EN 4258:1998
Current
Current
The latest, up-to-date edition.
Aerospace series - Metallic materials - General organization of standardization - Links between types of EN standards and their use
Published date
20-05-1998
Publisher
0 Introduction
1 Scope
2 Normative references
3 Definitions
4 Description of the types of EN standards
5 Links between types of EN standards and use
6 Overview
Annex A (normative) New organization
Annex B (normative) Use of the material standard
Annex C (normative) Intermediate procedure
This standard specifies the general organization of metallic material standards, their links with other types of EN standards and their use, for aerospace applications. It corresponds to level 0 (see 4.1).
| Committee |
ASD-STAN
|
| DevelopmentNote |
Supersedes PREN 4258. (10/2002)
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| UNE-EN 4258:1998 | Identical |
| NBN EN 4258 : 1998 | Identical |
| NEN EN 4258 : 1998 | Identical |
| NS EN 4258 : 1ED 1998 | Identical |
| I.S. EN 4258:1998 | Identical |
| PN EN 4258 : 2002 | Identical |
| SNV DIN EN 4258 : 1998 | Identical |
| UNI EN 4258 : 1999 | Identical |
| BS EN 4258:1998 | Identical |
| NF EN 4258 : 1998 | Identical |
| DIN EN 4258:1998-07 | Identical |
| EN 2306 : 2017 | AEROSPACE SERIES - HEAT RESISTING - NICKEL BASE ALLOY NI-CR[20]CO[3]FE[3] - ANNEALED - BARS |
| BS EN 2206:2008 | Aerospace series. Steel FE-PL1502 (25CrMo4). 650 MPa ≤ Rm ≤ 850 MPa. Bars. De ≤ 150 mm |
| 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 |
| BS EN 4700-001:2010 | Aerospace series. Steel and heat resisting alloys. Wrought products. Technical specification Plate, sheet and strip |
| 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 |
| 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 |
| 96/716593 DC : 0 | PREN 2403 - HEAT RESISTING ALLOY NI-CH2601 (NICR19FE19NB5MO3) SOLUTION AND PRECIPITATION TREATED - PRECISION CASTING D[E] <= 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 |
| 96/716618 DC : DRAFT DEC 1996 | PREN 4383 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-CH2601 - (NICR19FE19NB5M03) AS CAST - REMELTING STOCK |
| 00/705877 DC : 0 | PREN 4400-3 - AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM ALLOY WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 3: BAR AND SECTION |
| 97/718299 DC : DRAFT OCT 1997 | PREN 2539 - AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - AIR MELTED SOLUTION TREATED AND PRECIPATION HARDENED BAR A OR D <= 150 MM - RM => 965 MPA |
| NF EN 2117 : 2009 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P5056A (5056A)-H32 - WIRE FOR SOLID RIVETS - D <= 10 MM |
| 05/30129558 DC : 0 | PREN 4700-7 - AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 7: REMELTING STOCK |
| BS EN 2542:2008 | Aerospace series. Steel FE-PL1502 (25CrMo4). Annealed. Bar and wire. De ≤ 40 mm. For prevailing torque nuts |
| NF EN 4655 : 2011 | AEROSPACE SERIES - STEEL FE-PM 1506 (X1CRNIMOALTI12-10-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BARS - A OR D < OR = 200 MM - RM > OR = 1400 MPA |
| 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 |
| 97/719253 DC : DRAFT NOV 1997 | PREN 4287 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7010 - FORGING STOCK |
| BS EN 2704:2015 | Aerospace series. Aluminium alloy AL-P2024. AlCu4Mg1. T3511. Drawn bars. De ≤ 75 mm |
| BS EN 2818:2009 | Aerospace series. Steel FE-PM1802 (X5CrNiCu15-5). Consumable electrode remelted. Solution treated and precipitation treated. Forgings. a or D ≤ 200 mm. Rm ≥ 1070 MPa |
| BS EN 2573:2007 | Aerospace series. Steel FE-PA3601 (X6CrNiTi18-10). Softened. Rm ≤ 780 MPa. Wire. 0,25 mm ≤ De ≤ 3 mm |
| 01/716453 DC : DRAFT JAN 2002 | PREN 2694 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6061 - T6 OR T62 SHEET AND STRIP - 0,4 MM < A < 6 MM |
| 17/30364757 DC : 0 | BS EN 2465 - AEROSPACE SERIES - STEEL FE-PA3901 (X2CRNI18-9) - SOFTENED - 450 MPA <= R[M] <= 680 MPA - BAR FOR MACHINING - 4 MM <= D[E] <= 100 MM |
| 99/705885 DC : DRAFT MAR 1999 | PREN 2002-1 - AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - PART 1: TENSILE TESTING AT AMBIENT TEMPERATURE |
| 96/716614 DC : 0 | PREN 4379 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH3601 (NICR22MO9NB) SOLUTION TREATED - FORGING D[E] <= 200 MM |
| BS EN 4379:2007 | Aerospace series. Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb).Solution treated, forging De ≤ 200 mm |
| BS EN 2399:2008 | Aerospace series. Heat resisting steel FE-PA2601 (X4NiCrTiMoV26-15). Rm ≥ 900 MPa. Bars for forged bolts. D ≤ 25 mm |
| 10/30228108 DC : 0 | BS EN 4400-9 - AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM- AND MAGNESIUM- ALLOYS - TECHNICAL SPECIFICATION - PART 9: PRE-PRODUCTION AND PRODUCTION CASTINGS |
| BS EN 4500-005:2012 | Aerospace series. Metallic materials. Rules for drafting and presentation of material standards Specific rules for steels |
| 11/30248019 DC : 0 | AEROSPACE SERIES - COPPER ALLOY CUBE 1.9 - SOLUTION TREATED AND PRECIPITATION TREATED - BAR - 5 MM <= A OR D <= 190 MM - R[M] >= 1050 MPA |
| BS EN 4725:2014 | Aerospace series. Aluminium alloy AL-P2024- Al Cu4Mg1. T351. Plate. 6 mm < a ≤ 150 mm |
| 96/716595 DC : 0 | PREN 2407 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2601 (NICR19FE19NB5MO3) SOLUTION AND PRECIPITATION TREATED - SHEET, STRIP AND PLATE 0,2 MM <= A <= 10 MM |
| I.S. EN 2032-1:2002 | AEROSPACE SERIES - METALLIC MATERIALS - PART 1: CONVENTIONAL DESIGNATION |
| 97/718302 DC : DRAFT OCT 1997 | PREN 2774 - AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - CONSUMABLE ELECTRODE REMELTED SOLUTION TREATED AND PRECIPATION HARDENED BAR A OR D <= 200 MM - RM => 1310 MPA |
| I.S. EN 3354:2013 | AEROSPACE SERIES - TITANIUM ALLOY TI-6AL-4V - ANNEALED - SHEET FOR SUPERPLASTIC FORMING - A <= 6 MM |
| BS EN 3813:2013 | Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Bar and wire for forged fasteners. D<sub>e</sub> ≤ 50 mm |
| 97/719239 DC : DRAFT NOV 1997 | PREN 2485 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2214 - FORGING STOCK |
| BS EN 3311:2009 | Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Bar for machining. D < 110 mm |
| 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 |
| 05/19993827 DC : 0 | BS EN 3120 - AEROSPACE SERIES - TITANIUM ALLOY TI-P64003 - COLD WORKED AND STRESS RELIEVED. SEAMLESS TUBE FOR PRESSURE SYSTEMS - 4 MM <= D <= 50 MM 690 MPA <= RM <= 1030 MPA |
| NF EN 3480 : 2008 | AEROSPACE SERIES - STEEL FE-PA3601 (X6CRNITI18-10) - AIR MELTED - SOFTENED - PLATE - 6 MM < A <= 50 MM - 500 MPA <= R[M] <= 700 MPA |
| UNI EN 4685 : 2011 | AEROSPACE SERIES - TITANIUM TI10V2FE3AL - BARS - D < 110 MM - R[M] >= 1240 MPA |
| BS EN 4262:2013 | Aerospace series. Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20). As forged. Forging stock. a or D ≤ 200 mm - 690 MPa ≤ Rm ≤ 880MPa |
| BS 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 ≤ 150 mm. 1750 MPa ≤ Rm ≤ 2000 MPa |
| BS EN 4471:2007 | Aerospace series. Steel FE-PM1505 (X1CrNiMoAITi12-9-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Forgings. a or D ≤ 150 mm. Rm ≥ 1300 MPa |
| 01/710777 DC : 0 | PREN 3875 - AEROSPACE SERIES - METALLIC MATERIALS - FILLER METAL FOR BRAZING - TECHNICAL SPECIFICATION |
| BS EN 4377:2015 | Aerospace series. Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668). Non heat treated. Forging stock. a or D ≤ 300 mm |
| 96/716570 DC : 0 | PREN 2091 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024-T4 - CLAD SHEET AND STRIP FOR STRETCH FORMING 0,3 MM <= A <= 6 MM |
| 95/715397 DC : 0 | PREN 4261-6 - AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF TEST METHOD STANDARDS - PART 6: SPECIFIC REQUIREMENTS FOR CHEMICAL ANALYSIS METHOD STANDARD |
| 05/30129551 DC : 0 | PREN 4700-5 - AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 5: FORGING STOCK |
| 96/716619 DC : 0 | PREN 4384 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-CH1303 (NICO20CR20MO5TI2A1) AS CAST - REMELTING STOCK |
| NF EN 3459 : 2010 | AEROSPACE SERIES - TITANIUM ALLOY TI-P63001 (TI-4AI-4MO-2SN) - SOLUTION TREATED AND AGED - PLATE - 6 MM < A < OR = 50 MM |
| 96/716574 DC : DRAFT DEC 1996 | PREN 2635 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2014A T6511 - EXTRUDED BARS AND SECTION 1,2 MM <= A <= D <= 200 MM WITH PERIPHERAL COARSE GRAIN CONTROL |
| DIN EN 2002-21:2000-07 (Draft) | AEROSPACE SERIES - METALLIC MATERIALS; TEST METHODS - PART 21: RADIOGRAPHIC TESTING OF CASTINGS |
| 02/702554 DC : DRAFT FEB 2002 | BS EN 2703 - ALUMINIUM ALLOY AL-P2024-T4 OR T42 - CLAD SHEET AND STRIP - 0,4 <= A <= 6 MM |
| I.S. EN 3359:2007 | AEROSPACE SERIES - STEEL FE-PM1503 (X3CRNIMOAL13-8-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOFTENED - FORGING STOCK - A OR D <= 300 MM |
| 01/713948 DC : 0 | PREN 4400-6 - AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM ALLOY WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 6: FORGING STOCK |
| 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 |
| 98/700452 DC : 0 | PREN 4448 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7050-T7452 - DIE FORGINGS A <= 150 MM |
| EN 2222 : 2017 | AEROSPACE SERIES - STEEL FE-PL31 - HARDENED AND TEMPERED - HAND AND DIE FORGINGS |
| 96/716567 DC : 0 | PREN 4400-1 - AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM ALLOY WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 1: GENERAL REQUIREMENTS |
| DIN EN 6025:1999-04 (Draft) | AEROSPACE SERIES - PLATES - ALUMINIUM ALLOYS 2024, TOLERANCE FLATNESS, THICKNESS 6 MM < A = 55 MM; DIMENSIONS |
| NF EN 4685 : 2012 | AEROSPACE SERIES - TITANIUM TI10V2FE3AL - BARS - D < 110 MM - R[M] > OR = 1240 MPA |
| BS EN 3310:2011 | Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Not heat treated. Forging stock, for annealed forgings. De ≤ 360 mm |
| 98/719299 DC : 0 | DRAFT EUROPEAN (AECMA) AEROSPACE STANDARD PREN 3125 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-C42201-T6 - INVESTMENT CASTING A LESS THAN OR EQUAL TO 20 MM |
| 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 4700-005:2010 | Aerospace series. Steel and heat resisting alloys. Wrought products. Technical specification Forging stock |
| BS EN 4500-003:2012 | Aerospace series. Metallic materials. Rules for drafting and presentation of material standards Specific rules for heat resisting alloys |
| BS EN 3469:2009 | Aerospace series. Steel FE-PM1802 (X5CrNiCu15-5). Consumable electrode remelted. Solution treated and precipitation treated. Forgings. a or D ≤ 200 mm. Rm ≥ 1310 MPa |
| BS EN 4631:2013 | Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Bar. De ≤ 200 mm. 900 MPa ≤ Rm ≤ 1 050 MPa |
| 98/712164 DC : DRAFT JULY 98 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2014A-T6 OR T62 - CLAD SHEETAND STRIP - 0,4 MM LESS THAN OR EQUAL TO A LESS THAN OR EQUAL TO 6 MM |
| BS EN 3330:2009 | Aerospace series. Steel FE-PL1503 (35CrMo4). Annealed. Bar and wire. De ≤ 40 mm. For prevailing torque nuts |
| 08/30181065 DC : DRAFT APR 2008 | BS EN 4670 - AEROSPACE SERIES - STEEL FE-PM(X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOFTENED - FORGING STOCK - A OR D <= 300 MM |
| I.S. EN 4685:2011 | AEROSPACE SERIES - TITANIUM TI10V2FE3AL - BARS - D < 110 MM - R[M] >= 1240 MPA |
| 97/718307 DC : DRAFT OCT 1997 | PREN 2917 - AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - CONSUMABLE ELECTRODE REMELTED SOLUTION TREATED AND PRECIPITATION HARDENED BAR A OR D <= 200 MM - RM => 1070 MPA |
| 99/710246 DC : JUL 99 | PREN 2002-21 - AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - PART 21: RADIOGRAPHIC TESTING OF CASTINGS |
| 97/700683 DC : DRAFT JAN 1997 | PREN 3638 - HEAT RESISTING ALLOY FE-PA2601 (X6NICRTIMOV26-15) - SOLUTION AND PRECIPITATION TREATED. SHEET, STRIP AND PLATE 0,5 MM <= A <= 10 MM |
| NF EN 3359 : A2008 | AEROSPACE SERIES - STEEL FE-PM1503 (X3CRNIMOAI13-8-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED, SOFTENED, FORGING STOCK A OR D <= 300 MM |
| BS EN 4526:2013 | Aerospace series. Metallic materials. Test methods. Sharp edge-notch tensile testing for sheet and strip |
| 09/30211096 DC : 0 | BS EN 2213 - AEROSPACE SERIES - STEEL FE-PL1505 (15CRMOV6) - 980 MPA <= R[M] <= 1180 MPA - BARS - D[E] <= 16 MM |
| 97/718312 DC : DRAFT OCT 1997 | AEROSPACE SERIES - STEEL FE-CM3801 (X5CRNICU16-4) - HOMOGENIZED, SOLUTION TREATED, PRECIPITATION HARDENED AND SUB ZERO SAND OR INVESTEMENT CASTING - RM >= 1240 MPA |
| 08/30181106 DC : DRAFT APR 2008 | |
| 04/30112065 DC : DRAFT APR 2004 | EN 2072 - AEROSPACE SERIES - ALUMINIUM ALLOY ALP1050A H14 - SHEET AND STRIP 0,4 MM <= A <= 6 MM |
| BS EN 4464:2007 | Aerospace series. Steel FE-PM1506 (X5CrNiMoAl13-8-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Forgings. a or D ≤ 150 mm. Rm ≥ 1200 MPa |
| PREN 2539 : 200P2 | AEROSPACE SERIES - STEEL FE-PM 3801 (X5CRNICU17-4) - AIR MELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BAR - A OR D <= 200 MM - R[M] >= 965 MPA |
| PREN 2187 : 200P2 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1301 (NICR19CO18MO4TI3AL3) - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - D[E] <= 200 MM - R[M] >= 1 300 MPA |
| PREN 2695 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6081-T6 - SHEET AND STRIP - 0,3 MM <= A <= 6 MM |
| PREN 2726 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-C42201 - T6 - SAND CASTING - A <= 20 MM |
| PREN 2804 : 200P3 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7075-T7651 - PLATE - 6 MM < A <= 25 MM |
| 97/717257 DC : DRAFT OCT 1997 | PREN 4094 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-CH1305 (NICR16CO10MO8AL4TI4) - VACUUM MELTED NOT HEAT TREATED REMELTING STOCK |
| 96/716598 DC : 0 | PREN 4314 - AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2602 (X4NICRTIMOV26-15) AS FORGED - FORGING STOCK A OR D <= 200 MM |
| PREN 2278 : 1 | AEROSPACE SERIES - STEEL X12CRNIMOV12-3 (1.4933) - 900 MPA <= R[M] <= 1100 MPA - BARS - D[E] <= 150 MM |
| NF EN 3115 : 2009 | AEROSPACE SERIES - ALUMINIUM ALLOY 7050-T73 - WIRE FOR SOLID RIVETS - D <= 10 MM |
| PREN 2203 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1303 (NICO20CR20MO5TI2AL) - SOLUTION TREATED - SHEET, STRIP AND PLATE - 0,2 MM <= A <= 10 MM |
| BS EN 4347:2007 | Aerospace series. Steel FE-PM1506 (X3CrNiMoAl13-8-2). Vacuum induction melted and consumable electrode remelted, softened, forging stock a or D ≤ 300 mm |
| 96/716596 DC : DRAFT DEC 1996 | PREN 3668 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2301 (NICR21FE18MO9) AS WROUGHT - FORGING STOCK A OR D <= 250 MM |
| 09/30205254 DC : 0 | BS EN 2481 - AEROSPACE SERIES - STEEL FE-PL76 - 1250 MPA <= R[M] <= 1400 MPA - FORGINGS D[E] <= 75 MM |
| 06/30146142 DC : 0 | EN 4627 - AEROSPACE SERIES - STEEL FE-PM 3504 (X4CRNIMO16-5-1) - AIR MELTED HARDENED AND TEMPERED FORGINGS-DE = 150 MM 1 100 MPA = RM = 1 300 MPA |
| BS EN 4466:2007 | Aerospace series. Steel FE-PM1506 (X5CrNiMoAl13-8-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Forgings. a or D ≤ 150 mm. Rm ≥ 1400 MPa |
| PREN 2407 : 200P1 | AEROSPACE SERIES - HEAT RESISTING NICKEL BASE ALLOY NI-PH2601 (NICR19FE19NB5MO3) - SOLUTION TREATED AND PRECIPITATION TREATED - SHEET, STRIP AND PLATE - 0,2 MM <= A <= 10 MM |
| 96/716612 DC : 0 | PREN 4377 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2601 (NICR19FE19NB5MO3) AS WROUGHT FORGING STOCK A OR D <= 300 MM |
| PREN 3160 : 200P1 | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - AIR MELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BAR - A OR D <= 200 MM - R[M] >= 1310 MPA |
| UNI EN 4800-006 : 2011 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 006: PRE-PRODUCTION AND PRODUCTION FORGINGS |
| I.S. EN 4725:2014 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024- AL CU4MG1 - T351 - PLATE - 6 MM < A <= 150 MM |
| BS EN 3163:2007 | Aerospace series. Steel FE-PM3801 (X5CrNiCu17-4). Air melted, softened, forging stock a or D ≤ 300 mm |
| 07/30171301 DC : 0 | BS EN 3238 - AEROSPACE SERIES - METALLIC MATERIALS - TEST METHOD - SHEAR TEST FOR WIRES AND RIVETS |
| PREN 3976 : 200P1 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TEST METHOD - CHEMICAL ANALYSIS FOR THE DETERMINATION OF HYDROGEN CONTENT |
| 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 |
