PREN 4700-002 : 200P3
Withdrawn
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
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AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 002: BAR AND SECTION
Available format(s)
Hardcopy , PDF
Withdrawn date
20-12-2023
Superseded by
Language(s)
English
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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
Specifies the requirements for the ordering, manufacture, testing, inspection and delivery of steel and heat resisting alloy bar and section.
| DevelopmentNote |
Supersedes PREN 3235-1, PREN 3235-3, PREN 4235-1 and PREN 4235-3. (06/2003)
|
| DocumentType |
Draft
|
| Pages |
31
|
| ProductNote |
Superseded by EN 4700-002:2016
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Withdrawn
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| SupersededBy | |
| Supersedes |
| I.S. EN 3161:2007 | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - AIR MELTED, SOLUTION TREATED AND PRECIPITATION TREATED, BAR A OR D <= 200 MM, R[M] >= 930 MPA |
| PREN 3487 : 200P2 | AEROSPACE SERIES - STEEL FE-PA3601 (X6CRNITI18-10) - AIR MELTED - SOFTENED - BAR FOR MACHINING - A OR D <= 250 MM - 500 MPA <= R[M] <= 700 MPA |
| BS EN 2465:2007 | Aerospace series. Steel FE-PA3901 (X2CrNi18-9). Softened. 450 MPa ≤ Rm ≤ 680 MPa. Bar for machining. 4 mm ≤ De ≤ 100 mm |
| PREN 4656 : 200P1 | 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] >= 1520 MPA |
| 06/30146139 DC : 0 | EN 2465 - AEROSPACE SERIES - STEEL FE-PA3901 (X2CRNI18.9) - SOFTENED 450 -RM - 680 MPA - BAR FOR MACHINING, 4 - DE - 100 |
| 09/30211106 DC : 0 | BS EN 2030 - AEROSPACE SERIES - STEEL FE-PM3501 (X105CRMO17) - HARDENED AND TEMPERED - BARS D <= 150 MM |
| BS EN 4642:2009 | Aerospace series. Steel FE-PM 3504 (X4CrNiMo16-5-1). Air melted. Hardened and tempered. Sheet and plate. 0,6 mm ≤ a ≤ 50 mm. 900 MPa ≤ Rm ≤ 1050 MPa |
| 08/30180761 DC : DRAFT APR 2008 | |
| BS EN 2398:2008 | Aerospace series. Heat resisting steel FE-PA2601(X6NiCrTiMoV26-15). Rm ≥ 900 MPa. Bars for machined bolts. D ≤ 25 mm |
| BS EN 4318:2007 | Aerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and precipitation treated, bar and section De ? 100 mm, Rm ? 960 MPa |
| BS EN 3490:2007 | Aerospace series. Steel FE-PM3901 (X15CrNi17-3). Air melted. Hardened and tempered. Bar for machining. De ≤ 200 mm. 900 MPa ≤ Rm ≤ 1100 MPa |
| 06/30146155 DC : 0 | EN 4631 - AEROSPACE SERIES - STEEL FE-PM 3504 (X4CRNIMO16-5-1) - AIR MELTED HARDENED AND TEMPERED BAR - DE = 200 MM 900 MPA = RM = 1 050 MPA |
| BS EN 2817:2009 | Aerospace series. Steel FE-PM1802 (X5CrNiCu15-5). Consumable electrode remelted. Solution treated and precipitation treated. Bar for machining. a or D ≤ 200 mm. Rm ≥ 1070 MPa |
| PREN 4657 : 200P1 | 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 |
