PREN 4050-4 : 200P1
Withdrawn
Withdrawn
View Superseded by
AEROSPACE SERIES - TEST METHOD FOR METALLIC MATERIALS - ULTRASONIC INSPECTION OF BARS, PLATES, FORGING STOCK AND FORGINGS - ACCEPTANCE CRITERIA
Available format(s)
Hardcopy , PDF
Language(s)
English
Withdrawn date
12-18-2023
Superseded by
US$31.30
Excluding Tax where applicable
1 Scope
2 Normative references
3 Acceptance criteria
4 Choice of technique
Covers the acceptance criteria for products ultrasonically inspected in accordance with EN 4050-1.
| Committee |
C5
|
| DocumentType |
Draft
|
| Pages |
4
|
| ProductNote |
Superseded by EN 4050-4:2012
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Withdrawn
|
| SupersededBy |
| Standards | Relationship |
| DIN EN 4050-4:2012-12 | Identical |
| 94/712749 DC : 0 | Identical |
| NF EN 4050-4 : 2013 | Identical |
| I.S. EN 2252:2012 | AEROSPACE SERIES - STEEL FE-PL1505 (15CRMOV6) - 1080 MPA <= R[M] <= 1250 MPA - FORGINGS - D[E] <= 100 MM |
| BS 3L500(2011) : 2011 | PROCEDURE FOR INSPECTION, TESTING AND ACCEPTANCE OF WROUGHT MAGNESIUM BASE ALLOYS |
| PREN 4400-6 : 200P1 | AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM- AND MAGNESIUM- ALLOYS - TECHNICAL SPECIFICATION - PART 6: ALUMINIUM ALLOY FORGING STOCK |
| PREN 3312 : 200P3 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AI-4V) - ANNEALED - FORGINGS - D[E] <= 150 MM |
| PREN 4050-2 : 200P1 | AEROSPACE SERIES - TEST METHOD FOR METALLIC MATERIALS - ULTRASONIC INSPECTION OF BARS, PLATES, FORGING STOCK AND FORGINGS - PERFORMANCE OF TEST |
| PREN 4700-005 : 200P2 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 005: FORGING STOCK |
| PREN 4800-006 : 200P2 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 6: PRE-PRODUCTION AND PRODUCTION FORGINGS |
| PREN 4800-005 : 200P2 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 5: FORGING STOCK |
| PREN 3813 : 200P2 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AI-4V) - ANNEALED - BAR AND WIRE FOR FORGED FASTENERS - D[E] <= 50 MM |
| PREN 4050-3 : 200P1 | AEROSPACE SERIES - TEST METHOD FOR METALLIC MATERIALS - ULTRASONIC INSPECTION OF BARS, PLATES, FORGING STOCK AND FORGINGS - REFERENCE BLOCKS |
| PREN 4700-006 : 200P2 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 006: PRE-PRODUCTION AND PRODUCTION FORGINGS |
| I.S. EN 4800-002:2010 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 002: BAR AND SECTION |
| I.S. EN 3312:2012 | AEROSPACE SERIES - TITANIUM ALLOY TI-6AL-4V - ANNEALED - FORGINGS - D[E] <= 150 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 |
| 12/30268169 DC | BS EN 8.4567. Aerospace series. Aluminium alloy AL-P7010. T76. Extruded bars. 150 mm < D ≤ 250 mm |
| BS 4HR100(2010):2010 | AEROSPACE SERIES - PROCEDURE FOR INSPECTION, TESTING AND ACCEPTANCE OF WROUGHT HEAT-RESISTING ALLOYS |
| BS EN 2483:2010 | Aerospace series. Steel FE-PL2108 (36NiCrMo16). 1100 MPa ≤ Rm ≤ 1300 MPa. Forgings. De ≤ 100 mm |
| 01/713948 DC : 0 | PREN 4400-6 - AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM ALLOY WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 6: FORGING STOCK |
| BS EN 3525:2007 | Aerospace series. Steel FE-PL1505 (15CrMoV6). Air melted. Hardened and tempered. Plate. 6 mm ≪ a ≤ 20 mm. 1080 MPa ≤ Rm ≤ 1280 MPa |
| 10/30227732 DC : 0 | BS EN 2419 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024- AL CU4MG1 - T351 - PLATE - 6 MM < A <= 150 MM |
| BS EN 4700-006:2010 | Aerospace series. Steel and heat resisting alloys. Wrought products. Technical specification Pre-production and production forgings |
| 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 |
| BS EN 2481:2010 | Aerospace series. Steel FE-PL2108 (36NiCrMo16). 1250 MPa ≤ Rm ≤ 1400 MPa. Forgings. De ≤ 75 mm |
| BS EN 13981-4:2006 | Aluminium and aluminium alloys. Products for structural railway applications. Technical conditions for inspection and delivery Forgings |
