EN 4700-006:2010
Current
Current
The latest, up-to-date edition.
Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 006: Pre-production and production forgings
Published date
01-09-2010
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Foreword
Introduction
1 Scope
2 Normative references
3 Terms and definitions
4 Wording of order
5 Health and safety
6 Technical requirements
This European Standard defines the requirements for the ordering, manufacture, testing, inspection and delivery of pre-production and production forgings in steel and heat resisting alloys.
| Committee |
ASD-STAN
|
| DevelopmentNote |
Supersedes PREN 4700-006. (04/2011)
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| UNE-EN 4700-006:2010 | Identical |
| NEN EN 4700-006 : 2010 | Identical |
| PN EN 4700-006 : 2010 | Identical |
| DIN EN 4700-006:2011-05 | Identical |
| I.S. EN 4700-006:2010 | Identical |
| SN EN 4700-006:2010 | Identical |
| UNI EN 4700-006 : 2011 | Identical |
| NBN EN 4700-006 : 2010 | Identical |
| BS EN 4700-006:2010 | Identical |
| NS EN 4700-006 : 1ED 2010 | Identical |
| NF EN 4700-006 : 2012 | Identical |
| BS EN 4671:2010 | Aerospace series. Steel FE-PM1506 (X1CrNiMoAlTi12-10-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Forgings. a or D ≤ 200 mm. Rm ≥ 1400 MPa |
| PREN 4630 : 200P2 | AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED - HARDENED AND TEMPERED - FORGINGS - D[E] <= 200 MM - 900 MPA <= R[M] <= 1050 MPA |
| NF EN 2483 : 2012 | AEROSPACE SERIES - STEEL FE-PL2108 (35NICRMO16) - 1100 MPA < OR = R[M] < OR = 1300 MPA - FORGINGS - D[E] < OR = 100 MM |
| NF EN 4658 : 2012 | AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D < OU = 200 MM - R[M] > OR = 1520 MPA |
| UNI EN 2252 : 2013 | AEROSPACE SERIES - STEEL FE-PL1505 (15CRMOV6) - 1080 MPA <= R[M] <= 1250 MPA - FORGINGS - D[E] <= 100 MM |
| 11/30243868 DC : 0 | BS EN 4630 - AEROSPACE SERIES - STEEL FE-PM 3504 (X4CRNIMO16-5-1) - AIR MELTED - HARDENED AND TEMPERED - FORGINGS - D[E] <= 200 MM - 900 MPA <= R[M] <= 1050 MPA |
| I.S. EN 2252:2012 | AEROSPACE SERIES - STEEL FE-PL1505 (15CRMOV6) - 1080 MPA <= R[M] <= 1250 MPA - FORGINGS - D[E] <= 100 MM |
| BS EN 2252:2012 | Aerospace series. Steel FE-PL1505 (15CrMoV6). 1 080 MPa ≤ Rm ≤ 1 250 MPa. Forgings. De ≤ 100 mm |
| BS EN 2483:2010 | Aerospace series. Steel FE-PL2108 (36NiCrMo16). 1100 MPa ≤ Rm ≤ 1300 MPa. Forgings. De ≤ 100 mm |
| BS EN 4658:2010 | Aerospace series. Steel FE-PM1507 (X1CrNiMoAlTi12-11-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Forgings. a or D ≤ 200 mm. R<sub>m</sub> ≥ 1520 MPa |
| I.S. EN 4659:2010 | AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 200 MM - R[M] >= 1650 MPA |
| NF EN 4659 : 2012 | AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D < OR = 200 MM - R[M] > OR = 1650 MPA |
| BS EN 4630:2014 | Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Forgings. De ≤ 200 mm. 900 MPa ≤ Rm ≤ 1 050 MPa |
| UNI EN 2483 : 2011 | AEROSPACE SERIES - STEEL FE-PL2108 (35NICRMO16) - 1100 MPA <= R[M] <= 1300 MPA - FORGINGS - D[E] <= 100 MM |
| BS EN 4659:2010 | Aerospace series. Steel FE-PM1507 (X1CrNiMoAlTi12-11-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Forgings. a or D ≤ 200 mm. R<sub>m</sub> ≥ 1650 MPa |