| PREN 2115 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY 2117-T42 WIRE FOR SOLID RIVETS D <= 10 MM |
| PREN 4400-6 : 200P1 | AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM- AND MAGNESIUM- ALLOYS - TECHNICAL SPECIFICATION - PART 6: ALUMINIUM ALLOY FORGING STOCK |
| NF EN 2815 : 2010 | AEROSPACE SERIES - STEEL FE-PM1802 (X5CRNICU15-5) - CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BAR FOR MACHINING - A OR D < OR = 200 MM - R[M] > OR = 965 MPA |
| 97/719252 DC : DRAFT NOV 1997 | PREN 4285 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2219-T851 - FORGINGS - A <= 400 MM |
| PREN 2483 : 200P1 | AEROSPACE SERIES - STEEL FE-PL2108 (36NICRMO16) - 1100 MPA <= R[M] <= 1300 MPA - FORGINGS - D[E] <= 100 MM |
| I.S. EN 4377:2015 | AEROSPACE SERIES - HEAT RESISTING ALLOY NICR19FE19NB5MO3 (2.4668) - NON HEAT TREATED - FORGING STOCK - A OR D <= 300 MM |
| PREN 2951 : 200P2 | AEROSPACE SERIES - METALLIC MATERIALS - TEST METHOD - MICROGRAPHIC DETERMINATION OF CONTENT OF NON-METALLIC INCLUSIONS |
| PREN 3312 : 200P3 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AI-4V) - ANNEALED - FORGINGS - D[E] <= 150 MM |
| PREN 3332 : 200P3 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7475-T762 - CLAD SHEET AND STRIP - 1,0 MM <= A <= 6 MM |
| PREN 3342 : 200P3 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6061-T4 OR T42 - DRAWN OR EXTRUDED BAR AND SECTION - A OR D <= 150 MM |
| PREN 3531 : 200P2 | AEROSPACE SERIES - STEEL FE-PM2701 (X2NICOMO18-8-5) - VACUUM INDUCTION MELTED AND VACUUM ARC REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - SHEET AND STRIP - A <= 6 MM - 1750 MPA <= R[M] <= 2000 MPA |
| PREN 3456 : 200P3 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - SHEET AND STRIP, HOT ROLLED - A <= 6 MM |
| PREN 3490 : 200P2 | |
| PREN 3677 : 200P1 | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - AIR MELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 200 MM - R[M] >= 1310 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 |
| PREN 2690 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7050-T7452 - HAND FORGINGS - A <= 200 MM |
| PREN 3524 : 200P2 | AEROSPACE SERIES - STEEL FE-PL1505 (15CRMOV6) - AIR MELTED - HARDENED AND TEMPERED - SHEET AND STRIP - 2 MM <= A <= 6 MM - 1080 MPA <= R[M] <= 1280 MPA |
| PREN 2702 : 200P3 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6061-T6 OR T62 - DRAWN OR EXTRUDED BAR AND SECTION - A OR D <= 200 MM |
| PREN 2402 : 200P1 | AEROSPACE SERIES - HEAT RESISTING NICKEL BASE ALLOY NICR20CO3FE3 - ANNEALED - WIRE - D <= 10 MM |
| PREN 2815 : 200P3 | |
| PREN 2917 : 200P2 | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BAR - A OR D <= 200 MM - R[M] >= 1 070 MPA |
| PREN 2635 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2014A - T6511 - EXTRUDED BAR AND SECTION - A OR D <= 200 MM - WITH PERIPHERAL COARSE GRAIN CONTROL |
| PREN 2475 : 200P1 | |
| PREN 2573 : 200P2 | AEROSPACE SERIES - STEEL FE-PA3601 (X6CRNITI18-10) - SOFTENED - R[M] <= 780 MPA - WIRE - 0,25 MM <= DE <= 3 MM |
| PREN 2632 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7075-T73511 - EXTRUDED BAR AND SECTION - A OR D <= 150 MM - WITH PERIPHERAL COARSE GRAIN CONTROL |
| PREN 2731 : 200P2 | AEROSPACE SERIES - MAGNESIUM ALLOY MG-C46001 - T6 - SAND CASTINGS |
| PREN 2764 : 200P3 | AEROSPACE SERIES - STEEL FE-PL1504 (33CRMOV12) - AIR MELTED - HARDENED AND TEMPERED - FORGINGS - D[E] <= 80 MM - 1200 MPA <= R[M] <= 1400 MPA |
| PREN 2774 : 200P2 | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU 17-4) - CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BAR - A OR D <= 200 MM - R[M] >= 1310 MPA |
| PREN 2805 : 200P3 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7475-T7651 - PLATE - 6 MM < A <= 40 MM |
| PREN 2818 : 200P3 | AEROSPACE SERIES - STEEL FE-PM1802 (X5CRNICU15-5) - CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 200 MM - R[M] >= 1 070 MPA |
| I.S. EN 4720:2014 | AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED AND ELECTROSLAG REMELTED (ESR) - HARDENED AND TEMPERED - BAR - D[E] <= 200 MM - 1150 MPA <= R[M] <= 1300 MPA |
| UNI EN 4003 : 2008 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2219-T87 - SHEET AND STRIP 0,5 MM <= A <= 6 MM |
| PREN 2049 : 200P1 | AEROSPACE SERIES - EXTRUDED CHANNEL SECTION, IN ALUMINIUM ALLOYS - DIMENSIONS |
| PREN 4700-004 : 200P2 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 4: WIRE |
| PREN 4283 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2219-T87 - PLATE - 6 MM < A <= 40 MM |
| PREN 4290 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2219 - FORGING STOCK |
| 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 4524 : 200P1 | AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - MEASUREMENT OF FATIGUE CRACK GROWTH RATES |
| PREN 4700-005 : 200P2 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 005: FORGING STOCK |
| PREN 4658 : 200P1 | AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION REMELTED - FORGINGS - A OR D <= 200 MM - R[M] >= 1520 MPA |
| PREN 4721 : DRAFT 2012 | AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED AND ELECTROSLAG REMELTED (ESR) - HARDENED AND TEMPERED - BAR - D[E] <=200 MM - 900 MPA <= R[M] <= 1050 MPA |
| PREN 4400-4 : DRAFT 2003 | AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM- AND MAGNESIUM-ALLOYS - TECHNICAL SPECIFICATION - PART 4: ALUMINIUM AND ALUMINIUM ALLOY TUBE |
| 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 |
| PREN 4800-006 : 200P2 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 6: PRE-PRODUCTION AND PRODUCTION FORGINGS |
| PREN 4659 : 200P1 | AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION REMELTED - FORGINGS - A OR D <= 200 MM - R[M] >= 1650 MPA |
| PREN 4449 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7050 - T76 - SHEET - 0,8 MM <= A <= 6 MM |
| PREN 4462 : 200P1 | |
| PREN 4470 : 200P1 | AEROSPACE SERIES - STEEL FE-PM1505 (X1CRNIMOALTI12-9-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 150 MM - R[M] >= 1 200 MPA |
| PREN 4313 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6013-T6 - SHEET AND STRIP - 0,5 MM <= A <= 6 MM |
| PREN 4545 : 200P1 | AEROSPACE SERIES - STEEL FE-PL1505 (15CRMOV6) - AIR MELTED - HARDENED AND TEMPERED - PLATE - 20 MM <= A <= 50 MM - 1080 MPA <= R[M] <= 1280 MPA |
| PREN 4007 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6082-T6 OR T62 - SHEET AND STRIP - 0,4 MM <= A <= 6 MM |
| PREN 4372 : 200P2 | AEROSPACE SERIES - HEAT RESISTING NICKEL ALLOY WITH COPPER NI-PD9001 (NICU31) - WIRE FOR SOLID RIVETS - D <= 10 MM |
| UNI EN 4500-003 : 2014 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 003: SPECIFIC RULES FOR HEAT RESISTING ALLOYS |
| PREN 4467 : 200P1 | |
| PREN 4472 : 200P1 | AEROSPACE SERIES - STEEL FE-PM1505 (X1CRNIMOALTI12-9-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 150 MM - R[M] >= 1 400 MPA |
| PREN 4100 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2219-T62 OR T62 - SHEET AND STRIP - 0,5 MM <= A <= 6 MM |
| I.S. EN 4347:2007 | AEROSPACE SERIES STEEL FE-PM1506 (X3CRNIMOAL13-8-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED, SOFTENED, FORGING STOCK A OR D <= 300 MM |
| PREN 4800-005 : 200P2 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 5: FORGING STOCK |
| PREN 4212 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P5086 - H111 - PLATE - 6 MM < A <= 80 MM |
| PREN 3813 : 200P2 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AI-4V) - ANNEALED - BAR AND WIRE FOR FORGED FASTENERS - D[E] <= 50 MM |
| PREN 4005 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P5052 - O - SHEET AND STRIP - 0,3 MM <= A <= 6 MM |
| PREN 2002-16 : 200P1 | AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - PART 16: NON-DESTRUCTIVE TESTING - PENETRANT TESTING |
| PREN 4720 : DRAFT 2012 | AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED AND ELECTROSLAG REMELTED (ESR) - HARDENED AND TEMPERED - BAR - D[E] <= 200 MM - 1150 MPA <= R[M] <= 1300 MPA |
| PREN 4286 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P8090-T89 - DIE FORGINGS - A <= 125 MM |
| PREN 2050 : 200P1 | AEROSPACE SERIES - EXTRUDED T-SECTION, IN ALUMINIUM ALLOYS - DIMENSIONS |
| PREN 3480 : 200P2 | AEROSPACE SERIES - STEEL FE-PA3601 (X6CRNITI18-10) - AIR MELTED - SOFTENED - PLATE - 6 MM < A <= 50 MM - 500 MPA <= R[M] <= 700 MPA |
| PREN 3512 : 200P2 | AEROSPACE SERIES - STEEL FE-PL1801 (100CR6) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - HARDENED AND TEMPERED - HOLLOW BARS FOR THE MANUFACTURER OF BEARINGS - 3,5 MM <= A <= 55 MM |
| PREN 3525 : 200P2 | AEROSPACE SERIES - STEEL FE-PL1505 (15CRMOV6) - AIR MELTED - HARDENED AND TEMPERED - PLATE - 6 MM < A <= 20 MM - 1080 MPA <= R[M] <= 1280 MPA |
| PREN 3678 : 200P1 | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - AIR MELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 200 MM - R[M] >= 930 MPA |
| PREN 2174 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2602 (X4NICRTIMOV26-15) - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - D[E] <= 100 MM - R[M] >= 850 MPA |
| PREN 4700-006 : 200P2 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 006: PRE-PRODUCTION AND PRODUCTION FORGINGS |
| PREN 4800-003 : 200P2 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 3: TUBE |
| 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 |
| PREN 4259 : 200P1 | AEROSPACE SERIES - METALLIC MATERIALS - DEFINITION OF GENERAL TERMS |
| PREN 4500-004 : 200P2 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 004: SPECIFIC RULES FOR TITANIUM AND TITANIUM ALLOYS |
| PREN 4291 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P8090- - FORGING STOCK |
| PREN 3879 : 200P2 | AEROSPACE SERIES - METALLIC MATERIALS - FILLER METAL FOR WELDING - TECHNICAL SPECIFICATION |
| PREN 4463 : 200P1 | |
| PREN 4526 : 200P1 | AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - SHARP EDGE-NOTCH TENSILE TESTING FOR SHEET AND STRIP |
| PREN 3999 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024-T351 - SHEET AND STRIP WITH IMPROVED CHEMICAL MILLING CAPABILITY - 1,6 MM <= A <= 6 MM |
| PREN 4568 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY CO-PH4101 (COCR20W15NI) - VACUUM MELTED - SOLUTION TREATED - SHEET AND STRIP - A <= 6 MM |
| DIN EN 2813:2000-04 (Draft) | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6061-T6 - DRAWN TUBE FOR PRESSURE APPLICATIONS 0,6 MM <= A <= 12,5 MM |
| PREN 3997 : 200P3 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024- AL CU4MG1 - T3 - SHEET AND STRIP - 0,4 MM <= A <= 6 MM |
| PREN 4292 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-R39002 - FORGING STOCK |
| PREN 3981 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P8090-T62 - SHEET - 0,6 MM <= A <= 6 MM |
| PREN 4003 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2219 - T87 - SHEET AND STRIP - 0,5 MM <= A <= 6 MM |
| PREN 4102 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2219-T81 - CLAD SHEET AND STRIP - 0,5 MM <= A <= 6 MM |
| PREN 4464 : 200P1 | AEROSPACE SERIES - STEEL FE-PM1506 (X5CRNIMOAL13-8-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 150 MM - R[M] >= 1 200 MPA |
| PREN 4471 : 200P1 | AEROSPACE SERIES - STEEL FE-PM1505 (X1CRNIMOALTI12-9-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 150 MM - R[M] >= 1 300 MPA |
| PREN 4469 : 200P1 | |
| PREN 4214 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7010-T651 - PLATE - 6 MM < A <= 20 MM |
| PREN 4570 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA4901 (X12CRNICOMOW21-20) - SOLUTION TREATED - FORGINGS - D[E] <= 100 MM |
| PREN 4685 : 200P1 | AEROSPACE SERIES - TITANIUM TI10V2FE3AL - BARS - D < 110 MM - R[M] >= 1240 MPA |
| PREN 4616 : 200P1 | AEROSPACE SERIES - MAGNESIUM ALLOY MG-C18002 - T4 - CHILL CASTING |
| I.S. EN 2221:2017 | AEROSPACE SERIES - STEEL FE-PL31 - HARDENED AND TEMPERED - HOLLOW BARS - 3,5 MM <= A <= 55 MM |
| I.S. EN 3355:2012 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - EXTRUDED SECTION - D[E] <= 150 MM - 900 MPA <= R[M] <= 1160 MPA |
| I.S. EN 2402:2014 | AEROSPACE SERIES - HEAT RESISTING NICKEL BASE ALLOY NICR20CO3FE3 - ANNEALED - WIRE - D <= 10 MM |
| I.S. EN 3361:2007 | AEROSPACE SERIES - STEEL FE-PM1802 (X5CRNICU15-5) - CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - SHEET AND STRIP A <= 6 MM - 1070 MPA <= R[M] <= 1220 MPA |
| 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 |
| I.S. EN 3312:2012 | AEROSPACE SERIES - TITANIUM ALLOY TI-6AL-4V - ANNEALED - FORGINGS - D[E] <= 150 MM |
| I.S. EN 2543:2009 | AEROSPACE SERIES - STEEL FE-PL1502 (25CRMO4) - ANNEALED - SHEET AND STRIP - 0,3 MM <= A <= 2 MM - FOR PREVAILING TORQUE NUTS |
| UNI EN 3355 : 2013 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - EXTRUDED SECTION - D[E] <= 150 MM - 900 MPA <= R[M] <= 1160 MPA |
| NF EN 2209 : 2009 | AEROSPACE SERIES - STEEL FE-PL1502 (25CRMO4) - 900 MPA <= R[M] <= 1100 MPA - SHEETS, STRIPS AND PLATES - 0,5 MM <= A <= 20 MM |
| NF EN 2483 : 2012 | AEROSPACE SERIES - STEEL FE-PL2108 (35NICRMO16) - 1100 MPA < OR = R[M] < OR = 1300 MPA - FORGINGS - D[E] < OR = 100 MM |
| BS EN 2135:2017 | Aerospace series. Steel FE-PL61. Carburized, hardened and tempered. Bar. De ≤ 40 mm |
| I.S. EN 4700-007:2010 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 007: REMELTING STOCK |
| 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 |
| NF EN 2002-002 : 2006 | AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - PART 002: TENSILE TESTING AT ELEVATED TEMPERATURE |
| NF EN 4463 : 2008 | |
| UNI EN 2252 : 2013 | AEROSPACE SERIES - STEEL FE-PL1505 (15CRMOV6) - 1080 MPA <= R[M] <= 1250 MPA - FORGINGS - D[E] <= 100 MM |
| NF EN 2399 : 2008 | AEROSPACE SERIES - HEAT RESISTING STEEL FE-PA2601 (X4NICRTIMOV26-15) - R[M] >= 900 MPA - BARS FOR FORGED BOLTS - D <= 25 MM |
| NF EN 3330 : 2009 | AEROSPACE SERIES - STEEL FE-PL1503 (35CRMO4) - ANNEALED - BAR AND WIRE - D[E] <= 40 MM - FOR PREVAILING TORQUE NUTS |
| NF EN 2205 : 2009 | AEROSPACE SERIES - STEEL FE-PL1502 (25CRMO4) - 900 MPA <= R[M] <= 1100 MPA - BARS - D[E] <= 40 MM |
| NF EN 4700-007 : 2012 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 007: REMELTING STOCK |
| I.S. EN 3528:2013 | AEROSPACE SERIES - STEEL X2NICOMO18-8-5 (1.6359) - VACUUM INDUCTION MELTED AND VACUUM ARC REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BAR - A OR D <= 150 MM - 1750 MPA <= R[M] <= 2000 MPA |
| BS EN 4335:2002 | Aerospace series. Steel FE-WA2602 (X4NiCrTiMoV26-15). Filler metal for welding. Wire and rod |
| BS EN 2622:2001 | Aerospace Series. Circular tubes, for fluids in heat resisting alloys. Diameter 3,2 mm ≤ D ≤ 100 mm. Dimensions |
| BS EN 4202:2005 | Aerospace series. Aluminium alloy AL-P6082-T651. Plate. 6 mm < a ≤ 25 mm |
| BS EN 4382:2006 | Aerospace series. Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb). Solution treated. Seamless tubes. For hydraulic application. D ≤ 50 mm, a ≤ 3 mm |
| BS EN 4045:2001 | Aerospace series. Capillary tubes, seamless in heat resisting alloys. Diameter 0,6 mm ≤ D ≤ 2 mm. Dimensions |
| BS EN 3333:2005 | Aluminium alloy AL-P7475-T762. Sheet and strip. 0,6 mm ≤ a ≤ 6 mm |
| BS EN 3918:1998 | Nickel base alloy NI-B41201 (NiCr14Si5B3C). Filler metal for brazing. Tape |
| 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 |
| BS EN 3887:2001 | Aerospace series. Heat resisting alloy CO-WH4101 (CoCr20W15Ni). Filler metal for welding |
| BS EN 2086:2004 | Aerospace series. Aluminium alloy AL-P2618A-T851. Hand and die forgings. a ≤ 150 mm |
| BS EN 2089:2005 | Aluminium alloy AL-P2014A T6 or T62. Sheet and strip. 0,4 mm ≤ a ≤ 6 mm |
| BS EN 4100:2005 | Aerospace series. Aluminium alloy AL-P2219-T6 or T62. Sheet and strip. 0,5 mm ≤ a ≤ 6 mm |
| BS EN 4001:2007 | Aerospace series. Aluminium alloy AL-P2024-T351. Clad sheet and strip with improved chemical milling capability 1,6 mm ≤ a ≤ 6 mm |
| BS EN 3146:2001 | Aerospace series. Round bars, hot rolled in steel. Close tolerances. Diameter 6mm ≤ D ≤ 250mm. Dimensions |
| BS EN 3347:2005 | Aerospace series. Aluminim alloy AL-P2024. T8511. Extruded bar and section. a or D ≤ 150 mm with peripheral coarse grain control |
| BS EN 3931:1998 | Nickel base alloy NI-B31001 (NiCr19Si10). Filler metal for brazing. Tape |