| NF EN 2465 : 2008 | AEROSPACE SERIES - STEEL FE-PA3901 (X2CRNI18-9) - SOFTENED - 450 MPA <= R[M] <= 680 MPA - BAR FOR MACHINING - 4 MM <= D[E] <= 100 MM |
| I.S. EN 4642:2009 | AEROSPACE SERIES - STEEL FE-PM 3504 (X4CRNIMO16-5-1) - AIR MELTED - HARDENED AND TEMPERED - SHEET AND PLATE - 0,6 MM <= A <= 50 MM - 900 MPA <= R[M] <= 1050 MPA |
| I.S. EN 3487:2007 | AEROSPACE SERIES - STEEL FE-PA3601 (X6CRNITI18-10) - AIR MELTED - SOFTENED - BAR FOR MACHINING - A OR D <= 250 MM - 500 MPA <= R[M] <= 700 MPA |
| 09/30205255 DC : 0 | BS EN 2482 - AEROSPACE SERIES - STEEL FE-PL2108 (36NICRMO16) - 1100 MPA <= R[M] <= 1300 MPA - BARS - D[E] <= 100 MM |
| 08/30181052 DC : DRAFT APR 2008 | |
| BS EN 4467:2007 | Aerospace series. Steel FE-PM1505 (X1CrNiMoAlTi12-9-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Bar. a or D ≤ 150 mm. Rm ≥ 1200 MPa |
| BS EN 2446:2008 | Aerospace series. Steel FE-PL1503 (35CrMo4). 1100 MPa ≤ Rm ≤ 1300 MPa. Bars. De ≤ 25 mm |
| I.S. EN 2448:2008 | AEROSPACE SERIES - STEEL FE-PL1503 (35CRMO4) - 900 MPA <= R[M] <= 1100 MPA - BARS - D[E] <= 40 MM |
| I.S. EN 4463:2007 | |
| PREN 2482 : 200P1 | AEROSPACE SERIES - STEEL FE-PL2108 (36NICRMO16) - 1100 MPA <= R[M] <= 1300 MPA - BARS - D[E] <= 100 MM |
| PREN 3528 : 200P2 | AEROSPACE SERIES - STEEL FE-PM2701 (X2NICOMO18-8-5) - VACUUM INDUCTION MELTED AND VACUUM ARC REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BAR - A OR D <= 150 MM - 1750 MPA <= R[M] <= 2000 MPA |
| I.S. EN 2399:2008 | AEROSPACE SERIES - HEAT RESISTING STEEL FE-PA2601 (X4NICRTIMOV26-15) - R[M] >= 900 MPA - BARS FOR FORGED BOLTS - D <= 25 MM |
| I.S. EN 3330:2009 | AEROSPACE SERIES - STEEL FE-PL1503 (35CRMO4) - ANNEALEAD - BAR AND WIRE - D[E] <= 40 MM - FOR PREVAILING TORQUE NUTS |
| I.S. EN 4467:2007 | |
| I.S. EN 2460:2009 | AEROSPACE SERIES - STEEL FE-PM1901 (X12CR13) - 600 MPA <= R[M] <= 800 MPA - BARS - D[E] <= 70 MM |
| I.S. EN 2205:2009 | AEROSPACE SERIES - STEEL FE-PL1502 (25CRMO4) - 900 MPA <= R[M] <= 1100 MPA - BARS - D[E] <= 40 MM |
| I.S. EN 3160:2007 | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - AIR MELTED, SOLUTION TREATED AND PRECIPITATION TREATED, BAR A OR D <= 200 MM, R[M] >= 1310 MPA |
| I.S. EN 2446:2008 | AEROSPACE SERIES - STEEL FE-PL1503 (35CRMO4) - 1100 MPA <= R[M] <= 1300 MPA - BARS - D[E] <= 25 MM |
| I.S. 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 - R[M] >= 1400 MPA |
| I.S. EN 2398:2008 | AEROSPACE SERIES - HEAT RESISTING STEEL FE-PA2601 (X6NICRTIMOV26-15) - R[M] >= 900 MPA - BARS FOR MACHINED BOLTS - D <= 25 MM |
| I.S. EN 2206:2008 | AEROSPACE SERIES - STEEL FE-PL1502 (25CRMO4) - 650 MPA <= R[M] <= 850 MPA - BARS - D[E] <= 150 MM |
| PREN 4631 : 200P2 | 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 2817:2009 | AEROSPACE SERIES - STEEL FE-PM1802 (X5CRNICU15-5) - CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BAR FOR MACHINING - A OR D <= 200 MM - R[M] >= 1070 MPA |
