support the AUT on weld repairs
unless the groove shape is controlled to be within given tolerances and the scanner head is configured
accordingly or if an AUT methodology that is qualified and documented to be capable to accurately detect
and size imperfections is applied (e.g. ultrasonic imaging techniques or phased array based setup groups.).
For supplementary UT, the provisions of App.D apply, meaning that ultrasonic testing shall be performed
according to best workmanship with the intention to confirm that no new imperfections are introduced by
repair welding.
E.2.1.6 The ultrasonic system shall incorporate facilities for detection of transverse imperfections, when
it is clearly identified that the weld process, parent material, application and environmental condition may
increase the risk for transversal type imperfections.
E.2.1.7 For each AUT setup, allowable wall thickness variations from nominal thickness is ±1.5 mm (total
range 3.0 mm) applicable for pipes exposed for a total nominal strain of less than 0.4%, and ±1.0 mm
(total range 2.0 mm) applicable for fatigue sensitive welds or when total nominal strains equal to and above
0.4%. For variations from nominal wall thickness outside these tolerances, additional AUT setups have to be
employed to ensure that any part of the weld is scanned with a setup within the tolerance defined above.
Any deviation from above has to be validated through a full validation scope according to [E.9], which
captures the applicable wall thickness variations. AUT setups that have the ability to accommodate larger
wall thicknesses than the limits provided above, shall demonstrate this during the general AUT system
qualification. When qualified, wall thickness variations within the qualified range shall be accepted for each
AUT setup instead of the requirement above.
E.2.1.8 Counter bores may be used to compensate for large thickness variations if the counter bore is
machined to provide parallel external and internal surfaces before the start of the taper. The length of the
parallel surfaces shall at least be sufficient to allow scanning from the external surface and sufficient for the
required reflection off the parallel internal surface.
E.2.1.9 An operating quality assurance system shall be used covering the development of ultrasonic
examination systems, testing, verification and documentation of the system and its components and software
against given requirements, qualification of personnel and operation of ultrasonic examination systems. The
quality assurance system employed shall be documented in sufficient detail to ensure that AUT systems
used for field inspection will be designed, assembled and operated within the essential variables established
during the qualification and in all significant aspects will be equal to the qualified AUT system. In addition
to the general requirements to quality assurance of Section 2, NDT contractors and organisations shall as a
minimum supplement this with the requirements given in ASTM E1212.
The following shall be documented:
—
—
—
—
—
—
—
—
—
—
—
—
—
—
document control
system development including establishing performance
requirements to the system, its components and calibration blocks
selection/qualification/follow-up/auditing of suppliers/subcontractors
procurement of system components and calibration blocks
verification of delivered system components and calibration blocks against given requirements
marking/identification of system components and calibration blocks complying with given requirements
control and verification of software development/changes
design of AUT system(s) set-up for specific field operation conditions/requirements
assembly of AUT systems for field operation from verified components in stock, including identification of
the system and identification/documentation of its components, calibration block(s) and spare parts
verification/testing of AUT systems for field operation
operational checks and field maintenance of AUT systems
documentation/verification of in field modifications of AUT systems
return of field systems, dismantling, check/repair/upgrading of system components
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— verification of repaired/upgraded system components against given requirements
— AUT operator training and qualification.
Project specific set-up files, to be included in project specific procedures:
—
—
—
—
—
—
Phased array focal laws (if applicable)
Probe stand off
Sound angles
Target depth
Required over trace
Applied thresholds.
E.2.1.10 If an embedded imperfection is located close to a surface, such that the ligament height is less than
half the imperfection height, the ligament height between the imperfection and the surface shall be included
in the imperfection height.
E.2.1.11 Velocity changes and attenuation variations in the longitudinal weld seam shall be determined
and compared to base pipe material. Those differences shall be documented through a comparison table. If
there are attenuation differences greater than ±2 dB (total range 4.0 dB) or angle changes greater than 1.5
degrees (total range 3.0 degrees) compared to base pipe material, then procedural consideration shall be
given to imperfection detection and evaluation in this area to ensure requirements of [E.2.1.1] are met.
Regardless of the difference, adequate inspection sensitivity in the longitudinal weld shall be confirmed
during AUT qualification/validation testing.
E.2.1.12 All requirements for applications experiencing strains over 0.4% shall also apply to fatigue sensitive
applications.
Requirements specific for CRA and coarse grain material examination
E.2.1.13 Weld deposits in duplex, austenitic stainless steels and nickel alloys may have a coarse grain
structure with variations in grain size and structure resulting in unpredictable fluctuations in attenuation.
Duplex and austenitic stainless steel base materials may have the same characteristics. Ultrasonic testing of
welds with CRA (duplex, other stainless steels and nickel alloy steel) weld deposits will in order to achieve an
adequate detection of imperfections require different AUT setup than for inspection of carbon steel materials.
The AUT setup selected for the inspection shall be capable to comply with the requirement to signal-to-noise
in [E.4.5.6].
E.2.1.14 Applicable to CRA weld deposits, AUT shall be verified on its capabilities on CRA boundary
penetration, which shall be demonstrated. Verification on the penetration shall be done by determine the
noise generated from the boundary, which shall not exceed a value 6 dB below the rejection threshold
applied for the documented defect height detected with 90% POD or 85% POR at a 95% confidence level
during qualification. In case these conditions cannot be met, internal visual inspection shall be used to aid on
the sentencing of the root integrity, in conjunction with AUT. The methods shall be validated in a combined
program. Defective welds shall be inspected with both AUT and using internal VT. Results shall be compared
with RT, macros sectioning.
The signal to noise ratio between reference reflector and the structural noise of the CRA material in the
weld area shall be minimum 6 dB. In any case the acoustical equivalent noise shall not exceed the smallest
allowable defect height (ECA).
E.2.1.15 For the determination of certain root indications in coarse grain materials (concavity, root
penetration) information may be used derived from laser profiling or camera having laser measurement tool
(if laser profiling or camera can access root area). The capabilities of these tools should be proven during the
validation program.
Requirements specific for carbon steel applications
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E.2.1.16 For AUT of girth welds in seamless pipes: Wall thickness monitoring channels shall be incorporated
into all AUT configurations. The thickness channel wedge placement shall allow continuous monitoring of
pipe wall thickness at the furthest possible ID sound interacting point. The output from these channels shall
be used to confirm that inspection is performed within the requirements of paragraph [E.2.1.7]. The wall
thickness monitoring channels can be waived if it is documented that the wall thickness variations are within
the ranges specified in paragraph [E.2.1.7] (e.g. with counter bored pipes).
E.2.1.17 Applicable to all fatigue sensitive carbon steel applications: ToFD shall be an integral part of
inspection, not to be considered an augment or safety net option. ToFD channel shall use conventional
transducers.
TOFD can be waived if AUT based on ultrasonic imaging technique is applied, provided that the full weld is
scanned with the imaging technique, and adequate sensitivity for tip diffracted signals are documented upon
the AUT qualification and/or validation.
E.2.2 Documentation
E.2.2.1 The configuration of the ultrasonic system shall for evaluation purposes be described and
documented with regard to:
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
brief functional description of the system
reference to the standard or recommended practice used for design and operation of the system
description of the quality assurance system
equipment description
limitations of the system with regard to material or weld features including sound velocity variations,
geometry, wall thickness, size, surface finish, material composition, etc.
number and type of transducers, or phased array set up with description of characteristics and set-up
number of and height of examination zones, where relevant
gate settings
function of scanning device
ultrasonic instrument, number of channels and data acquisition system
recording and processing of data
calibration blocks
coupling monitoring method
temperature range for testing and limitations
coverage achieved
maximum scanning speed, PRF and direction
reporting of indications and documentation of calibration and sensitivity settings.
E.2.3 Ultrasonic system equipment and components
General requirements
E.2.3.1 The system shall be capable of examining a complete weld including the heat affected zone in one
circumferential scan. This requirement may, as agreed, be deviated from for very thick/small diameter pipe,
if it is not possible to cover the whole depth range in one scan.
E.2.3.2 There shall be recordable signal outputs for at least each 1 mm of weld length for each inspection
channel.
E.2.3.3 The ultrasonic instrument shall provide a linear A-scan presentation. The instrument linearity shall
be determined according to the procedures detailed in ASTM-317-01 or EN12668. Instrument linearity
shall not deviate by more than 5% from ideal. Alternatively, tests performed according to the manufacturer
requirements and specifications can be carried-out.
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The assessment of ultrasonic instrument linearity shall have been performed within 12 months of the
intended end use date. For production AUT with an expected duration exceeding 6 months, but less than one
year, the assessment of instrument linearity may be performed immediately before the start of work.
A calibration certificate shall be made available upon request.
E.2.4 Specific requirements for ultrasonic instruments using multiple
channels, pulse echo, tandem and/or through transmission techniques.
E.2.4.1 The instrument shall provide an adequate number of inspection channels to ensure the examination
of the complete weld through thickness in one circumferential scan, if possible (see [E.2.4.1]). Each
inspection channel shall provide:
—
—
—
—
—
—
—
—
pulse echo or through transmission modes
one or more gates, each adjustable for start position and length
gain adjustment
recording threshold between 5 and 100% of full screen height
recording of either the first or the largest signal in the gated region
signal delay to enable correlation to distance marker positions (real time analogue recording only)
recordable signal outputs representing signal amplitude and sound travel distance
specific requirements to ultrasonic instruments using the ToFD technique
E.2.4.2 The instrument shall provide a ToFD B-scan image. ToFD function software shall incorporate
adequate facilities for online indication assessment using range calibrated cursors. A-scan reference and
numerical translation of time of flight positions shall be incorporated.
Depth range efficiency shall be identified for each ToFD set up. For wall thickness greater than 35mm, at
least two ToFD channels shall be required and coverage overlap of ToFD channels shall be demonstrated.
TOFD channels can be waived for AUT using ultrasonic imaging technique to display the whole weld, provided
that capability to capture tip diffraction signals in the images are documented in qualification and validation.
E.2.4.3 The instrument shall fulfil the requirements to ultrasonic instruments described in EN12668-1 and
ISO 16828, Chapter 6 Equipment requirements
Specific requirements to ultrasonic instruments using phased arrays.
E.2.4.4 The phased array system shall incorporate means for periodical verification of the function of
required active elements necessary to maintain a specific focal law in compliance with ISO 18563.
E.2.4.5 A system preventing any unqualified alterations to agreed focal laws shall be implemented for the
phased array AUT system. This system shall be verified and documented. Phased array focal law controlling
parameters (may be a combination of: angle, start element, center element, total number of elements,
index, etc) shall be indicated in the AUT procedure. Unqualified change limits shall comply with [E.5.3.1].
Unqualified alterations on agreed single focal laws to setups can be accepted if the changes are made
according to a qualified and validated concept that adapts the focal laws to one or several essential variables
which are monitored in real time. In such case, the concept shall be validated through a full validation scope
of minimum 29 observations according to [E.9]. This option is in particular applicable for adaptive focal laws
to wall thickness variations.
E.2.4.6 If additional conventional transducers to the phased array ones are used, for example for transverse
inspection and ToFD, the information for all transducers shall be available in the same set up and recording
system.
The recording system
E.2.4.7 The recording or marking system shall clearly indicate the location of imperfections relative to the
12 o'clock position of the weld, with a ± 1% accuracy or 10 mm, whichever is greater. The system resolution
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shall be such that each segment of recorded data from an individual inspection channel does not represent
more than 2 mm of circumferential weld distance.
Acoustic coupling
E.2.4.8 Acoustic coupling shall be achieved by contact or couplant column using a liquid medium suitable for
the purpose. An environmentally safe agent may be required to promote wetting, however, no residue shall
remain on the pipe surface after the liquid has evaporated.
The method used for acoustic coupling monitoring and the loss in signal strength defining a loss of return
signal (loss of coupling) shall be described.
Transducers
E.2.4.9 Prior to the start of field weld examination, details of the types and numbers of transducers or
focal laws shall be specified. Once agreed, there shall not be any transducer or focal law design changes
made without prior agreement. Transducers other than phased arrays shall be characterised according to
EN12668-2. Transducers shall be documented with respect to manufacturer, type, characteristics and unique
identification (serial number).
Transducer characteristics shall include (not all parameters are applicable to phased array transducers):
—
—
—
—
—
—
—
—
frequency
beam angle
wedge characteristics
beam size (Not relevant for PA probes)
pulse shape
pulse length
signal to noise (Not relevant for PA probes)
focus point and length for focused transducers.
In addition, the following characteristics shall be included for phased array probes:
— Number of elements
— pitch
— Size of elements
E.2.4.10 Transducers used for zonal discrimination shall give signals from adjacent zones (over-trace), given
that there is no shift in weld bevel angle between the zones. For adjacent zones of comparable size and with
equal calibration sensitivity, the over-trace shall be within 15% FSH to 50% FSH when the peak signal from
the calibration reflector representing the zone of interest is set to 80% FSH.
E.2.4.11 TOFD (frequency, standoff, crystal size, pulse length, etc) shall be optimized for detection
sensitivity, spatial resolution, OD and ID dead zones (See [E.2.4.5]).
E.2.4.12 Transducer wedges shall be contoured to match the curvature of the pipe.
E.2.4.13 Transducer/wedge surface wear shall be monitored during the course of operations.
E.2.4.14 Software modules which allows for automated compensation and correction for any essential
parameter can be used, provided that correct function is qualified and demonstrated prior to use.
E.2.5 Calibration blocks
E.2.5.1 Calibration blocks shall be used to set AUT system sensitivity, and to verify the inspection system for
field inspection and to monitor the ongoing system performance. Calibration blocks shall be manufactured
from a section of pipeline specific linepipe. The wall thickness of the pipe used for calibration blocks shall
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preferably correspond to the nominal wall thickness of the pipes used, unless a number of calibration blocks
are needed to cover wall thickness variations outside the limitations given in [E.2.1.7].
E.2.5.2 Acoustic velocity and attenuation measurements shall be performed on material from all sources of
pipe material supply to be used. These measurements shall be performed according to [E.11.1] unless an
equivalent method is agreed. If differences in acoustic velocity for the same nominal wall thickness from any
source of supply results in a beam angle variation of more than 1.5°, specific calibration blocks shall be made
for material from each source of supply showing such variations.