| BS EN 4383:2006 | Aerospace series. Heat resisting alloy NI-CH2601 (NiCr19Fe19Nb5Mo3). Non heat treated. Remelting stock |
| BS EN 3958:2001 | Aerospace series. Silver base alloy AG-B14001 (AgCu42Ni2). Filler metal for brazing. Rolled foil |
| BS EN 2486:2005 | Aerospace series. Aluminium alloy AL-P2618A. Forging stock |
| 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 |
| BS EN 4331:2002 | Aerospace series. Steel FE-WL1804 (25CrMnMo4-2-2). Filler metal for welding. Wire and rod |
| BS EN 4105:1998 | Nickel base alloy NI-B40002 (NiSi4B2). Filler metal for brazing. Tape |
| BS EN 3939:2001 | Aerospace series. Nickel base alloy NI-B46001 (NiCo20Si5B3). Filler metal for brazing. Powder or paste |
| BS EN 4616:2005 | Aerospace series. Magnesium alloy MG-C18002. T4. Chill casting |
| BS EN 3671:2007 | Aerospace series. Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb). Non heat treated. Forging stock. a or D ≤ 250 mm |
| BS EN 4002:2007 | Aerospace series. Aluminium alloy AL-P2219-T81. Sheet and strip 0,5 mm ≤ a ≤ 6 mm |
| BS EN 2732:2005 | Magnesium alloy MG-C46001-T6. Chill casting |
| BS EN 4060:2001 | Aerospace series. Filler rods and filler wires for welding in heat resisting alloys. Diameter 0,5 mm ≤ D ≤ 5,0 mm. Dimensions |
| BS EN 3959:2001 | Aerospace series. Cobalt base alloy CO-B41601 (CoCr19Ni17Si8W4). Filler metal for brazing. Powder or paste |
| BS EN 2003-010:2007 | Aerospace series. Titanium and titanium alloys. Test methods Sampling for determination of hydrogen content |
| BS EN 4006:2007 | Aerospace series. Aluminium alloy AL-P6082-T4 or T42. Sheet and strip 0,4 mm ≤ a ≤ 6 mm |
| BS EN 3668:2006 | Aerospace series. Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9). Non heat treated. Forging stock. a or D ≤ 250 mm |
| BS EN 4373:2007 | Aerospace series. Heat resisting alloy NI-PD9001 (NiCu31). Annealed, seamless tube D ? 75 mm, a ? 3 mm |
| BS EN 3872:2005 | Aerospace series. Aluminium alloy AL-R39002-H112. Die forgings. a ≤ 200mm |
| 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 |
| BS EN 4283:2005 | Aerospace series. Aluminium alloy AL-P2219-T87. Plate. 6 mm < a ≤ 40 mm |
| BS EN 3342:2005 | Aerospace series. Aluminim alloy AL-P6061. T4 or T42. Drawn or extruded bar and section. a or D ≤ 150 mm |
| BS EN 2045:2001 | Aerospace series. Square bars, drawn, in aluminium and aluminium alloys. Tolerance class h 11. Thickness 6 mm ≤ a ≤ 50 mm. Dimensions |
| BS EN 3964:2001 | Aerospace series. Copper CU-BU9001. Filler metal for brazing. Wire |
| BS EN 4103:2001 | Aerospace series. Nickel base alloy NI-B40002 (NiSi4B2). Filler metal for brazing. Borided foil |
| BS EN 2344:2001 | Aerospace series. Round bars, machined in heat resisting alloys. Diameter 10 mm < D < 180 mm. Dimensions |
| BS EN 4344:2001 | Aerospace series. Steel FE-WM1002 (X13Cr13). Filler metal for welding. Wire and rod |
| BS EN 2072:2005 | Aerospace series. Aluminium AL-P1050A. H14. Sheet and strip. 0,4 mm ≤ a ≤ 6 mm |
| BS EN 3955:2001 | Aerospace series. Silver base alloy AG-B12401 (AgCu40Zn5Ni). Filler metal for brazing. Rolled foil |
| BS EN 2066:2002 | Aerospace series. Extruded section in aluminium alloys. General tolerances |
| BS EN 4250:2001 | Aerospace series. Nickel base alloys NI-B41001 (NiCr19Si7B). Filler metal for brazing. Amorphous foil |
| BS EN 2633:2015 | Aerospace series. Aluminium alloy AL-P2024. AlCu4Mg1. T3511. Extruded bars and sections. 1,2 mm ≤ De ≤ 160 mm with peripheral coarse grain control |
| BS EN 2092:2005 | Aerospace series. Aluminium alloy AL-P7075-T6 or T62. Clad sheet and strip. 0,4 mm ≤a ≤6 mm |
| BS EN 4324:2002 | Aerospace series. Aluminium alloy AL-W42201. Filler metal for welding. Rod |
| BS EN 3552:2005 | Aerospace series. Aluminium alloy AL-P2618A-T6 or T62. Clad sheet and strip. 0,4 mm ≤ a ≤ 6 mm |
| BS EN 4328:2002 | Aerospace series. Steel FE-WM1601 (X18CrWNi13-3-2). Filler metal for welding. Wire and rod |
| I.S. EN 2092:2005 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7075 - T6 OR T62 - CLAD SHEET AND STRIP - 0,4 MM <= A <= 6 MM |
| I.S. EN 2633:2015 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024 - ALCU4MG1 - T3511 - EXTRUDED BARS AND SECTIONS - 1,2 MM <= D[E] <= 160 MM WITH PERIPHERAL COARSE GRAIN CONTROL |
| ONORM EN 2573 : 2007 | AEROSPACE SERIES - STEEL FE-PA3601 (X6CRNITI18-10) - SOFTENED - R[M] <= 780 MPA - WIRE - 0,25 MM <= D[E] <= 3 MM |
| I.S. 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 <= R[M] <= 1220 MPA |
| ONORM EN 3364 : 2007 | AEROSPACE SERIES - STEEL FE-PM1802 (X5CRNICU15-5) - CONSUMABLE ELECTRODE REMELTED, SOFTENED, FORGING STOCK A OR D <= 300 MM |
| NF EN 4471 : 2008 | AEROSPACE SERIES - STEEL FE-PM1505 (X1CRNIMOALTI12-9-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 150 MM - R[M] >= 1300 MPA |
| UNI EN 2213 : 2013 | AEROSPACE SERIES - STEEL FE-PL1505 (15CRMOV6) - AIR MELTED - HARDENED AND TEMPERED - BARS - D[E] <= 16 MM - 980 MPA <= R[M] <= 1180 MPA |
| 06/30160262 DC : 0 | BS EN 4642 - AEROSPACE SERIES - STEEL FE-PM 3504 (X4CRNIMO16-5-1) - AIR MELTED - HARD END AND TEMPERED - SHEET - 0.6 MM |
| 08/30181052 DC : DRAFT APR 2008 | |
| 01/716446 DC : DRAFT JAN 2002 | PREN 2089 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2014A - T6 OR T62 - SHEET AND STRIP - 0,4 MM < A < 6 MM |
| I.S. EN 2030:2013 | AEROSPACE SERIES - STEEL X105CRMO17 (1.3544) - HARDENED AND TEMPERED - BARS - D[E] <= 150 MM |
| I.S. EN 4526:2013 | AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - SHARP EDGE-NOTCH TENSILE TESTING FOR SHEET AND STRIP |
| BS EN 3351:2012 | Aerospace series. Titanium alloy Ti-4Al-4Mo-2Sn. Solution treated and aged. Forgings. De ≤ 150 mm |
| BS EN 3162:2007 | Aerospace series. Steel FE-PM3801 (X5CrNiCu17-4). Air melted, solution treated and precipitation treated, sheet and strip a ≤ 6 mm, Rm ≥ 930 MPa |
| NF EN 4472 : 2008 | AEROSPACE SERIES - STEEL FE-PM1505 (X1CRNIMOALTI12-9-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 150 MM - R[M] >= 1400 MPA |
| UNI EN 4263 : 2014 | Aerospace series - Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20) - As forged - Forging stock - a or D ≤ 200 mm - 690 MPa ≤ Rm ≤ 960 MPa |
| NF EN 3160 : 2008 | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - AIR MELTED, SOLUTION TREATED AND PRECIPITATION TREATED, BAR A OR D <= 200 MM, R[M] >= 1310 MPA |
| BS EN 3364:2007 | Aerospace series. Steel FE-PM1802 (X5CrNiCu15-5). Consumable electrode remelted, softened, forging stock a or D ≤ 300 mm |
| DIN EN 2772:2000-02 (Draft) | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4), AIR MELTED, SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS, A OR D = 200 MM, R(INDEX)M = 965 MPA |
| BS EN 2439:2009 | Aerospace series. Steel FE-PL2102 (34NiCr6). 900 MPa ≤ Rm ≤ 1100 MPa. Forgings. De ≤ 40 mm |
| BS EN 4470:2007 | Aerospace series. Steel FE-PM1505 (X1CrNiMoAITi12-9-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Forgings. a or D ≤ 150 mm. Rm ≤ 1200 MPa |
| 01/710778 DC : 0 | PREN 3879 - AEROSPACE SERIES - METALLIC MATERIALS - FILLER METAL FOR WELDING - TECHNICAL SPECIFICATION |
| BS EN 3488:2007 | Aerospace series. Steel FE-PA3601 (X6CrNiTi18-10). Air melted. Softened. Sheet and strip. a ≤ 6 mm. 500 MPa ≤ Rm ≤ 700 MPa |
| UNI EN 4656 : 2011 | AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BARS - A OR D <= 200 MM - R[M] >= 1520 MPA |
| BS EN 2043:2013 | Aerospace series. Metallic materials. General requirements for semi-finished product qualification (excluding forgings and castings) |
| NF EN 3361 : 2008 | AEROSPACE SERIES - STEEL FE-PM1802 (X5CRNICU15-5) - CONSUMABLE ELECTRODE REMELTED, SOLUTION TREATED AND PRECIPITATION TREATED, SHEET AND STRIP A <= 6 MM, 1070 MPA <= R[M] <= 1220 MPA |
| 96/716609 DC : 0 | PREN 4374 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1301 (NICR19CO18MO4TI3A13) SOLUTION AND PRECIPITATION TREATED - BARS AND SECTIONS A OR D <= 200 MM |
| 99/710245 DC : 0 | PREN 2002-16 - AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - NON-DESTRUCTIVE TESTING - PART 16: PENETRANT TESTING |
| I.S. EN 3120:2012 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64003 - COLD WORKED AND STRESS RELIEVED - SEAMLESS TUBE FOR PRESSURE SYSTEMS - 4 MM <= D <= 51 MM - 690 MPA <= R[M] <= 1030 MPA |
| 11/30248021 DC : 0 | AEROSPACE SERIES - COPPER ALLOY CUBE 1.9 - SOLUTION TREATED, COLD WORKED TO [1/2] HARD AND PRECIPITATION TREATED - BAR - 5 MM <= A OR D <= 190 MM - R[M] >= 1220 MPA |
| BS EN 3451:2017 | Aerospace series. Titanium TI-P99002. Not heat treated. Grade 2 forging stock, for annealed forgings - a or D ≤ 300 mm |
| NF EN 4683 : 2012 | AEROSPACE SERIES - STEEL FE-WM 3504 (X4CRNIMO16-5-1) - AIR MELTED - FILLER METAL FOR WELDING - WIRE AND ROD |
| BS EN 3312:2012 | Aerospace series. Titanium alloy Ti-6Al-4V. Annealed. Forgings De ≤ 150 mm |
| 99/710247 DC : DRAFT JUN 1999 | PREN 2003-2 - AEROSPACE SERIES - STEELS - TEST METHODS - PART 2: IZOD IMPACT TEST |
| 09/30207942 DC : 0 | BS EN 2252 - AEROSPACE SERIES - STEEL FE-PL2108 (36NICRMO16) - 1100 MPA <= R[M] <= 1300 MPA - FORGINGS - D[E] <= 100 MM |
| 96/716615 DC : 0 | PREN 4380 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH3601 (NICR22MO9NB) SOLUTION TREATED - BAR AND SECTION A OR D <= 200 MM |
| 09/30205256 DC : 0 | BS EN 2483 - AEROSPACE SERIES - STEEL FE-PL2108 (36NICRMO16) - 1100 MPA <= R[M] <= 1300 MPA - FORGINGS - D[E] <= 100 MM |
| BS EN 4657:2010 | Aerospace series. Steel FE-PM1507 (X1CrNiMoAlTi12-11-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Bars. a or D ≤ 200 mm. Rm ≥ 1650 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 3464:2012 | Aerospace series. Titanium alloy (Ti-6Al-4V). Annealed. Plate. 6 mm < a ≤ 100 mm |
| 09/30210361 DC : 0 | BS EN 3456 EDP3 - AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - SHEET AND STRIP, HOT ROLLED - A <= 6 MM |
| DIN EN 2775:2000-02 (Draft) | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4), CONSUMABLE ELECTRODE REMELTED, SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS, A OR D = 200 MM, R(INDEX)M = 1310 MPA |
| 96/700091 DC : 0 | PREN 4500-6 - AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 6: SPECIFIC RULES FOR FILLER METALS FOR BRAZING |
| BS EN 4656:2010 | Aerospace series. Steel FE-PM1507 (X1CrNiMoAlTi12-11-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Bars. a or D ≤ 200 mm. Rm ≥ 1520 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 |
| NF EN 3311 : 2010 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AI-4V) - ANNEALED - BAR FOR MACHINING - D < 110 MM |
| EN 4700-002:2016 | Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 002: Bar and section |
| NF EN 4470 : 2008 | AEROSPACE SERIES - STEEL FE-PM1505 (X1CRNIMOALTI12-9-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 150 MM - R[M] >= 1200 MPA |
| NF EN 3469 : 2010 | AEROSPACE SERIES - STEEL FE-PM1802 (X5CRNICU15-5) - CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D < OR = 200 MM - R[M] > OR = 1310 MPA |
| NF EN 2467 : 2008 | AEROSPACE SERIES - STEEL FE-PA3901 (X2CRNI18-9) - AIR MELTED - SOFTENED - PLATE, SHEET AND STRIP - 0,4 MM <= A <= 20 MM - 520 MPA <= R[M] <= 670 MPA |
| 10/30227742 DC : 0 | BS EN 2704 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024 - T3511 - DRAWN BAR - D[E] <= 75 MM |
| 01/716451 DC : DRAFT JAN 2002 | PREN 2511 - AEROSPACE SERIES - ALUMINIUM ALLOY - AL-P7075-T7351 - PLATE - 6 MM < A < 100 MM |
| NF EN 2115 : 2009 | AEROSPACE SERIES - ALUMINIUM ALLOY 2117-T42 - WIRE FOR SOLID RIVETS - D <= 10 MM |
| 96/716572 DC : 0 | PREN 2391 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6061-T4 - STRUCTURAL TUBE 0,6 MM <= A <= 12,5 MM |
| 95/715394 DC : 0 | PREN 4261-3 - AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF TEST METHOD STANDARDS - PART 3: SPECIFIC REQUIREMENTS FOR NON-DESTRUCTIVE TEST METHOD STANDARD |
| I.S. EN 4672:2011 | AEROSPACE SERIES - STEEL FE-PM1504 (X1CRNIMOALTI12-10-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOFTENED - FORGING STOCK - A OR D <= 300 MM |
| NF EN 2438 : 2009 | AEROSPACE SERIES - STEEL FE-PL2102 (35NICR6) - 900 MPA <= R[M] <= 1100 MPA - BARS - D[E] <= 40 MM |
| 95/715392 DC : 0 | PREN 4261-1 - AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF TEST METHOD STANDARDS - PART 1: GENERAL REQUIREMENTS |
| BS EN 4685:2011 | Aerospace series. Titanium Ti10V2Fe3Al. Bars. D < 110 mm. Rm ≥ 1240 MPa |
| 96/716573 DC : 0 | PREN 2392 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6061-T6 - STRUCTURAL TUBE 0,6 MM <= A <= 12,5 MM |
| 96/700090 DC : 0 | PREN 4500-5 - AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 5: SPECIFIC RULES FOR STEELS |
| UNI EN 2402 : 2014 | AEROSPACE SERIES - HEAT RESISTING NICKEL BASE ALLOY NICR20CO3FE3 - ANNEALED - WIRE - D <= 10 MM |
| NF EN 4464 : 2008 | AEROSPACE SERIES - STEEL FE-PM1506 (X5CRNIMOAL13-8-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 150 MM - R[M] >= 1200 MPA |
| NF EN 2116 : 2009 | AEROSPACE SERIES - ALUMINIUM ALLOY 2017A-T42 - WIRE FOR SOLID RIVETS - D <= 10 MM |
| 96/716571 DC : 0 | PREN 2388 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024-T351 - STRUCTURAL TUBE 0,6 MM <= A <= 12,5 MM |
| NF 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 |
| 08/30181155 DC : DRAFT APR 2008 | BS EN 4672 - AEROSPACE SERIES - STEEL FE-PM(X1CRNIMOALTI12-10-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOFTENED - FORGING STOCK - A OR D <= 300 MM |
| NF EN 3329 : 2009 | AEROSPACE SERIES - STEEL FE-PL1503 (35CRMO4) - ANNEALED - SHEET AND STRIP - 0,3 MM <= A <= 2 MM - FOR PREVAILING TORQUE NUTS |
| 08/30181037 DC : DRAFT APR 2008 | |
| UNI EN 4800-004 : 2011 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 004: WIRE |
| NF EN 4465 : 2008 | AEROSPACE SERIES - STEEL FE-PM1506 (X5CRNIMOAL13-8-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 150 MM - R[M] >= 1300 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 |
| UNI EN 4500-001 : 2014 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 001: GENERAL RULES |
| NF EN 4700-005 : 2012 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 005: FORGING STOCK |
| 97/719242 DC : DRAFT NOV 1997 | PREN 2682 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7010-T7452 - HAND AND DIE FORGINGS - A <= 150 MM |
| NF EN 2573 : 2008 | AEROSPACE SERIES - STEEL FE-PA3601 (X6CRNITI18-10) - SOFTENED - R[M] <= 780 MPA - WIRE - 0,25 MM <= D[E] <= 3 MM |
| 06/30146136 DC : 0 | EN 2573 - AEROSPACE SERIES - STEEL FE-PA3601 (X6CRNITI18.10) - RM - 780 MPA 0,25 - DE - 3 MM |
| 07/19990771 DC : 0 | BS EN 2857-001 - AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS FOR FERROMAGNETIC MATERIALS - NON-DESTRUCTIVE TESTING - MAGNETIC PARTICLE INSPECTION - PART 1: MAGNETIC PARTICLE TESTING - GENERAL REQUIREMENTS |
| BS EN 2543:2009 | Aerospace series. Steel FE-PL1502 (25CrMo4). Annealed. Sheet and strip. 0,3 mm ≤ a ≤ 2 mm. For prevailing torque nuts |
| UNI EN 4631 : 2013 | 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 4721:2014 | AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED AND ELECTROSLAG REMELTED (ESR) - HARDENED AND TEMPERED - BAR - D[E] <= 200 MM - 900 MPA <= R[M] <= 1050 MPA |
| 16/30337543 DC : 0 | BS EN 8.4577 - AEROSPACE SERIES - X5CRNICU15-5 (1.4545) - CONSUMABLE ELECTRODE REMELTED (ESR OR VAR) - SOLUTION TREATED AND PRECIPITATION TREATED (H1025) - BAR FOR MACHINING - A OR D <= 250 MM - 1070 MPA <= R[M] <= 1200 MPA - PREMIUM QUALITY (PQ) |
| 01/716455 DC : DRAFT JAN 2002 | PREN 2696 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7075 - T6 OR T62 - SHEET AND STRIP - 0,4 MM < A < 6 MM |
| 98/712167 DC : DRAFT JULY 1998 | PREN 2803 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7475-T761 - CLAD SHEET AND STRIP 1 MM <= A <= 6 MM |
| 09/30201382 DC : 0 | BS EN 4685 - AEROSPACE SERIES - TITANIUM TI10V2FE3AL - BARS - D < 110 MM - R[M] >= 1240 MPA |
| 97/718304 DC : DRAFT OCT 1997 | PREN 2816 - AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - CONSUMABLE ELECTRODE REMELTED SOLUTION TREATED AND PRECIPATION HARDENED - FORGINGS A OR D <= 200 MM - RM => 965 MPA |
| 11/30248020 DC : 0 | AEROSPACE SERIES - COPPER ALLOY CUBE 1.9 - SOLUTION TREATED, COLD WORKED TO [1/4] HARD AND PRECIPITATION TREATED - BAR - 5 MM <= A OR D <= 190 MM - R[M] >= 1100 MPA |
