EN 4700-006:2010
Withdrawn
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 006: Pre-production and production forgings
Published date
01-09-2010
Publisher
Withdrawn date
31-03-2011
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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 |
Withdrawn
|
| Supersedes |
| Standards | Relationship |
| 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 |
| 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 |
| UNE-EN 4700-006:2010 | 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 |
| 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 |
| 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 |
| EN 2174:2017 | Aerospace series - Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) - Solution treated and precipitation treated - Forgings - De ≤ 100 mm - Rm ≥ 850 MPa |
| 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 |
| 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 |
| 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 |
| 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 |
| 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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