| BS EN 3677:2007 | Aerospace series. Steel FE-PM3801 (X5CrNiCu17-4). Air melted. Solution treated and precipitation treated. Forgings. a or D ≤ 200 mm. Rm ≥ 1310 MPa |
| 09/30209802 DC : 0 | BS EN 2252 - AEROSPACE SERIES - STEEL FE-PL1505 (15CRMOV6) - 1080 MPA <= R[M] <= 1250 MPA - FORGINGS - D[E] <= 100 MM |
| 01/716044 DC : 0 | EN 4800-6 - AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 6: PRE-PRODUCTION AND PRODUCTION FORGINGS |
| 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 3678:2007 | Aerospace series. Steel FE-PM3801 (X5CrNiCu17-4). Air melted. Solution treated and precipitation treated. Forgings. a or D ≤ 200 mm. Rm ≥ 930 MPa |
| 11/30243867 DC : 0 | BS EN 4629 - AEROSPACE SERIES - STEEL FE-PM 3504 (X4CRNIMO16-5-1) - AIR MELTED - HARDENED AND TEMPERED - FORGING STOCK - D[E] <= 300 MM |
| I.S. EN 4700-001:2010 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 001: PLATE, SHEET AND STRIP |
| PREN 2483 : 200P1 | AEROSPACE SERIES - STEEL FE-PL2108 (36NICRMO16) - 1100 MPA <= R[M] <= 1300 MPA - FORGINGS - D[E] <= 100 MM |
| I.S. EN 3464:2012 | AEROSPACE SERIES - TITANIUM ALLOY TI-6AL-4V - ANNEALED - PLATE - 6 MM < A <= 100 MM |
| NF EN 4700-002 : 2012 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 002: BAR AND SECTION |
| BS EN 4700-001:2010 | Aerospace series. Steel and heat resisting alloys. Wrought products. Technical specification Plate, sheet and strip |
| I.S. EN 4800-005:2010 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 005: FORGING STOCK |
| I.S. EN 2482:2010 | AEROSPACE SERIES - STEEL FE-PL2108 (35NICRMO16) - 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 |
| PREN 3464 : 200P3 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - PLATE - 6 MM < A <= 100 MM |
| 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 3163:2007 | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - AIR MELTED, SOFTENED, FORGING STOCK A OR D <= 300 MM |
| I.S. EN 4700-006:2010 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 006: PRE-PRODUCTION AND PRODUCTION FORGINGS |
| DIN EN 13981-4:2007-02 | Aluminium and aluminium alloys - Products for structural railway applications - Technical conditions for inspection and delivery - Part 4: Forgings |
| 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 |
| PREN 2252 : 200P1 | AEROSPACE SERIES - STEEL FE-PL1505 (15CRMOV6) - 1080 MPA <= R[M] <= 1250 MPA - FORGINGS - D[E] <= 100 MM |
| PREN 2633 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024 - T3511 - EXTRUDED BARS AND SECTIONS 1,2 MM <= D[E] <= 160 MM WITH PERIPHERAL COARSE GRAIN CONTROL |
| 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 |
| PREN 4629 : 200P2 | AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED - SOFTENED - FORGING STOCK - D[E] <= 300 MM |
| PREN 4642 : 200P1 | 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 |
| PREN 4800-002 : 200P2 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 2: BAR AND SECTION |
| 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 2483:2010 | AEROSPACE SERIES - STEEL FE-PL2108 (35NICRMO16) - 1100 MPA <= R[M] <= 1300 MPA - FORGINGS - D[E] <= 100 MM |
| I.S. EN 4700-005:2010 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 005: FORGING STOCK |
| I.S. EN 2481:2010 | AEROSPACE SERIES - STEEL FE-PL2108 (35NICRMO16) - 1250 MPA <= R[M] <= 1400 MPA - FORGINGS - D[E] <= 75 MM |
| BS EN 4800-005:2010 | Aerospace series. Titanium and titanium alloys. Technical specification Forging stock |
| 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 3464:2012 | Aerospace series. Titanium alloy (Ti-6Al-4V). Annealed. Plate. 6 mm < a ≤ 100 mm |
| 12/30268163 DC : 0 | BS EN 8.4569 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024- AL CU4MG1 - T351 - PLATE - 6 MM < A <= 150 MM |
| BS EN 3459:2010 | Aerospace series. Titanium alloy TI-P63001 (Ti-4Al-4Mo-2Sn). Solution treated and aged. Plate. 6 mm < a ≤ 50 mm |
| 01/716043 DC : 0 | PREN 4800-5 - AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 5: FORGING STOCK |