| UNI EN 4800-005 : 2011 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 005: FORGING STOCK |
| 96/716611 DC : 0 | PREN 4376 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2601 (NICR19FE19NB5MO3) SOLUTION AND PRECIPITATION TREATED - BARS AND SECTIONS A OR D <= 200 MM |
| 96/716613 DC : 0 | PREN 4378 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2601 (NICR19FE19NB5MO3) SOLUTION AND PRECIPITATION TREATED - WIRE FOR RIVETS D <= 1,6 MM |
| PREN 2202 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1303 (NICO20CR20MO5TI2AL) - SOLUTION TREATED - SEAMLESS TUBE - D <= 50 MM, A <= 3 MM |
| PREN 2199 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1303 (NICO20CR20MO5TI2AL) - SOLUTION TREATED AND PRECIPITATION TREATED - BAR AND SECTION - D[E] <= 200 MM |
| PREN 2233 : 200P2 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-CD1701 (NICO15CR10AL6TI5MO3) - VACUUM MELTED - NON HEAT TREATED - PRECISION CASTING - A OR D <= 50 MM |
| I.S. EN 4800-006:2010 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 006: PRE-PRODUCTION AND PRODUCTION FORGINGS |
| I.S. EN 2818:2009 | AEROSPACE SERIES - STEEL FE-PM1802 (X5CRNICU15-5) - CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 200 MM - R[M] >= 1070 MPA |
| 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 |
| I.S. EN 4800-005:2010 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 005: FORGING STOCK |
| I.S. EN 2032-001:2014 | AEROSPACE SERIES - METALLIC MATERIALS - PART 001: CONVENTIONAL DESIGNATION |
| 96/716587 DC : 0 | PREN 2199 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1303 (NICO20CR20MO5TI2AL) SOLUTION AND PRECIPITATION TREATED - BAR AND SECTION A OR D <= 200 MM |
| 96/716610 DC : 0 | PREN 4375 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1301 (NICR19CO18MO4TI3A13) AS WROUGHT FORGING STOCK A OR D <= 250 MM |
| 01/716043 DC : 0 | PREN 4800-5 - AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 5: FORGING STOCK |
| 97/719258 DC : DRAFT NOV 1997 | PREN 4313 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6013-T6 - SHEET AND STRIP - 0,5 MM <= A <= 6 MM |
| PREN 4569 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY CO-PH4101 (COCR20W15NI) - VACUUM MELTED - SOLUTION TREATED - WIRE - D <= 4 MM |
| PREN 4523 : 200P1 | AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - COMPRESSION TESTING |
| PREN 4566 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY CO-PH4101 (COCR20W15NI) - VACUUM MELTED - SOLUTION TREATED - FORGINGS - D[E] <= 100 MM |
| PREN 4575 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA4901 (X12CRNICOMOW21-20) - SOLUTION TREATED AND DESCALED - SHEET AND PLATE - 3 MM < A <= 50 MM |
| PREN 2959 : 200P2 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1302 (NICR20CO13MO4TI3AL) - SOLUTION TREATED AND COLD WORKED - BAR FOR FORGED FASTENERS - 3 MM <= D <= 30 MM |
| NF EN 4800-003 : 2012 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 003: TUBE |
| PREN 3120 : 200P3 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64003 - COLD WORKED AND STRESS RELIEVED - SEAMLESS TUBE FOR PRESSURE SYSTEMS - 4 MM <= D <= 51 MM - 690 MPA <= R[M] <= 1030 MPA |
| NF EN 4469 : 2008 | |
| PREN 2226 : 200P1 | AEROSPACE SERIES - STEEL FE-PM 3501 (X105CRMO17) - HARDENED AND TEMPERED - HAND AND DIE FORGINGS D[E] <= 150 MM |
| PREN 2467 : 200P1 | AEROSPACE SERIES - STEEL FE-PA3901 (X2CRNI18-9) - AIR MELTED - SOFTENED - PLATE, SHEET AND STRIP - 0,4 MM <= A <= 20 MM - 520 MPA <= R[M] <= 670 MPA |
| PREN 3336 : 200P3 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7150-T651 - PLATE - 6 MM < A <= 40 MM |
| PREN 2419 : 200P3 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024-T351 - PLATE - 6 MM < A <= 80 MM |
| PREN 2918 : 200P2 | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 200 MM - R[M] >= 1 070 MPA |
| PREN 3115 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY 7050- T73 WIRE FOR SOLID RIVETS D <= 10 MM |
| PREN 2538 : 200P3 | AEROSPACE SERIES - STEEL FE-PM 3801 (X5CRNICU17-4) - AIR MELTED - SOLUTION TREATED AND PRECIPITATION TREATED - SHEET AND STRIP - A <= 6 MM - R[M] >= 1310 MPA |
| PREN 2403 : 200P1 | AEROSPACE SERIES - HEAT RESISTING NICKEL BASE ALLOY NI-CH2601 (NICR19FE19NB5MO3) - VACUUM MELTED - SOLUTION TREATED AND PRECIPITATION TREATED - PRECISION CASTING - A OR D <= 50 MM |
| PREN 2422 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2124-T351 - PLATE - 25 MM < A <= 120 MM |
| PREN 3526 : 200P2 | AEROSPACE SERIES - STEEL FE-PL1505 (15CRMOV6) - AIR MELTED - HARDENED AND TEMPERED - SHEET AND STRIP - 0,5 MM <= A <= 6 MM - 980 MPA <= R[M] <= 1180 MPA |
| PREN 3357 : 200P2 | AEROSPACE SERIES - STEEL FE-PM1503 (X3CRNIMOAL 13-8-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BAR FOR MACHINING - A OR D <= 150 MM - 1 200 MPA <= R[M] <= 1 400 MPA |
| I.S. EN 4384:2007 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-CH1303 (NICO20CR20MO5TI2AL) - NON HEAT TREATED - REMELTING STOCK |
| PREN 3338 : 200P3 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7050-T74511 - EXTRUDED BAR AND SECTION - A OR D <= 150 MM - WITH PERIPHERAL COARSE GRAIN CONTROL |
| PREN 3347 : 200P3 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024-T8511 - EXTRUDED BAR AND SECTION - A OR D <= 150 MM - WITH PERIPHERAL COARSE GRAIN CONTROL |
| PREN 3333 : 200P3 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7475-T762 - SHEET AND STRIP - 0,6 MM <= A <= 6 MM |
| PREN 3552 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2618A - T6 OR T62 - CLAD SHEET AND STRIP - 0,4 MM <= A <= 6 MM |
| PREN 3341 : 200P3 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6061-T4 OR T42 - SHEET AND STRIP - 0,4 MM <= A <= 6 MM |
| PREN 3358 : 200P3 | |
| I.S. EN 2252:2012 | AEROSPACE SERIES - STEEL FE-PL1505 (15CRMOV6) - 1080 MPA <= R[M] <= 1250 MPA - FORGINGS - D[E] <= 100 MM |
| PREN 3508 : 200P2 | |
| PREN 3529 : 200P2 | 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 4376:2016 | AEROSPACE SERIES - HEAT RESISTING ALLOY NICR19FE19NB5MO3 (2.4668) SOLUTION TREATED AND PRECIPITATION TREATED - BAR AND SECTION, D[E] <= 200 MM |
| PREN 2047 : 200P1 | AEROSPACE SERIES - BEADED L-SECTION EXTRUDED, IN ALUMINIUM ALLOYS - DIMENSIONS |
| PREN 4671 : 200P1 | AEROSPACE SERIES - STEEL FE-PM1506 (X1CRNIMOALTI12-10-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION REMELTED - FORGINGS - A OR D <= 200 MM - R[M] >= 1400 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 |
| PREN 4293 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7175-T73511 - EXTRUDED BAR AND SECTION - A OR D <= 150 MM |
| PREN 4725 : DRAFT 2013 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024- AL CU4MG1 - T351 - PLATE - 6 MM < A <= 150 MM |
| PREN 4347 : 200P1 | AEROSPACE SERIES - STEEL FE-PM1506 (X3CRNIMOAL13-8-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOFTENED - FORGING STOCK - A OR D <= 300 MM |
| PREN 4461 : 200P1 | |
| PREN 4511 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2301 (NICR22FEMO) - SOLUTION TREATED AND COLD WORKED - WIRE FOR RIVETS - 1,6 MM <= D <= 10 MM |
| PREN 4525 : 200P1 | AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM ALLOYS - TEST METHODS - SHEAR TESTING |
| PREN 4567 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY CO-PH4101 (COCR20W15NI) - VACUUM MELTED - SOLUTION TREATED - BAR AND SECTION - A OR D <= 100 MM |
| PREN 4571 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA4901 (X12CRNICOMOW21-20) - SOLUTION TREATED - BAR AND SECTION - D[E] <= 100 MM |
| PREN 4215 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7175-T651 - PLATE - 6 MM < A <= 80 MM |
| I.S. EN 2278:2014 | AEROSPACE SERIES - STEEL X12CRNIMOV12-3 (1.4933) - 900 MPA <= R[M] <= 1100 MPA - BARS - D[E] <= 150 MM |
| I.S. EN 4372:2009 | AEROSPACE SERIES - HEAT RESISTING NICKEL ALLOY WITH COPPER NI-PD9001 (NICU31) - WIRE FOR SOLID RIVETS - D <= 10 MM |
| I.S. EN 4657:2010 | 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 |
| UNI EN 4657 : 2011 | AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BARS - A OR D <= 200 MM - R[M] >= 1650 MPA |
| NF EN 2439 : 2009 | AEROSPACE SERIES - STEEL FE-PL2102 (35NICR6) - 900 MPA <= R[M] <= 1100 MPA - FORGINGS - D[E] <= 40 MM |
| I.S. EN 3464:2012 | AEROSPACE SERIES - TITANIUM ALLOY TI-6AL-4V - ANNEALED - PLATE - 6 MM < A <= 100 MM |
| I.S. EN 2033:2017 | AEROSPACE SERIES - STRIPS, COLD ROLLED IN STEEL, THICKNESS 0,1 MM <= A <= 2,5 MM - DIMENSIONS |
| I.S. EN 4675:2011 | AEROSPACE SERIES - TITANIUM TI-P63002 (TI5AL5MO5V3CR0.4FE) - R[M] >= 1300 MPA - BARS - D[E] < 110 MM |
| I.S. EN 4800-002:2010 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 002: BAR AND SECTION |
| I.S. EN 2119:2017 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2601 (X6NICRTIMOV26-15) - SOLUTION TREATED AND PRECIPITATION TREATED -WIRES FOR RIVETS - 2 MM <= D <= 10 MM - R[M] >= 960 MPA |
| I.S. EN 3983:2013 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7050-T7651 - PLATE - 6 MM < A <= 160 MM |
| NF EN 4800-006 : 2012 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 006: PRE-PRODUCTION AND PRODUCTION FORGINGS |
| UNI EN 4526 : 2014 | AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - SHARP EDGE-NOTCH TENSILE TESTING FOR SHEET AND STRIP |
| I.S. EN 4629:2013 | AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED - SOFTENED - FORGING STOCK - D[E] <= 300 MM |
| I.S. EN 3469:2009 | AEROSPACE SERIES - STEEL FE-PM1802 (X5CRNICU15-5) - CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 200 MM - R[M] >= 1310 MPA |
| I.S. EN 4683:2011 | AEROSPACE SERIES - STEEL FE-WM 3504 (X4CRNIMO16-5-1) - AIR MELTED - FILLER METAL FOR WELDING - WIRE AND ROD |
| NF EN 4800-002 : 2012 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 002: BAR AND SECTION |
| I.S. EN 4800-004:2010 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 004: WIRE |
| UNI EN 4700-007 : 2011 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 007: REMELTING STOCK |
| NF EN 4700-002 : 2012 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 002: BAR AND SECTION |
| I.S. 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 <= 150 MM - 1750 MPA <= R[M] <= 2000 MPA |
| EN 3875:2017 | Aerospace series - Metallic materials, Filler metal for brazing - Technical specification |
| I.S. EN 4098:2007 | AEROSPACE SERIES - STEEL FE-PL1507 (40CRMOV12) - REMELTED, HARDENED AND TEMPERED, FORGINGS D[E] <= 50 MM, 1250 MPA <= R[M] <= 1400 MPA |
| I.S. EN 4466:2007 | AEROSPACE SERIES - STEEL FE-PM1506 (X5CRNIMOAL13-8-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 150 MM - R[M] >= 1 400 MPA |
| 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 4202:2005 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6082 - T651 - PLATE - 6 MM < A <= 25 MM |
| 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 |
| I.S. EN 2002-001:2006 | AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - PART 1: TENSILE TESTING AT AMBIENT TEMPERATURE |
| I.S. EN 4464:2007 | AEROSPACE SERIES - STEEL FE-PM1506 (X5CRNIMOAL13-8-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 150 MM - R[M] >= 1 200 MPA |
| BS EN 3917:1998 | Nickel base alloy NI-B41201 (NiCr14Si5B3C). Filler metal for brazing. Powder or paste |
| BS EN 2085:2004 | Aerospace series. Aluminium alloy AL-P2618A-T6. Hand and die forgings. a ≤ 150 mm |
| BS EN 2617:2001 | Aerospace Series. Plates in titanium and titanium alloys. Thickness 6 mm < a ≤ 100 mm. Dimensions |
| BS EN 4333:2002 | Aerospace series. Steel FE-WA4902 (X5CrNiCoMoWMn21-20-20-3-3-2). Filler metal for welding. Wire and rod |
| BS EN 3892:2001 | Aerospace series. Titanium alloy TI-W64001. Filler metal for welding |
| BS EN 3926:2001 | Aerospace series. Nickel base alloy NI-B40001 (NiSi5B3). Filler metal for brazing. Borided foil |
| BS EN 3927:2001 | Aerospace series. Nickel base alloy NI-B40001 (NiSi5B3). Filler metal for brazing. Powder or paste |
| BS EN 3524:2007 | Aerospace series. Steel FE-PL1505 (15CrMoV6). Air melted. Hardened and tempered. Sheet and strip. 2 mm ≤ a ≤ 6 mm. 1080 MPa ≤ Rm ≤1280 MPa |
| BS EN 3883:2001 | Aerospace series. Heat resisting alloy NI-WH2301 (NiCr22Fe19Mo9Co2). Filler metal for welding |
| BS EN 2703:2005 | Aerospace series. Aluminium alloy AL-P2024-T4 or T42. Clad sheet and strip. 0,3 mm ≤ a ≤ 6 mm |
| BS EN 2422:2005 | Aluminium alloy AL-P2124-T351. Plate. 25 mm < a ≤ 120 mm |
| BS EN 4341:2001 | Aerospace series. Aluminium alloy AL-W46431. Filler metal for welding. Wire and rod |
| BS EN 2687:2004 | Aerospace series. Aluminium alloy AL-P7010-T7451. Plate. 6 mm < a ≤ 160 mm |
| BS EN 4342:2001 | Aerospace series. Titanium TI-W99001. Filler metal for welding. Wire and rod |
| BS EN 4203:2005 | Aerospace series. Aluminium alloy AL-P8090-T89. Sheet. 0,6 mm ≤ a ≤ 6 mm |
| BS EN 2681:2004 | Aerospace series. Aluminium alloy AL-P7010-T74. Hand and die forgings. a ≤ 150 mm |
| BS EN 3962:2001 | Aerospace series. Gold base alloy AU-B40001. Filler metal for brazing. Wire |
| BS EN 3882:2001 | Aerospace series. Heat resisting alloy NI-WH1801 (NiCr20Co18Ti3Al2). Filler wire for welding |
| BS EN 3339:2006 | Aerospace series. Aluminium alloy AL-P7010-T76. Die Forgings. a ≤ 200 mm |
| BS EN 3941:2001 | Aerospace series. Nickel base alloy NI-B41204 (NiCr13Si4B3). Filler metal for brazing. Amorphous foil |
| BS EN 3526:2007 | Aerospace series. Steel FE-PL1505 (15CrMoV6). Air melted. Hardened and tempered. Sheet and strip. 0,5 mm ≤ a ≤ 6 mm. 980 MPa ≤ Rm ≤ 1180 MPa |
| BS EN 3885:2001 | Aerospace series. Heat resisting alloy NI-WH3601 (NiCr22Mo9Nb4). Filler metal for welding |
| BS EN 3896:2002 | Aerospace series. Steel FE-WM1501 (X13CrNiMoCo12-3-2-2. Filler metal for welding |
| BS EN 4339:2001 | Aerospace series. Heat resisting alloy CO-WH4001 (CoCr29W9). Filler metal for welding. Wire and rod |
| BS EN 4326:2001 | Aerospace series. Heat resisting alloy CO-WH4102 (CoCr28W20Ni5V1). Filler metal for welding. Wire and rod |
| I.S. EN 2693:2005 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P5086 - H111 - SHEET AND STRIP - 0,3 MM <= A <= 6 MM |
| I.S. EN 2694:2005 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6061 - T6 OR T62 - SHEET AND STRIP - 0,4 MM <= A <= 6 MM |
| I.S. EN 2632:2005 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7075 - T73511 - EXTRUDED BAR AND SECTION - A OR D <= 150 MM WITH PERIPHERAL COARSE GRAIN CONTROL |
| I.S. EN 2072:2005 | AEROSPACE SERIES - ALUMINIUM AL-P1050A - H14 - SHEET AND STRIP - 0,4 MM <= A <= 6 MM |
| I.S. EN 2395:2005 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2014A - T4 OR T42 - SHEET AND STRIP 0.4 MM <= A <= 6 MM |
| I.S. EN 3997:2015 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024- AL CU4MG1 - T3 - SHEET AND STRIP - 0,4 MM <= A <= 6 MM |
| I.S. EN 2089:2005 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2014A - T6 OR T62 - SHEET AND STRIP - 0,4 MM <= A <= 6 MM |
| I.S. EN 2695:2005 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6081 - T6 - SHEET AND STRIP - 0,3 MM <= A <= 6 MM |
| I.S. EN 2696:2005 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7075 - T6 OR T62 - SHEET AND STRIP - 0,4 MM <= A <= 6 MM |
| I.S. EN 3338:2005 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7050 - T74511 - EXTRUDED BAR AND SECTION - A OR D <= 150 MM WITH PERIPHERAL COARSE GRAIN CONTROL |
| 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 |
| NF EN 4379 : 2008 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH3601 (NICR22MO9NB) - SOLUTION TREATED, FORGING D[E] <= 200 MM |
| BS EN 2252:2012 | Aerospace series. Steel FE-PL1505 (15CrMoV6). 1 080 MPa ≤ Rm ≤ 1 250 MPa. Forgings. De ≤ 100 mm |
| 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 |
| UNI EN 2030 : 2014 | AEROSPACE SERIES - STEEL X105CRMO17 (1.3544) - HARDENED AND TEMPERED - BARS - D[E] <= 150 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 2512:2014 | Aerospace series. Aluminium alloy AL-P7175. T7351. Plate. 6mm < a ≤ 100 mm |
| 01/716450 DC : DRAFT JAN 2002 | PREN 2422 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2124 - T351 - PLATE 25 MM < A < 120 MM |
| 97/719244 DC : DRAFT NOV 1997 | PREN 2686 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7010-T7451 - HAND FORGINGS - A <= 150 MM |