| I.S. EN 2438:2008 | AEROSPACE SERIES - STEEL FE-PL2102 (35NICR6) - 900 MPA <= R[M] <= 1100 MPA - BARS - D[E] <= 40 MM |
| I.S. EN 2465:2007 | AEROSPACE SERIES - STEEL FE-PA3901 (X2CRNI18-9) - SOFTENED - 450 MPA <= R[M] <= 680 MPA - BAR FOR MACHINING - 4 MM <= D[E] <= 100 MM |
| I.S. EN 4461:2007 | |
| BS EN 2448:2008 | Aerospace series. Steel FE-PL1503 (35CrMo4). 900 MPa ≤ Rm ≤ 1100 MPa. Bars. De ≤ 40 mm |
| 06/30146957 DC : 0 | EN 3488 - AEROSPACE SERIES - STEEL FE-PA3601 (X6CRNITI18.10) - AIR MELTED SOFTENED SHEET AND STRIP A = 6 MM 500 = RM = 700 MPA |
| BS EN 2399:2008 | Aerospace series. Heat resisting steel FE-PA2601 (X4NiCrTiMoV26-15). Rm ≥ 900 MPa. Bars for forged bolts. D ≤ 25 mm |
| BS EN 3487:2007 | Aerospace series. Steel FE-PA3601 (X6CrNiTi18-10). Air melted. Softened. Bar for machining. a or D ≤ 250 mm. 500 MPa ≤ Rm ≤ 700 MPa |
| 10/30239354 DC : 0 | BS EN 4720 - AEROSPACE SERIES - STEEL FE-PM 3504 (X4CRNIMO16-5-1) - AIR MELTED AND ELECTROSLAG REMELTED (ESR) - HARDENED AND TEMPERED - BAR - D[E] <= 200 MM - 1150 MPA <= R[M] <= 1300 MPA |
| BS EN 4468:2007 | Aerospace series. Steel FE-PM1505 (X1CrNiMoAlTi12-9-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Bar. a or D ≤ 150 mm. Rm ≥ 1300 MPa |
| BS EN 4461:2007 | Aerospace series. Steel FE-PM1506 (X5CrNiMoAl13-8-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Bar. a or D ≤ 150 mm. Rm ≥ 1200 MPa |
| BS EN 3523:2007 | Aerospace series. Steel FE-PL1505 (15CrMoV6). Air melted. Hardened and tempered. Bar for machining. De ≤ 100 mm. 1080 MPa ≤ Rm ≤ 1280 MPa |
| 12/30263296 DC : 0 | BS EN 2278 - AEROSPACE SERIES - STEEL FE-PM1502 (Z12CNDV12) - 900 MPA <= R[M] <= 1100 MPA - BARS - D[E] <= 150 MM |
| BS EN 2206:2008 | Aerospace series. Steel FE-PL1502 (25CrMo4). 650 MPa ≤ Rm ≤ 850 MPa. Bars. De ≤ 150 mm |
| BS EN 3161:2007 | Aerospace series. Steel FE-PM3801 (X5CrNiCu17-4). Air melted, solution treated and precipitation treated, bar a or D ≤ 200 mm, Rm ≥ 930 MPa |
| BS EN 2478:2008 | Aerospace series. Steel FE-PL2107 (30NiCrMo16). 1220 MPa ≤ Rm ≤ 1370 MPa. Bars. De ≤ 40 mm |
| BS EN 2542:2008 | Aerospace series. Steel FE-PL1502 (25CrMo4). Annealed. Bar and wire. De ≤ 40 mm. For prevailing torque nuts |
| 06/30146677 DC : 0 | EN 3487 - AEROSPACE SERIES - STEEL FE-PA3601 (X6CRNITI18-10) AIR MELTED SOFTENED BAR FOR MACHINING A OR D - 250 MM 500 - RM - 700 MPA |
| 09/30204515 DC : DRAFT MAY 2009 | BS EN 3528 - AEROSPACE SERIES - STEEL FE-PM2701 (X2NICOMO18-8-5) - CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BAR - D[E] <= 150 MM - 1750 MPA <= R[M] <= 2000 MPA |
| BS EN 4463:2007 | Aerospace series. Steel FE-PM1506 (X5CrNiMoAl13-8-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Bar. a or D ≤ 150 mm. Rm ≥ 1400 MPa |
| BS EN 2438:2008 | Aerospace series. Steel FE-PL2102 (35NiCr6). 900 MPa ≤ Rm ≤ 1100 MPa. Bars. De ≤ 40 mm |