E.2.5.3 Details of the specific weld bevel geometries including relevant dimensions and tolerances shall be
provided in order to determine the particulars and numbers of calibration blocks required.
E.2.5.4 Type and size of reference reflectors shall be determined by the required sensitivity to achieve
the necessary probability of detection (PoD) and sizing capability as determined by the smallest allowable
imperfection deriving from the agreed acceptance criteria. The calibration block design shall provide
adequate reflectors for the relevant defects at inspection, taking into account the applied ultrasonic
technique. The principal reference reflectors shall be flat bottom holes (FBHs) and surface notches. Other
reflector dimensions and types may be used, if it is demonstrated during the system qualification that the
imperfection detection and sizing capabilities of the system is acceptable. Specific reflectors for ToFD shall be
incorporated, to confirm TOFD system functionality.
E.2.5.5 The calibration blocks shall be designed with sufficient surface area so that the complete transducer
array will traverse the target areas in a single pass.
E.2.5.6 Drawings showing the design details for each type of calibration block shall be prepared. The
drawings shall show:
— the specific weld bevel geometry, dimensions and tolerances
— the height and position of examination zones, if applicable
— the reference reflectors required and their relative positions, dimensions and orientations.
E.2.5.7 The calibration block shall be identified with a hard stamped unique serial number providing
traceability to the examination work and the material source of supply for which the standard was
manufactured. Records of the correlation between serial number and wall thickness, bevel design, diameter,
and ultrasound velocity shall be kept and be available.
The machining tolerances for calibration reflectors are:
-
Hole diameters
± 0.2 mm
-
Flatness of FBH
± 0.1 mm
-
All pertinent angles
± 1°
-
Notch depth
± 0.1 mm
-
Notch length
± 0.5 mm
-
Central position of reference reflectors
± 0.1 mm
-
Hole depth
± 0.2 mm.
E.2.5.8 The lateral position of all reference reflectors shall be such that there will be no interference from
adjacent reflectors, or from the edges of the blocks.
E.2.5.9 Holes shall be protected from degradation by covering the hole with a suitable sealant. If it can be
proven that filling of surface notches and other near surface reflectors may influence the reflecting ability of
the reference reflector, avoidance of filling can be subject to agreement.
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E.2.5.10 Dimensional verification of all reference reflectors and their position shall be performed and
recorded according to a documented procedure. Replicas of all reflectors shall be produced and appropriately
labelled and stored for reference to the calibration block and shall be available for review for all parties
involved. Each reflector shall be verified by manual ultrasonic testing with a probe relevant for the AUT
testing to ensure that the reference reflector pairs yield reflective signals within ±3dB. This requirement is
not applicable for asymmetric reference block designs.
E.2.5.11 Whenever possible, an AUT system similar to that used during field inspection shall be successfully
calibrated against the calibration block after dimensional verification of the block. The set-up data shall
be recorded and the same data used to verify that any additional/spare calibration blocks will not give
significantly different calibration results.
E.2.5.12 A calibration block register shall be established. The register shall include all calibration blocks,
including spare blocks, to be used, identified with a unique serial number and include the drawings,
dimensional verification records, ultrasound velocity, name of the plate/pipe manufacturer and the heat
number.
E.2.5.13 Acoustic properties of calibration block material shall be determined as defined in [E.11]. For
seamed pipe, the acoustic property comparison between pipe and seam welds shall be provided. When
attenuation due to surface condition shows variation of one standard deviation greater than ±3dB (total
range 6 dB), impact of surface condition on detection and sizing accuracy shall be analyzed. The data
and analysis shall be reviewed with the involved parties. Calibration block design shall take this data into
consideration. The inspection company should decide the best methodology for measurement of attenuation,
which shall be accepted by all involved parties.
E.2.5.14 The calibration block shall include the following reflectors for TOFD, as a minimum:
— An ID V-notch of suitable size to document the size of the ID surface dead zone
— An OD V-notch of suitable size to document the size of the ID surface dead zone.
E.2.5.15 Applicable to clad and lined pipe welds applications: A transfer measurement procedure shall be
estabilshed in order to ensure adequate inspection sensitivity of welds. The procedure shall include tests on a
piece of an acutal project weld. The weld shall be made from representative production material using project
specific approved welding procedure.
E.2.5.16 Applicable to carbon steel zonal discrimination setup: The reference block shall include: FBH of not
larger than 3 mm positioned on the position of the theoretical weld fusion line in the reference block, OD and
ID surface notches, volumetric reflectors 1.5 mm FBH.
E.2.5.17 Applicable to ultrasonic imaging techniques: The reference block shall include embedded reflectors
not larger than 3 mm at different depths and orientations in the weld, in addition to surface notches at OD
and ID surface.
The amount, position and orientations of the reflectors shall be sufficient to document adequate inspection
sensitivity in the full weld area. It shall be demonstrated that the system procedure covers the HAZ,
reference is made to [E.2.1.3].
E.2.5.18 For calibration blocks made of seamless pipes (SMLS), thickness survey shall be performed on
calibration block blank in no greater than 20mm x 20mm grids. The wall thickness variation shall be within
the specified wall thickness variation. The average thickness shall be used to define calibration block’s
applicable thickness range. Maximum and minimum wall thickness of each strip shall be included in the
calibration block package.
E.2.5.19 Applicable for all calibration blocks used with AUT setups including thickness measurement channel:
The accuracy of the wall thickness channels shall be verified. The thickness channel shall have the capability
to measure pipe wall thickness to accuracy better than ±1.0% of the total wall thickness.
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E.2.6 Recorder set-up
E.2.6.1 The maximum allowable circumferential scanning velocity shall be determined so that there are at
least 3 pulse firings within each 6 dB beam width at the appropriate operating distance of all transducers
within the an array, as described in [D.8.4.12].
E.2.6.2 Distance markers shall be provided on the recording at intervals not exceeding 100 mm of
circumferential weld length.
E.2.7 Circumferential scanning velocity
E.2.7.1 The maximum scanning velocity shall be determined such that there is no evidence of strip losing
data in the recorded scans.The same scanning velocity shall be used during calibration verification and weld
inspection.
E.2.8 Power supply
E.2.8.1 Constant power supply shall be ensured for the ultrasonic system. There shall be provisions for
alternative power supply in case of failure in the main power supply. There shall be no loss of inspection data
as a result of a possible power failure.
E.2.9 Software
E.2.9.1 All recording, data handling and presenting software, including changes thereto, shall be covered by
the quality assurance system and all software versions shall be identifiable by a unique version number.
E.2.9.2 The software version number, and for phased array equipment also each identified set-up
(executable focal law programme) in use, shall be clearly observable on all display and printout presentations
of calibration and examination results.
E.2.9.3 For phased array equipment, each identified set-up shall be available for review. Focal law versioning
software shall allow tracking of all parameter changes through the entire course of operation. The cumulative
change during production shall be in accordance with [E.5.3.1].
E.2.9.4 Software updates shall not be performed on systems during field examination use.
E.2.10 Reference line, band position and coating cut-back
Reference line
E.2.10.1 Prior to welding a reference line shall be placed on the pipe surface at a fixed distance from the
centerline of the weld preparation on the inspection band side. This reference line shall be used to ensure
that the band is adjusted to the same distance from the weld centerline as to that of the calibration block.
Guiding band positioning
E.2.10.2 The tolerance for band positioning is ± 1 mm relative to the weld centerline, unless it can be
demonstrated and qualified wider tolerance for band offset for the AUT scanner setup applied (e.g. for
ultrasonic imaging techniques).
The band can be positioned either wholly on the bare pipe or on the corrosion coating.
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Positioning of the band on the corrosion coating will require that the coating thickness is not excessive and
that the coating is sufficiently flat and will remain hard enough at the temperatures in the pipe resulting from
preheat and welding to avoid that the band supports slips or penetrates the coating.
Positioning of the band partly on bare pipe and partly on the corrosion coating may result in instability
problems for scanner and should be avoided, unless corrective actions to band saddles are made to
accommodate its position.
Coating cut back
E.2.10.3 The cut-back of the corrosion coating to bare pipe shall be wide enough to accommodate the
footprint of all transducers at the required stand-off distance + minimum 20 mm. The cut-back of any weight
coating shall allow placing the band wholly on the bare pipe or on the corrosion coating or partly on both, as
applicable, and sufficient to avoid interference between weight coating and scanner.
The coating cut back required allowing for scanner mounting and movement shall be clearly identified in the
operating manuals.
E.2.11 Reference line tools
E.2.11.1 The tool used to align the scanning band to the reference line shall be adjusted to account for weld
shrinkage, when shrinkage is considered to be greater than 1 mm. Shrinkage is determined by marking
the reference line on both pipe ends during WPQ or for the first 25 welds, and then measuring the distance
between them after welding.
The tools used for marking the reference line for band positioning, shall give accuracy in the position of the
reference line of ± 0.5 mm relative to the bevel root face. The accuracy of each reference line tool shall be
documented and each tool shall be uniquely identified.
E.2.12 Operators
E.2.12.1 Details of each AUT operator shall be provided prior to start of field weld examination.
E.2.12.2 Operators performing interpretation shall be certified to Level 2 by a Certification body or
Authorised qualifying body in accordance with ISO 9712 or the ASNT Central Certification Program (ACCP).
In addition they shall document adequate training and field experience with the equipment in question, by
passing a specific and practical examination. If requested, they shall be able to demonstrate their capabilities
with regard to calibrating the equipment, performing an operational test under field conditions and evaluating
size, nature and location of imperfections.
E.2.12.3 Operators who are not accepted shall not be used, and operators shall not be substituted without
prior approval. In case additional operators are required, details of these shall be accepted before they start
to work.
E.2.12.4 One individual shall be designated to be responsible for the conduct of the ultrasonic personnel, the
performance of equipment, spare part availability and inspection work, including reports and records.
E.2.12.5 The operators shall have access to technical support from one individual qualified to Level 3 at any
time during execution of the examination work.
E.2.13 Spares
E.2.13.1 There shall be a sufficient number of spare parts available at the place of examination to ensure
that the work can proceed without interruptions.
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E.2.14 Slave monitors
E.2.14.1 The system shall include the possibility to provide slave monitors for use by supervising personnel,
if agreed.
E.3 Procedure
E.3.1 General
E.3.1.1 A detailed AUT Procedure shall be prepared for each weld joint geometry to be examined prior to
the start of any welding. The procedure is as a minimum, and as relevant for the equipment in question, to
include:
— functional description of equipment
— reference standards and guidelines controlling equipment maintenance
— instructions for scanning device, ultrasonic instrument, ultrasonic electronics, hard- and software for
recording, processing, display, presentation and storage of inspection data
— number of examination zones for each wall thickness to be examined, as relevant
— transducer configuration(s), characteristics, types, coverage; and/or focal law details
— description/drawings of calibration block(s), including type, size and location of all calibration reflectors
— pre-examination checks of equipment
— methodology for sensitivity setting and for fusion zone transducers; overtrace (signal amplitude from
adjacent zones) requirements consistent with the overtrace used as basis for establishing height sizing
corrections for amplitude sizing
— gate settings
— equipment settings
— threshold settings
— the added gain above PRL ([E.4.1.2]) to be used for mapping channels
— dynamic verification of set-up
— signal strength defining a loss of return signal (loss of coupling)
— visual examination of scanning area, including surface condition and preparation
— identification of inspection starting point, scanning direction, and indication of length inspected
— method for scanner alignment and maintenance of alignment
— verification of reference line and guide band positioning
— maximum allowed temperature range
— control of temperature differentials (pipe and calibration block)
— calibration intervals
— calibration records
— couplant, coupling and coupling control
— operational checks and field maintenance
— transducer and overall functional checks
— height, depth and length sizing methodology
— acceptance criteria, or reference thereto
— instructions for reporting including example of recorder chart and forms to be used
— spare part philosophy.
— TOFD crossover and corresponding depth
— Focal law versioning system to track parameter changes and prevent unauthorised changes beyond
agreed limits
— Focal law controlling parameters and their equivalences in terms of required changing limits.
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E.3.1.2 The AUT procedure shall be submitted for acceptance.
E.4 Calibration (sensitivity setting)
E.4.1 Initial static calibration
Transducer positioning and primary reference sensitivity
E.4.1.1 The system shall be optimised for field inspection in accordance with the details given in the AUT
procedure and using the relevant calibration block(s). The calibration block shall have the same orientation
(vertical/horizontal) as the pipe to be tested, unless it has been proven through the qualification tests that
differences in response are negligible.
E.4.1.2 The gain level required to produce the peak signal response is the Primary Reference Level (PRL) for
that reflector.
Zonal discrimination fusion zone channels
E.4.1.3 Pulse echo and tandem transducers shall be positioned at its operating (stand-off) position and
adjusted to provide a peak signal from its calibration reflector. In the case of phased arrays, the focal laws
shall be designed to provide a peak signal from each of the calibration reflectors as appropriate. This signal
shall be adjusted to the specified percentage of full screen height (FSH).
Carbon steel applications
E.4.1.4 For single TOFD channels, the transducer spacing shall be selected to place the theoretical crossing
of beam centres at the weld centreline at 66 to 95% of the wall thickness.
For double TOFD channels the theoretical crossing of beam centres at the weld centreline shall be at 66
to 95% of the wall thickness for one channel and approximately 33% of the wall thickness for the other
channel.
The amplitude of the lateral wave shall be between 40 and 80% of full screen height (FSH). In cases when
use of the lateral wave is not applicable, e.g. surface conditions and steep beam angles, the amplitude of the
back wall signal shall be set at between 12 to 24 dB above FSH. When use of neither the lateral wave nor the
back wall signal is applicable, the sensitivity should be set such that the noise level is between 5 and 10% of
FSH.
Mapping channels
E.4.1.5 Each transducer shall be positioned at its operating (stand-off) position and adjusted to provide a
peak signal from its calibration reflector. In the case of phased arrays, the focal laws shall be designed to
provide a peak signal from each of the calibration reflectors as appropriate. This signal shall be adjusted to
the specified percentage of FSH.
Additional gain shall not be added during sensitivity setting, dynamic calibration and calibration verification
during field examination.
E.4.1.6 The required added gain for volumetric mapping channels shall be no smaller than 8 dB above PRL.
Exception can be for inspection of clad and lined weld.