| DIN EN 2805:2000-04 (Draft) | Aerospace series - Aluminium alloy AL-P7475-T7651 - Plate, 6 mm < a <kleiner |
| BS EN 4672:2011 | Aerospace series. Steel FE-PM1504 (X1CrNiMoAlTi12-10-2). Vacuum induction melted and consumable electrode remelted. Softened. Forging stock. a or D ≤ 300 mm |
| 09/30207945 DC : 0 | BS EN 3310 - AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - NOT HEAT TREATED - FORGING STOCK, FOR ANNEALED FORGINGS - A OR D <= 360 MM |
| BS EN 4700-004:2010 | Aerospace series. Steel and heat resisting alloys. Wrought products. Technical specification Wire |
| 96/716601 DC : 0 | PREN 4317 - AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2601 (X6NICRTIMOV26-15) AS FORGED - FORGING STOCK A OR D <= 200 MM - R[M] => 900 MPA |
| I.S. EN 2704:2015 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024 - ALCU4MG1 - T3511 - DRAWN BAR - D[E] <= 75 MM |
| I.S. EN 2306:2017 | AEROSPACE SERIES - HEAT RESISTING - NICKEL BASE ALLOY NI-CR[20]CO[3]FE[3] - ANNEALED - BARS |
| BS EN 2483:2010 | Aerospace series. Steel FE-PL2108 (36NiCrMo16). 1100 MPa ≤ Rm ≤ 1300 MPa. Forgings. De ≤ 100 mm |
| 97/719247 DC : DRAFT NOV 1997 | PREN 4277 - AEROSPACE SERIES - ALUMINIUM AL-P7175-T73 - HAND AND DIE FORGINGS - A <= 125 MM |
| 09/30207946 DC : 0 | BS EN 3312 - AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - FORGINGS - D[E] <= 150 MM |
| NF EN 2543 : 2009 | AEROSPACE SERIES - STEEL FE-PL1502 (25CRMO4) - ANNEALED - SHEET AND STRIP - 0,3 MM <= A <= 2 MM - FOR PREVAILING TORQUE NUTS |
| BS EN 4675:2011 | Aerospace series. Titanium Ti-P63002 (Ti5Al5Mo5V3Cr0.4Fe). Rm ≥ 1 300 MPa. Bars. De < 110 mm |
| 96/717406 DC : 0 | PREN 2185 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2301 (NICR21FE18MO9) SOLUTION TREATED - SHEET, STRIP AND PLATE 0,2 MM <= A <= 10 MM |
| 07/19990769 DC : 0 | BS EN 2857-002 - AEROSPACE SERIES - METALLIC MATERIALS - TESTS FOR FERROMAGNETIC MATERIALS - NON-DESTRUCTIVE TESTING - MAGNETIC PARTICLE INSPECTION - PART 2: INSPECTION REQUIREMENTS |
| 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 |
| 08/30180761 DC : DRAFT APR 2008 | |
| 08/30181055 DC : DRAFT APR 2008 | |
| 08/30189750 DC : DRAFT SEP 2008 | BS EN 4675 - AEROSPACE SERIES - TITANIUM - TI 5AL 5MO 5V 3CR 0.4FE - 1300 MPA <= R[M] <= 1400 MPA - BARS - D[E] <= 110 MM |
| 10/30227751 DC : 0 | BS EN 3997 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024- AL CU4MG1 - T3 - SHEET AND STRIP - 0,4 MM <= A <= 6 MM |
| BS EN 4721:2014 | Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted and electroslag remelted (ESR). Hardened and tempered. Bar. De ≤ 200 mm. 900 MPa ≤ Rm ≤ 1 050 MPa |
| BS EN 3875:2017 | Aerospace series. Metallic materials, Filler metal for brazing. Technical specification |
| DIN EN 2773:2000-02 (Draft) | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4), CONSUMABLE ELECTRODE REMELTED, SOLUTION TREATED AND PRECIPITATION TREATED - SHEET AND STRIP, A = 6 MM, R(INDEX)M = 1310 MPA |
| NF EN 4800-005 : 2012 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 005: FORGING STOCK |
| 10/30227732 DC : 0 | BS EN 2419 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024- AL CU4MG1 - T351 - PLATE - 6 MM < A <= 150 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 |
| BS EN 4500-001:2012 | Aerospace series. Metallic materials. Rules for drafting and presentation of material standards General rules |
| 96/717407 DC : 0 | PREN 2187 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1301 (NICR19CO18MO4TI3A13) SOLUTION AND PRECIPITATION TREATED - FORGINGS D[E] <= 200 MM |
| 11/30248022 DC : 0 | AEROSPACE SERIES - COPPER ALLOY CUBE 1.9 - SHEET AND STRIP |
| 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 |
| UNI EN 4700-005 : 2011 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 005: FORGING STOCK |
| DIN EN 2774:2000-02 (Draft) | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4), CONSUMABLE ELECTRODE REMELTED, SOLUTION TREATED AND PRECIPITATION TREATED - BAR, A OR D = 200 MM, R(INDEX)M = 1310 MPA |
| BS EN 2446:2008 | Aerospace series. Steel FE-PL1503 (35CrMo4). 1100 MPa ≤ Rm ≤ 1300 MPa. Bars. De ≤ 25 mm |
| 11/30254398 DC : 0 | BS EN 4685 - AEROSPACE SERIES - TITANIUM TI10V2FE3AL - BARS - D < 110 MM - R[M] >= 1240 MPA |
| BS EN 2482:2010 | Aerospace series. Steel FE-PL2108 (36NiCrMo16). 1100 MPa ≤ Rm ≤ 1300 MPa. Bars. De ≤ 100 mm |
| 95/715395 DC : 0 | PREN 4261-4 - AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF TEST METHOD STANDARDS - PART 4: SPECIFIC REQUIREMENTS FOR SURFACE EXAMINATION METHOD STANDARD |
| I.S. EN 2448:2008 | AEROSPACE SERIES - STEEL FE-PL1503 (35CRMO4) - 900 MPA <= R[M] <= 1100 MPA - BARS - D[E] <= 40 MM |
| BS EN 2402:2014 | Aerospace series. Heat resisting nickel base alloy NiCr20Co3Fe3. Annealed. Wire. D ≤ 10 mm |
| 95/712874 DC : 0 | PREN 4500-1 - AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 1: GENERAL RULES |
| NF EN 2448 : 2009 | AEROSPACE SERIES - STEEL FE-PL1503 (35CRMO4) - 900 MPA <= R[M] <= 1100 MPA - BARS - D[E] <= 40 MM |
| UNI EN 3456 : 2013 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - SHEET AND STRIP, HOT ROLLED - A <= 6 MM |
| UNI EN 4382 : 2008 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH3601 (NICR22MO9NB) - SOLUTION TREATED - SEAMLESS TUBES - FOR HYDRAULIC APPLICATION - D <= 50 MM, A <= 3 MM |
| BS EN 4700-002:2016 | Aerospace series. Steel and heat resisting alloys. Wrought products. Technical specification Bar and section |
| 03/306584 DC : 0 | EN 4400-5 - AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM- AND MAGNESIUM-ALLOY PRODUCTS - TECHNICAL SPECIFICATION - PART 5: ALUMINIUM AND ALUMINIUM ALLOY RIVET WIRE |
| 95/715398 DC : 0 | PREN 4261-7 - AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF TEST METHOD STANDARDS - PART 7: SPECIFIC REQUIREMENTS FOR CORROSION AND STRESS-CORROSION TEST METHOD STANDARD |
| BS EN 3456:2012 | Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Sheet and strip, hot rolled. a ≤ 6 mm |
| 97/719240 DC : DRAFT NOV 1997 | PREN 2486 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2618A - FORGING STOCK |
| UNI EN 4683 : 2011 | AEROSPACE SERIES - STEEL FE-WM 3504 (X4CRNIMO16-5-1) - AIR MELTED - FILLLER METAL FOR WELDING - WIRE AND ROD |
| UNI EN 4700-004 : 2011 | Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 004: Wire |
| BS EN 4800-006:2010 | Aerospace series. Titanium and titanium alloys. Technical specification Pre-production and production forgings |
| 09/30210353 DC : 0 | BS EN 3464 EDP3 - AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - PLATE - 6 MM < A <= 100 MM |
| UNI EN 4500-004 : 2014 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 004: SPECIFIC RULES FOR TITANIUM AND TITANIUM ALLOYS |
| UNI EN 3813 : 2013 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - BAR AND WIRE FOR FORGED FASTENERS - DE <= 50 MM |
| BS EN 4800-005:2010 | Aerospace series. Titanium and titanium alloys. Technical specification Forging stock |
| NF EN 2542 : 2009 | AEROSPACE SERIES - STEEL FE-PL1502 (25CRMO4) - ANNEALED - BAR AND WIRE - D[E] <= 40 MM - FOR PREVAILING TORQUE NUTS |
| 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 |
| 96/716569 DC : 0 | PREN 2090 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024-T3 - CLAD SHEET AND STRIP 0,3 MM <= A <= 6 MM |
| 96/716617 DC : DRAFT DEC 1996 | PREN 4382 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH3601 (NICR22MO9NB) SOLUTION TREATED - SEAMLESS TUBES - FOR HYDRAULIC APPLICATION D <= 50 MM, A <= 3 MM |
| 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 |
| 97/718301 DC : DRAFT OCT 1997 | PREN 2773 - AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - CONSUMABLE ELECTRODE REMELTED SOLUTION TREATED AND PRECIPATION HARDENED SHEET AND STRIP A <= 6 MM - RM => 1310 MPA |
| 97/719254 DC : DRAFT NOV 1997 | PREN 4288 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7050 - FORGING STOCK |
| I.S. EN 4463:2007 | |
| BS EN 4720:2014 | Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted and electroslag remelted (ESR). Hardened and tempered. Bar. De ≤ 200 mm. 1 150 MPa ≤ Rm ≤ 1 300 MPa |
| BS EN 4384:2007 | Aerospace series. Heat resisting alloy NI-CH1303 (NiCo20Cr20Mo5Ti2Al). Non heat treated. Remelting stock |
| 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 |
| I.S. EN 2043:2013 | AEROSPACE SERIES - METALLIC MATERIALS - GENERAL REQUIREMENTS FOR SEMI-FINISHED PRODUCT QUALIFICATION (EXCLUDING FORGINGS AND CASTINGS) |
| 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 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 |
| BS EN 4628:2013 | Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Bar. De ≤ 200 mm. 1 150 MPa ≤ Rm ≤ 1 300 MPa |
| BS EN 2033:2017 | Aerospace series. Strips, cold rolled in steel, Thickness 0,1 mm ≤ a ≤ 2,5 mm. Dimensions |
| 01/716447 DC : DRAFT JAN 2002 | PREN 2090 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024 - T3 - CLAD SHEET AND STRIP - 0,3 MM < A < 6 MM |
| BS EN 3359:2007 | Aerospace series. Steel FE-PM1503 (X3CrNiMoAl13-8-2). Vacuum induction melted and consumable electrode remelted, softened, forging stock a or D ≤ 300 mm |
| BS EN 4800-004:2010 | Aerospace series. Titanium and titanium alloys. Technical specification Wire |
| 96/716602 DC : 0 | PREN 4318 - AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2601 (X6NICRTIMOV26-15) SOLUTION AND PRECIPITATION TREATED - BARS AND SECTIONS A OR D <= 100 MM - R[M] => 960 MPA |
| NF EN 3161 : 2008 | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - AIR MELTED, SOLUTION TREATED AND PRECIPITATION TREATED, BAR A OR D <= 200 MM, R[M] >= 930 MPA |
| BS EN 4655:2010 | Aerospace series. Steel FEPM1506 (X1CrNiMoAlTi12-10-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Bars. a or D ≤ 200 mm. Rm ≥ 1400 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 |
| BS EN 3480:2007 | Aerospace series. Steel FE-PA3601 (X6CrNiTi18-10). Air melted. Softened. Plate. 6 mm < a ≤ 50 mm. 500 MPa ≤ Rm ≤ 700 MPa |
| I.S. EN 3311:2009 | AEROSPACE SERIES - TITANIUM ALLOY TIP64001 (TI-6AL-4V) - ANNEALED - BAR FOR MACHINING - D < 110 MM |
| 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 |
| 97/717258 DC : DRAFT OCT 1997 | PREN 4095 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-CH1305 (NICR16CO10MO8AL4TI4) - VACUUM MELTED NOT HEAT TREATED PRECISION CASTINGS |
| UNI EN 4800-008 : 2011 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 008: PRE-PRODUCTION AND PRODUCTION CASTINGS |
| 96/716608 DC : 0 | PREN 4373 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PD9201 (NICU31) ANNEALED - SEAMLESS TUBE D <= 75 MM - 3 <= 3 MM |
| 01/716452 DC : DRAFT JAN 2002 | PREN 2693 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P5086 - H111 - SHEET AND STRIP - 0,3 MM < A < 6 MM |
| BS EN 4465:2007 | Aerospace series. Steel FE-PM1506 (X5CrNiMoAl13-8-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Forgings. a or D ≤ 150 mm. Rm ≥ 1300 MPa |
| BS EN 3115:2009 | Aerospace series. Aluminium alloy 7050-T73. Wire for solid rivets. D ≤ 10 mm |
| UNI EN 2483 : 2011 | AEROSPACE SERIES - STEEL FE-PL2108 (35NICRMO16) - 1100 MPA <= R[M] <= 1300 MPA - FORGINGS - D[E] <= 100 MM |
| UNI EN 4293 : 2014 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7175 - T73511 - EXTRUDED BAR AND SECTION - A OR D <= 150 MM |
| I.S. EN 2512:2014 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7175 - T7351 - PLATE - 6 MM < A <= 100 MM |
| I.S. EN 4500-004:2012 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 004: SPECIFIC RULES FOR TITANIUM AND TITANIUM ALLOYS |
| 12/30263035 DC : 0 | BS EN 4825 - AEROSPACE SERIES - STEEL X12CRNIMOV12-3 (1.4933) - AIR MELTED AND CONSUMABLE ELECTRODE REMELTED - HARDENED AND TEMPERED - BAR - D[E] <= 150 MM - 900 MPA <= R[M] <= 1100 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 |
| XP PREN 4346 : 1996 XP | AEROSPACE SERIES - STEEL FE-PM1505 (X1CRNIMOALTI12-9-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOFTENED - FORGING STOCK - A OR D =< 300 MM |
| BS EN 2226:2014 | Aerospace series. Steel X105CrMo17 (1.4125). Hardened and tempered. Hand and die forgings. De ≤ 150 mm |
| PREN 2184 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2301 (NICR21FE18MO9) - SOLUTION TREATED - BAR AND SECTION - D[E] <= 200 MM |
| BS EN 2116:2009 | Aerospace series. Aluminium alloy 2017A-T42. Wire for solid rivets. D ≤ 10 mm |
| 96/716597 DC : DRAFT DEC 1996 | PREN 3671 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH3601 (NICR22MO9NB) AS WROUGHT - FORGING STOCK A OR D <= 250 MM |
| 96/716599 DC : 0 | PREN 4315 - AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2601 (X6NICRTIMOV26-15) SOLUTION AND PRECIPITATION TREATED - BARS AND SECTIONS A OR D <= 100 MM - R[M] => 900 MPA |
| BS EN 3361:2007 | Aerospace series. Steel FE-PM1802 (X5CrNiCu15-5). Consumable electrode remelted, solution treated and precipitation treated, sheet and strip a ≤ 6mm, 1070 MPa ≤ Rm ≤ 1220 MPa |
| 96/716600 DC : 0 | PREN 4316 - AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2601 (X6NICRTIMOV26-15) AS FORGED - FORGING STOCK A OR D <= 200 MM - R[M] => 900 MPA |
| PREN 2304 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2601 (X6NICRTIMOV26-15) - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - D[E] <= 100 MM - R[M] >= 960 MPA |
| BS EN 4500-004:2012 | Aerospace series. Metallic materials. Rules for drafting and presentation of material standards Specific rules for titanium and titanium alloys |
| I.S. EN 2482:2010 | AEROSPACE SERIES - STEEL FE-PL2108 (35NICRMO16) - 1100 MPA <= R[M] <= 1300 MPA - BARS - D[E] <= 100 MM |
| UNI EN 3351 : 2013 | AEROSPACE SERIES - TITANIUM ALLOY TI-4AL-4MO-2SN - SOLUTION TREATED AND AGED - FORGINGS - D[E] <= 150 MM |
| 07/30171298 DC : 0 | BS EN 2954-001 - AEROSPACE SERIES - MACROSTRUCTURE OF TITANIUM AND TITANIUM ALLOY WROUGHT PRODUCTS - PART 1: GENERAL REQUIREMENTS |
| 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 |
| PREN 4528 : 200P1 | AEROSPACE SERIES - STEEL FE-PA3903 (X10CRNI18-8) - COLD ROLLED - STRIP FOR SPRINGS A <= 3 MM 1250 MPA <= RM <= 1640 MPA |
| PREN 2072 : 200P1 | AEROSPACE SERIES - ALUMINIUM AL-P1050A - H14 - SHEET AND STRIP - 0,4 MM <= A <= 6 MM |
| PREN 2087 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2014A - T6 OR T62 - CLAD SHEET AND STRIP - 0,4 MM <= A <= 6 MM |
| PREN 4247 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024-T42 - PLATE - 6 MM < A <= 140 MM |
| PREN 2696 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7075-T6 OR T62 - SHEET AND STRIP - 0,4 MM <= A <= 6 MM |
| PREN 2763 : 200P3 | |
| PREN 2817 : 200P3 | |
| PREN 3125 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-C42201 - T6 - INVESTMENT CASTING - A <= 20 MM |
| PREN 2482 : 200P1 | AEROSPACE SERIES - STEEL FE-PL2108 (36NICRMO16) - 1100 MPA <= R[M] <= 1300 MPA - BARS - D[E] <= 100 MM |
| PREN 2395 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2014A-T4 OR T42 - SHEETS AND STRIP - 0,4 MM <= A <= 6 MM |
| PREN 4450 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7050 - T762 - SHEET - 0,8 MM <= A <= 6 MM |
| PREN 4465 : 200P1 | AEROSPACE SERIES - STEEL FE-PM1506 (X5CRNIMOAL13-8-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 150 MM - R[M] >= 1 300 MPA |
| XP PREN 4500-6 : 1997 XP | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 6: SPECIFIC RULES FOR FILLER METALS FOR BRAZING |
| PREN 4346 : 200P1 | AEROSPACE SERIES - STEEL FE-PM1505 (X1CRNIMOALTI12-9-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOFTENED - FORGING STOCK - A OR D <= 300 MM |
| NF EN 4462 : 2008 | |
| NF EN 4467 : 2008 | |
| I.S. EN 4500-003:2012 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 003: SPECIFIC RULES FOR HEAT RESISTING ALLOYS |
| PREN 3477 : 200P3 | AEROSPACE SERIES - STEEL FE-PM3503 (X7CRNIMO15-7-3) - AIR MELTED - SOLUTION TREATED AND PRECIPITATION TREATED - PLATE - 6 MM < A <= 15 MM - 1310 MPA <= R[M] <= 1550 MPA |
| PREN 3483 : 200P1 | AEROSPACE SERIES - STEEL FE-CM3801 (X5CRNICU16-4) - HOMOGENIZED, SOLUTION TREATED, PRECIPITATION HARDENED AND SUB ZERO SAND OR INVESTEMENT CASTING - RM >= 1240 MPA |
| PREN 3488 : 200P2 | AEROSPACE SERIES - STEEL FE-PA3601 (X6CRNITI18-10) - AIR MELTED - SOFTENED - SHEET AND STRIP - A <= 6 MM - 500 MPA <= R[M] <= 700 MPA |