| 12/30263296 DC : 0 | BS EN 2278 - AEROSPACE SERIES - STEEL FE-PM1502 (Z12CNDV12) - 900 MPA <= R[M] <= 1100 MPA - BARS - D[E] <= 150 MM |
| 11/30243872 DC : 0 | BS EN 8.4553 - AEROSPACE SERIES - COPPER ALLOY CUBE 1.9 - BARS |
| 00/705877 DC : 0 | PREN 4400-3 - AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM ALLOY WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 3: BAR AND SECTION |
| 09/30209898 DC : DRAFT SEP 2009 | BS EN 3813 - AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - BAR AND WIRE FOR FORGED FASTENERS - D[E] <= 50 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 |
| BS EN 3479:2007 | Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Plate - 6 mm < a ≤ 20 mm - 1070 MPa ≤ Rm ≤ 1220 MPa |
| 09/30199939 DC : 0 | BS 4HR 100 - PROCEDURE FOR INSPECTION, TESTING AND ACCEPTANCE OF WROUGHT HEAT-RESISTING ALLOYS |
| 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 |
| 11/30243873 DC : 0 | BS EN 8.4554 - AEROSPACE SERIES - COPPER ALLOY CUBE 1.9 - SHEET AND STRIP |
| BS EN 3163:2007 | Aerospace series. Steel FE-PM3801 (X5CrNiCu17-4). Air melted, softened, forging stock a or D ≤ 300 mm |
| BS EN 4800-001:2010 | Aerospace series. Titanium and titanium alloys. Technical specification Plate, sheet and strip |
| BS EN 4800-002:2010 | Aerospace series. Titanium and titanium alloys. Technical specification Bar and section |
| BS 4HR 100:2010+A1:2012 | Aerospace series. Procedure for inspection, testing and acceptance of wrought heat-resisting alloys |
| 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 |
| EN 2482:2010 | Aerospace series - Steel FE-PL2108 (36NiCrMo16) - 1 100 MPa ≤ Rm ≤ 1 300 MPa - Bars - De ≤ 100 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 4800-002:2010 | Aerospace series - Titanium and titanium alloys - Technical specification - Part 002: Bar and section |
| EN 4800-001:2010 | Aerospace series - Titanium and titanium alloys - Technical specification - Part 001: Plate, sheet and strip |
| EN 3464:2012 | Aerospace series - Titanium alloy Ti-6Al-4V - Annealed - Plate - 6 mm < a ≤ 100 mm |
| EN 3677:2007 | Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted - Solution treated and precipitation treated - Forgings - a or D ≤ 200 mm - Rm ≥ 1 310 MPa |
| EN 13981-4:2006 | Aluminium and aluminium alloys - Products for structural railway applications - Technical conditions for inspection and delivery - Part 4: Forgings |
| EN 4700-005:2010 | Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 005: Forging stock |
| EN 2399:2008 | Aerospace series - Heat resisting steel FE-PA2601 (X4NiCrTiMoV26-15) - Rm ≥ 900 MPa - Bars for forged bolts - D ≤ 25 mm |
| EN 3163:2007 | Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted, softened, forging stock a or D ≤ 300 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 3525:2007 | Aerospace series - Steel FE-PL1505 (15CrMoV6) - Air melted - Hardened and tempered - Plate - 6 mm < a ≤ 20 mm - 1 080 MPa ≤ Rm ≤ 1 280 MPa |
| EN 3479:2007 | Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Plate - 6 mm < a ≤ 20 mm - 1 070 MPa ≤ Rm ≤ 1 220 MPa |
| EN 2398:2008 | Aerospace series - Heat resisting steel FE-PA2601 (X6NiCrTiMoV26-15) - Rm ≥ 900 MPa - Bars for machined bolts - D ≤ 25 mm |
| 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 4800-006:2010 | Aerospace series - Titanium and titanium alloys - Technical specification - Part 006: Pre-production and production forgings |
| EN 2483:2010 | Aerospace series - Steel FE-PL2108 (36NiCrMo16) - 1 100 MPa ≤ Rm ≤ 1 300 MPa - Forgings - De ≤ 100 mm |
| EN 3638:2007 | Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Consumable electrode remelted - Solution and precipitation treated - Sheet, strip and plate - 0,5 mm ≤ a ≤ 10 mm |
| EN 3678:2007 | Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted - Solution treated and precipitation treated - Forgings - a or D ≤ 200 mm - Rm ≥ 930 MPa |