| BS EN 2226:2014 | Aerospace series. Steel X105CrMo17 (1.4125). Hardened and tempered. Hand and die forgings. De ≤ 150 mm |
| UNI EN 2481 : 2011 | AEROSPACE SERIES - STEEL FE-PL2108 (35NICRMO16) - 1250 MPA <= R[M] <= 1400 MPA - FORGINGS - D[E] <= 75 MM |
| EN 2174:2017 | Aerospace series - Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) - Solution treated and precipitation treated - Forgings - De ≤ 100 mm - Rm ≥ 850 MPa |
| UNI EN 2226 : 2014 | Aerospace series - Steel X105CrMo17 (1.4125) - Hardened and tempered - Hand and die forgings - De ≤ 150 mm |
| I.S. EN 4627:2014 | AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED - HARDENED AND TEMPERED - FORGINGS - D[E] <= 200 MM - 1150 MPA <= R[M] <= 1300 MPA |
| EN 2252:2012 | Aerospace series - Steel FE-PL1505 (15CrMoV6) - 1 080 MPa ≤ Rm ≤ 1 250 MPa - Forgings - De ≤ 100 mm |
| UNI EN 4659 : 2011 | AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 200 MM - R[M] >= 1650 MPA |
| BS EN 2174:2017 | Aerospace series. Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15). Solution treated and precipitation treated. Forgings. De ≤ 100 mm - Rm ≥ 850 MPa |
| UNI EN 3529 : 2011 | AEROSPACE SERIES - STEEL FE-PM2701 (X2NICOMO18-8-5) - VACUUM INDUCTION MELTED AND VACUUM ARC REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 150 MM - 1750 MPA <= R[M] <= 2000 MPA |
| I.S. EN 4671:2010 | AEROSPACE SERIES - STEEL FE-PM1506 (X1CRNIMOALTI12-10-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 200 MM - R[M] >= 1400 MPA |
| BS EN 4627:2014 | Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Forgings. De ≤ 200 mm. 1 150 MPa ≤ Rm ≤ 1 300 MPa |
| UNI EN 4671 : 2011 | AEROSPACE SERIES - STEEL FE-PM1506 (X1CRNIMOALTI12-10-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 200 MM - R[M] >= 1400 MPA |
| UNI EN 4627 : 2014 | AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED - HARDENED AND TEMPERED - FORGINGS - D[E] <= 200 MM - 1150 MPA <= R[M] <= 1300 MPA |
| I.S. EN 2483:2010 | AEROSPACE SERIES - STEEL FE-PL2108 (35NICRMO16) - 1100 MPA <= R[M] <= 1300 MPA - FORGINGS - D[E] <= 100 MM |
| I.S. EN 2226:2014 | AEROSPACE SERIES - STEEL X105CRMO17 (1.4125) - HARDENED AND TEMPERED - HAND AND DIE FORGINGS - D[E] <= 150 MM |
| I.S. EN 2481:2010 | AEROSPACE SERIES - STEEL FE-PL2108 (35NICRMO16) - 1250 MPA <= R[M] <= 1400 MPA - FORGINGS - D[E] <= 75 MM |
| EN 4659:2010 | Aerospace series - Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D ≤ 200 mm - Rm ≥ 1 650 MPa |
| EN 4658:2010 | Aerospace series - Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D ≤ 200 mm - Rm ≥ 1 520 MPa |
| EN 2226:2014 | Aerospace series - Steel X105CrMo17 (1.4125) - Hardened and tempered - Hand and die forgings - De ≤ 150 mm |
| EN 4627:2014 | Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Forgings - De ≤ 200 mm - 1 150 MPa ≤ Rm ≤ 1 300 MPa |
| EN 4630:2014 | Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Forgings - De ≤ 200 mm - 900 MPa ≤ Rm ≤ 1 050 MPa |
| EN 2483:2010 | Aerospace series - Steel FE-PL2108 (36NiCrMo16) - 1 100 MPa ≤ Rm ≤ 1 300 MPa - Forgings - De ≤ 100 mm |
| EN 4671:2010 | Aerospace series - Steel FE-PM1506 (X1CrNiMoAlTi12-10-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D ≤ 200 mm - Rm ≥ 1400 MPa |
| EN 2481:2010 | Aerospace series - Steel FE-PL2108 (36NiCrMo16) - 1 250 MPa ≤ Rm ≤ 1 400 MPa - Forgings - De ≤ 75 mm |
