EN 4700-002:2016
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 002: Bar and section
Superseded date
05-19-2021
Superseded by
Published date
04-13-2016
Publisher
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European Foreword
Introduction
1 Scope
2 Normative references
3 Terms and definitions
4 Wording of order
5 Health and safety
6 Technical requirements
This standard defines the requirements for the ordering, manufacture, testing, inspection and delivery of steel and heat resisting alloy bar and section. It shall be applied when referred to and in conjunction with the EN material standard unless otherwise specified on the drawing, order or inspection schedule.
| Committee |
ASD-STAN
|
| DevelopmentNote |
Supersedes PREN 4700-002. (06/2016)
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| Standards | Relationship |
| BS EN 4700-002:2016 | Identical |
| UNE-EN 4700-002:2010 | Identical |
| NF EN 4700-002 : 2012 | Identical |
| UNE-EN 4700-002:2016 | Identical |
| PN EN 4700-002 : 2016 | Identical |
| DIN EN 4700-002:2016-08 | Identical |
| I.S. EN 4700-002:2016 | Identical |
| NBN EN 4700-002 : 2016 | Identical |
| NS EN 4700-002 : 2010 | Identical |
| SN EN 4700-002 : 2016 | Identical |
| NEN EN 4700-002 : 2016 | Identical |
| UNI EN 4700-002 : 2011 | Identical |
| UNI EN 4700-002:2016 | Identical |
| ONORM EN 4700-002 : 2016 | Identical |
| EN 2306:2017 | Aerospace series - Heat resisting - Nickel base alloy Ni-Cr20Co3Fe3 - Annealed - Bars |
| BS EN 2213:2012 | Aerospace series. Steel FE-PL1505 (15CrMoV6). Air melted. Hardened and tempered. Bars. De ≤ 16 mm. 980 MPa ≤ Rm ≤ 1 180 MPa |
| NF EN 4655 : 2011 | AEROSPACE SERIES - STEEL FE-PM 1506 (X1CRNIMOALTI12-10-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BARS - A OR D < OR = 200 MM - RM > OR = 1400 MPA |
| BS EN 4500-005:2012 | Aerospace series. Metallic materials. Rules for drafting and presentation of material standards Specific rules for steels |
| BS EN 4500-003:2012 | Aerospace series. Metallic materials. Rules for drafting and presentation of material standards Specific rules for heat resisting alloys |
| BS EN 4631:2013 | Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Bar. De ≤ 200 mm. 900 MPa ≤ Rm ≤ 1 050 MPa |
| PREN 2278 : 1 | AEROSPACE SERIES - STEEL X12CRNIMOV12-3 (1.4933) - 900 MPA <= R[M] <= 1100 MPA - BARS - D[E] <= 150 MM |
| I.S. EN 4720:2014 | AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED AND ELECTROSLAG REMELTED (ESR) - HARDENED AND TEMPERED - BAR - D[E] <= 200 MM - 1150 MPA <= R[M] <= 1300 MPA |
| PREN 4721 : DRAFT 2012 | AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED AND ELECTROSLAG REMELTED (ESR) - HARDENED AND TEMPERED - BAR - D[E] <=200 MM - 900 MPA <= R[M] <= 1050 MPA |
| UNI EN 4500-003 : 2014 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 003: SPECIFIC RULES FOR HEAT RESISTING ALLOYS |
| PREN 4720 : DRAFT 2012 | AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED AND ELECTROSLAG REMELTED (ESR) - HARDENED AND TEMPERED - BAR - D[E] <= 200 MM - 1150 MPA <= R[M] <= 1300 MPA |
| I.S. EN 2221:2017 | AEROSPACE SERIES - STEEL FE-PL31 - HARDENED AND TEMPERED - HOLLOW BARS - 3,5 MM <= A <= 55 MM |
| I.S. EN 2213:2012 | AEROSPACE SERIES - STEEL FE-PL1505 (15CRMOV6) - AIR MELTED - HARDENED AND TEMPERED - BARS - D[E] <= 16 MM - 980 MPA <= R[M] <= 1180 MPA |
| BS EN 2135:2017 | Aerospace series. Steel FE-PL61. Carburized, hardened and tempered. Bar. De ≤ 40 mm |
| I.S. EN 3528:2013 | AEROSPACE SERIES - STEEL X2NICOMO18-8-5 (1.6359) - VACUUM INDUCTION MELTED AND VACUUM ARC REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BAR - A OR D <= 150 MM - 1750 MPA <= R[M] <= 2000 MPA |