| PREN 3523 : 200P2 | |
| PREN 3355 : 200P3 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AI-4V) - ANNEALED - EXTRUDED SECTION - D[E] <= 150 MM - 900 MPA <= R[M] <= 1160 MM MPA |
| PREN 3509 : 200P2 | AEROSPACE SERIES - STEEL FE-PL1501 (30CRMO12) - AIR MELTED - HARDENED AND TEMPERED - BAR - D[E] <= 40 MM = 1050 MPA <= R[M] <= 1250 MPA |
| PREN 3516 : 200P2 | AEROSPACE SERIES - STEEL FE-PL8201 (41NICRMO2) - AIR MELTED - SOFTENED - FORGING STOCK - A OR D <= 300 MM |
| PREN 3344 : 200P3 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7050-T76511 - EXTRUDED BAR AND SECTION - A OR D <= 150 MM - WITH PERIPHERAL COARSE GRAIN CONTROL |
| PREN 3470 : 200P2 | |
| PREN 3515 : 200P2 | AEROSPACE SERIES - STEEL FE-PL8201 (41NICRMO2) - AIR MELTED - HARDENED AND TEMPERED - FORGINGS - D[E] <= 25 MM - 1100 MPA <= R[M] <= 1300 MPA |
| 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 2032-001 : 200P5 | AEROSPACE SERIES - METALLIC MATERIALS - PART 001: CONVENTIONAL DESIGNATION |
| PREN 3335 : 200P3 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7475-O2 - SHEET FOR SUPERPLASTIC FORMING (SPF) - 0,8 MM <= A <= 6 MM |
| PREN 3359 : 200P2 | AEROSPACE SERIES - STEEL FE-PM1503 (X3CRNIMOAL 13-8-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOFTENED - FORGING STOCK - A OR D <= 300 MM |
| PREN 3310 : 200P3 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - NOT HEAT TREATED - FORGING STOCK, FOR ANNEALED FORGINGS - D[E] <= 360 MM |
| PREN 3464 : 200P3 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - PLATE - 6 MM < A <= 100 MM |
| I.S. EN 4700-001:2010 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 001: PLATE, SHEET AND STRIP |
| EN 2221 : 2017 | AEROSPACE SERIES - STEEL FE-PL31 - HARDENED AND TEMPERED - HOLLOW BARS - 3,5 MM <= A <= 55 MM |
| I.S. EN 4262:2013 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA4901 (X12CRNICOMOW21-20) - AS FORGED - FORGING STOCK - A OR D <= 200 MM - 690 MPA <= R[M] <= 880 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 |
| BS EN 3355:2012 | Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Extruded section. De ≤ 150 mm. 900 MPa ≤ Rm ≤ 1 160 MPa |
| UNI EN 2481 : 2011 | AEROSPACE SERIES - STEEL FE-PL2108 (35NICRMO16) - 1250 MPA <= R[M] <= 1400 MPA - FORGINGS - D[E] <= 75 MM |
| NF EN 2466 : 2009 | AEROSPACE SERIES - STEEL FE-PA3901 (X2CRNI19-11) - SOFTENED - FORGINGS - D[E] <= 100 MM |
| UNI EN 4700-003 : 2011 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 003: TUBE |
| NF EN 2818 : 2010 | AEROSPACE SERIES - STEEL FE-PM1802 (X5CRNICU15-5) - CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D < OR = 200 MM - R[M] > OR = 1070 MPA |
| I.S. EN 3982:2015 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7050 - ALZN6CUMGZR - T7451 - PLATES - 6 MM < A <= 160 MM |
| NF EN 4700-003 : 2012 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 003: TUBE |
| NF EN 4675 : 2012 | AEROSPACE SERIES - TITANIUM TI-P63002 (TI5AL5MO5V3CR0,4FE) - R[M] > OU = TO 1300 MPA - BARS - D[E] < 110 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 3163:2007 | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - AIR MELTED, SOFTENED, FORGING STOCK A OR D <= 300 MM |
| I.S. EN 4263:2013 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA4901 (X12CRNICOMOW21-20) - AS FORGED - FORGING STOCK - A OR D <= 200 MM - 690 MPA <= R[M] <= 960 MPA |
| EN 2135:2017 | Aerospace series - Steel FE-PL61 - Carburized, hardened and tempered - Bar - De ≤ 40 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 |
| UNI EN 4800-007 : 2011 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 007: REMELTING STOCK |
| NF EN 4384 : 2008 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-CH1303 (NICO20CR20MO5TI2AL) - NON HEAT TREATED - REMELTING STOCK |
| NF EN 4347 : 2008 | AEROSPACE SERIES - STEEL FE-PM1506 (X3CRNIMOAL13-8-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED, SOFTENED, FORGING STOCK A OR D <= 300 MM |
| UNI EN 4655 : 2011 | AEROSPACE SERIES - STEEL FE-PM1506 (X1CRNIMOAITI12-10-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BARS - A OR D <= 200 MM - R[M] >= 1400 MPA |
| NF EN 2398 : 2008 | AEROSPACE SERIES - HEAT RESISTING STEEL FE-PA2601 (X6NICRTIMOV26-15) - R[M] >= 900 MPA - BARS FOR MACHINED BOLTS - D <= 25 MM |
| UNI EN 3983 : 2014 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7050-T7651 - PLATE - 6 MM < A <= 160 MM |
| EN 2119 : 2017 | Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated - Wires for rivets - 2 mm ≤ D ≤ 10 mm - Rm ≥ 960 MPa |
| 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 3162:2007 | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - AIR MELTED - SOLUTION TREATED AND PRECIPITATION TREATED - SHEET AND STRIP A <= 6 MM - R[M] >= 930 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 |
| I.S. EN 4346:2007 | AEROSPACE SERIES - STEEL FE-PM1505 (X1CRNIMOALTI12-9-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED, SOFTENDED, FORGING STOCK A OR D <= 300 MM |
| I.S. EN 2467:2007 | AEROSPACE SERIES - STEEL FE-PA3901 (X2CRNI18-9) - AIR MELTED - SOFTENED - PLATE, SHEET AND STRIP - 0,4 MM <= A <= 20 MM - 520 MPA <= R[M] <= 670 MPA |
| 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 2115:2009 | AEROSPACE SERIES - ALUMINIUM ALLOY 2117-T42 - WIRE FOR SOLID RIVETS - D <= 10 MM |
| I.S. EN 2446:2008 | AEROSPACE SERIES - STEEL FE-PL1503 (35CRMO4) - 1100 MPA <= R[M] <= 1300 MPA - BARS - D[E] <= 25 MM |
| BS EN 2635:2005 | Aerospace series. Aluminium alloy AL-P2014A. T6511. Extruded bar and section. a or D ≤ 200 mm with peripheral coarse grain control |
| BS EN 4340:2002 | Aerospace series. Magnesium alloy MG-W68001. Filler metal for welding. Wire and rod |
| BS EN 3532:2007 | Aerospace series. Steel FE-PM2701 (X2NiCoMo18-8-5).Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated.Plate. 6 mm < a ≤ 40 mm. 1750 MPa ≤ Rm ≤ 2000 MPa |
| BS EN 4099:2005 | Aerospace series. Aluminium alloy AL-P2219-T6 or T62. Clad sheet and strip. 0,5 mm ≤ a ≤ 6 mm |
| BS EN 2090:2005 | Aerospace series. Aluminium alloy AL-P2024-T3. Clad sheet and strip 0,3 mm ≤ a ≤ 6 mm |
| BS EN 2044:2001 | Aerospace series. Round bars, drawn, in aluminium and aluminium alloys. Tolerance class h 11. Diameter 4 mm ≤ D ≤ 63 mm. Dimensions |
| BS EN 3924:1998 | Nickel base alloy NI-B41203 (NiCr7Si5B3). Filler metal for brazing. Tape |
| BS EN 2395:2005 | Aerospace series. Aluminium alloy AL-P2014A-T4 or T42. Sheet and strip. 0,4 mm ≤a ≤6 mm |
| BS EN 2131:2002 | Aerospace series. Plates in aluminium alloys. Thickness 6 mm < a ≤ 160 mm. Dimensions |
| BS EN 3965:2001 | Aerospace series. Titanium alloy TI-B17001. Filler metal for brazing. Rolled foil |
| BS EN 3956:2001 | Aerospace series. Silver base alloy AG-B14001 (AgCu42Ni2). Filler metal for brazing. Wire |
| EN 2469 : 2007 | AEROSPACE SERIES - STEEL FE-PA3901 (X1CRNI18-10) - AIR MELTED - SOFTENED - WIRES - 0,4 MM <= D <= 12,5 MM - 450 MPA <= R[M] <= 650 MPA |
| EN 3507 : 2006 | AEROSPACE SERIES - STEEL FE-PL1501 (30CRMO12) - AIR MELTED - HARDENED AND TEMPERED - FORGINGS - D[E] <= 100 MM - 930 MPA <= R[M] <= 1080 MPA |
| EN 3945:2001 | Aerospace series - Nickel base alloy NI-B48801 (NiMn19Si6Cu4B) - Filler metal for brazing - Powder or paste |
| EN 3897:2001 | Aerospace series - Steel FE-WA4801 (X6CrNiMnNb18-10) - Filler metal for welding |
| EN 2696:2005 | Aerospace series - Aluminium alloy AL-P7075-T6 or T62 - Sheet and strip - 0,4 mm |
| EN 3310 : 2011 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - NOT HEAT TREATED - FORGING STOCK, FOR ANNEALED FORGINGS - D[E] <= 360 MM |
| EN 3944:1998 | Aerospace series - Nickel base alloy NI-B41204 (NiCr13Si4B3) - Filler metal for brazing - Tape |
| EN 3921:2001 | Aerospace series - Nickel base alloy NI-B41203 (NiCr7Si5B3) - Filler metal for brazing - Amorphous foil |
| EN 3958:2001 | Aerospace series - Silver base alloy AG-B14001 (AgCu42Ni2) - Filler metal for brazing - Rolled foil |
| EN 4347:2007 | Aerospace series Steel FE-PM1506 (X3CrNiMoAl13-8-2) - Vacuum induction melted and consumable electrode remelted, softened, forging stock a or D ≤ 300 mm |
| EN 2045 : 2001 | AEROSPACE SERIES - SQUARE BARS, DRAWN IN ALUMINIUM AND ALUMINIUM ALLOYS - TOLERANCE CLASS H 11 - THICKNESS 6 MM <= A <= 50 MM - DIMENSIONS |
| EN 2511 : 2005 | Aerospace series - Aluminium alloy AL-P7075-T7351 - Plate -6 mm |
| EN 4283:2005 | Aerospace series - Aluminium alloy AL-P2219-T87 - Plate - 6 mm |
| EN 3338 : 2005 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7050 - T74511 - EXTRUDED BAR AND SECTION - A OR D <= 150 MM WITH PERIPHERAL COARSE GRAIN CONTROL |
| EN 2731:2005 | Aerospace series - Magnesium alloy MG-C46001 - T6 - Sand casting |
| EN 2252:2012 | Aerospace series - Steel FE-PL1505 (15CrMoV6) - 1 080 MPa ≤ Rm ≤ 1 250 MPa - Forgings - De ≤ 100 mm |
| EN 3883:2001 | Aerospace series - Heat resisting alloy NI-WH2301 (NiCr22Fe19Mo9Co2) - Filler metal for welding |
| UNI EN 2632 : 2007 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7075 - T73511 - EXTRUDED BAR AND SECTION - A OR D <= 150 MM WITH PERIPHERAL COARSE GRAIN CONTROL |
| UNI EN 4800-001 : 2011 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 001: PLATE, SHEET AND STRIP |
| 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 |
| 97/717260 DC : DRAFT OCT 1997 | PREN 4097 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-CD1401 (NICO10W10CR9AL6TA3) - VACUUM MELTED PRECIPITATION TREATED PRECISION CASTINGS |
| 96/716568 DC : 0 | PREN 4400-2 - AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM ALLOY WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 2: PLATE |
| 97/719220 DC : DRAFT NOV 1997 | PREN 3557 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6061-T4 - DRAWN TUBE FOR PRESSURE APPLICATIONS - 0,6 MM <= A <= 3 MM |
| 96/716586 DC : 0 | PREN 2197 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1701 (NICR15CO14A15TIMO4) SOLUTION AND PRECIPITATION TREATED - FORGINGS D[E] <= 200 MM |
| 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 |
| NF EN 4468 : 2008 | |
| 97/719251 DC : DRAFT NOV 1997 | PREN 4284 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2219-T852 - FORGINGS - A <= 400 MM |
| BS EN 3329:2009 | Aerospace series. Steel FE-PL1503 (35CrMo4). Annealed Sheet and strip. 0,3 mm ≤ a ≤ 2 mm. For prevailing torque nuts |
| 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 4379:2007 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH3601 (NICR22MO9NB) - SOLUTION TREATED, FORGING D[E] <= 200 MM |
| 97/719255 DC : DRAFT NOV 1997 | PREN 4289 - AEROSPACE SERIES - ALUMINIUM AL-P7175 - FORGING STOCK |
| BS EN 4346:2007 | Aerospace series. Steel FE-PM1505 (X1CrNiMoAlTi12-9-2). Vacuum induction melted and consumable electrode remelted, softened, forging stock a or D ≤ 300 mm |
| NF EN 4098 : 2008 | AEROSPACE SERIES - STEEL FE-PL1507 (40CRMOV12) - REMELTED, HARDENED AND TEMPERED, FORGINGS D[E] <= 50 MM, 1250 MPA <= R[M] <= 1400 MPA |
| NF EN 4800-008 : 2012 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 008: PRE-PRODUCTION AND PRODUCTION CASTINGS |
| NF EN 4800-007 : 2012 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 007: REMELTING STOCK |
| 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 |
| 95/715393 DC : 0 | PREN 4261-2 - AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF TEST METHOD STANDARDS - PART 2: SPECIFIC REQUIREMENTS FOR MECHANICAL TEST METHOD STANDARD |
| NF EN 2460 : 2009 | AEROSPACE SERIES - STEEL FE-PM1901 (X12CRNI13) - 600 MPA <= R[M] <= 800 MPA - BARS - D[E] <= 70 MM |
| 98/712165 DC : 0 | PREN 2690 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7050-T7452 - HAND FORGINGS - A <= 200 MM |
| UNI EN 3464 : 2013 | AEROSPACE SERIES - TITANIUM ALLOY TI-6AL-4V - ANNEALED - PLATE - 6 MM < A <= 100 MM |
| UNI EN 4675 : 2012 | AEROSPACE SERIES - TITANIUM TI-P63002 (TI5AL5MO5V3CR0.4FE) - R[M] >= 1300 MPA - BARS - D[E] < 110 MM |
| 09/30211110 DC : 0 | BS EN 2226 - AEROSPACE SERIES - STEEL FE-PM3501 (X105CRMO17) - HARDENED AND TEMPERED - HAND AND DIE FORGINGS D[E] <= 150 MM |
| NF EN 2206 : 2009 | AEROSPACE SERIES - STEEL FE-PL1502 (25CRMO4) - 650 MPA <= R[M] <= 850 MPA - BARS - D[E] <=150 MM |
| 97/718298 DC : DRAFT OCT 1997 | PREN 2538 - AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - AIR MELTED SOLUTION TREATED AND PRECIPITATION HARDENED SHEET AND STRIP A <= 6 MM - RM => 1310 MPA |
| BS EN 3528:2013 | Aerospace series. Steel X2NiCoMo18-8-5 (1.6359). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Bar. a or D ≤ 150 mm. 1 750 MPa ≤ Rm ≤ 2 000 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 3451:2017 | AEROSPACE SERIES - TITANIUM TI-P99002 - NOT HEAT TREATED - GRADE 2 FORGING STOCK, FOR ANNEALED FORGINGS - A OR D <= 300 MM |
| NF EN 3487 : 2008 | AEROSPACE SERIES - STEEL FE-PA3601 (X6CRNITI18-10) - AIR MELTED - SOFTENED - BAR FOR MACHINING - A OR D <= 250 MM - 500 MPA <= R[M] <= 700 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 |
| UNI EN 4800-003 : 2011 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 003: TUBE |
| BS EN 2448:2008 | Aerospace series. Steel FE-PL1503 (35CrMo4). 900 MPa ≤ Rm ≤ 1100 MPa. Bars. De ≤ 40 mm |
| BS EN 4098:2007 | Aerospace series. Steel FE-PL1507 (40CrMoV12). Remelted, hardened and tempered, forgings De ≤ 50 mm, 1250 MPa ≤ Rm ≤ 1400 MPa |
| BS 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 ≥ 1400 MPa |
| 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 |
| 97/718306 DC : DRAFT OCT 1997 | PREN 2916 - AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - CONSUMABLE ELECTRODE REMELTED SOLUTION TREATED AND PRECIPITATION HARDENED FORGINGS A OR D <= 150 MM - RM => 965 MPA |
| BS EN 2438:2008 | Aerospace series. Steel FE-PL2102 (35NiCr6). 900 MPa ≤ Rm ≤ 1100 MPa. Bars. De ≤ 40 mm |
| PREN 2252 : 200P1 | AEROSPACE SERIES - STEEL FE-PL1505 (15CRMOV6) - 1080 MPA <= R[M] <= 1250 MPA - FORGINGS - D[E] <= 100 MM |
| 12/30268169 DC : 0 | BS EN 8.4567 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7010 - T76 - EXTRUDED BARS - 150 MM < D <= 250 MM |
| I.S. EN 2222:2017 | AEROSPACE SERIES - STEEL FE-PL31 - HARDENED AND TEMPERED - HAND AND DIE FORGINGS |
| 01/716449 DC : DRAFT JAN 2002 | PREN 2395 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2014A - T4 OR T42 - SHEET AND STRIP - 0,4 MM < A < 6 MM |
| 02/708860 DC : 0 | PREN 4800-1 - AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 1: PLATE, SHEET AND STRIP |
| I.S. EN 2206:2008 | AEROSPACE SERIES - STEEL FE-PL1502 (25CRMO4) - 650 MPA <= R[M] <= 850 MPA - BARS - D[E] <= 150 MM |
| 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 2480:2008 | Aerospace series. Steel FE-PL2108 (36NiCrMo16). 1250 MPa ≤ Rm ≤ 1400 MPa. Bars. De ≤ 75 mm |
| 97/719256 DC : DRAFT NOV 1997 | PREN 4293 - AEROSPACE SERIES - ALUMINIUM AL-P7175-T73511 - EXTRUDED BAR AND SECTION - A OR D <= 150 MM |
| NF EN 2480 : 2008 | AEROSPACE SERIES - STEEL FE-PL2108 (36NICRMO16) - 1250 MPA <= R[M] <= 1400 MPA - BARS - D[E] <= 75 MM |
| 97/718305 DC : DRAFT OCT 1997 | PREN 2915 - AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - CONSUMABLE ELECTRODE REMELTED SOLUTION TREATED AND PRECIPITATION HARDENED BAR A OR D <= 200 MM - RM => 965 MPA |
| UNI EN 3310 : 2012 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - NOT HEAT TREATED - FORGING STOCK, FOR ANNEALED FORGINGS - D[E] <= 360 MM |
| NF EN 2478 : 2008 | AEROSPACE SERIES - STEEL FE-PL2107 (30NICRMO16) - 1220 MPA <= R[M] <= 1370 MPA - BARS - D[E] <= 40 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 |
| BS EN 3459:2010 | Aerospace series. Titanium alloy TI-P63001 (Ti-4Al-4Mo-2Sn). Solution treated and aged. Plate. 6 mm < a ≤ 50 mm |
| 09/30208131 DC : DRAFT AUG 2009 | BS EN 3354 - AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - SHEET FOR SUPERPLASTIC FORMING - A <= 6 MM |
| BS EN 2478:2008 | Aerospace series. Steel FE-PL2107 (30NiCrMo16). 1220 MPa ≤ Rm ≤ 1370 MPa. Bars. De ≤ 40 mm |
| 97/712106 DC : DRAFT JUL 1997 | PREN 3994 - AEROSPACE SERIES - STEEL FE-CM15XX (X13CRNIMOCO12-3-2-2) - NOT HEAT TREATED - REMELTING STOCK |
| 97/719243 DC : DRAFT NOV 1997 | PREN 2683 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7010-T7651 - HAND FORGINGS - A <= 150 MM |
| 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 |