| BS EN 2205:2009 | Aerospace series. Steel FE-PL1502 (25CrMo4). 900 MPa ≤ Rm ≤ 1100 MPa. Bars. De ≤ 40 mm |
| BS EN 3330:2009 | Aerospace series. Steel FE-PL1503 (35CrMo4). Annealed. Bar and wire. De ≤ 40 mm. For prevailing torque nuts |
| BS EN 2460:2009 | Aerospace series. Steel FE-PM1901 (X12CrNi13). 600 MPa ≤ Rm ≤ 800 MPa. Bars. De ≤ 70 mm |
| BS EN 3160:2007 | Aerospace series. Steel FE-PM3801 (X5CrNiCu17-4). Air melted, solution treated and precipitation treated, bar a or D ≤ 200 mm, Rm ≥ 1310 MPa |
| BS EN 2821:2007 | Aerospace series. Steel FE-PM1802 (X5CrNiCu15-5). Consumable electrode remelted. Solution treated and precipitation treated. Bar for machining. a or D ≤ 200 mm. Rm ≥ 1310 MPa |
| 06/30146391 DC : 0 | EN 2467 - AEROSPACE SERIES - STEEL FE-PA3901 (X2CRNI18.9) - AIR MELTED SOFTENED PLATE SHEET AND STRIP 0,4 = A = 20 MM 520 = RM = 670 MPA |
| EN 3487:2007 | Aerospace series - Steel FE-PA3601 (X6CrNiTi18-10) - Air melted - Softened - Bar for machining - a or D ≤ 250 mm - 500 MPa ≤ Rm ≤ 700 MPa |
| EN 2446:2008 | Aerospace series - Steel FE-PL1503 (35CrMo4) - 1 100 MPa ≤ Rm ≤ 1 300 MPa - Bars - De ≤ 25 mm |
| EN 2438:2008 | Aerospace series - Steel FE-PL2102 (35NiCr6) - 900 MPa ≤ Rm ≤ 1 100 MPa - Bars - De ≤ 40 mm |
| EN 2821:2007 | Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Bar for machining - a or D ≤ 200 mm - Rm ≥ 1 310 MPa |
| EN 4315:2007 | Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section a or D ≤ 100 mm, Rm ≥ 900 MPa |
| EN 2480:2008 | Aerospace series - Steel FE-PL2108 (36NiCrMo16) - 1 250 MPa ≤ Rm ≤ 1 400 MPa - Bars - De ≤ 75 mm |
| EN 2448:2008 | Aerospace series - Steel FE-PL1503 (35CrMo4) - 900 MPa ≤ Rm ≤ 1 100 MPa - Bars - De ≤ 40 mm |
| EN 2460:2009 | Aerospace series - Steel FE-PM1901 (X12CrNi13) - 600 MPa ≤ Rm ≤ 800 MPa - Bars - De ≤ 70 mm |
| EN 2399:2008 | Aerospace series - Heat resisting steel FE-PA2601 (X4NiCrTiMoV26-15) - Rm ≥ 900 MPa - Bars for forged bolts - D ≤ 25 mm |
| EN 4642:2009 | Aerospace series - Steel FE-PM 3504 (X4CrNiMo16-5-1) - Air melted - Hardened and tempered - Sheet and plate - 0,6 mm ≤ a ≤ 50 mm - 900 MPa ≤ Rm ≤ 1 050 MPa |
| EN 4469:2007 | Aerospace series - Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bar - a or D ≤ 150 mm - Rm ≥ 1 400 MPa |
| EN 2478:2008 | Aerospace series - Steel FE-PL2107 (30NiCrMo16) - 1 220 MPa ≤ Rm ≤ 1 370 MPa - Bars - De ≤ 40 mm |
| EN 4462:2007 | Aerospace series - Steel FE-PM1506 (X5CrNiMoAl13-8-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bar - a or D ≤ 150 mm - Rm ≥ 1 300 MPa |
| EN 4463:2007 | Aerospace series - Steel FE-PM1506 (X5CrNiMoAl13-8-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bar - a or D ≤ 150 mm - Rm ≥ 1 400 MPa |
| EN 3490:2007 | Aerospace series - Steel FE-PM3901 (X15CrNi17-3) - Air melted - Hardened and tempered - Bar for machining - De ≤ 200 mm - 900 MPa ≤ Rm ≤ 1 100 MPa |