E.4.1.7 The mapping display threshold for the root, cap, and volumetric channels shall be set at as close
as possible to background levels to provide additional information on potential defects. The software shall
provide means to continuously adjust display threshold level for ease of defect characterization.
CRA and coarse grain applications
E.4.1.8 For CRA applications, added gain for mapping channels shall be determined through AUT
qualification/validation and scanning results of development and procedure qualification welds.
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E.4.2 Gate settings
E.4.2.1 With each transducer positioned for a peak signal response from the calibration reflector the
detection gates shall be set as detailed in the agreed AUT procedure and as detailed below.
Fusion zone channels
E.4.2.2 Applicable for zonal discrimination setup: The detection gates are to be set with each transducer/
focal law positioned for the peak signal response from the calibration reflector. The gate shall start before
the theoretical weld preparation and a suitable allowance shall be included to allow for the width of the heat
affected zone, so that complete coverage of the heat affected zone is achieved. The gate ends shall at least
be after the theoretical weld centreline, including a suitable allowance for offset of the weld centreline after
welding.
E.4.2.3 For specific applications, e.g. for CRA weldments with angle compression waves with the reference
reflectors positioned at the far side of the weld, an extension of the gate onto the far bevel and HAZ is
required.
Similar considerations may apply in the root area related to monitoring of guidance band offset.
ToFD technique
E.4.2.4 Ideally the time gate start should be at least 1 μs prior to the time of arrival of the lateral wave,
and should at least extend up to the first back wall echo. Because mode converted echoes can be of use in
identifying imperfections, it is required that the time gate also includes the time of arrival of the first mode
converted back wall echo.
E.4.2.5 As a minimum requirement, the time gate shall at least cover the depth region of interest.
E.4.2.6 Where a smaller time gate is appropriate, it will be necessary to demonstrate that the imperfection
detection capabilities are not impaired.
Mapping channels
E.4.2.7 The mapping channels shall encompass the HAZ and the total weld volume dedicated to the
transducer or focal law.
E.4.3 Evaluation threshold
Threshold level
E.4.3.1 It shall be verified that the evaluation threshold level, based on data from the AUT system
qualification, is set low enough to detect the minimum height critical defect identified in the acceptance
criteria (see [E.8.3]).
E.4.3.2 The evaluation threshold levels shall in any case not be set higher than required in the following.
Fusion zone channels
E.4.3.3 The evaluation threshold for fusion zone channels shall be at least 6 dB more sensitive than the
reference reflector, unless a different sensitivity is required for detection of indications depending upon the
size of reflectors used and the applicable acceptance criteria.
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E.4.4 TOFD technique
E.4.4.1
E.4.4.2 The recording threshold for ToFD is not recommended to be changed from the calibration threshold.
However, a change of threshold may be prescribed in the procedure.
Mapping channels
E.4.4.3 The evaluation threshold for mapping channels shall be at least 12 dB more sensitive than the
reference reflector signal PRL for volumetric indications and at least 8 dB more sensitive than PRL for linear
indications.
For CRA material welds the evaluation threshold for mapping channels shall be at least 8 dB more sensitive
than the reference reflector signal or as qualified during the validation of the system.
E.4.5 Dynamic calibration
General requirements, Detection channels
E.4.5.1 With the system optimised, the calibration block shall be scanned. The position accuracy of the
recorded reflectors relative to each other shall be within ± 2 mm, and with respect to the zero start within ±
10 mm.
E.4.5.2 For all phased array focal laws or transducers the recording media shall indicate the required
percentage of FSH and locate signals from each calibration reflector in its correctly assigned position.
E.4.5.3 For all reference reflectors used to set and verify sensitivity for the setup, amplitude response shall
not deviate by more than ±2dB from the initial calibration.
E.4.5.4 If the dynamic calibration of out of above defined limits, recalibration shall be performed to verify
that it is not caused by scanner mechanical instability. More than three attempts shall not be permitted in
production to bring the calibration within tolerance. When this occurs, the operator shall perform thorough
operational check and perform re-calibration. The changes in parameters shall be logged.
Coupling monitor channels
E.4.5.5 The coupling monitor channels shall indicate no loss of return signal as required by the procedure.
CRA and coarse grain applications
E.4.5.6 Applicable to all CRA applications: It shall be demonstrated an adequate signal-to-noise ratio with
the AUT setup selected for inspection, the noise level shall be minimum 6 dB below PRL at the target area for
each channel or focal law. This does not apply to creeping wave channels.
Carbon steel applications
E.4.5.7 Over trace shall meet the requirements of [E.2.4.13].
E.4.6 Recording of set-up data
E.4.6.1 Sufficient data shall be recorded on a set-up sheet to enable a duplication of the original set-up at
any stage during field inspection.
As a minimum the PRL, the signal to noise (S/N) ratio, the stand-off distance for each transducer, and
settings for gate start and gate length for each channel shall be recorded.
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E.4.6.2 The calibration qualification chart shall be used as the inspection quality standard to which
subsequently produced calibration charts may be judged for acceptability. This recording shall be kept
with the system Log Book. For phased array equipment also the identified set-up (executable focal law
programme) used shall be recorded.
E.4.6.3 In addition to the qualification chart required above, any changes in the data records made in
accordance with [E.4.6.1] above shall be recorded.
The set-up sheet shall after dynamic calibration include as a minimum:
—
—
—
—
—
—
—
PRL and the signal to noise (S/N) ratio for each transducer or focal law (if phased array)
the stand-off distance for each transducer and alignment of tandem transducers
the settings for gate start and gate length for each channel
the gain to be added to any channel during field examination
filtering settings, when applicable
the order of transmitters and receivers
calibration block identification.
E.5 Field inspection
E.5.1 Inspection requirements
General requirements
E.5.1.1 The ultrasonic system used for examination during production shall in all essential aspects be in
compliance with the set-up and configuration of the system used for system qualification (see [E.8]). Any
change of set-up data, components, calibration block from the qualified procedure shall be noted to all
involved parties and be made available for review upon request.
Documentation
E.5.1.2 The following documentation shall be available at the place of field examination:
An AUT system dossier for each operating AUT system including performance/characteristics data and
identification of at least:
—
—
—
—
—
—
pulser/receiver
transducers
umbilical
encoder
software version and executable focal law programmes (when applicable)
other essential equipment.
An AUT system spare parts dossier including:
— performance/characteristics data and identification of essential spare parts.
A calibration block register including:
— the documentation for each calibration block, including spares, as required by [E.2.5.13].
An AUT personnel qualification dossier including:
— certificates for all AUT personnel.
An AUT procedures dossier including:
— AUT procedures to be applied
— AUT system check and maintenance instructions
— work instructions for AUT personnel.
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Additional information including:
— other NDT procedures
— AUT and NDT acceptance criteria.
E.5.1.3 The AUT system dossier shall be updated when changes of parts/components are made and shall at
all times reflect the current configuration of the AUT system in use.
The AUT system spare parts dossier shall be updated whenever parts/components are replaced or new parts/
components arrive and shall at all times reflect the number of spares available.
System log book
E.5.1.4 The system log book shall be kept at the place of inspection, and be made available for review upon
request.
The system log book shall be continuously updated and at least include the following information:
—
—
—
—
—
—
set-up data as required in [E.4.5]
the calibration qualification chart(s)
replacement of main components with spares from stock
replacement of calibration block
results from operational checks
results of periodical verifications (linearity checks, calibration block wear, element verification for phased
array transducers etc.).
E.5.1.5 Soft copy recordings for each calibration scan (and phased array set up file, if appropriate) shall be
included sequentially with the weld inspection charts. If agreed, 1 calibration for each 10 consecutive ones,
shall be provided in hard copy together with each weld inspection scans. The last weld number examined
before calibration and the time at which the calibration was performed shall appear on each calibration chart.
Pre- examination tests
E.5.1.6 Before the ultrasonic system is used for field examination of production welds the system shall be
tested. After calibration of the complete system using the applicable set-up sheet parameters, the calibration
block shall be scanned. If any of the echo amplitudes from the reflectors of the calibration block deviate more
than 2 dB from the initial calibration, corrections shall be made.
The system shall not be used until 5 consecutive satisfactory scans are obtained.
The total noise level from transducer, material including weld, electronics and any other sources shall not
exceed the single output representing the smallest critical defect.
At least one scan shall be performed with the scanning surface wiped dry. The coupling monitor channels
shall indicate loss of return signal as required by the procedure.
In addition, a power failure shall be simulated and operation of the system on the alternative power source
with no loss or corruption of examination data shall be verified.
Verification of calibration
E.5.1.7 The calibration of the system shall be verified by scanning the calibration block before and after
inspection of each weld. The gain added to any channel for field examination shall be removed during
verification scans.
E.5.1.8 One calibration scan is required before and after each weld inspected for following welds: procedure
welds, welder qualification welds, fatigue sensitive welds, first 20 production welds, first 20 consecutive
welds after an unacceptable calibration, fatigue sensitive welds, repair welds, CRA welds. For other types of
welds, the frequency of calibration scans may be reduced to a minimum of 1 scan for each 10 consecutive
welds. If a calibration scan fails, the preceeding welds counting back to last acceptable calibration shall be rescanned.
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E.5.1.9 The verification scans shall not show amplitude changes in any channel outside ± 2 dB from the
reference calibration chart (see [E.4.5.1]).
E.5.1.10 The peak signal responses from each verification scan shall be recorded. Any gain changes required
to maintain the PRL in the set-up sheet (see [E.4.5.2]) shall be recorded.
Re-calibration
E.5.1.11 The system shall be re-calibrated and a new reference calibration chart shall be established
according to [E.4] if a verification scans shows amplitude changes in any channel outside ± 2 dB from the
reference calibration chart or if gain changes outside ± 2 dB are required to maintain the PRL in the set-up
sheet.
E.5.1.12 The system shall also be re-calibrated and a new reference calibration chart and a new set-up sheet
established:
—
—
—
—
—
—
at any change of calibration block
at any change of nominal wall thickness
at any change of components, transducers, wedges or after resurfacing of transducers
before and after examination of repairs, if system is outside initial tolerances
after any adjustments to scanner head or transducers
after any change in the order of transmitters and receivers and filtering settings.
Weld identification
E.5.1.13 Each weld shall be numbered in the sequence used in the pipe tracking system.
E.5.1.14 The starting point for each scan shall be clearly marked on the pipe and the scan direction shall be
clearly marked using an arrow. If the scanning direction is changed from the regular direction, this shall be
noted on the records of the scan.
E.5.2 Operational checks
E.5.2.1 Operational checks shall be performed according to a documented procedure. The execution of and
the results of the operational checks shall be recorded in the system log book.
E.5.2.2 The following operational checks shall be performed for every weld inspected:
— reference line shall be within required tolerance and clearly marked around the pipe circumference
— the scanning surface shall be free of weld spatter and other that may interfere with the movement of
transducers
— physical damage and loose connections in the band. band position shall be within a tolerance of maximum
± 1.0 mm
— the pipe surface temperature and the difference between calibration block temperature and pipe
temperature shall be within the required tolerance.
— The entire circumference of the weld has been completely inspected with sufficient overlap
E.5.2.3 The following operational checks shall be performed daily or at least once per shift:
— the scanner head shall be checked for physical damage and loose connections
— the bevel prepared at the bevelling station shall be of the specific weld bevel geometry, dimensions and
tolerances shown on the drawings of the calibration block in use
— the calibration block in use shall be checked for physical damage and scanning tracks
— transducers shall not be rocking in the scanner and shall be in firm contact with the scanning surface.
the transducers shall be firmly screwed onto the wedges. the transducer wear faces (wedges) shall be
checked for scores which may cause local loss of contact
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— the transducer stand-off distance shall be as recorded in the set-up sheet within ± 0.5 mm
— the position accuracy of the chart distance markers shall be shall be ± 1 cm or better.
— Transducer element verification check
E.5.2.4 Other operational checks such as linearity checks and field maintenance shall be performed
according to the AUT system check and maintenance instructions.
Guidance note:
Checking of transducer angles may require a custom made block since the standard V1 block may not be wide enough to include
the carbide tips during checks and due to that the gap between the V1 block and transducers with radiused surfaces will be too
large for adequate checks.
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
E.5.2.5 A verification scan shall be performed prior to resuming inspection after the operational checks
required in [E.5.2.3] and any field maintenance. The verification scan shall meet the requirements given in
[E.5.1.9].
If necessary, a re-calibration shall be performed and a new reference calibration chart shall be established
according to [E.4].
E.5.2.6 Phased Array transducer with 2 adjacent dead elements or minimum 10% dead elements of the full
array shall be replaced, unless:
— The identical probe and wedge configuration (with dead elements) has been used and successfully passed
qualification program or
— Justification that channels with dead element(s) can maintain US/DS symmetry requirements has been
approved by all involved parties.
E.5.3 Adjustments of the automated ultrasonic testing system
E.5.3.1 Adjustments to the AUT system other than correcting deviations from the qualified set-up sheet
following operational checks and maintenance shall not be performed.
During production, cumulative change of parameters shall be limited to: gain adjustment of ±6dB, effective
inspection angles of ±1.5 degrees, effective index change ±2.0mm while over trace requirements in
[E.2.4.13] are still maintained.
E.5.3.2 Practices such as changing transducer angles by lifting transducer front and back by adjusting
of carbides, changing stand-off distances and changing the order of transmitter/receivers etc. are not
permitted.
E.5.4 Workmanship acceptance criteria
E.5.4.1 Acceptance criteria applicable for automated ultrasonic testing (AUT) of pipeline girth welds exposed
to total nominal strains <0.4% are given in Table E-1. Table E-1 is not applicable to C-Mn pipes and low
alloy steel subjected to sour service conditions or to fatigue sensitive welds. Acceptance criteria for fatigue
sensitive welds are provided in Table E-2. The AUT system shall be qualified according to this appendix.
The acceptance criteria of Table E-1 and Table E-2 assumes a height sizing accuracy within ±1 mm, a
depth estimate accuracy of ±2 mm and a length sizing accuracy within ±5 mm, as evaluated according to
clause [E.8.4.2]. The acceptance criteria of Table E-1 and Table E-2 are therefore only valid as long as the
height sizing accuracy is documented to be within ±1mm upon the qualification. The inspection threshold
is recommended set at 40% FSH for pulse echo zones. In addition, clause [E.8.4.1] shall be satisfied for
maximum acceptable imperfection heights specified in Table E-1.