| EN 4800-005:2010 | Aerospace series - Titanium and titanium alloys - Technical specification - Part 005: Forging stock |
| EN 3459:2010 | Aerospace series - Titanium alloy TI-P63001 (Ti-4Al-4Mo-2Sn) - Solution treated and aged - Plate - 6 mm < a ≤ 50 mm |
| EN 4700-001:2010 | Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 001: Plate, sheet and strip |
| EN 4700-006:2010 | Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 006: Pre-production and production forgings |
| EN 2481:2010 | Aerospace series - Steel FE-PL2108 (36NiCrMo16) - 1 250 MPa ≤ Rm ≤ 1 400 MPa - Forgings - De ≤ 75 mm |
| I.S. EN 4800-006:2010 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 006: PRE-PRODUCTION AND PRODUCTION FORGINGS |
| 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 4800-001 : 200P2 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 1: PLATE, SHEET AND STRIP |
| PREN 2481 : 200P1 | AEROSPACE SERIES - STEEL FE-PL2108 (36NICRMO16) - 1250 MPA <= R[M] <= 1400 MPA - FORGINGS - D[E] <= 75 MM |
| 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 2512 : 200P3 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7175-T7351 - PLATE - 6 MM < A <= 100 MMM |
| PREN 2704 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024 - T3511 - DRAWN BAR D[E] <= 75 MM |
| PREN 3163 : 200P1 | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - AIR MELTED - SOFTENED - FORGING STOCK - A OR D <= 300 MM |
| PREN 4400-1 : 200P1 | AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM ALLOY WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 1: PLATE |
| PREN 4050-1 : 200P1 | AEROSPACE SERIES - TEST METHOD FOR METALLIC MATERIALS - ULTRASONIC INSPECTION BARS, PLATES, FORGING STOCK AND FORGINGS - GENERAL INFORMATION |
| PREN 2030 : 200P1 | AEROSPACE SERIES - STEEL FE-PM3501 (X105CRMO17) - HARDENED AND TEMPERED - BARS D[E] <= 150 MM |
| PREN 4700-001 : 200P2 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 001: PLATE, SHEET AND STRIP |
| PREN 4400-3 : 200P1 | AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM ALLOY WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 3: BAR AND SECTION |
| I.S. EN 4800-001:2010 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 001: PLATE, SHEET AND STRIP |
| I.S. EN 3459:2010 | AEROSPACE SERIES - TITANIUM ALLOY TI-P63001 (TI-4AL-4MO-2SN) - SOLUTION TREATED AND AGED - PLATE - 6 MM < A <= 50 MM |
| 10/30239368 DC : 0 | BS EN 2512 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7175- AL ZN5,5MGCU(B) - T7351 - PLATE - 6 MM < A <= 100 MM |
| 12/30263035 DC | BS EN 4825. Aerospace series. Steel X12CrNiMoV12-3 (1.4933). Air melted and consumable electrode remelted. Hardened and tempered. Bar. De ≤ 150 mm. 900 MPa ≤ Rm ≤ 1100 MPa |
| 13/30290101 DC : 0 | BS EN 4700-2 - AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 002: BAR AND SECTION |
| BS EN 4800-006:2010 | Aerospace series. Titanium and titanium alloys. Technical specification Pre-production and production forgings |
| BS EN 3638:2007 | Aerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Consumable electrode remelted. Solution and precipitation treated. Sheet, strip and plate. 0,5 mm ≤ a ≤ 10 mm |
| BS EN 4700-005:2010 | Aerospace series. Steel and heat resisting alloys. Wrought products. Technical specification Forging stock |
| 09/30210353 DC : 0 | BS EN 3464 EDP3 - AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - PLATE - 6 MM < A <= 100 MM |
| 09/30205254 DC : 0 | BS EN 2481 - AEROSPACE SERIES - STEEL FE-PL76 - 1250 MPA <= R[M] <= 1400 MPA - FORGINGS D[E] <= 75 MM |
| BS EN 2482:2010 | Aerospace series. Steel FE-PL2108 (36NiCrMo16). 1100 MPa ≤ Rm ≤ 1300 MPa. Bars. De ≤ 100 mm |
| 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 |
| 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 |
| PREN 4050-1 : 200P1 | AEROSPACE SERIES - TEST METHOD FOR METALLIC MATERIALS - ULTRASONIC INSPECTION BARS, PLATES, FORGING STOCK AND FORGINGS - GENERAL INFORMATION |
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