| EN 2206:2008 | Aerospace series - Steel FE-PL1502 (25CrMo4) - 650 MPa ≤ Rm ≤ 850 MPa - Bars - De ≤ 150 mm |
| EN 3160:2007 | Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted, solution treated and precipitation treated, bar a or D ≤ 200 mm, Rm ≥ 1 310 MPa |
| EN 4467:2007 | Aerospace series - Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bar - a or D ≤ 150 mm - Rm ≥ 1 200 MPa |
| EN 3330:2009 | Aerospace series - Steel FE-PL1503 (35CrMo4) - Annealead - Bar and wire - De ≤ 40 mm - For prevailing torque nuts |
| EN 2398:2008 | Aerospace series - Heat resisting steel FE-PA2601 (X6NiCrTiMoV26-15) - Rm ≥ 900 MPa - Bars for machined bolts - D ≤ 25 mm |
| EN 2465:2007 | Aerospace series - Steel FE-PA3901 (X2CrNi18-9) - Softened - 450 MPa ≤ Rm ≤ 680 MPa - Bar for machining - 4 mm ≤ De ≤ 100 mm |
| EN 3161:2007 | Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted, solution treated and precipitation treated, bar a or D ≤ 200 mm, Rm ≥ 930 MPa |
| EN 2542:2008 | Aerospace series - Steel FE-PL1502 (25CrMo4) - Annealed - Bar and wire - De ≤ 40 mm - For prevailing torque nuts |
| EN 3523:2007 | Aerospace series - Steel FE-PL1505 (15CrMoV6) - Air melted - Hardened and tempered - Bar for machining - De ≤ 100 mm - 1 080 MPa ≤ Rm ≤ 1 280 MPa |
| EN 4461:2007 | Aerospace series - Steel FE-PM1506 (X5CrNiMoAl13-8-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bar - a or D ≤ 150 mm - Rm ≥ 1 200 MPa |
| EN 4468:2007 | Aerospace series - Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bar - a or D ≤ 150 mm - Rm ≥ 1 300 MPa |
| EN 2815:2009 | Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Bar for machining - a or D ≤ 200 mm - Rm ≥ 965 MPa |
| EN 3972:2006 | Aerospace series - Steel FE-PL1507 (40CrMoV12) - Consumable electrode remelted - Hardened and tempered - Bar for machining - De ≤ 50 mm - 1 250 MPa ≤ Rm ≤ 1 400 MPa |
| EN 4318:2007 | Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section De ≤ 100 mm, Rm ≥ 960 MPa |
| EN 2205:2009 | Aerospace series - Steel FE-PL1502 (25CrMo4) - 900 MPa ≤ Rm ≤ 1 100 MPa - Bars - De ≤ 40 mm |
| EN 2817:2009 | Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Bar for machining - a or D ≤ 200 mm - Rm ≥ 1 070 MPa |
| PREN 4628 : 200P2 | AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED - HARDENED AND TEMPERED - BAR - D[E] <= 200 MM - 1150 MPA <= R[M] <= 1300 MPA |
| PREN 2213 : 200P1 | AEROSPACE SERIES - STEEL FE-PL1505 (15CRMOV6) - AIR MELTED - HARDENED AND TEMPERED - BARS - D[E] <= 16 MM - 980 MPA <= R[M] <= 1180 MPA |
| PREN 4500-005 : 200P2 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 005: SPECIFIC RULES FOR STEELS |
| PREN 4655 : 200P1 | AEROSPACE SERIES - STEEL FE-PM1506 (X1CRNIMOALTI12-10-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION REMELTED - BARS - A OR D <= 200 MM - R[M] >= 1400 MPA |
| PREN 2030 : 200P1 | AEROSPACE SERIES - STEEL FE-PM3501 (X105CRMO17) - HARDENED AND TEMPERED - BARS D[E] <= 150 MM |