E.5.4.2 For AUT system used for inspection of girth welds in pipelines of duplex stainless steel, CRA
and clad/lined materials, a probability of rejection of 85% at a 95% confidence level or higher shall be
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documented through the qualification for defects in the root of heights smaller than 1.0 mm, considering the
applied AUT rejection criteria for root defects.
E.5.4.3 In order for Table E-1 to be applicable, requirements of [E.2.1.1] and [E.8.4.1] shall be satisfied.
Table E-1 Acceptance criteria for automated ultrasonic testing of girth welds
Base material
C-Mn and low alloy steels
5,7)
1) 2) 3)
Defect location
Acceptance criteria
Individual defect indications
Maximum accumulated length of
defect indications in any 300 mm
weld length
Root
Height: the lesser of 3.0 mm and
0.2 t
Surface
Length: t, but max. 25 mm
Embedded
6)
4)
Height: the lesser of 3.0 mm and
0.2 t
Length: 2t, but max. 50 mm
Root
8)
Up to 3 mm from inside surface,
and up to 1.5 mm above clad/liner
thickness for clad/lined steel
Height: max. 1 mm, the lesser of a
third of clad/liner thickness and 1
mm for clad/lined steel
Length: t, but max. 25 mm
Height: the lesser of 3.0 mm and
0.2 t
Duplex stainless steel, CRAs and clad/lined
Surface
steel
Length: t, but max. 25 mm
Embedded
6)
At least 3 mm from inside surface,
and at least 1.5 mm above clad/liner
thickness for clad/lined steel
Height: the lesser of 3.0 mm and
0.2 t
Length: 2t, but max. 50 mm
Cracks are not permitted.
9)
Porosity :
Accumulated length of porosity signals exceeding a threshold 12 dB below the PRL in the volumetric channels: For single
layer welds: 1.5% of the full circumferential length. For multi layer welds 3 t, max 100 mm in any 300 mm of weld
length. Isolated pores shall be evaluated as planar imperfections.
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Notes:
1)
Planar defects interaction shall be assessed according to the criteria of BS 7910. Interacting planar defects shall be
attributed effective defect dimensions according to BS 7910, and the effective defects so obtained shall meet the
above acceptance criteria.
2)
Imperfections above evaluation threshold in any intersection of the weld, which are located at the weld bevel of the
same side as the intersection, are not permitted.
3)
Systematic imperfections that are distributed at regular distances over the length of the weld are not permitted even
if the size of any single imperfection meets the requirements above.
4)
Acceptance criteria of Table D-4 shall also be satisfied.
5)
This table is not applicable for C-Mn and low alloy steels in sour service.
6)
If an embedded defect is located close to a surface, such that the ligament height is less than half the defect height,
the ligament height between the defect and the surface shall be included in the defect height, and the defect shall
be considered as a root or surface defect, as applicable.
7)
POD and sizing accuracy of the AUT system shall be according to [E.5.4.1].
8)
The probability of rejection (PoR) for a 1 mm high imperfection shall be qualified to be higher or equal to 85% at
95% confidence level.
9)
Any addition of gain from PRL during scanning shall be added to the threshold
E.5.4.4 Workmanship acceptance criteria, fatigue sensitive welds
Acceptance criteria and the AUT system performance for fatigue sensitive welds shall be in accordance with
[E.5.4] and additional requirements of Table E-2.
Table E-2 Acceptance criteria for automated ultrasonic testing of girth welds, fatigue sensitive
welds
Acceptance criteria
Base material
C-Mn and low alloy steels
5,7)
Defect location
Individual defect
indications
Maximum accumulated
length of defect
indications in any 300
mm weld length
Root
Height: the lesser
of 1 mm and 0.2 t
Length: t, but max. 25
4)
mm
Height: the lesser
of 3 mm and 0.2 t
Length: 2t, but max. 50
mm
Surface
Embedded
Duplex stainless steel, CRAs and clad/lined
steel
1) 2) 3)
6)
8)
Root
Up to 3 mm from
inside surface, and up to
1.5 mm above clad/liner
thickness for clad/lined steel
Height: max. 1
Length: t, but max. 25
mm, the lesser of
mm
a third of clad/liner
thickness and 1
mm for clad/lined
steel;
Surface
Height: the lesser
of 1 mm and 0.2 t
Length: t, but max. 25
mm
Height: the lesser
of 3 mm and 0.2 t
Length: 2t, but max. 50
mm
6)
Embedded
At least 3 mm
from inside surface, and at
least 1.5 mm above clad/
liner thickness for clad/lined
steel
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Cracks are not permitted.
9)
Porosity Accumulated length of porosity signals exceeding a threshold 12 dB below the PRL in the volumetric channels:
For single layer welds: 1.5% of the full circumferential length. For multi layer welds 3 t, max 100 mm in any 300 mm of
weld length. Isolated pores shall be evaluated as planar imperfections.
1)
Planar defects interaction shall be assessed according to the criteria of BS 7910. Interacting planar defects shall be
attributed equivalent defect dimensions according to BS 7910, and the effective defects so obtained shall meet the
above acceptance criteria.
2)
Imperfections above threshold in any intersection of the weld, which are located at the weld bevel of the same side
as the intersection, are not permitted.
3)
Systematic imperfections that are distributed at regular distances over the length of the weld are not permitted even
if the size of any single imperfection meets the requirements above.
4)
Acceptance criteria of Table D-4 shall also be satisfied.
5)
This table is not applicable for C-Mn and low alloy steels in sour service.
6)
If an embedded defect is located close to a surface, such that the ligament height is less than half the defect height,
the ligament height between the defect and the surface shall be included in the defect height, and the defect shall
be considered as a root or surface defect, as applicable.
7)
POD and sizing accuracy of the AUT system shall be according to [E.5.4.1].
8)
The Probability of Rejection (PoR) for a 1 mm high imperfection shall be qualified to be higher or equal to 85% at
95% confidence level.
9)
Any addition of gain from PRL during scanning shall be added to the threshold
E.6 Re-examination of welds
E.6.1 General
E.6.1.1 Welds shall be re-examined whenever any of the following occur:
Sensitivity
E.6.1.2 Welds examined at a sensitivity outside ± 2 dB from the PRL shall be re-examined.
Coupling loss
E.6.1.3 Welds exhibiting a loss of acoustic coupling over a circumferential distance which exceeds the
minimum allowable defect length as derived from applicable acceptance criteria, shall be re-examined. If the
coupling loss still persist and cannot be resolved after cleaning/brushing the surface, then the affected area
of weld may be subjected to Manual UT assessment and any other channels generated by separate probes
(i.e. TOFD) if these channels are considered not affected.
Out of calibration
E.6.1.4 If a verification scan shows that the system is in any way out of calibration, all welds examined since
the last successful verification scan shall be re-examined.
E.7 Evaluation and reporting
E.7.1 Evaluation of indications
E.7.1.1 Indications from weld imperfections shall be evaluated against the defect acceptance criteria.
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E.7.1.2 The AUT procedure shall describe the methodology to determine indications height, depth and length
sizing. This includes rules to account for over trace and beam spread correction. All information available
shall be used in the evaluation to avoid under-sizing, - and excessive over-sizing of imperfections.
E.7.1.3 Indications recorded from sources other than weld imperfections shall be evaluated. Their nature
shall be clearly identified in the examination report.
E.7.1.4 All evaluations shall be completed immediately after examination of the weld.
E.7.2 Examination reports
E.7.2.1 The examination results shall be recorded on a standard ultrasonic report form. The reports shall be
made available on a daily basis or on demand.
E.7.2.2 The following items are as a minimum to be reported for each indication found to be not acceptable:
—
—
—
—
—
—
—
—
—
—
project reference
pipeline identification
weld identification/number
date
ultrasonic procedure number with associated revision
circumferential position of indication
height, depth and length of indication
transverse location of imperfections/indications (US, DS, Central)
maximum amplitude for each reported indication
indication type.
E.7.3 Inspection records
E.7.3.1 The following inspection records shall be provided:
—
—
—
—
a hard copy record of each weld examined
an assessment of the weld quality according to the acceptance criteria
hard copy records of all calibration scans
examination data in electronic form.
E.7.3.2 In lieu of hard copy records an alternative recording media is acceptable. Where weld interpretation
has been performed using digitally processed signals, the data files shall be stored and backed up
immediately following
the examination of each weld. The stored data shall be in the same format as used by the operator to assess
the acceptability of welds at the time of examination.
E.7.3.3 If agreed, a software package and one set of compatible hardware shall be provided in order to
allow the weld data file to be retrieved in the same manner as the operator viewed the data at the time of
inspection.
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E.8 Qualification
E.8.1 Scope and qualification
E.8.1.1 Automated ultrasonic systems used for linepipe girth weld inspection shall be qualified and the
performance of the system shall be documented.
For applications other than carbon steel girth weld examinations, specific requirements can apply and should
be agreed upon.
Prior to project use, any qualified AUT system shall be subject to project specific AUT validation if the
system is within the qualified range of validity, as specified in [E.9]. The scope of AUT validation shall be in
accordance with [E.9]. A reduced scope of validation may be agreed for welds exposed to nominal strains
< 0.4%, but shall comprise at least 12 imperfections, including minimum 3 observations for each group (ID
Surface, fill, OD Surface) and/or critical imperfection type.
E.8.2 General
E.8.2.1 The AUT system shall be qualified according to DNVGL-RP-F118 for the applications it is intended
used for. The qualification shall be based on the required performance as identified by the requirements for
Probability of Detection (PoD) and sizing ability; or, alternatively a requirement to defect rejection.
E.8.2.2 The qualification is AUT system specific and shall only be valid when all essential variables remain
nominally the same as covered by the documented qualification. This standard does not require a new
qualification to be performed provided that the documented performance i.e. PoD and sizing ability meets or
exceeds the requirements for the specific application being considered.
E.8.2.3 Qualification involves a technical evaluation of the AUT system and application in question combined
with any required practical tests.
E.8.2.4 The qualification shall be based on a detailed and agreed qualification programme, that covers the
following:
— Qualification objective, i.e. materials, weld process, groove geometries and performance requirement
(PoD and Sizing accuracy).
— Details of trials to establish and document environmental and application related tolerances such as
temperature consistency, beam and focal law consistency, mechanical stability and electronic interference
sensitivity.
— Details of reliability trials and trial welds, including trial weld seeded imperfection map.
E.8.2.5 The agreed qualification programme and its implementation shall be supervised and endorsed by a
recognised and competent independent 3rd party.
E.8.2.6 The requirements in this section are applicable for the following types of qualification programs:
— Full scale qualification program aimed to quantify probability and sizing accuracy of an AUT procedure to
document fitness for purpose for a specific application;
— Pre qualification to document the capabilities of an AUT procedure prior to employment on specific
applications.
— When required by fitness for purpose approach to define AUT acceptance criteria by ECA.
E.8.2.7 A qualification methodology document shall be established and agreed upon by all involved parties
upfront qualification.
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E.8.3 Scope
E.8.3.1 A qualification programme shall document the following:
—
—
—
—
—
—
fulfilment of the requirements to AUT systems according to this appendix
the repeatability of the AUT system under variable examination conditions
the sensitivity of the AUT system to the temperature of tested objects
the ability of the AUT system to detect defects of relevant types and sizes in relevant locations
the accuracy in sizing and locating imperfections.
correct functioning of automated features and interpretation driven by software.
E.8.4 Requirements
Detection
E.8.4.1 The detection ability of an AUT system shall be deemed sufficient if the probability of detecting a
defect of the smallest allowable height determined by an Engineering Critical Assessment (ECA) or by other
considerations is 90% shown at a 95% confidence level (i.e. a 90%|95% PoD).
Sizing accuracy
E.8.4.2 Sizing accuracy shall be established during the qualification programme. For this purpose it
is required to demonstrate the accuracy over the range of expected imperfection sizes. Based on the
determined sizing errors, the under sizing error tolerances giving less than or equal to 5% probability of
under sizing shall be determined and used in relation to any ECA specified defect sizes.
No specific tolerance is required for over sizing of indications. Over sizing of indications should however
be within reasonable limits since excessive oversizing will result in unnecessary repairs during pipeline
construction. A systematic over sizing, i.e. over sizing on average, of 0.8 mm or above shall lead to
investigations and corrective actions to reduce the over sizing in the affected parts of the AUT set-up.
Rejection
E.8.4.3 The detection criterion of [E.8.4.1] and the undersizing tolerance specified in [E.8.4.2] may be
combined into one rejection criterion: There shall be more than 85% probability of rejecting a defect, which
is not acceptable according to determined ECA criteria. This shall be shown at a 95% confidence level, i.e. a
Probability of Rejection (PoR) of 85%|95% is required. This rejection criterion approach may be preferable
when the two step process detection-sizing is not followed, e.g. when acceptance or rejection is based
directly on echo amplitudes, or solely on AUT reported imperfection sizes.
E.8.4.4 The AUT system shall be deemed unqualified for its purpose with respect to ECA determined nonacceptable defects if it is not possible to document adequate detection and sizing abilities according to
[E.8.4.1] and [E.8.4.2], or adequate rejection abilities according to [E.8.4.3].
E.8.5 Variables
E.8.5.1 Variables, which shall be taken into account during a qualification, include, but are not necessarily
limited to:
— welding method and groove geometry
— welding consumables (Distinction is made on materials with substantially differences in ultrasonic
response, for instance between C-Mn, 13% Cr, duplex or austenitic steels)
— base material (Distinction is made on materials with substantially differences in ultrasonic response, for
instance between C-Mn, 13% Cr, duplex or austenitic steels).
— wall thickness limitations
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—
—
—
—
—
—
—
—
—
—
—
—
pipe diameter limitations
temperature consistency
root and cap channels transducer set-up
transducer set-up for other channels (the number of these channels may be increased or decreased
provided there are no set-up changes)
focal law design procedure (Phased array probes only)
reference reflectors
system, data acquisition and data treatment
software version (except changes affecting viewing or display only)
AUT operator/interpreter training and qualification.
inspection sensitivity in longitudinal seam area
interpretation methodology
for CRA applications: clad thickness, pre-existing imperfections in clad layer, type of clad layer and clad
material.
