PREN 4700-002 : 200P3
Withdrawn
Withdrawn
View Superseded by
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 002: BAR AND SECTION
Available format(s)
Hardcopy , PDF
Language(s)
English
Withdrawn date
12-20-2023
Superseded by
US$296.20
Excluding Tax where applicable
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Superseded by EN 4700-002:2016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Withdrawn
|
| 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 MPaAerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and precipitation treated, bar and section De ≤ 100 mm, Rm ≤ 960 MPaAerospace 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 MPaAerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and precipitation treated, bar and section a or D ≤ 100 mm, Rm ≤ 900 MPaAerospace 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 AMS2750E | 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 AMS2315G | 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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