| I.S. EN 4630:2014 | AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED - HARDENED AND TEMPERED - FORGINGS - D[E] <= 200 MM - 900 MPA <= R[M] <= 1050 MPA |
| I.S. EN 2174:2017 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2602 (X4NICRTIMOV26-15) - SOLUTION TREATED AND PRECIPITATION TREATED -FORGINGS - DE <= 100 MM R[M] => 850 MPA |
| BS EN 2481:2010 | Aerospace series. Steel FE-PL2108 (36NiCrMo16). 1250 MPa ≤ Rm ≤ 1400 MPa. Forgings. De ≤ 75 mm |
| PREN 4627 : 200P2 | AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED - HARDENED AND TEMPERED - FORGINGS - D[E] <= 200 MM - 1150 MPA <= R[M] <= 1300 MPA |
| NF EN 2481 : 2011 | AEROSPACE SERIES - STEEL FE-PL2108 (35NICRMO16) - 1250 MPA < OR = R[M] < OR = 1400 MPA - FORGINGS - D[E] < OR = 75 MM |
| UNI EN 4658 : 2011 | AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 200 MM - R[M] >= 1520 MPA |
| NF EN 3529 : 2010 | AEROSPACE SERIES - STEEL FE-PM2701 (X2NICOMO18-8-5) - VACUUM INDUCTION MELTED AND VACUUM ARC REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D < OR = 150 MM - 1750 MPA < OR = R[M] < OR = 2000 MPA |
| I.S. EN 4658:2010 | AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 200 MM - R[M] >= 1520 MPA |
| 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 |
| 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 |
| PREN 4050-1 : 200P1 | AEROSPACE SERIES - TEST METHOD FOR METALLIC MATERIALS - ULTRASONIC INSPECTION BARS, PLATES, FORGING STOCK AND FORGINGS - GENERAL INFORMATION |
| 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 |
| EN ISO 6892-1:2016 | Metallic materials - Tensile testing - Part 1: Method of test at room temperature (ISO 6892-1:2016) |
| 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 |
| SAE AMS2750E | Pyrometry |
| EN 10045-1 : 1990 | METALLIC MATERIALS - CHARPY IMPACT TEST - PART 1: TEST METHOD |
| PREN 3874 : 200P1 | AEROSPACE SERIES - TEST METHODS FOR METALLIC MATERIALS - CONSTANT AMPLITUDE FORCE-CONTROLLED LOW CYCLE FATIGUE TESTING |
| PREN 2003-2 : 200P1 | AEROSPACE SERIES - STEELS - TEST METHODS - PART 2: IZOD IMPACT TEST |
| 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 2032-1:2001 | Aerospace series - Metallic materials - Part 1: Conventional designation |
| 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) |
| PREN 3987 : 200P1 | AEROSPACE SERIES - TEST METHODS FOR METALLIC MATERIALS - CONSTANT AMPLITUDE FORCE-CONTROLLED HIGH CYCLE FATIGUE TESTING |
| 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 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 |
| 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 |
| SAE AMS2315G | Determination of Delta Ferrite Content |
| ASTM E 709 : 2015 : REDLINE | Standard Guide for Magnetic Particle Testing |
| EN 2002-005:2007 | Aerospace series - Test methods for metallic materials - Part 005: Uninterrupted creep and stress-rupture testing |
| 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 4050-4 : 200P1 | AEROSPACE SERIES - TEST METHOD FOR METALLIC MATERIALS - ULTRASONIC INSPECTION OF BARS, PLATES, FORGING STOCK AND FORGINGS - ACCEPTANCE CRITERIA |
| 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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