E.8.6 Qualification programme
General
E.8.6.1 A full qualification programme for a specific application of an AUT system will in general comprise the
following stages:
1)
2)
3)
Review of the technical documentation of the AUT system
Review of the operating methodology for the AUT system
Review of the quality assurance system for development, verification, maintenance and operation of the
AUT system.
4) Review of available performance data for the AUT system.
5) Evaluation and conclusions based on the information made available.
6) Identification and evaluation of significant parameters and their variability.
7) Planning and execution of a repeatability test programme, see [E.8.8.5] and [E.8.8.6].
8) Planning and execution of a temperature sensitivity test programme, see [E.8.8.7] and [E.8.8.8].
9) Planning and execution of a reliability test programme, see [E.8.8.9] and [E.8.8.10].
10) Documentation of results from the repeatability and reliability test programmes.
11) Reference investigations by supplementary NDT and destructive testing.
12) Evaluation of results from repeatability, temperature sensitivity and detection ability and sizing accuracy
trials.
E.8.6.2 The extent of the qualification programme will reflect the range for which the AUT system is intended
to be used, as described in the general AUT procedure.
E.8.6.3 Practical tests of the AUT system is a requirement. Information pertaining to these practical tests is
given in [E.8.8].
For a full qualification historical qualification data, in compliance to the requirements of [E.8.7] and [E.8.8],
can be utilised if these data can be clearly identified and supported with all relevant documentation. However
the minimum amount of new data shall at least represent 50% of the total minimum required qualification
observations according to [E.8.7.4]. It shall be noted that once undergone a full qualification, the results are
valid as historical data for use according to this standard on similar configuration, see [E.10.1.1]. Validity for
specific configurations can be documented through validation scopes including a limited number of defective
welds and defects if deemed relevant.
E.8.6.4 Functioning of software modules that performs automated considerations with impact on the
inspection performance shall be demonstrated. Either by manufacturing and testing of suitable test blocks
or by designing the scope of defective welds such as the functionality will be demonstrated during reliability
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trials. Automated AUT scan interpretation algorithms will be sufficiently documented by the scope of
reliability trials described in this sub-section, and does not require specific trials. Function demonstration of
software module for automatic compensation of wall thickness variations requires a test piece where the full
wall thickness range is represented.
E.8.7 Test welds
E.8.7.1 Qualification testing shall be performed using test welds containing intentionally induced
imperfections typical of those expected to be present in welds produced with the welding methods to be
used. The preferred method for seeding intentional imperfections is by varying welding process parameters
to induce natural imperfections. However, machined imperfection techniques may substitute 70% of the
total number of imperfections in each imperfection group. See Table E-3. Hence a minimum of 30% natural
imperfections shall be part of the data population.
Machined planar imperfections shall be positioned and oriented at the weld fusion line. Machined imperfection
techniques shall not be used to produce ID and OD surface breaking imperfections due to the similarity to the
reference reflector for these channels. Small depth machined surface breaking imperfections, <0.5 mm, can
be accepted upon agreement between all involved parties.
E.8.7.2 The material and the weld geometry shall be as for the actual use of the equipment. Minor variations
to for instance the weld root groove, which are regarded irrelevant in relation to the AUT system, may be
acceptable.
If repair welds are to be covered by the qualification, a representative selection of these should also be
included.
E.8.7.3 The intentionally introduced imperfections shall vary in length, height and location. Too close spacing
and stacking of the imperfections shall be avoided. Due to the POD analysis requirement, it is required also
to include sizes which are smaller than, or around those expected using anticipated AUT threshold settings.
If a POR analysis shall be performed, imperfections of vertical sizes below the rejection threshold is required.
For the height sizing analysis, it is required to include some imperfections with sizes around the critical
imperfection sizes in Table E-1 and E-2.
E.8.7.4 As a minimum 29 imperfections, or ultrasonically independent parts of imperfections, is required for
each group of imperfections. Ultrasonically independent parts of imperfections are those several beam widths
apart. In order to show sufficient detection ability (90% POD) at the required confidence level (95%) the
number of imperfections and their variation in imperfection types and location is referenced in Table E-3.
E.8.7.5 The locations where imperfections were intentionally induced shall be recorded. The presence and
sizes of the induced imperfections in the test welds shall be confirmed as soon as possible after completion.
For this purpose the test welds shall be subject to supplementary NDT. For carbon steel applications, this
includes as a minimum independent TOFD inspection for buried imperfections, supplemented by PA-UT or
manual UT to cover the ID and OD surface areas. In addition, radiographic testing and any surface technique
(MT, ET) might be performed. For CRA applications, radiographic testing of the test welds shall be performed.
The reference point for all testing shall be the same and shall be indicated by hard stamping on the test
welds. The techniques used for this testing shall be optimised for the weld geometries in question. If agreed
by all parties, the AUT system to be qualified can be used for verification of quality of the seeded defective
welds.
E.8.7.6 The report from the supplemental NDT shall identify the actual imperfections present in the test
welds with respect to circumferential position, length, and height. The required number of observations
for the agreed scope of qualification, i.e. according to number and distribution provided in Table E-3,
shall be confirmed by supplemental NDT. Additional test welds shall be made if the number of confirmed
imperfections does not fulfill the requirements. The report shall be kept confidential.
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Table E-3 Numbers of deliberate imperfections for AUT qualification
Zonal discrimination, Cs-steel
Imperfection type
group
ID Surface
1,2,6,9
General
4
requirements
Clad and weld
overlay CRA
J-Bevel
V-Bevel
X-Bevel
29
29
29
29
29
29
29
29
29
29
29
29
29
29
29
29
29
2
4
2
2
2
Inter-Run LOF:
2
Slag
Inclusion:
2 Inter-run
LOF: 2
Slag inclusion: 2
120
93
91
1,5
Hot Pass Zone
1,7
Buried
OD Surface
Volumetric
1,3,8
10, 11
Other
Slag inclusion: 2
Inter-run LOF: 2
Total
93
120
1)
Shall be planar imperfections relevant for the weld in the specific area
2)
Shall also encompass subsurface imperfections with bottom part maximum 2 mm from ID surface. Does not apply to
X-bevel
3)
Shall also encompass subsurface imperfections with bottom part maximum 5 mm from OD surface. Does not apply
to X-bevel
4)
Applicable to all applications not specified elsewhere in this table
5)
Hot pass area refers to particular weld bevel geometry for the hot pass with J-bevel. For CRA clad and weld overlay
applications the hot pass area covers the embedded parts of the CRA layer at the ID surface and the transition zone
between CRA layer and backing pipe.
6)
Applicable for X-bevel: OD surface group is encompassing the cross-section from OD surface to one welding pass
above the root region. This group shall include surface breaking imperfections and min 10 sub surface imperfections
with bottom part maximum 5 mm from the root.
7)
Applicable for X-bevel: Fill group is encompassing the root/cross penetration area. Imperfections shall be located at
the cross penetration including areas where a shift in groove geometry is made.
8)
Applicable for X-bevel: ID surface group is encompassing the cross-section from ID surface to the root region. shall
include surface breaking imperfections and min 10 sub surface imperfections.
9)
ID surface Imperfection group in CRA clad and weld overlay shall include imperfections with heights <1.0 mm.
10) Volumetric type shall include Cluster porosity or scattered porosity, and minimum 1 copper inclusion when relevant
for the welding process.
11) Cluster porosity and copper inclusions shall not be included in the PoD analyses, but are included to demonstrate
detection and recognition
E.8.8 Qualification testing
E.8.8.1 The testing described in the following is required for a full qualification. If validation testing is
performed, the testing and documentation requirements given shall apply as applicable to the actual testing
performed.
E.8.8.2 The test welds shall be subjected to testing by the AUT system.
For testing, a low echo amplitude recording threshold shall be used. This threshold should be selected
somewhat above the noise level. PoD analysis will determine the actual detection capability and shall be
expressed as the smallest detectable flaw height at 90/95% PoD at the agreed reporting threshold.
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E.8.8.3 The reference point for circumferential positioning shall be a hard stamped on the test welds.
E.8.8.4 The AUT system shall be set-up, calibrated and subject to test runs before starting the formal
qualification.
Repeatability testing
E.8.8.5 The testing shall include:
— one initial scan of the calibration block in the horizontal (5G) position
— minimum 10 scans of the calibration block(s) in the 5G position with the centre of the calibration block(s)
in the 12 o’clock and 6 o’clock positions
— if relevant for the application of the AUT system, series of 3 consecutive scans shall be repeated with the
calibration block(s) in the vertical (2G) position and/or in the 45º (6G) position.
E.8.8.6 All scans shall be given a unique number and the documentation of the test scans shall include:
— hard copy and electronic output of all scans
— a table for repeatability test scans showing for each scan the maximum amplitude response of each
transducer to its dedicated calibration reflector and the deviation for each scan from the initial calibration
scan.
Temperature sensitivity testing
E.8.8.7 The test welds shall after the initial scans be heated to the elevated temperature expected during
field inspection. Typical test welds containing at least 6 clearly identifiable and distinct AUT indications
each shall be used for scanning with the pipe axis in the horizontal position. Clearly identifiable indications
shall include 2 root/ID indications, 2 embedded indications and 2 OD indications. The calibration block(s)
shall be kept at environmental temperature or be heated to an agreed temperature and maintained at this
temperature during scanning. The temperature of the heated weld shall be logged and reported for each
scan, in addition the ambient temperature shall be logged.
The testing shall include:
—
—
—
—
one initial scan of the calibration block
one initial scan of the non-heated weld
one scan of the heated test weld immediately followed by a scan of the calibration block(s)
within 5 minutes repeat one scan of the heated test weld immediately followed by a scan of the calibration
block(s). Repeat this sequence for at least 15 cycles.
If the AUT system shows unacceptable temperature sensitivity the test can be repeated with agreed different
test conditions.
E.8.8.8 All scans shall be given a unique number and the documentation of the test scans shall include:
— hard copy and electronic output of all scans
— a table for the temperature sensitivity test scans of the defective weld showing the maximum amplitude
response and AUT sized height for each identified indication for each scan.
Detection ability and sizing accuracy testing
E.8.8.9 The test welds shall be scanned with the pipe axis horizontal.
The scanning directions identified as clockwise or counter clockwise (CW or CCW) shall be hard stamped on
the test weld. The calibration block shall be in the least favourable position as determined by the repeatability
testing. See [E.8.8.5]. The welds shall be scanned and all indications above defined thresholds shall be
evaluated.
The testing shall include:
— one initial scan of the calibration block
— one scan of the test weld in the CW direction
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—
—
—
—
one scan of the calibration block(s)
one scan of the test weld in the CCW direction
one scan of the calibration block(s)
assessment and sizing of indications.
Scans in CCW direction requires the band to be moved to the opposite side of the weld compared to the CW
direction scans. It is recommended that the full test programme described above should be performed twice,
with two independent sets of operators.
E.8.8.10 All scans shall be given a unique number indicating weld number, the scan sequence and the
scanning direction and the documentation of the test scans shall include:
a)
b)
hard copy and electronic output of all scans
imperfection/indication number with reference to sizing method and for each imperfection/indication the
dimensions:
—
—
—
—
—
—
—
—
circumferential position
length
height
depth to bottom of indication
transverse location of imperfection/indications (US, DS, C(entral))
maximum amplitude for each scan and variations in maximum amplitude between scans
main AUT zone
imperfection type.
It may further be required to report height, location, depth and echo amplitude at certain additional local
defect positions (see also [E.8.7.3]).
In addition the following information shall be provided:
—
—
—
—
—
—
weld identification
pipe material
pipe thickness/diameter
welding method
groove geometry
calibration block documentation.
Verification of coupling alarm settings
E.8.8.11 Scans shall be performed on different test welds. The couplant flow shall be reduced and the
surface wiped dry between scans until the coupling alarm level/coupling monitor channels indicates loss of
return signal. The level at which the coupling alar/coupling monitor channels indicates loss of return signal
shall be recorded. The final level for coupling alarm/coupling monitor channels settings shall be at least 4 dB
lower than the recorded value.
E.8.8.12 Band offset sensitivity trial The tolerance on band offset sensitivity shall be documented
through repeated scans of a defective weld. The tolerance might vary for different AUT procedures. Zonal
discrimination AUT procedures shall be qualified for a band offset variation of minimum ±1 mm. For other
inspection concepts, for instance multishoot Phased array and ultrasonic imaging, larger band offset
tolerances should be qualified to a tolerance to minimum ±3 mm. The testing shall include
—
—
—
—
one initial scan of a defective weld with no band offset
minimum 3 scans of a defective weld with the band offset 1 mm or 3 mm to the DS side
minimum 3 scans of a defective weld with the band offset 1 mm or 3 mm to the US side
The defective weld selected for the band offset scans shall include at least 6 imperfections, and contain at
least 1 imperfection in each the cap, root and fill areas.
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E.8.9 Reference destructive testing
E.8.9.1 The reports from the AUT qualification testing shall be validated for accuracy in the determination of
imperfection circumferential position, length, height and depth by reference destructive testing.
E.8.9.2 The testing shall be by cross-sectioning, preferably by the salami method, by making more crosssections around each location chosen. The imperfections as reported in the AUT reports shall be used when
selecting the areas for cross-sectioning.
In addition, locations where the AUT shows indications near the agreed reporting threshold level, locations
where indications are identified by the supplementary NDT (see [E.8.7.5]), locations where intentionally
induced imperfections were planned but not reported and randomly chosen locations shall be included.
E.8.9.3 Mark-up of welds should be performed using the AUT scanner. Each position for a cross-section
should preferably be hard stamped close to the weld cap, consistently at the same side (US or DS) for the
whole weld. Cross-section indication number and clockwise scanning position should be hard stamped for
each position. Alternatively, reports from Immersion UT can be accepted for weld macro location mark-up if
agreed between all parties. Immersion UT shall be performed in accordance with the guidelines of DNVGLRP-F118.
E.8.9.4 The cross-sections shall be referenced to and validated against the recording chart positions.
E.8.9.5 The weld sections containing imperfections shall be machined in increments of maximum 2.0 mm.
Each machined cross-section of the weld shall be polished with 800 grit and etched and the imperfection
location, height and depth measured with accuracy better than ± 0.1 mm.
E.8.9.6 Each cross-section shall be documented by a photograph with 5 - 10x magnification, and the
photograph shall include:
—
—
—
—
—
—
Weld number
Specimen number
Imperfection/indication number
Circumferential position
US and DS side of the weld
A millimetre reference scale.