| UNI EN 2213 : 2013 | AEROSPACE SERIES - STEEL FE-PL1505 (15CRMOV6) - AIR MELTED - HARDENED AND TEMPERED - BARS - D[E] <= 16 MM - 980 MPA <= R[M] <= 1180 MPA |
| I.S. EN 2030:2013 | AEROSPACE SERIES - STEEL X105CRMO17 (1.3544) - HARDENED AND TEMPERED - BARS - D[E] <= 150 MM |
| UNI EN 4656 : 2011 | AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BARS - A OR D <= 200 MM - R[M] >= 1520 MPA |
| BS EN 4657:2010 | Aerospace series. Steel FE-PM1507 (X1CrNiMoAlTi12-11-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Bars. a or D ≤ 200 mm. Rm ≥ 1650 MPa |
| BS EN 4656:2010 | Aerospace series. Steel FE-PM1507 (X1CrNiMoAlTi12-11-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Bars. a or D ≤ 200 mm. Rm ≥ 1520 MPa |
| UNI EN 4631 : 2013 | AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED - HARDENED AND TEMPERED - BAR - D[E] <= 200 MM - 900 MPA <= R[M] <= 1050 MPA |
| I.S. EN 4721:2014 | AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED AND ELECTROSLAG REMELTED (ESR) - HARDENED AND TEMPERED - BAR - D[E] <= 200 MM - 900 MPA <= R[M] <= 1050 MPA |
| 16/30337543 DC : 0 | BS EN 8.4577 - AEROSPACE SERIES - X5CRNICU15-5 (1.4545) - CONSUMABLE ELECTRODE REMELTED (ESR OR VAR) - SOLUTION TREATED AND PRECIPITATION TREATED (H1025) - BAR FOR MACHINING - A OR D <= 250 MM - 1070 MPA <= R[M] <= 1200 MPA - PREMIUM QUALITY (PQ) |
| EN 2221:2017 | Aerospace series - Steel FE-PL31 - Hardened and tempered - Hollow bars - 3,5 mm ≤ a ≤ 55 mm |
| I.S. EN 4376:2016 | AEROSPACE SERIES - HEAT RESISTING ALLOY NICR19FE19NB5MO3 (2.4668) SOLUTION TREATED AND PRECIPITATION TREATED - BAR AND SECTION, D[E] <= 200 MM |
| I.S. EN 2278:2014 | AEROSPACE SERIES - STEEL X12CRNIMOV12-3 (1.4933) - 900 MPA <= R[M] <= 1100 MPA - BARS - D[E] <= 150 MM |
| I.S. EN 4657:2010 | AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION REMELTED - BARS - A OR D <= 200 MM - R[M] >= 1650 MPA |
| UNI EN 4657 : 2011 | AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BARS - A OR D <= 200 MM - R[M] >= 1650 MPA |
| I.S. EN 2119:2017 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2601 (X6NICRTIMOV26-15) - SOLUTION TREATED AND PRECIPITATION TREATED -WIRES FOR RIVETS - 2 MM <= D <= 10 MM - R[M] >= 960 MPA |
| UNI EN 2030 : 2014 | AEROSPACE SERIES - STEEL X105CRMO17 (1.3544) - HARDENED AND TEMPERED - BARS - D[E] <= 150 MM |
| I.S. EN 2306:2017 | AEROSPACE SERIES - HEAT RESISTING - NICKEL BASE ALLOY NI-CR[20]CO[3]FE[3] - ANNEALED - BARS |
| BS EN 4721:2014 | Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted and electroslag remelted (ESR). Hardened and tempered. Bar. De ≤ 200 mm. 900 MPa ≤ Rm ≤ 1 050 MPa |
| BS EN 2482:2010 | Aerospace series. Steel FE-PL2108 (36NiCrMo16). 1100 MPa ≤ Rm ≤ 1300 MPa. Bars. De ≤ 100 mm |
| I.S. EN 2137:2017 | AEROSPACE SERIES - STEEL FE-PL75 - 1100 MPA <= R[M] <= 1250 MPA - BARS - DE <= 100 MM |
| BS EN 4720:2014 | Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted and electroslag remelted (ESR). Hardened and tempered. Bar. De ≤ 200 mm. 1 150 MPa ≤ Rm ≤ 1 300 MPa |
| BS EN 4628:2013 | Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Bar. De ≤ 200 mm. 1 150 MPa ≤ Rm ≤ 1 300 MPa |
| BS EN 4655:2010 | Aerospace series. Steel FEPM1506 (X1CrNiMoAlTi12-10-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Bars. a or D ≤ 200 mm. Rm ≥ 1400 MPa |
| 12/30263035 DC : 0 | BS EN 4825 - AEROSPACE SERIES - STEEL X12CRNIMOV12-3 (1.4933) - AIR MELTED AND CONSUMABLE ELECTRODE REMELTED - HARDENED AND TEMPERED - BAR - D[E] <= 150 MM - 900 MPA <= R[M] <= 1100 MPA |
| I.S. EN 2482:2010 | AEROSPACE SERIES - STEEL FE-PL2108 (35NICRMO16) - 1100 MPA <= R[M] <= 1300 MPA - BARS - D[E] <= 100 MM |