| NF EN 4461 : 2008 | |
| 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 |
| BS EN 2002-2:2005 | Aerospace series. Metallic materials. Test methods Tensile testing at elevated temperature |
| 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 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 2032-001:2014 | Aerospace series. Metallic materials Conventional designation |
| 96/716589 DC : 0 | PREN 2203 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1303 (NICO20CR20MO5TI2A1) - SOLUTION TREATED - SHEET, STRIP AND PLATE 0,2 MM <= A <= 10 MM |
| 01/716440 DC : DRAFT JAN 2002 | PREN 2088 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2014A - T4 OR T42 CLAD SHEET AND STRIP - 0,4 MM < A < 6 MM |
| BS EN 4700-003:2010 | Aerospace series. Steel and heat resisting alloys. Wrought products. Technical specification Tube |
| 96/716575 DC : 0 | PREN 2814 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024 T3 - DRAWN TUBES FOR STRUCTURAL APPLICATIONS 0,6 MM <= A <= 12,5 MM |
| BS EN 4800-001:2010 | Aerospace series. Titanium and titanium alloys. Technical specification Plate, sheet and strip |
| 11/30242528 DC : DRAFT JAN 2011 | BS EN 4628 - AEROSPACE SERIES - STEEL FE-PM 3504 (X4CRNIMO16-5-1) - AIR MELTED - HARDENED AND TEMPERED - BAR D[E] <= 200 MM - 1150 MPA <= R[M] <= 1300 MPA |
| DIN EN 2633:2016-02 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024 - ALCU4MG1 - T3511 - EXTRUDED BARS AND SECTIONS - 1,2 MM <= D[E] <= 160 MM WITH PERIPHERAL COARSE GRAIN CONTROL |
| 97/719245 DC : DRAFT NOV 1997 | PREN 2688 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7050-T74 - DIE FORGINGS - A <= 150 MM |
| 97/718303 DC : DRAFT OCT 1997 | PREN 2775 - AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - CONSUMABLE ELECTRODE REMELTED SOLUTION TREATED AND PRECIPATION HARDENED FORGINGS A OR D <= 150 MM - RM => 1310 MPA |
| 96/717408 DC : 0 | PREN 2662 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH3601 (NICR22MO9NB) ANNEALED - SHEET, STRIP AND PLATE 0,2 MM <= A <= 10 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 2030:2013 | Aerospace series. Steel X105CrMo17 (1.3544). Hardened and tempered. Bars. De ≤ 150 mm |
| BS EN 2460:2009 | Aerospace series. Steel FE-PM1901 (X12CrNi13). 600 MPa ≤ Rm ≤ 800 MPa. Bars. De ≤ 70 mm |
| 02/702910 DC : 0 | PREN 3980 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P8090-T6 - SUPERPLASTIC SHEET FORMINGS (SPF) - 0,8 MM <= A <= 6 MM |
| 96/717409 DC : 0 | PREN 2663 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH3601 (NICR22MO9NB) SOLUTION TREATED - SHEET, STRIP AND PLATE 0,2 MM <= A <= 10 MM |
| 11/30253929 DC : 0 | BS EN 4820 - AEROSPACE SERIES - COPPER AND COPPER ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION |
| UNI EN 2043 : 2014 | AEROSPACE SERIES - METALLIC MATERIALS - GENERAL REQUIREMENTS FOR SEMI-FINISHED PRODUCT QUALIFICATION (EXCLUDING FORGINGS AND CASTINGS) |
| 96/716604 DC : 0 | PREN 4369 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1701 (NICR15CO14A15TI4MO4) SOLUTION AND PRECIPITATION TREATED - BARS AND SECTIONS A OR D <= 100 MM |
| BS EN 4800-002:2010 | Aerospace series. Titanium and titanium alloys. Technical specification Bar and section |
| 03/306585 DC : 0 | EN 4400-7 - AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM- AND MAGNESIUM- ALLOY PRODUCTS - TECHNICAL SPECIFICATION - PART 7: ALUMINIUM ALLOY FORGINGS |
| 96/716590 DC : 0 | PREN 2204 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-CH1303 (NICO20CR20MO5TI2A1) - SOLUTION AND PRECIPITATION TREATED - PRECISION CASTING D[E] <= 50 MM |
| 11/30242532 DC : DRAFT JAN 2011 | BS EN 3351 - AEROSPACE SERIES - TITANIUM ALLOY TI-P63001 (TI-4AL-4MO-2SN) - SOLUTION TREATED AND AGED - FORGINGS - D[E] <= 150 MM |
| BS EN 4216:2007 | Aerospace series. Steel FE-CM3801 (GX5CrNiCuNb16-4). Homogenized, solution treated and precipitation hardened, investment casting De ≤ 50 mm, Rm ≥ 900 MPa |
| BS EN 4800-003:2010 | Aerospace series. Titanium and titanium alloys. Technical specification Tube |
| UNI EN 2482 : 2011 | AEROSPACE SERIES - STEEL FE-PL2108 (35NICRMO16) - 1100 MPA <= R[M] <= 1300 MPA - BARS - D[E] <= 100 MM |
| 98/700293 DC : DRAFT JAN 1998 | PREN 4290 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2219 - FORGING STOCK |
| BS EN 4372:2009 | Aerospace series. Heat resisting nickel alloy with copper NI-PD9001 (NiCu31). Wire for solid rivets. D ≤ 10 mm |
| BS EN 2209:2008 | Aerospace series. Steel FE-PL1502 (25CrMo4). 900 MPa ≤ Rm ≤ 1100 MPa. Sheets, strips and plates. 0,5 mm ≤ a ≤ 20 mm |
| BS EN 2205:2009 | Aerospace series. Steel FE-PL1502 (25CrMo4). 900 MPa ≤ Rm ≤ 1100 MPa. Bars. De ≤ 40 mm |
| BS EN 3120:2012 | Aerospace series. Titanium alloy TI-P64003. Cold worked and stress relieved. Seamless tube for pressure systems. 4 mm ≤ D ≤ 51 mm. 690 MPa ≤ Rm ≤ 1 030 MPa |
| BS EN 4670:2010 | Aerospace series. Steel FEPM1507 (X1CrNiMoAlTi12-11-2). Vacuum induction melted and consumable electrode remelted. Softened. Forging stock. a or D ≤ 300 mm |
| 07/19989213 DC : 0 | BS EN 2954-2 - AEROSPACE SERIES - MACROSTRUCTURE OF TITANIUM AND TITANIUM ALLOY WROUGHT PRODUCTS - PART 2: MACROSTRUCTURE OF BAR, SECTION, FORGING STOCK AND FORGINGS |
| BS EN 3983:2013 | Aerospace series. Aluminium alloy AL-P7050-. T7651. Plate. 6 mm < a ≤ 160 mm |
| PREN 2183 : 200P2 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2301 (NICR21FE18MO9) - SOLUTION TREATED - FORGINGS - D[E] <= 200 MM |
| 01/716044 DC : 0 | EN 4800-6 - AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 6: PRE-PRODUCTION AND PRODUCTION FORGINGS |
| NF EN 4700-001 : 2012 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 001: PLATE, SHEET AND STRIP |
| PREN 2204 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-CH1303 (NICO20CR20MO5TI2AL) - VACUUM MELTED - SOLUTION TREATED AND PRECIPITATION TREATED - PRECISION CASTING - D[E] <= 50 MM |
| 08/30181062 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 |
| PREN 2703 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024-T4 OR T42 - CLAD SHEET AND STRIP - 0,3 MM <= A <= 6 MM |
| 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 3365:2007 | Aerospace series. Steel FE-PM3901 (X15CrNi17-3). Air melted, softened, forging stock a or D ≤ 300 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 |
| NF EN 4700-004 : 2012 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 004: WIRE |
| NF EN 2461 : 2009 | AEROSPACE SERIES - STEEL FE-PM1901 (X12CRNI13) - 600 MPA <= R[M] <= 800 MPA - FORGINGS - D[E] <= 70 MM |
| PREN 2003-2 : 200P1 | AEROSPACE SERIES - STEELS - TEST METHODS - PART 2: IZOD IMPACT TEST |
| 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 |
| PREN 3998 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024-T4 OR T42 - SHEET AND STRIP - 0,3 MM <= A <= 6 MM |
| PREN 2161 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY CO-CH1401 (COCR26NI11W) NOT HEAT TREATED - PRECISION CASTINGS |
| PREN 4700-003 : 200P2 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 003: TUBE |
| PREN 2134 : 200P1 | AEROSPACE SERIES - ROUND BARS, EXTRUDED, IN ALUMINIUM AND ALUMINIUM ALLOYS - DIAMETER 10 MM <= D <= 220 MM - DIMENSIONS |
| 97/719246 DC : DRAFT NOV 1997 | PREN 4276 - AEROSPACE SERIES - ALUMINIUM AL-P7175-T7351 - HAND FORGINGS - A <= 150 MM |
| PREN 4317 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2601 (X6NICRTIMOV26-15) - NON HEAT TREATED - FORGING STOCK - A OR D <= 200 MM |
| PREN 2090 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024-T3 - CLAD SHEET AND STRIP - 0,3 MM <= A <= 6 MM |
| PREN 2119 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2601 (X6NICRTIMOV26-15) - SOLUTION TREATED AND PRECIPITATION TREATED - WIRES FOR RIVETS - 2 MM <= D <= 10 MM - R[M] >= 960 MPA |
| NF EN 3365 : 2008 | AEROSPACE SERIES - STEEL FE-PM3901 (X15CRNI17-3) - AIR MELTED, SOFTENED, FORGING STOCK A OR D <= 300 MM |
| PREN 2178 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2501 (X4NICRMOTI43-13) - SOLUTION TREATED AND PRECIPITATION TREATED - BAR AND SECTION - D[E] <= 200 MM |
| NF EN 4528 : 2009 | AEROSPACE SERIES - STEEL FE-PA3903 (X10CRNI18-8) - COLD ROLLED - STRIP FOR SPRINGS - A <= 3 MM - 1250 MPA <= R[M] <= 1640 MPA |
| UNI EN 3976 : 2008 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TEST METHOD - CHEMICAL ANALYSIS FOR THE DETERMINATION OF HYDROGEN CONTENT |
| PREN 2915 : 200P2 | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BAR - A OR D <= 200 MM - R[M] >= 965 MPA |
| NF EN 4800-004 : 2012 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 004: WIRE |
| PREN 2916 : 200P2 | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 200 MM - R[M] >= 965 MPA |
| 05/30129555 DC : 0 | PREN 4700-6 - AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 6: PRE-PRODUCTION AND PRODUCTION FORGINGS |
| DIN EN 2704:2016-02 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024 - ALCU4MG1 - T3511 - DRAWN BARS - D[E] <= 75 MM |
| PREN 3474 : 200P3 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024-T81 - SHEET AND STRIP - 0,25 MM <= A <= 6 MM |
| PREN 3507 : 200P2 | AEROSPACE SERIES - STEEL FE-PL1501 (30CRMO12) - AIR MELTED - HARDENED AND TEMPERED - FORGINGS - D[E] <= 100 MM - 930 MPA <= R[M] <= 1080 MPA |
| PREN 3532 : 200P2 | AEROSPACE SERIES - STEEL FE-PM2701 (X2NICOMO18-8-5) - VACUUM INDUCTION MELTED AND VACUUM ARC REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - PLATE - 6 MM < A <= 40 MM - 1750 MPA <= R[M] <= 2000 MPA |
| PREN 3476 : 200P2 | AEROSPACE SERIES - STEEL FE-PL1501 (30CRMO12) - AIR MELTED - SOFTENED - FORGING STOCK - A OR D <= TO 300 MM |
| I.S. EN 4293:2014 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7175 - T73511 - EXTRUDED BAR AND SECTION - A OR D <= 150 MM |
| PREN 3521 : 200P2 | |
| PREN 3339 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7010-T76 - DIE FORGINGS - A <= 200 MM |
| PREN 3354 : 200P4 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AI-4V) - ANNEALED - SHEET FOR SUPERPLASTIC FORMING - A <= 6 MM |
| I.S. EN 4800-008:2010 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 008: PRE-PRODUCTION AND PRODUCTION CASTINGS |
| 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 4209 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2219 - T851 - PLATE - 6 MM < A <= 50 MM |
| PREN 2044 : 200P1 | AEROSPACE SERIES - ROUND BARS, DRAWN, IN ALUMINIUM AND ALUMINIUM ALLOYS - TOLERANCE CLASS H 11 - DIAMETER 4 MM <= D <= 63 MM - DIMENSIONS |
| PREN 4683 : 200P1 | AEROSPACE SERIES - STEEL FE-WM 3504 (X4CRNIMO16-5-1) - AIR MELTED - FILLER METAL FOR WELDING - WIRE AND ROD |
| PREN 4400-2 : 200P1 | AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM ALLOY WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 2: SHEET AND STRIP |
| 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 4202 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6082 - T651 - PLATE - 6 MM < A <= 25 MM |
| PREN 4207 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P8090 - T89 - EXTRUDED BAR AND SECTION - A OR D <= 15 MM WITH PERIPHERAL COARSE GRAIN CONTROL |
| PREN 3872 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-R39002 - H112 - DIE FORGINGS - A <= 200 MM |
| PREN 4800-008 : 200P2 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 8: PRE-PRODUCTION AND PRODUCTION CASTINGS |
| PREN 4099 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2219-T62 OR T62 - CLAD SHEET AND STRIP - 0,5 MM <= A <= 6 MM |
| PREN 4002 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2219 - T81 - SHEET AND STRIP - 0,5 MM <= A <= 6 MM |
| PREN 4203 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P8090 - T89 - SHEET - 0,6 MM <= A <= 6 MM |
| PREN 4204 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P8090 - T841 - SHEET - 0,6 MM <= A <= 6 MM |
| PREN 2002-02 : 200P3 | AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - PART 2: TENSILE TESTING AT ELEVATED TEMPERATURE |
| PREN 2088 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2014A-T4 OR T42 - CLAD SHEETS AND STRIP - 0,4 MM <= A <= 6 MM |
| PREN 2123 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2618A - T851 - PLATE - 6 MM < A <= 140 MM |
| PREN 2002-06 : 200P2 | AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - PART 6: BEND TESTING |
| PREN 4800-002 : 200P2 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 2: BAR AND SECTION |
| PREN 2002-01 : 200P3 | AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - PART 1: TENSILE TESTING AT AMBIENT TEMPERATURE |
| PREN 2002-21 : 200P2 | AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - PART 21: RADIOGRAPHIC TESTING OF CASTINGS |
| DIN EN 2959:2000-03 (Draft) | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1302 (NICR20CO13MO4TI3AL), SOLUTION TREATED AND COLD WORKED - BAR FOR FORGED FASTENERS 3 MM = D = 30 MM |
| I.S. EN 2117:2009 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P5056A (5056A)-H32 - WIRE FOR SOLID RIVETS - D <= 10 MM |
| NF EN 3364 : A2008 | AEROSPACE SERIES - STEEL FE-PM1802 (X5CRNICU15-5)- CONSUMABLE ELECTRODE REMELTED, SOFTENED, FORGING STOCK A OR D <= 300 MM |
| I.S. EN 4528:2009 | AEROSPACE SERIES - STEEL FE-PA3903 (X10CRNI18-8) - COLD ROLLED - STRIP FOR SPRINGS - A <= 3 MM - 1250 MPA <= R[M] <= 1640 MPA |
| UNI EN 4500-005 : 2014 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 005: SPECIFIC RULES FOR STEELS |
| I.S. EN 4216:2007 | AEROSPACE SERIES - STEEL FE-CM3801 (GX5CRNICUNB16-4) - HOMOGENIZED, SOLUTION TREATED AND PRECIPITATION HARDENED, INVESTMENT CASTING - D[E] <= 50 MM, R[M] >= 900 MPA |
| NF EN 4800-001 : 2012 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 001: PLATE, SHEET AND STRIP |
| 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 4471:2007 | AEROSPACE SERIES - STEEL FE-PM1505 (X1CRNIMOALTI12-9-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 150 MM - 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 |
| UNI EN 3120 : 2013 | Aerospace series - Titanium alloy TI-P64003 - Cold worked and stress relieved - Seamless tube for pressure systems - 4 mm ≤ D ≤ 51 mm - 690 MPa ≤ Rm ≤ 1 030 MPa |
| I.S. EN 2438:2008 | AEROSPACE SERIES - STEEL FE-PL2102 (35NICR6) - 900 MPA <= R[M] <= 1100 MPA - BARS - D[E] <= 40 MM |
| BS EN 2222:2017 | Aerospace series. Steel FE-PL31. Hardened and tempered. Hand and die forgings |
| 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 2002-002:2006 | AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - PART 2: TENSILE TESTING AT ELEVATED TEMPERATURE |
| I.S. EN 4670:2010 | AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOFTENED - FORGING STOCK - A OR D <= 300 MM |
| UNI EN 4700-001 : 2011 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 001: PLATE, SHEET AND STRIP |
| 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 2116:2009 | AEROSPACE SERIES - ALUMINIUM ALLOY 2017A-T42 - WIRE FOR SOLID RIVETS - D <= 10 MM |
| I.S. EN 2439:2009 | AEROSPACE SERIES - STEEL FE-PL2102 (34NICR6) - 900 MPA <= R[M] <= 1 100 MPA - FORGINGS - D[E] <= 40 MM |
| I.S. EN 4461:2007 | |
| I.S. EN 2481:2010 | AEROSPACE SERIES - STEEL FE-PL2108 (35NICRMO16) - 1250 MPA <= R[M] <= 1400 MPA - FORGINGS - D[E] <= 75 MM |
| I.S. EN 2209:2008 | AEROSPACE SERIES - STEEL FE-PL1502 (25CRMO4) - 900 MPA <= R[M] <= 1100 MPA - SHEETS, STRIPS AND PLATES - 0,5 MM <= A <= 20 MM |
| I.S. EN 4472:2007 | AEROSPACE SERIES - STEEL FE-PM1505 (X1CRNIMOALTI12-9-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 150 MM - R[M] >= 1400 MPA |
| I.S. EN 2461:2009 | AEROSPACE SERIES - STEEL FE-PM1901 (X12CR13) - 600 MPA <= R[M] <= 800 MPA - FORGINGS - D[E] <= 70 MM |
| I.S. EN 3115:2009 | AEROSPACE SERIES - ALUMINIUM ALLOY 7050-T73 - WIRE FOR SOLID RIVETS - D <= 10 MM |
| I.S. EN 3488:2007 | AEROSPACE SERIES - STEEL FE-PA3601 (X6CRNITI18-10) - AIR MELTED - SOFTENED - SHEET AND STRIP - A <= 6 MM - 500 MPA <= R[M] <= 700 MPA |
| I.S. EN 3875:2017 | AEROSPACE SERIES - METALLIC MATERIALS, FILLER METAL FOR BRAZING - TECHNICAL SPECIFICATION |
| BS EN 4204:2005 | Aerospace series. Aluminium alloy AL-P8090. T841. Sheet. 0,6 mm ≤ a ≤ 6 mm |
| BS EN 3332:2005 | Aerospace series. Aluminium alloy AL-P7475-T762. Clad sheet and strip. 1,0 mm ≤ a ≤ 6 mm |
| BS EN 3344:2005 | Aerospace series. Aluminim alloy AL-P7050. T76511. Extruded bar and section. a or D ≤ 150 mm with peripheral coarse grain control |