E.8.9.7 Destructive testing shall be in accordance with ISO 17639. The extent of macro sectioning shall
include:
— Sufficient locations so the requirements to minimum number of imperfection observations in different weld
areas and of different types as provided in Table E-3 are fulfilled. Each independent observation shall be
from an independent weld imperfection.
— Imperfection of sizes around the critical imperfection heights provided in Table E-1 and/or Table E-2
— For determination of detection and sizing capabilities the position of a clearly defined local or total
maximum height of the imperfection, as defined by AUT, shall be selected for salami cross-sectioning.
— Areas where the AUT shows indications near or below the agreed reporting threshold level shall be
selected for sectioning.
— Areas with single imperfection indications at weld bevel should be preferred as cross-section positions.
Stacked imperfections should be avoided.
— Areas of uniform imperfection height should be the preferred positions for cross-sectioning.
— Minimum 1 imperfections from each of the main imperfection groups according to Table E3 (i.e. ID
surface, buried, OD surface, volumetric) shall be macro sectioned at ends for length sizing accuracy
evaluation. Macro sectioning shall start at least 5 mm from each end of the imperfection as defined by
AUT and the applicable recording threshold, and continue until no indication of the imperfection can be
found at the macro.
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— If the supplementary NDT indicates presence of imperfections not identified in the AUT reports, these
areas shall also be selected for sectioning.
— Areas without any observations from supplementary NDE or AUT shall be randomly subject to sectioning.
If IUT has been performed this requirement can be omitted.
E.8.9.8 The position of maximum imperfection height shall be the location for cross-sectioning at each
selected AUT indication. The tool used to mark the reference line should facilitate an accuracy in marking of
± 0.5 mm or better.
E.8.10 Analysis
Repeatability
E.8.10.1 The data from the repeatability test programme shall be analysed with respect to system
repeatability and stability. The maximum deviations in amplitude from each reference reflector between the
initial scan and the scans performed with each calibration block position shall be determined.
The acceptable variation in amplitude on repeated calibration block scans is ± 2 dB. For band offset scans
on defective welds, the same ± 2 dB criteria can be applied for maximum channel amplitude variations or
variations in sized defect heights can be evaluated. For the latter approach, the variation in sized defect
heights shall not exceed ± 1 mm when used with workmanship acceptance criteria, or alternatively exceed
the sizing inaccuracy allowance subtracted from the ECA derived acceptance criteria.
Temperature sensitivity
E.8.10.2 The data from the temperature sensitivity test programme shall be analysed with respect to the
influence of temperature build-up in the transducers over time. The maximum variations in amplitude from
each selected indication between the initial scan and the scans performed with heated test weld shall be
determined.
Based upon an acceptable variation in amplitude of ± 2 dB or in height sizing not exceeding the sizing
accuracy derived at the analysis described in paragraph [E.8.10.3], the analysis shall determine the:
—
—
—
—
acceptable maximum temperature of welds
the sum of transducer inactive time on weld and scanning time
the minimum time between scanning of hot welds
the maximum temperature difference between weld and calibration block.
Detection ability and sizing accuracy
E.8.10.3 The data recorded during the tests and reference investigations shall be analysed with respect to:
— accuracy in height sizing (random and systematic deviation, and 5% fractile)
— accuracy in length sizing
— accuracy in imperfection depth estimate and ligament determination for sub-surface imperfections within
5 mm from ID and OD surfaces
— AUT imperfection characterisation abilities compared to the results of the destructive tests and the other
NDT performed
— as relevant, determination of PoD/PoR values or curves for different assumed echo amplitude or other
employed threshold settings to determine the threshold to be used during examination.
E.8.10.4 The analysis shall be performed by recognised and applicable statistical methods, e.g. according
to Nordtest NT Techn. Report 394 (Guidelines for NDE Reliability Determination and Description, Approved
1998-04). The omission of any reported indication in the analysis shall be justified.
E.8.10.5 Reference imperfection height used in the analysis shall be the maximum height identified by
macro sectioning for each observation.
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E.8.11 Reporting
E.8.11.1 A qualification report shall as a minimum contain:
—
—
—
—
—
—
—
—
—
a technical documentation of the AUT system
outcome of the technical evaluation of the AUT system according to this appendix
description of the specimens and tests performed, including sensitivities used
definitions of the essential variables (see [E.9.2]) for the welds and equipment used during qualification
testing
data recorded for each imperfection and each imperfection cross-section (sizes, locations, types,
measured and determined during reference investigation, echo amplitudes)
outcome of the analysis of data ([E.8.10])
justification of any omission of destructive data from analysis
conclusion of the qualification
Range of validity of the essential parameters listed in paragraph [E.10.2.1].
E.9 Project specific automated ultrasonic testing procedure
validation
E.9.1 Scope
E.9.1.1 Project specific AUT procedure validation shall be performed in order to demonstrate that the project
specific AUT procedure can accomplish the qualified performance capabilities, provided that all essential
variables remain within reason equivalent to what has been pre-qualified. The scope of project specific
validation shall be detailed in a document, which shall provide justification for that the essential variables of
the procedure are within reasonable equivalency to referenced pre-qualification.
E.9.1.2 For a project with multiple pipe sizes and bevel geometries, etc., it shall be regarded as sufficient if
the validation program is conducted on pipe sizes that may present more AUT challenges, provided that the
pipe configurations are covered by the same pre-qualification status. The selected pipe sizes are to be agreed
to by the involved parties.
E.9.1.3 If software upgrade not impacting data collection and signal processing is foreseen prior to
production after validation program, software equivalence shall be verified.
E.9.1.4 In case one or several essential variables as listed in [E.8.5.1] are outside the pre-qualified range
of validity, the validation scope shall comprise welds with at least 29 deliberately induced imperfections for
the affected weld configurations. The variables that are identified to be outside the range of validity has to be
addressed in the validation scope.
E.9.1.5 For fatigue sensitive welds when acceptance criteria Table E-2 is applicable, the validation scope shall
comprise welds with at least 29 deliberately induced imperfections.
E.9.1.6 When the project specific pipe configurations are covered by the range of validity of the prequalification, the validation scope shall comprise minimum 12 imperfections, including 3 observations for
each group (ID surface, fill, OD Surface and volumetric).
E.9.1.7 A project specific AUT procedure validation shall consist of the following minimum activities:
— Review of project specific AUT procedure including any pertaining ITP, cal block design reports (WPS), AUT
set up files and project specific AUT acceptance criteria including supporting ECA or fatigue reports.
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— A compliance assessment of the proposed project specific AUT procedure and AUT system qualification
results and pre requisites.
— Verification of hardware and software including calibration block fabrication tolerances.
— Verification of AUT set up on relevant calibration block.
— Review deliberately induced defective weld plan and verify that welds are made with relevant process and
geometries.
— Perform supplementary NDT as per clause [E.8.7.5].
— Perform AUT inspection on deliberately defective welds.
— Perform weld evaluation at relevant interpretation/reporting threshold, report imperfection height, depth
and length.
— Destructive testing of agreed number of observations.
E.9.1.8 One defective weld, similar to and additional to the validation welds, shall be made available for AUT
setup adjustments and fine-tuning upfront the AUT validation trials. This weld shall not be used as a part of
any of the AUT validation trials.
E.9.2 Assessment
E.9.2.1 The performance requirement i.e AUT system capabilities in terms of PoD and sizing accuracy shall
be verified adequate in relation to the smallest allowable weld imperfection permitted by either ECA/fatigue
analysis derived acceptance criteria or other quality standard description. If the AUT system performance
results as concluded in the AUT system qualification are not in compliance with the project specific demands
then this situation shall lead to a new qualification as per this document.
E.9.2.2 Performance of the AUT scanning shall be conducted at ambient temperature unless otherwise
agreed and at project specific reporting threshold in compliance with pre requisites given by the AUT system
Qualification report. Scanning shall be performed with nominal band setting unless otherwise agreed.
Reverse scanning shall be performed unless otherwise agreed. All relevant AUT indications exceeding noise
level shall be reported on a suitable format containing all relevant signal information.
E.9.2.3 The number of locations for destructive testing shall be agreed upon between all involved parties,
and shall as a minimum include 12 independent locations for all project pipe configurations covered by the
same AUT pre-qualification. The minimum number of independent locations is 29 if the pipe configurations
are not fully covered by the AUT pre-qualification. The selection criteria shall be as follows:
Imperfection indications exhibiting dimensions equivalent or larger than the AUT system PoD but smaller
or equivalent to the project specific smallest allowable imperfection as identified in the project specific
acceptance criteria adjusted for sizing accuracy.
The type and distribution of defect types, including sizes, shall be typical for the welding methods and weld
groove geometries the AUT system is to be qualified for.
E.9.2.4 One volumetric indication shall be included for verification.
E.9.2.5 Reference block repeatability trials shall be evaluated according to paragraph [E.8.10.1].
E.9.2.6 Band offset trials shall be evaluated according to paragraph [E.8.10.1].
E.9.2.7 AUT setup symmetry shall be evaluated according to paragraph [E.8.10.5].
E.9.2.8 A summary report containing all collected data shall be prepared and a comparison between
supplementary NDT, AUT and macro section data shall be made. Evaluation of sizing accuracy according to
clause [E.8.4.2] shall be performed.
E.9.2.9 Based on validation results, acceptance of AUT system for project use and Imperfection undersize
correction used for ECA correction shall be justified. The justification shall include all observations of
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performance outside the pre-qualified results. When the justification is accepted by all parties, the project
specific AUT procedure shall be regarded as validated.
The purpose of the validation is not to perform a PoD analysis but to verify that the project specific AUT
procedure capability is adequate for detection of the smallest project specific critical defect.
E.9.2.10 Detailed project specific AUT set-up shall be reported in a specific document. It shall contain all
the necessary information to allow all involved parties to check that the set-up is strictly similar for the
production phase.
E.10 Validity of qualification
E.10.1 Validity
E.10.1.1 A qualification is AUT procedure and system specific.
Upon successful completion of the qualification scope it is assumed that the AUT system will remain qualified
within the range of qualification for an infinite time period provided that the AUT system remains virtually
unchanged, i.e. with no changes that are judged to have an impact on the performance parameters.
E.10.1.2
AUT Qualification conducted on larger diameter and heavier wall thickness pipes shall not be regarded as
valid for AUT examination of weld dimensions with OD below 4" OD and/or when wall thickness is below 8.0
mm.
Guidance note:
Girth welds of small diameter and/or thin wall thickness pipes can provide limitations for efficient inspection with AUT, and UT
inspection in general. In particular low wall thickness configurations with corresponding acceptance criteria can be challenging
for AUT with regards to accurate height sizing and depth positioning. AUT qualification or validation according to this appendix
requirements is therefore required for dimensions when OD is below 4" OD and/or when wall thickness is below 8.0 mm,
regardless of qualification status for larger diameter and heavier wall thickness pipes.
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E.10.2 Essential variables
E.10.2.1 The following essential variables apply:
—
—
—
—
—
—
—
—
—
—
—
welding method and groove geometry (including repair welds, if relevant)
root and cap transducer set-up
wall thickness (wall thickness variation requiring any change in focal law set up, adding or removing legs.
diameter (diameter variation requiring transducer curvature which may impact on length accuracy.
Systems qualified on sample larger than 12” may not be readily qualified on smaller diameter. Beam
profile and effect of transducer curvature shall be determined.
base material and welding consumables (The distinction is made on materials with substantially
differences in ultrasonic response, for instance between C-Mn, 13% Cr, duplex or austenitic steels.)
transducer set-up for other channels (the number of these channels may be increased or decreased to
accommodate changes in wall thickness provided there are no set-up changes)
focal laws
reference reflectors
working temperature range
system, data acquisition and data treatment
software version (except changes affecting viewing, display or bug-fixing only).
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E.10.2.2 Changes in the essential variables for an existing qualified system will require validation trials of
the modified system, in order to demonstrate validity of the qualification results. Validation trials shall be
according to [E.9].
E.11 Determination of wave velocities in pipe steels
E.11.1 General
E.11.1.1 The procedure defined covers methods that may be used to determine acoustic velocity of
ultrasonic waves in linepipe steels. Equivalent methods may be used subject to agreement.
Linepipe used in oil and natural gas transmission exhibit varying degrees of anisotropy with varying acoustic
velocities depending on the propagation direction with resultant changes in the refracted angle of the sound
in the steel. This is especially critical where focused beams are used for zonal discrimination. It is thus
required to determine the ultrasonic shear or longitudinal (as appropriate) wave velocity for propagation in
different directions.
E.11.2 Equipment
E.11.2.1 To determine the wave velocity (shear or compression) directional dependency an ultrasonic wave
transducer of the same frequency used in the inspection with a crystal diameter of 6 - 10 mm should be
used in combination with an ultrasonic apparatus with bandwidth at least up to 10 MHz and a recommended
capability of measuring ultrasonic pulse transit times with a resolution of 10 ns and an accuracy of ± 25 ns.
Devices for measuring mechanical dimension of the specimens should have a recommended accuracy of ±
0.1 mm. As couplant an easily removable glue or special high viscosity shear or compression wave couplant
(as appropriate) is recommended.
E.11.3 Specimens
E.11.3.1 A specimen is cut from a section of pipe to be tested and the corresponding results are specific for
a particular pipe diameter, wall thickness and manufacturer. Specimen dimensions should be a minimum of
50 × 50 mm.
A similar arrangement can also be used for measuring velocities in a plane normal to pipe axis.A minimum
of three parallel surfaces are machined for the plane to be evaluated; one pair of surfaces is made in the
radial direction (perpendicular to the D surface) and the other pair made 20° from the perpendicular to the D
surface, see Figure E-1. Additional pairs of parallel surfaces may be machined at other angles in the plane to
be evaluated if more data points are desired.
The machined surfaces should be smooth to a 20 μm finish or better. Minimum width of the specimen surface
to be measured should be 20 mm and the minimum thickness between the parallel surfaces to be measured
should be 10 mm. Vertical extent of the test surface will be limited by the pipe wall thickness.
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Figure E-1 Test specimen and transducer placement
E.11.4 Test method
E.11.4.1 Using the machined slots as reflectors for the wave pulses with the transducer in the appropriate
positions and measuring the pulse transit times determines together with the mechanically measured pulse
travelling distances the wave velocities in the axial and 20° direction (Figure E-1).