| I.S. EN 4500-003:2012 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 003: SPECIFIC RULES FOR HEAT RESISTING ALLOYS |
| EN 2135:2017 | Aerospace series - Steel FE-PL61 - Carburized, hardened and tempered - Bar - De ≤ 40 mm |
| UNI EN 4655 : 2011 | AEROSPACE SERIES - STEEL FE-PM1506 (X1CRNIMOAITI12-10-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BARS - A OR D <= 200 MM - R[M] >= 1400 MPA |
| EN 2119:2017 | Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated - Wires for rivets - 2 mm ≤ D ≤ 10 mm - Rm ≥ 960 MPa |
| BS EN 3528:2013 | Aerospace series. Steel X2NiCoMo18-8-5 (1.6359). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Bar. a or D ≤ 150 mm. 1 750 MPa ≤ Rm ≤ 2 000 MPa |
| 11/30243869 DC : 0 | BS EN 4631 - AEROSPACE SERIES - STEEL FE-PM 3504 (X4CRNIMO16-5-1) - AIR MELTED - HARDENED AND TEMPERED - BAR - D[E] <= 200 MM - 900 MPA <= R[M] <= 1050 MPA |
| 11/30242528 DC : DRAFT JAN 2011 | BS EN 4628 - AEROSPACE SERIES - STEEL FE-PM 3504 (X4CRNIMO16-5-1) - AIR MELTED - HARDENED AND TEMPERED - BAR D[E] <= 200 MM - 1150 MPA <= R[M] <= 1300 MPA |
| BS EN 2030:2013 | Aerospace series. Steel X105CrMo17 (1.3544). Hardened and tempered. Bars. De ≤ 150 mm |
| UNI EN 2482 : 2011 | AEROSPACE SERIES - STEEL FE-PL2108 (35NICRMO16) - 1100 MPA <= R[M] <= 1300 MPA - BARS - D[E] <= 100 MM |
| UNI EN 4500-005 : 2014 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 005: SPECIFIC RULES FOR STEELS |
| EN 2482:2010 | Aerospace series - Steel FE-PL2108 (36NiCrMo16) - 1 100 MPa ≤ Rm ≤ 1 300 MPa - Bars - De ≤ 100 mm |
| EN 4500-005:2012 | Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 005: Specific rules for steels |
| EN 4721:2014 | Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electroslag remelted (ESR) - Hardened and tempered - Bar - De ≤ 200 mm - 900 MPa ≤ Rm ≤ 1 050 MPa |
| EN 4376:2016 | Aerospace series - Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) solution treated and precipitation treated - Bar and section, De ≤ 200 mm |
| EN 4631:2013 | Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bar - De ≤ 200 mm - 900 MPa ≤ Rm ≤ 1 050 MPa |
| EN 4655:2010 | Aerospace series - Steel FE-PM1506 (X1CrNiMoAlTi12-10-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bars - a or D ≤ 200 mm - Rm ≥ 1 400 MPa |
| EN 2278:2014 | Aerospace series - Steel X12CrNiMoV12-3 (1.4933) - 900 MPa ≤ Rm ≤ 1 100 MPa - Bars - De ≤ 150 mm |
| EN 2030:2013 | Aerospace series - Steel X105CrMo17 (1.3544) - Hardened and tempered - Bars - De ≤ 150 mm |
| EN 3528:2013 | Aerospace series - Steel X2NiCoMo18-8-5 (1.6359) - Vacuum induction melted and vacuum arc remelted - Solution treated and precipitation treated - Bar - a or D ≤ 150 mm - 1 750 MPa ≤ Rm ≤ 2 000 MPa |
| EN 4500-003:2012 | Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 003: Specific rules for heat resisting alloys |
| EN 2213:2012 | Aerospace series - Steel FE-PL1505 (15CrMoV6) - Air melted - Hardened and tempered - Bars - De ≤ 16 mm - 980 MPa ≤ Rm ≤ 1 180 MPa |
| EN 4628:2013 | Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bar - De ≤ 200 mm — 1 150 MPa ≤ Rm ≤ 1 300 MPa |
| EN 4657:2010 | Aerospace series - Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bars - a or D ≤ 200 mm - Rm ≥ 1 650 MPa |
| EN 4656:2010 | Aerospace series - Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bars - a or D ≤ 200 mm - Rm ≥ 1520 MPa |
| EN 4720:2014 | Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electroslag remelted (ESR) - Hardened and tempered - Bar - De ≤ 200 mm - 1 150 MPa ≤ Rm ≤ 1 300 MPa |