| PREN 4500-003 : 200P2 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 003: SPECIFIC RULES FOR HEAT RESISTING SLLOYS |
| I.S. EN 2542:2008 | AEROSPACE SERIES - STEEL FE-PL1502 (25CRMO4) - ANNEALED - BAR AND WIRE - D[E] <= 40 MM - FOR PREVAILING TORQUE NUTS |
| I.S. EN 4462:2007 | |
| I.S. EN 2480:2008 | AEROSPACE SERIES - STEEL FE-PL2108 (36NICRMO16) - 1250 MPA <= R[M] <= 1400 MPA - BARS - D[E] <= 75 MM |
| I.S. EN 4468:2007 | |
| I.S. EN 2815:2009 | AEROSPACE SERIES - STEEL FE-PM1802 (X5CRNICU15-5) - CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BAR FOR MACHINING - A OR D <= 200 MM - R[M] >= 965 MPA |
| I.S. EN 4469:2007 | |
| I.S. EN 2478:2008 | AEROSPACE SERIES - STEEL FE-PL2107 (30NICRMO16) - 1220 MPA <= R[M] <= 1370 MPA - BARS - D[E] <= 40 MM |
| BS EN 2480:2008 | Aerospace series. Steel FE-PL2108 (36NiCrMo16). 1250 MPa ≤ Rm ≤ 1400 MPa. Bars. De ≤ 75 mm |
| 09/30211096 DC : 0 | BS EN 2213 - AEROSPACE SERIES - STEEL FE-PL1505 (15CRMOV6) - 980 MPA <= R[M] <= 1180 MPA - BARS - D[E] <= 16 MM |
| 06/30146146 DC : 0 | EN 4628 - AEROSPACE SERIES - STEEL FE-PM 3504 (X4CRNIMO16-5-1) - AIR MELTED HARDENED AND TEMPERED BAR - DE = 150 MM 1 100 MPA = RM = 1 300 MPA |
| 06/30146674 DC : 0 | EN 3480 - AEROSPACE SERIES - STEEL FE-PA3601 (X6CRNITI18.10) AIR MELTED SOFTENED PLATE 6 |
| BS EN 4462:2007 | Aerospace series. Steel FE-PM1506 (X5CrNiMoAl13-8-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Bar. a or D ≤ 150 mm. Rm ≥ 1300 MPa |
| BS EN 2815:2009 | Aerospace series. Steel FE-PM1802 (X5CrNiCu15-5). Consumable electrode remelted. Solution treated and precipitation treated. Bar for machining. a or D ≤ 200 mm. Rm ≥ 965 MPa |
| BS EN 4315:2007 | Aerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and precipitation treated, bar and section a or D ? 100 mm, Rm ? 900 MPa |
| BS EN 3972:2006 | Aerospace series. Steel FE-PL1507 (40CrMoV12). Consumable electrode remelted. Hardened and tempered. Bar for machining. De ≤ 50 mm. 1250 MPa ≤ Rm ≤ 1400 MPa |
| 08/30181037 DC : DRAFT APR 2008 | |
| 10/30239355 DC : 0 | BS EN 4721 - AEROSPACE SERIES - STEEL FE-PM 3504 (X4CRNIMO16-5-1) - AIR MELTED AND ELECTROSLAG REMELTED (ESR)-HARDENED AND TEMPERED - BAR - D[E] <= 200 MM - 900 MPA <= R[M] <= 1050 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 |
| 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 |
| ISO 148-1:2016 | Metallic materials — Charpy pendulum impact test — Part 1: Test method |
| EN 10045-1 : 1990 | METALLIC MATERIALS - CHARPY IMPACT TEST - PART 1: TEST METHOD |
| 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) |
| 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) |
| 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 |
| 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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