A similar measurement in the through thickness direction determines the radial velocity. Pulse transit times
st
nd
shall be measured between the faster reflection signals of 1 and 2 back wall echo.
In case SAWH pipes are used, the velocity derived using the slower reflection signals of 1st and 2nd back wall
echo shall also be determined. The mode with the highest signal-to-noise ratio shall be used as the sound
velocity for the tested material.
A minimum of three readings shall be made for each plane in which testing shall be done.
E.11.5 Accuracy
Errors in velocity determination shall not be greater than ± 20 m/s.
E.11.6 Recording
Values for the velocities determined can be tabulated and graphed. By plotting velocities on a two
dimensional polar graph for a single plane, velocities at angles other than those made directly can be
estimated.
The effect of temperature on velocity can be significant under extreme test conditions; therefore the
temperature at which these readings have been made should also be recorded.
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APPENDIX F REQUIREMENTS FOR SHORE CROSSING AND ONSHORE
SECTIONS
F.1 General
F.1.1 Objective
F.1.1.1 The objective of this appendix is to provide the complementary requirements to the shore crossing
zone, including the onshore part of the submarine pipeline system compliant with the safety philosophy for
the offshore part. This appendix specifies the requirements for design, construction and operation of parts of
pipeline systems in the shore crossing zone.
This appendix is meant to assist the project execution of submarine pipeline developments where parts are
going onshore.
Guidance note:
A submarine pipeline system always includes the shore crossing up to a point above the highest astronomical tidal water level
plus storm surge and wave run-up. Thus, the engineering design, construction, operation and abandonment of the pipeline section
at the shore crossing shall be undertaken in compliance with this offshore standard. The location of the code break between this
offshore standard and the relevant onshore standard will usually differ for all pipeline systems depending on the site conditions
and on the length of the onshore pipeline section. The presence of valves or isolation joints may also have an impact on where to
select the code break. This implies that a, sometimes significant, part of the pipeline system can be located onshore. This part of
the pipeline system may have different legislations, failure modes and failure consequences compared to the submarine part.
The exact limit of the submarine pipeline system at the onshore end may differ from this definition herein based on different
statutory regulations which may govern.
Onshore standards or recommended practices may also take precedence of this part due to legislation aspects.
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F.1.1.2 The appendix also covers the requirements for the shore approach.
F.1.2 Scope and application
F.1.2.1 The limitations found in [E.8.8.8] are in general also applicable for this appendix.
F.1.2.2 The onshore section is limited by the definition of submarine pipeline system.
F.1.2.3 This appendix does not cover regular onshore pipelines, i.e. pipelines starting and ending onshore
not having any submarine parts. River crossings or crossing of fresh water lakes are not considered as
submarine sections.
Guidance note:
This appendix is not meant to replace current industry practice onshore standards or recommended practices or any national
requirements.
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F.1.2.4 Specific requirements for the onshore parts given in this appendix overrule requirements given
elsewhere in the standard.
F.1.2.5 At the shore crossing of a pipeline, the code break with the onshore standards or recommended
practices should be defined on a case by case basis with consideration given to the following:
— The code break should occur immediately to one side of a pipe connection such as a weld, mechanical
connector, or isolation joint, such that the connection itself falls under one code or the other.
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— The application of multiple pipeline standards to the same section of pipeline (an overlap) should be
avoided.
— There should not be a section of pipeline where no pipeline standard applies (a gap).
F.1.2.6 The code break for an open cut and cover shore crossing design should be defined on a case by case
basis, once a sufficient level of engineering definition has been achieved, see . Consideration should be given
to the:
— extreme low and extreme high water levels, and the length along the pipeline between them (extreme
water level is that water level resulting from the design environmental event being a combination of tide,
storm surge and wave run-up)
— system design aspects that may influence the code break;
— electrical isolation points
— beach valves
— pipeline construction method, such as;
— method of pipeline installation
— offshore to onshore tie-in weld or mechanical connector
— pre-commissioning requirements
— implications for design
— construction practicalities
— ongoing maintenance of the pipeline.
Figure F-1 Typical application of this standard and relevant onshore standards or recommended
practices for conventional open cut and cover solution
F.1.2.7 The code break for a HDD shore crossing design should be at the onshore tie-in weld, assuming that
a fabricated bend is introduced between the inclined pipeline section (installed by the HDD method) and the
onshore pipeline section, see . However, deviation of this principle is possible, for instance, when the HDD
section of the pipeline transitions to the onshore section of the pipeline in an elastic bend.
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Figure F-2 Typical application of this standard and relevant onshore standard or recommended
practice for HDD solution
F.1.2.8 The code break for a jetty-based shore crossing design should be at the first weld or mechanical
connector between the riser and the pipeline section on the jetty. The relevant onshore pipeline standard
should be applied to the pipeline section on the jetty.
Figure F-3 Typical application of this standard and relevant onshore standard or recommended
practice for jetty solution
F.1.2.9 A tunnelled shore crossing designs may or may not include a tie-in riser or metrology spool on the
onshore side of the crossing, see . The location of the code break may differ, and could either be at the base
(case 1) or at the top (case 2) of the riser/tie-in spool (Figure 1d). If there is no tie-in riser or metrology
spool, then the code break should be at the onshore tie-in weld to the pipeline section installed through the
tunnel.
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Figure F-4 Typical application of this standard and relevant onshore standards for tunnel solutions
F.1.2.10 Onshore pipelines are normally regulated by national regulations and cover a wide range of areas
from public safety, traffic and roads, waterways, environmental impact, etc. Some of these regulations
may be stricter than the requirements given in this standard and care shall be exercised when assuring
compliance with different national regulations.
F.1.3 Other standards or recommended practices
F.1.3.1 This appendix is fully aligned with the requirements given in ISO 13623
Guidance note:
ISO 13623 requires a specific utilisation for shore crossing (landfalls). According to this standard the assessment of risk will
constitute selection of safety class for each specific pipeline and pipeline sections. The safety class classification for a shore
crossing will normally give the same utilisation as required by ISO 13623 however this does not always need to be the case. This
implies that the utilisation at shore crossings may differ from the ISO 13623 requirements and care should be taken when stating
compliance with ISO 13623 for a specific pipeline development.
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F.1.3.2 Onshore pipelines are normally regulated by national regulations and cover a wide range of areas
from public safety, traffic and roads, water ways, environmental impact, etc. Some of these regulations
may be stricter than the requirements given in this standard and care shall be exercised when assuring
compliance with different national regulations.
F.1.4 Systematic review
F.1.4.1 The overall requirement to systematic review in Sec.2 shall be reflected in the concept development,
design, construction, operation and decommissioning of the pipeline section at the shore crossing.
F.1.4.2 Typical potential threats at shore crossings, over and above those relevant to the other sections of
the pipeline system, may include, but may not necessarily be limited to:
— congested areas (human population, tourism, industry, ports and harbors, existing pipelines, live
hydrocarbon plants, and the like)
— environmentally sensitive areas (flora and fauna)
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—
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—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
heritage and cultural sites
fishing and boating (recreational and professional)
ship/plane wrecks and unexploded ordnances
geohazards (e.g. eroding coastline, unstable cliffs, acid sulphate soils)
surface and subsurface hydrology
coastal geomorphology processes
breaking waves and strong tidal currents
long term still water level fluctuations
seismic events and tsunamis
Functionality of different cathodic protection systems, at the interface of the subsea and onshore pipeline
sections
cathodic protection current shielding from casings and tunnel pipes
differences between onshore and offshore standards or recommended practices requirements
bundled pipelines or pipelines in close proximity to each other (potential cathodic protection system
interference, consequence of failure of one pipeline onto the others, inspectability, and the like)
wetting and drying cycles from tidally driven water level fluctuations, and their impact on pipeline coating
degradation, external corrosion and cathodic protection system functionality
construction risk in relation to shallow water, hostile nearshore seastate, geotechnical conditions and novel
construction methods
design, construction and operational interface between onshore and offshore
interface of potentially different regulatory regimes
potential new infrastructure which may impact shoreline geomorphology processes
external impact (vehicle impact, dropped objects, vessel grounding/beaching, and the like)
axial expansion
external coating wear and tear, during construction and during the operational life of the pipeline system
security threats.
F.1.4.3 At a shoreline crossing where a code break occurs, the classification system may vary between
the standards or recommended practices. In this case the standards or recommended practices should
be assessed to determine the most appropriate way to manage the classification definition for the shore
crossing.
F.1.4.4 The requirement for a beach valve should be subject to a risk assessment, which should consider
the:
— requirements to isolate inventory of the onshore pipeline section from the offshore pipeline section
— risks associated with having a beach valve in the system.
F.1.4.5 The functional requirements for a beach valve should include, but not necessarily be limited to:
—
—
—
—
—
—
onshore isolation integrity requirement
type of valve and valve connection to the pipeline
bleed valve vent requirements
corrosion protection, protection from the elements, and earthing
environmental impact and aesthetics
accessibility and protection against security threats.
F.1.5 Definitions
F.1.5.1 Battery limit - the limit at which the scope of work ends. The battery limit can be different for
designer, installation contractor, verifier and operators. Normally defined at as including or up to a certain
weld.
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F.1.5.2 Code break - the exact point at which the design standards or recommended practicees changes
from submarine to onshore pipeline system. Normally defined at as including or up to a certain weld. This is
often defined at the location of the first flange or valve onshore. Note that this may differ based on different
statutory regulations.
F.1.5.3 First (or last) valve onshore - valve separating the offshore and onshore pipeline. Often the position
of the battery limit and the code break. Often an emergency shut down valves (ESDV)
F.1.5.4 Isolation joint - a special component separating (isolating) the offshore cathodic protection from
the onshore cathodic protection system and installed within the onshore part of the offshore pipeline. It is
normally positioned very close to the high water mark as the offshore cathodic protecting system has limited
protection capabilities when the pipeline is not submerged in water.
F.1.5.5 Shore crossing - the section of the pipeline which transitions between a permanently submerged
(subsea) pipeline to a permanently dry (onshore) pipeline.
F.1.5.6 Near shore - the transition from the offshore pipeline to the shore approach area. Often not well
defined, but can be the area in where the pipeline goes from laying on the sea-bed to being positioned
in an open trench to where it is buried. Sometimes the extent of the areas is defined by the reach of the
installation vessel or trenching equipment, and sometimes this area is given special attention by the fishing
industry.
F.1.5.7 Onshore part of offshore pipeline - the first part of the pipeline on shore. It is distinct as the offshore
design standard is still applicable, while the pipeline is not permanently submerged. The length is normally
short, up to some kilometres.
F.1.5.8 Onshore pipeline - the pipeline on shore following onshore standard and normally subject to different
authority regulations
F.1.5.9 Right-of-way – corridor of land within which the pipeline operator has the right to conduct activities
in accordance with the agreement with the land owner.
F.1.5.10 Shore approach - the last part of the pipeline before it comes on shore. The need for burying the
pipeline in the shore approach area should be evaluated and include:
—
—
—
—
environmental loading (breaking waves, current and tide)
requirements to a clean beach for recreation
shipping activity or
protection (reduced access by 3rd parties).
F.2 Safety philosophy
F.2.1 General
F.2.1.1 The design philosophy for the shore approach and the onshore pipeline shall comply with Sec.2. This
implies that the consequences of failure (economical, environmental and human) shall be quantified by the
concept of safety class. The safety class should be determined by fluid category, location class and phase
(construction, operation) of the pipeline.
F.2.1.2 The presence of people and facilities necessitates a further refinement of the location classes used
offshore. In highly populated areas the consequences may be more severe than for offshore, requiring a
higher safety class, very high. These complementary issues are described in this sub-section.
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Guidance note:
It should be noted that ISO 13623 contain even more stringent utilisation requirements than safety class very high. However, as
this standard is meant to only cover onshore parts of an offshore pipeline system it is not foreseen that such a line will be located
in areas with even higher population densities.
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F.2.2 Safety philosophy
F.2.2.1 The safety philosophy outlined in [2.2] is applicable for shore approach and onshore sections.
Guidance note:
In particular is it important to perform a systematic review of all hazards to identify consequences as third party presence is more
significant onshore.
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F.2.2.2 The health, safety and environmental aspects outlined in [2.2] is applicable for shore approach and
onshore sections also.
F.2.3 Quantification of consequence
F.2.3.1 Fluids shall be categorised in line with Sec.2 of this standard.
F.2.3.2 A location class shall be determined for each part of the pipeline as shown in Table F-1.
Table F-1 Location classes onshore
Location class
Description
1 (equivalent to location
class 1 as defined in Sec.2)
Locations subject to infrequent human activity with no permanent human habitation.
Location class 1 is intended to reflect inaccessible areas such as deserts and tundra
regions
2
Locations with a population density of less than 50 persons per square kilometre.
Location class 2 is intended to reflect such areas as wasteland, grazing land, farmland
and other sparsely populated areas
3 (equivalent to location
class 2 as defined in Sec.2)
Locations with a population density of 50 persons or more but less than 250 persons
per square kilometre, with multiple dwelling units, with hotels or office buildings
where no more than 50 persons may gather regularly and with occasional industrial
buildings. Locations class 3 is intended to reflect areas where the population density is
intermediate between location class 2 and location class 4, such as fringe areas around
cities and towns, and ranches and country estates.
4
Locations with a population density of 250 persons or more per square kilometre,
except where a location class 5 prevails. A locations class 4 is intended to reflect areas
such as suburban housing developments, residential areas, industrial areas and other
populated areas not meeting location class 5.
5
Location with areas where multi-storey buildings (four or more floors above ground
level) are prevalent and where traffic is heavy or dense and where there may be
numerous other utilities underground.
F.2.3.3 The population density in Table F-1, expressed as the number of persons per square kilometre, shall
be determined by laying out zones along the pipeline route, with the pipeline in the centreline of this zone
having a width of:
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— 400 m for category D fluids, and
— to be determined for category E fluid pipelines, but not less than 400 m. The determination shall include
the possibility of very low temperature during a leakage of high pressure pipelines, giving high density gas
that may float significant distance prior to ignition.
F.2.3.4 Half the zone width shall not be less than the effective distance of fluid release.