| I.S. EN 4500-005:2012 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 005: SPECIFIC RULES FOR STEELS |
| BS EN 4376:2016 | Aerospace series. Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) solution treated and precipitation treated. Bar and section, De ≤ 200 mm |
| NF EN 4657 : 2011 | AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION REMELTED - BARS - A OR D < OR = 200 MM - R[M] > OR = 1650 MPA |
| BS EN 2278:2014 | Aerospace series. Steel X12CrNiMoV12-3 (1.4933). 900 MPa ≤ Rm ≤ 1 100 MPa. Bars. De ≤ 150 mm |
| UNI EN 4628 : 2013 | AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED - HARDENED AND TEMPERED - BAR - D[E] <= 200 MM - 1150 MPA <= R[M] <= 1300 MPA |
| EN 2137:2017 | Aerospace series - Steel FE-PL75 - 1 100 MPa ≤ Rm ≤ 1 250 MPa - Bars - De ≤ 100 mm |
| PREN 4842 : DRAFT 2016 | AEROSPACE SERIES - X5CRNICU15-5 (1.4545) CONSUMABLE ELECTRODE REMELTED (ESR OR VAR) - SOLUTION TREATED AND PRECIPITATION TREATED (H1025) BAR FOR MACHINING A OR D <= 250 MM 1070 MPA <= R[M] <= 1200 MPA PREMIUM QUALITY (PQ) |
| PREN 2465 : 200P1 | AEROSPACE SERIES - STEEL X2CRNI18-9 (1.4307) - SOFTENED 450 MPA <= R[M] <= 680 MPA BAR FOR MACHINING 4 MM <= D[E] <= 100 MM |
| I.S. EN 2135:2017 | AEROSPACE SERIES - STEEL FE-PL61 - CARBURIZED, HARDENED AND TEMPERED - BAR - DE <= 40 MM |
| I.S. EN 4656:2010 | AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BARS - A OR D <= 200 MM - R[M] >= 1520 MPA |
| I.S. EN 4628:2013 | AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED - HARDENED AND TEMPERED - BAR - D[E] <= 200 MM - 1150 MPA <= R[M] <= 1300 MPA |
| I.S. EN 4631:2013 | AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED - HARDENED AND TEMPERED - BAR - D[E] <= 200 MM - 900 MPA <= R[M] <= 1050 MPA |
| BS EN 2306:2017 | Aerospace series. Heat resisting. Nickel base alloy Ni-Cr20Co3Fe3. Annealed. Bars |
| EN 9100:2009 | Quality Management Systems - Requirements for Aviation, Space and Defense Organizations |
| ISO 6507-1:2005 | Metallic materials Vickers hardness test Part 1: Test method |
| EN ISO 6508-1:2016 | Metallic materials - Rockwell hardness test - Part 1: Test method (ISO 6508-1:2016) |
| PREN 2002-16 : 200P1 | AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - PART 16: NON-DESTRUCTIVE TESTING - PENETRANT TESTING |
| EN ISO 6506-1:2014 | Metallic materials - Brinell hardness test - Part 1: Test method (ISO 6506-1:2014) |
| ISO 6506-1:2014 | Metallic materials Brinell hardness test Part 1: Test method |
| ISO 4967:2013 | Steel — Determination of content of non-metallic inclusions — Micrographic method using standard diagrams |
| EN 10079:2007 | Definition of steel products |
| EN 2950:2008 | Aerospace series - Test method - Wrought heat resisting alloys Semi-finished products and parts - Conditions for macrographic and micrographic examination - Atlas of structures and defects |
| TR 2410 : 2 | AEROSPACE SERIES - METALLIC MATERIALS - RELATIONSHIP BETWEEN DIMENSIONAL STANDARDS AND MATERIAL STANDARDS |
| EN 2032-2:1994 | Aerospace series - Metallic materials - Part 2: Coding of metallurgical condition in delivery condition |
| ISO 642:1999 | Steel — Hardenability test by end quenching (Jominy test) |
| EN ISO 6892-1:2016 | Metallic materials - Tensile testing - Part 1: Method of test at room temperature (ISO 6892-1:2016) |
| EN ISO 643:2012 | Steels - Micrographic determination of the apparent grain size (ISO 643:2012) |
| ISO 6508-1:2016 | Metallic materials — Rockwell hardness test — Part 1: Test method |
| ISO 6892-1:2016 | Metallic materials Tensile testing Part 1: Method of test at room temperature |
| EN 4050-4:2012 | Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 4: Acceptance criteria |