F.2.3.5 The length of the zones shall be 1.5 km and located at any location along the pipeline. The length
of the random sections may be reduced where physical barriers or other factors exist, which will limit the
extension of the more densely populated area to a distance less than 1.5 km.
F.2.3.6 The possible increase in population density and level of human activity from planned future
developments shall be determined and accounted for when determining population density.
F.2.3.7 Additional considerations shall be given to the possible consequences of a failure near a
concentration of people such as found in a church, school, multiple-dwelling unit, hospital, or recreational
area of an organised character in location classes 2 and 3.
F.2.3.8 Pipeline design according to this standard is based on potential failure consequence and is quantified
by the concept of safety class. These may vary for different phases and locations and are defined in Table
F-2.
Table F-2 Definition of safety classes
Safety class
Description
Low
Where failure implies low risk of human injury and minor environmental and economic
consequences.
Medium
Where failure implies risk of human injury, significant environmental pollution or very high economic
or political consequences.
High
Where failure during operating conditions implies high risk of human injury, significant
environmental pollution or very high economic or political consequences.
Very high
Where failure during operating conditions implies very high risk of human injury.
F.2.3.9 The acceptable failure probability of safety class Very High is one order of magnitude lower than for
safety class high as given in Sec.2 of this standard.
F.2.3.10 The safety class determined by the crossing shall apply from:
— for road crossings
— the road right-of-way boundary
— if this boundary has not been defined, to 10 m from the edge of the hard surface of major roads and 5 m
for minor roads
— for railways
— 5 m beyond the railway boundary or
— if this boundary has not been defined, to 10 m from the rail.
F.2.3.11 The safety class can often be determined based on the location class and fluid category. Typical
selection of safety class is given in Table F-3.
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Table F-3 Classification of safety classes
Phase
Location class
Fluid category
1
Temporary
1
2
All
4
Low
A,C
Operating onshore
3
2
5
-
Low
Medium
-
B
Medium
Medium
High
Very High
-
D,E
Medium
Medium
High
Very High
-
1)
Installation until commissioning (temporary) will normally be classified as safety class low. During temporary
conditions after commissioning of the pipeline, special considerations shall be made to the consequences of failure,
i.e. giving a higher safety class than low.
2)
This standard is not applicable for areas in location class 5.
F.3 Design premise
F.3.1 General
F.3.1.1 The basis for design premises for the shore approach shall be as given in Sec.3. Special attention
shall be given to aspects related to installation, on-bottom stability, fatigue due to direct wave loading and
3rd party activities. Statutory requirements apply.
F.3.1.2 The shore crossing should be constructed by either
—
—
—
—
—
open cut and cover
horizontal directional drilling (HDD)
tunnelling
jetty, or
combinations of the above.
F.3.2 Routing
F.3.2.1 The requirements in [3.3] apply to the shore approach section. Additional requirements are given
below.
F.3.2.2 The routing shall be selected and prepared so that risk of fire, explosions and un-intended
occurrences is at an acceptable level. Spacing between pipelines, associated equipment, harbours, ship traffic
and buildings shall be evaluated by risk assessments considering the service of the pipeline.
Guidance note:
The preferred means of routing for shore approach pipeline will be to bury them. Examples of additional protective means are
Concrete coating or cover, additional steel wall thickness, deeper trenching, additional marking and means to minimize the
possibility for impacts from ship traffic and vehicles.
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F.3.2.3 Special focus shall be on:
— safety of public
— protection of environment
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— 3rd party activities
— access
— other property and facilities.
F.3.2.4 Pipeline conveying category B, C, D and E fluids should avoid built-up areas or areas with frequent
human activity.
F.3.2.5 In absence of public safety statutory requirements, a safety evaluation shall be performed in
accordance with the general requirements for:
— Pipeline conveying category D fluids in locations where multi-storey buildings are prevalent, where traffic
is heavy or dense, and where there may be numerous other utilities underground.
— Pipelines conveying category E fluids.
F.3.2.6 An Environmental Impact Assessment (EIA) shall be performed. The EIA shall consider as a
minimum:
— temporary works during construction and operation (e.g. repair, modifications etc.)
— the long-term presence of the pipeline
— leakage.
F.3.2.7 The route shall permit the required access and working width for the construction and operation
(including any replacement), of the pipeline. The availability of utilities necessary for construction and
operation should also be reviewed.
F.3.2.8 The route shall be tidy and free from flammable materials on and in the vicinity of the pipeline
system. A safety area along the pipeline shall be defined which may restrict public access and activities. The
extent of the area shall be established based on risk analyses and shown on the plan for the pipeline system.
F.3.2.9 Facilities along the pipeline route should be identified and their impact evaluated in consultation with
the operator of these facilities. Facilities should not be allowed closer than 4 m from the pipeline.
F.3.2.10 A wider restriction zone compared to public access may apply to future development (buildings
etc.).
F.3.3 Environmental data
F.3.3.1 Environmental data shall be collected as described in Sec.3. Long term shore profile shall be
considered. Special attention shall be given to tidal variations.
F.3.4 Survey
F.3.4.1 Route and geophysical and geotechnical surveys shall be carried out to identify and locate with
sufficient accuracy the relevant geographical, geological, geotechnical, corrosive, topographical and
environmental features, and other facilities such as other pipelines, cables and obstructions, which may
impact the pipeline route selection. The surveys shall be continuous, and the accuracy and tolerance should
be selected with regard to the adjoining land and offshore surveys.
F.3.4.2 Nearshore and shore crossing survey coverage should be continuous and in agreement within
specified tolerances and accuracies of both adjoining land and offshore route surveys.
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F.3.5 Marking
F.3.5.1 The pipeline system shall be marked in such a way that its location in the terrain is clearly visible.
Provisions shall be made to restrict public access to pipelines that are not buried.
F.3.5.2 Warning signs shall be placed within visible distance and at each side of crossings with rivers, roads
and rail ways giving information on:
— content
— operator
— phone number to nearest manned station which may be alerted in the event of fault on the pipeline.
F.4 Design
F.4.1 General
F.4.1.1 The pigging requirements in [3.4.1.2] and [3.4.1.2] applies to the pipeline system.
F.4.2 System design
F.4.2.1 Any electrical equipment within the location class areas shall comply with the location class
requirements.
F.4.2.2 The need for lightening rod and means to avoid build up of static electricity shall be considered.
F.4.2.3 Branch connections for pipelines on land shall be supported by consolidated backfill or provided with
adequate flexibility.
F.4.2.4 Braces and damping devices required to prevent vibration of piping shall be attached to the pipe by
full encirclement members.
F.4.2.5 For structural items, doubler plates and rings welded directly to pressure containing parts, the
following apply:
— Design shall be performed for all relevant failure modes, e.g. fracture and instability.
— For duplex stainless steels and 13Cr martensitic stainless steels a stress analysis shall be performed in
each case to determine that local stresses will not initiate HISC. Recommended practice for design of
duplex stainless steels is given in DNVGL-RP-F112.
— Welding directly to the pressure containing parts shall be performed in accordance with qualified welding
procedures according to App.C.
— NDT shall be performed to ensure structural integrity of the pressure containing parts.
— The toe-to-toe distance from other welds shall be minimum 2 · t or 50 mm, whichever is larger.
F.4.2.6 For doubler plates or rings the following apply:
—
—
—
—
Design shall be performed for all relevant failure modes.
Doubler plates should be circular.
Welds shall be performed in accordance with qualified welding procedures.
Doubler rings shall be made as fully encircling sleeves with the longitudinal welds made with backing
strips, and avoiding penetration into the main pipe material.
— Other welds shall be continuous, and made in a manner minimising the risk of root cracking and lamellar
tearing.
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F.4.3 Design loads
F.4.3.1 The loads shall be established as described in Sec.4. Special attention shall be given calculations of
loads from 3rd party activities such as traffic (potential cyclic loading) and other construction work.
F.4.3.2 The loads shall be classified into functional, environmental, interference or accidental loads as per
Sec.4 of this standard with the additional requirements below.
F.4.3.3 Traffic axle loads and frequency shall be established in consultation with the appropriate authorities
or other relevant sources and with recognition of existing and forecast residential, commercial and industrial
developments.
F.4.4 Design criteria
F.4.4.1 The design should comply with the requirements in Sec.5. Special attention shall be given to
statutory requirements.
F.4.4.2 For safety class Very High the safety class factors in Table F-4 apply.
Table F-4 Partial safety class resistance factor for safety class very high
Limit state
γSC
Pressure containment
1.593
Other limit states
1.5
F.4.4.3 Buried pipelines on land should be installed with a cover depth not less than shown in Table F-5.
Table F-5 Minimum cover depth for buried pipelines on land (alternative, preferred formulation to
the table above)
Safety class
3)
Cover depth [m]
1) 2) 4) 5) 6) 7)
Trench blasted in rock
Low
Other
0.8
Medium
High
0.5
Very high
0.8
1.2
1.2
1)
Cover depth shall be measured from the lowest possible ground surface level to the top of the pipe, including
coatings and attachments.
2)
Special consideration for cover may be required in areas with frost heave.
3)
River crossings, road crossings and railway crossing shall in this context be classified as safety class High.
4)
Cover shall not be less than the depth of normal cultivation +0.3 m.
5)
For river crossings; to be measured from the lowest anticipated bed.
6)
For roads and railway crossings; to be measured from the bottom of the drain ditches
7)
The top of pipe shall be at least 0.15 m below the surface of the rock.
F.4.4.4 The effect of cover depth shall be considered in the expansion evaluations.
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F.4.4.5 If the pipeline is not laid at a frost free depth, the mass below the pipe’s centre line must be frost
proof.
F.4.4.6 Pipelines may be installed with less cover depth than indicated in Table F-5, provided a similar level
of protection is provided by alternative methods. The design of alternative protection methods should take
into account:
—
—
—
—
—
any hindrance caused to other users of the area
soil stability and settlement
pipe stability cathodic protection
pipeline expansion
access for maintenance.
F.4.4.7 Pipelines running parallel to a road or railway should be routed outside the corresponding right-ofway.
F.4.4.8 The vertical separation between the top of the pipe and the top of the rail should be a minimum of
1.4 m for open-cut crossings and 1.8 m for bored or tunnelled crossings.
F.4.4.9 Protection requirements for pipeline crossings of canals, rivers and lakes should be designed in
consultation with local water and waterways authorities.
F.4.4.10 Crossings of flood defences can require additional design measures for prevention of flooding and
limiting the possible consequences.
F.4.4.11 Crossing pipelines and cables should be kept separated by a minimum vertical distance of 0.3 m.
F.4.4.12 Pipeline bridges may be considered when buried crossings are not practicable. Pipe bridges shall be
designed in accordance with structural design standards, with sufficient clearance to avoid possible damage
from the movement of traffic, and with access for maintenance. Interference between the cathodic protection
of the pipelines and the supporting bridge structure shall be considered.
F.4.4.13 Provisions shall be made to restrict public access to pipe bridges.
F.4.4.14 If other criteria are used, the nominal failure probabilities shall be demonstrated to be as specified
in Sec.2.
F.5 Construction
F.5.1 General
F.5.1.1 The same requirements as for the Offshore part of the pipeline system shall be applied to the
onshore part, if applicable. Where this is not applicable, the requirements of ISO 13623 should be complied
with.
F.5.2 Linepipe
F.5.2.1 The material selection should comply with the requirements of Sec.6 and manufacture of line pipe
should comply with the requirements in Sec.7.
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F.5.3 Components and assemblies
F.5.3.1 The requirements to components and structural items as well as assemblies should comply with
Sec.8.
F.5.3.2 Field, i.e. cold, bends with a bend radius corresponding to a permanent strain up to 1.25% are
permitted provided that a qualification programme is performed, documenting that the material requirements
are met after bending. Field bends shall be made on bending machines that provide sufficient support to the
pipe cross-section to prevent buckling or wrinkling of the pipe wall and to maintain coating integrity. Bends
should not be made from pipe lengths containing girth welds that are within 1 m of the bend. Longitudinal
weld seams should be placed near the neutral axis of field bends. Tangent length (i.e. distance from end of
bend to first girth weld) should be at least 1.5 pipe diameters or 500 mm, whichever is larger.
F.5.4 Corrosion protection and coatings
F.5.4.1 The corrosion protection shall comply with Sec.9.
F.5.4.2 All metal pipelines should be provided with an external coating and, for buried or submerged
sections, cathodic protection. Corrosion protection should be provided by impressed current.
F.5.4.3 The design of the impressed current protection system shall strive for a uniform current distribution
along the pipelines and shall define the permanent location for the measurement of the protection potentials.
F.5.4.4 Protected pipelines should be electrically isolated from other structures, such as compressor stations
and terminals, by suitable in-line isolation components.
F.5.4.5 Isolation joints should be provided with protective devices to prevent damage from lightning or highvoltage earth current where possible. Low-resistance grounding to other buried metallic structures shall be
avoided. Electrical continuity shall be provided across components, other than couplings/flanges, which would
otherwise increase the longitudinal resistance of the pipeline. Spark gaps shall be installed between protected
pipelines and lightning protection systems.
F.5.4.6 Test points for the routine monitoring and testing of the cathodic protection should be installed at the
following locations:
—
—
—
—
—
—
—
crossings with DC tractions systems
road, rail and river crossings and large embankments
sections installed in sleeve pipes or casings
isolated couplings
where the pipeline runs parallel to high-voltage cables
sheet piles
crossings with other major metallic structures with, or without, cathodic protection.
F.5.4.7 The primary corrosion control for internal corrosion is identical with the submarine part, see Sec.9.
F.6 Operation
F.6.1 General
F.6.1.1 The requirements to safe and reliable operation of the pipeline systems and the pipeline integrity
management (PIM) as described in Sec.11 apply.
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F.6.1.2 The whole route shall regularly be checked for:
— any required re-classification of location class due to changes in premises like populations etc.
— new facilities
— new intruders or changed configurations that may cause increase risk of threats.
F.7 Documentation
F.7.1 General
F.7.1.1 In addition to the requirements in Sec.12, the following apply:
—
—
—
—
crossing locations related to lakes, straits, rivers, streams, transport communication arteries and similar
maps necessary to evaluate the proposed route classification
relevant drawings on bridges etc.
maps with any crossing services (cables, sewage etc.).
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Changes – historic
CHANGES – HISTORIC
There are currently no historical changes for this document.
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