| EN 4050-1:2012 | Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 1: General requirements |
| EN 3987:2009 | Aerospace series - Test methods for metallic materials - Constant amplitude force-controlled high cycle fatigue testing |
| SAE AMS 2750 : 2012 | PYROMETRY |
| EN 2032-001:2014 | Aerospace series - Metallic materials - Part 001: Conventional designation |
| ISO 3887:2003 | Steels Determination of depth of decarburization |
| PREN 3874 : 200P1 | AEROSPACE SERIES - TEST METHODS FOR METALLIC MATERIALS - CONSTANT AMPLITUDE FORCE-CONTROLLED LOW CYCLE FATIGUE TESTING |
| ISO 3651-2:1998 | Determination of resistance to intergranular corrosion of stainless steels — Part 2: Ferritic,austenitic and ferritic-austenitic (duplex) stainless steels — Corrosion test in media containing sulfuric acid |
| EN ISO 642:1999 | Steel - Hardenability test by end quenching (Jominy test) (ISO 642:1999) |
| ASTM E 1444 : 2005 | Standard Practice for Magnetic Particle Testing |
| EN ISO 3651-1 : 1998 | DETERMINATION OF RESISTANCE TO INTERGRANULAR CORROSION OF STAINLESS STEELS - PART 1: AUSTENITIC AND FERRITIC-AUSTENITIC (DUPLEX) STAINLESS STEELS - CORROSION TEST IN NITRIC ACID MEDIUM BY MEASUREMENT OF LOSS IN MASS (HUEY TEST) |
| ISO 3651-1:1998 | Determination of resistance to intergranular corrosion of stainless steels — Part 1: Austenitic and ferritic-austenitic (duplex) stainless steels — Corrosion test in nitric acid medium by measurement of loss in mass (Huey test) |
| EN ISO 6892-2:2011 | Metallic materials - Tensile testing - Part 2: Method of test at elevated temperature (ISO 6892-2:2011) |
| EN ISO 3651-2 : 1998 | DETERMINATION OF RESISTANCE TO INTERGRANULAR CORROSION OF STAINLESS STEELS - FERRITIC, AUSTENITIC AND FERRITIC-AUSTENITIC (DUPLEX) STAINLESS STEELS - CORROSION TEST IN MEDIA CONTAINING SULFURIC ACID |
| ISO 15549:2008 | Non-destructive testing Eddy current testing General principles |
| ISO 643:2012 | Steels Micrographic determination of the apparent grain size |
| PREN 4259 : 200P1 | AEROSPACE SERIES - METALLIC MATERIALS - DEFINITION OF GENERAL TERMS |
| EN 10027-1:2016 | Designation systems for steels - Part 1: Steel names |
| EN 2002-002:2005 | Aerospace series - Metallic materials - Test methods - Part 2: Tensile testing at elevated temperature |
| ISO 6892-2:2011 | Metallic materials Tensile testing Part 2: Method of test at elevated temperature |
| EN ISO 15549:2010 | Non-destructive testing - Eddy current testing - General principles (ISO 15549:2008) |
| SAE AMS 2315 : 2013 | DETERMINATION OF DELTA FERRITE CONTENT |
| EN ISO 148-1:2016 | Metallic materials - Charpy pendulum impact test - Part 1: Test method (ISO 148-1:2016) |
| EN 2002-005:2007 | Aerospace series - Test methods for metallic materials - Part 005: Uninterrupted creep and stress-rupture testing |
| EN 4258:1998 | Aerospace series - Metallic materials - General organization of standardization - Links between types of EN standards and their use |
| EN 2002-001:2005 | Aerospace series - Metallic materials - Test methods - Part 1: Tensile testing at ambient temperature |
| PREN 3988 : 200P1 | AEROSPACE SERIES - TEST METHODS FOR METALLIC MATERIALS - CONSTANT AMPLITUDE STRAIN-CONTROLLED LOW CYCLE FATIGUE TESTING |
| PREN 2951 : 200P1 | AEROSPACE SERIES - METALLIC MATERIALS - TEST METHOD - MICROGRAPHIC DETERMINATION OF CONTENT OF NON-METALLIC INCLUSIONS |
| EN 2078:2001 | Aerospace series - Metallic materials - Manufacturing schedule, inspection schedule, inspection and test report - Definition, general principles, preparation and approval |
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