| BS EN 3923:2001 | Aerospace series. Nickel base alloy NI - B41203 (NiCr7Si5B3Fe3). Filler metal for brazing. Powder or paste |
| BS EN 2049:2001 | Aerospace series. Extruded channel section, in aluminium alloys. Dimensions |
| BS EN 3341:2005 | Aluminium alloy AL-P6061-T4 or T42. Sheet and strip. 0,4 mm ≤ a ≤ 6 mm |
| BS EN 3335:2005 | Aluminium alloy AL-P7475-O2. Sheet for superplastic forming (SPF). 0,8 mm ≤ a ≤ 6 mm |
| BS EN 4212:2005 | Aerospace series. Aluminium alloy AL-P5086-H111. Plate. 6mm < a ≤8 0mm |
| BS EN 3925:2001 | Aerospace series. Nickel base alloy NI-B40001 (NiSi5B3). Filler metal for brazing. Amorphous foil |
| BS EN 2511:2005 | Aluminium alloy AL-P7075-T7351. Plate. 6 mm < a ≤ 100 mm |
| BS EN 3960:2001 | Aerospace series. Gold base alloy AU-B40001 (AuNi18). Filler metal for brazing. Powder or paste |
| BS EN 2134:2002 | Aerospace series. Round bars, extruded in aluminium and aluminium alloys. Diameter 10 mm ≤ D ≤ 220 mm. Dimensions |
| BS EN 3930:2001 | Aerospace series. Nickel base alloy NI-B31001 (NiCr19Si10). Filler metal for brazing. Powder or paste |
| BS EN 4343:2002 | Aerospace series. Steel FE-WM1001 (X13Cr12). Filler metal for welding. Wire and rod |
| BS EN 4327:2001 | Aerospace series. Heat resisting alloy CO-WH1401 (CoCr26Ni11W8). Filler metal for welding. Wire and rod |
| BS EN 4007:2005 | Aerospace series. Aluminium alloy AL-P6082-T6 or T62. Sheet and strip. 0,4 mm 3L a 3L 6 mm |
| BS EN 2684:2004 | Aerospace series. Aluminium alloy AL-P7010-T7651. Plate. 6 mm < a ≤ 140 mm |
| BS EN 3971:2006 | Aerospace series. Steel FE-PL1507 (40CrMoV12). Consumable electrode remelted. Annealed. Forging stock. a or D ≤ 350 mm |
| BS EN 3934:2001 | Aerospace series. Nickel base alloy NI-B21001 (NiCr15B4). Filler metal for brazing. Amorphous foil |
| BS EN 3999:2007 | Aerospace series. Aluminium alloy AL-P2024-T351. Sheet and strip with improved chemical milling capability 1,6 mm ≤ a ≤ 6 mm |
| BS EN 4211:2005 | Aerospace series. Aluminium alloy AL-P2024-T42. Clad plate. 6mm < a ≤ 25mm |
| BS EN 3889:2002 | Aerospace series. Steel FE-WM3801 (X5CrNiCu17-4). Filler metal for welding |
| BS EN 2047:2001 | Aerospace series. Beaded L-section extruded, in aluminium and aluminium alloys. Dimensions |
| BS EN 4180:2002 | Aerospace series. Circular tubes, for fluids in titanium and titanium alloys. Wide tolerances. Diameter 4 mm ≤ D ≤ 40 mm. Dimensions |
| BS EN 4314:2007 | Aerospace series. Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15). Non heat treated, forging stock a or D ? 250 mm |
| BS EN 3895:2001 | Aerospace series. Heat resisting alloy NI-WH3901 (NiCr16Mo15). Filler metal for welding |
| BS EN 4329:2001 | Aerospace series. Heat resisting alloy NI-WH0001 (NiCr20). Filler metal for welding. Wire and rod |
| BS EN 4338:2001 | Aerospace series. Heat resisting alloy. NI-WH3902 (NiCr25Mo10C). Filler metal for welding. Wire and rod |
| BS EN 4005:2007 | Aerospace series. Aluminium alloy AL-P5052-O. Sheet and strip 0,3 mm ≤ a ≤ 6 mm |
| BS EN 3553:2004 | Aerospace series. Aluminium alloy AL-P2618A-T6511. Extruded bar and section. a or D ≤ 160 mm |
| BS EN 3946:2001 | Aerospace series. Nickel base alloy NI-B15701 (NiPd34Au30). Filler metal for brazing. Powder or paste |
| BS EN 3953:2001 | Aerospace series. Silver base alloy AG-B12401 (AgCu40Zn5Ni). Filler metal for brazing. Wire |
| 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 |
| BS EN 4449:2005 | Aluminium alloy AL-P7050. T76. Sheet. 0,8 mm ≤ a ≤ 6 mm |
| BS EN 4336:2002 | Aerospace series. Steel FE-WA3801 (X4CrNiMn20-10-2). Filler metal for welding. Wire and rod |
| BS EN 4213:2005 | Aerospace series. Aluminium alloy AL-P6061-T651. Plate. 6mm |
| BS EN 3937:2001 | Aerospace series. Nickel base alloy NI-B44101 (NiW12Cr10Si4Fe3B3). Filler metal for brazing. Powder or paste |
| BS EN 4286:2005 | Aerospace series. Aluminium alloy AL-P8090-T89. Die forgings. a ≤ 125 mm |
| BS EN 3942:2001 | Aerospace series. Nickel base alloy NI-B41204 (NiCr13Si4B3). Filler metal for brazing. Borided foil |
| BS EN 3998:2007 | Aerospace series. Aluminium alloy AL-P2024-T4 or T42. Sheet and strip. 0,3 mm ≤ a ≤ 6 mm |
| BS EN 4058:2001 | Aerospace series. Filler rods and filler wires for welding in titanium and titanium alloys. Diameter 0,5 mm ≤ D ≤ 5,0 mm. Dimensions |
| BS EN 2693:2005 | Aerospace series. Aluminium alloy AL-P5086-H111. Sheet and strip. 0,3 mm ≤a ≤6 mm |
| BS EN 3944:1998 | Nickel base alloy NI-B41204 (NiCr13Si4B3). Filler metal for brazing. Tape |
| BS EN 3893:2001 | Aerospace series. Titanium alloy TI-W19001. Filler metal for welding |
| BS EN 4334:2002 | Aerospace series. Steel FE-WL1806 (15CrMnMoV5-4-9-3). Filler metal for welding. Wire and rod |
| BS EN 3842:2001 | Aerospace series. Circular tubes for fluids in corrosion resistant steel. Diameter 3,2 mm ≤ D ≤ 100 mm. Thickness 0,32 mm ≤ a ≤ 2,5 mm. Dimensions |
| BS EN 4215:2005 | Aerospace series. Aluminium alloy AL-P7175-T651. Plate. 6 mm |
| BS EN 4337:2001 | Aerospace series. Heat resisting alloy NI-WH8901 (NiCr16Ti3Mn2). Filler metal for welding. Wire and rod |
| BS EN 3474:2005 | Aerospace series. Aluminium alloy AL-P2024-T81. Sheet and strip. 0,25 mm ≤ a ≤ 6 mm |
| BS EN 3922:1998 | Nickel base alloy NI-B41203 (NiCr7Si5B3). Filler metal for brazing. Borided foil |
| BS EN 3933:2001 | Aerospace series. Nickel base alloy NI-B13001 (NiP11). Filler metal for brazing. Powder or paste |
| BS EN 4004:2007 | Aerospace series. Aluminium alloy AL-P3103-H16. Sheet and strip. 0,4 mm ≤ a ≤ 6 mm |
| BS EN 3932:2001 | Aerospace series. Nickel base alloy NI-B13001 (NiP11). Filler metal for brazing. Amorphous foil |
| 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 |
| BS EN 2088:2005 | Aerospace series. Aluminium alloy AL-P2014A. T4 or T42. Clad sheet and strip. 0,4 mm ≤ a ≤ 6 mm |
| BS EN 2048:2001 | Aerospace series. Extruded L-section in aluminium alloys. Dimensions |
| BS EN 2599:2001 | Aerospace series. Strips in aluminium and aluminium alloys. Thickness 0,25 mm ≤ a ≤ 3.2 mm. Dimensions |
| BS EN 2087:2005 | Aerospace series. Aluminium alloy AL-P2014A. T6 or T62. Clad sheet and strip 0,4 mm ≤ a ≤ 6 mm |
| BS EN 3961:2001 | Aerospace series. Gold base alloy AU-B4000. Filler metal for brazing. Rolled foil |
| BS EN 3928:1998 | Nickel base alloy NI-B40001 (NiSi5B3). Filler metal for brazing. Tape |
| BS EN 3954:2001 | Aerospace series. Silver base alloy AG-B12401 (AgCu40Zn5Ni). Filler metal for brazing. Powder or paste |
| BS EN 3940:1998 | Nickel base alloy NI-B46001 (NiCo20Si5B3). Filler metal for brazing. Tape |
| BS EN 3886:2001 | Aerospace series. Heat resisting alloy NI-WH1303 (NiCo20Cr20Mo5Ti2Al). Filler metal for welding |
| BS EN 3531:2007 | Aerospace series. Steel FE-PM2701 (X2NiCoMo18-8-5). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Sheet and strip. a ≤ 6 mm. 1750 MPa ≤ Rm ≤ 2000 MPa |
| BS EN 4101:2005 | Aerospace series. Aluminium alloy AL-P2024-T4. Sheet and strip with improved stretch forming capability. 0,4 mm ≤ a ≤ 6 mm |
| BS EN 2078:2002 | Aerospace series. Metallic materials. Manufacturing schedule, inspection schedule, inspection and test report. Definition, general principles, preparation and approval |
| BS EN 4330:2002 | Aerospace series. Steel FE-WA4802 (X8CrNiMn27-22-2). Filler metal for welding. Wire and rod |
| BS EN 4450:2005 | Aerospace series. Aluminium alloy AL-P7050-T762. Sheet. 0,8 mm ≤a ≤6 mm |
| BS EN 3145:2002 | Round bars, hot rolled in steel. Normal tolerances. Diameter 6 mm ≤ D ≤ 250 mm. Dimensions |
| BS EN 3491:2006 | Aerospace series. Steel FE-PM3901 (X15CrNi17-3). Air melted. Hardened and tempered. Forgings. De ≤ 100 mm. 900 MPa ≤ Rm ≤ 1100 MPa |
| BS EN 4292:2005 | Aerospace series. Aluminium alloy AL-R39002. Forging stock |
| BS EN 4615:2005 | Aerospace series. Magnesium alloy MG-C18002. T4. Sand casting |
| BS EN 3888:2001 | Aerospace series. Heat resisting alloy CO-WH1402 (CoCr22Ni22W15). Filler metal for welding |
| BS EN 3897:2002 | Aerospace series. Steel FE-WA4801 (X6CrNiMnNb18-10). Filler metal for welding |
| BS EN 4102:2005 | Aerospace series. Aluminium alloy AL-P2219-T81. Clad sheet and strip. 0,5 mm ≤a ≤6 mm |
| BS EN 4287:2005 | Aerospace series. Aluminium alloy AL-P7010. Forging stock |
| BS EN 3884:2001 | Aerospace series. Heat resisting alloy NI-WH2601 (NiCr19Nb5Mo3Ti). Filler metal for welding |
| BS EN 2046:2001 | Hexagonal bars, drawn, in aluminium and aluminium alloys. Tolerance class h 11. Width across flats 7 mm ≤ a ≤ 50 mm. Dimensions |
| BS EN 4291:2005 | Aerospace series. Aluminium alloy AL-P8090. Forging stock |
| BS EN 3507:2006 | Aerospace series. Steel FE-PL1501 (30CrMo12). Air melted. Hardened and tempered. Forgings. De ≤ 100 mm. 930 MPa ≤ Rm ≤ 1080 MPa |
| BS EN 2947:2006 | Aerospace series. Steel FE-PA3004 (X10CrNi18-09). Air melted. Non heat treated. Cold drawn wire. a or D ≤ 2,3 mm |
| BS EN 3948:1998 | Nickel base alloy NI-B15701 (NiPd34Au30). Filler metal for brazing. Wire |
| BS EN 3938:2001 | Aerospace series. Nickel base alloy NI-B46001 (NiCo20Si5B3) Filler metal for brazing. Amorphous foil |
| BS EN 3920:2001 | Aerospace series. Nickel base alloy NI-B41202 (NiCr14Fe5Si5B3). Filler metal for brazing. Powder or paste |
| BS EN 2632:2005 | Aerospace series. Aluminim alloy AL-P7075. T73511. Extruded bar and section. a or D ≤ 150 mm with peripheral coarse grain control |
| 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 |
| BS EN 2694:2005 | Aerospace series. Aluminium alloy AL-P6061-T6 or T62. Sheet and strip. 0,4 mm ≤ a ≤ 6 mm |
| BS EN 2696:2005 | Aerospace series. Aluminium alloy AL-P7075-T6 or T62. Sheet and strip. 0,4 mm ≤a ≤6 mm |
| BS EN 4325:2001 | Aerospace series. Heat resisting alloy NI-WH1302 (NiCr20Co13Mo4Ti3AI). Filler metal for welding. Wire and rod |
| BS EN 3957:2001 | Aerospace series. Silver base alloy AG-B14001 (AgCu42Ni2). Filler metal for brazing. Powder or paste |
| BS EN 4104:2001 | Aerospace series. Nickel base alloy NI-B40002. Filler metal for brazing. Powder or paste. |
| EN 2482 : 2010 | AEROSPACE SERIES - STEEL FE-PL2108 (36NICRMO16) - 1100 MPA <= R[M] <= 1300 MPA - BARS - D[E] <= 100 MM |
| EN 2512 : 2014 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7175 - T7351 - PLATE - 6 MM < A <= 100 MM |
| EN 4500-005:2012 | Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 005: Specific rules for steels |
| EN 3926:2001 | Aerospace series - Nickel base alloy NI-B40001 (NiSi5B3) - Filler metal for brazing - Borided foil |
| EN 3526:2007 | Aerospace series - Steel FE-PL1505 (15CrMoV6) - Air melted - Hardened and tempered - Sheet and strip - 0,5 mm ≤ a ≤ 6 mm - 980 MPa ≤ Rm ≤ 1 180 MPa |
| EN 3524:2007 | Aerospace series - Steel FE-PL1505 (15CrMoV6) - Air melted - Hardened and tempered - Sheet and strip - 2 mm ≤ a ≤ 6 mm - 1 080 MPa ≤ Rm ≤ 1 280 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 4211:2005 | Aerospace series - Aluminium alloy AL-P2024-T42 - Clad plate - 6 mm |
| EN 2802:2005 | Aerospace series - Aluminium alloy AL-P7475-T761 - Sheet and strip - 0,6 mm |
| EN 4800-003:2010 | Aerospace series - Titanium and titanium alloys - Technical specification - Part 003: Tube |
| EN 2439 : 2009 | AEROSPACE SERIES - STEEL FE-PL2102 (34NICR6) - 900 MPA <= R[M] <= 1100 MPA - FORGINGS - D[E] <= 40 MM |
| EN 4721 : 2014 | Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electroslag remelted (ESR) - Hardened and tempered - Bar - De ≤ 200 mm - 900 MPa ≤ Rm ≤ 1 050 MPa |
| EN 4470:2007 | Aerospace series - Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D ≤ 150 mm - Rm ≥ 1 200 MPa |
| EN 4293 : 2014 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7175 - T73511 - EXTRUDED BAR AND SECTION - A OR D <= 150 MM |
| EN 2046 : 2001 | AEROSPACE SERIES - HEXAGONAL BARS, DRAWN IN ALUMINIUM AND ALUMINIUM ALLOYS - TOLERANCE CLASS H 11 - WIDTH ACROSS FLATS 7 MM <= A <= 50 MM - DIMENSIONS |
| EN 4105:1998 | Aerospace series - Nickel base alloy NI-B40002 (NiSi4B2) - Filler metal for brazing - Tape |
| EN 2446 : 2008 | AEROSPACE SERIES - STEEL FE-PL1503 (35CRMO4) - 1100 MPA <= R[M] <= 1300 MPA - BARS - D[E] <= 25 MM |
| EN 3925:2001 | Aerospace series - Nickel base alloy NI-B40001 (NiSi5B3) - Filler metal for brazing - Amorphous foil |
| EN 3456:2012 | Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Sheet and strip, hot rolled — a ≤ 6 mm |
| EN 4286:2005 | Aerospace series - Aluminium alloy AL-P8090-T89 - Die forgings - a |
| EN 4098:2007 | Aerospace series - Steel FE-PL1507 (40CrMoV12) - Remelted, hardened and tempered, forgings De ≤ 50 mm, 1 250 MPa ≤ Rm ≤ 1 400 MPa |
| EN 4324:2001 | Aerospace series - Aluminium alloy AL-W42201 - Filler metal for welding - Rod |
| EN 2438 : 2008 | Aerospace series - Steel FE-PL2102 (35NiCr6) - 900 MPa ≤ Rm ≤ 1 100 MPa - Bars - De ≤ 40 mm |
| EN 3923:2001 | Aerospace series - Nickel base alloy NI-B41203 (NiCr7Si5B3Fe3) - Filler metal for brazing - Powder or paste |
| EN 4006:2007 | Aerospace series - Aluminium alloy AL-P6082-T4 or T42 - Sheet and strip 0,4 mm ≤ a ≤ 6 mm |
| EN 4287:2005 | Aerospace series - Aluminium alloy AL-P7010 - Forging stock |
| EN 4329:2001 | Aerospace series - Heat resisting alloy NI-WH0001 (NiCr20) - Filler metal for welding - Wire and rod |
| 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 3488:2007 | AEROSPACE SERIES - STEEL FE-PA3601 (X6CRNITI18-10) - AIR MELTED - SOFTENED - SHEET AND STRIP - A <= 6 MM - 500 MPA <= R[M] <= 700 MPA |
| EN 4800-002:2010 | Aerospace series - Titanium and titanium alloys - Technical specification - Part 002: Bar and section |
| EN 2033:2017 | Aerospace series - Strips, cold rolled in steel, Thickness 0,1 mm ≤ a ≤ 2,5 mm - Dimensions |
| EN 2818:2009 | Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D ≤ 200 mm - Rm ≥ 1 070 MPa |
| EN 3928:1998 | Aerospace series - Nickel base alloy NI-B40001 (NiSi5B3) - Filler metal for brazing - Tape |
| EN 4376:2016 | Aerospace series - Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) solution treated and precipitation treated - Bar and section, De ≤ 200 mm |
| EN 3932:2001 | Aerospace series - Nickel base alloy NI-B13001 (NiP11) - Filler metal for brazing - Amorphous foil |
| EN 4800-001:2010 | Aerospace series - Titanium and titanium alloys - Technical specification - Part 001: Plate, sheet and strip |
| EN 3355 : 2012 | Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Extruded section - De ≤ 150 mm - 900 MPa ≤ Rm ≤ 1 160 MPa |
| 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 3936:2001 | Aerospace series - Nickel base alloy NI-B21001 (NiCr15B4) - Filler metal for brazing - Powder or paste |
| EN 3531:2007 | Aerospace series - Steel FE-PM2701 (X2NiCoMo18-8-5) - Vacuum induction melted and vacuum arc remelted - Solution treated and precipitation treated - Sheet and strip - a ≤ 6 mm - 1 750 MPa ≤ Rm ≤ 2 000 MPa |
| EN 3464:2012 | Aerospace series - Titanium alloy Ti-6Al-4V - Annealed - Plate - 6 mm < a ≤ 100 mm |
| EN 4466:2007 | Aerospace series - Steel FE-PM1506 (X5CrNiMoAl13-8-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D ≤ 150 mm - Rm ≥ 1 400 MPa |
| EN 2695:2005 | Aerospace series - Aluminium alloy AL-P6081-T6 - Sheet and strip - 0,3 mm |
| EN 3335 : 2005 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7475 - O2 - SHEET FOR SUPERPLASTIC FORMING (SPF) - 0,8 MM <= A <= 6 MM |
| EN 3999:2007 | Aerospace series - Aluminium alloy AL-P2024-T351 - Sheet and strip with improved chemical milling capability 1,6 mm ≤ a ≤ 6 mm |
| EN 4631:2013 | Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bar - De ≤ 200 mm - 900 MPa ≤ Rm ≤ 1 050 MPa |
| EN 3943:2001 | Aerospace series - Nickel base alloy NI-B41204 (NiCr13Fe4Si4B3) - Filler metal for brazing - Powder or paste |
| EN 4335:2002 | Aerospace series - Steel FE-WA2602 (X4NiCrTiMoV26-15) - Filler metal for welding - Wire and rod |
| EN 4526:2013 | Aerospace series - Metallic materials - Test methods - Sharp edge-notch tensile testing for sheet and strip |
| 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 - Rm ≥ 1 400 MPa |
| EN 3882:2001 | Aerospace series - Heat resisting alloy NI-WH1801 (NiCr20Co18Ti3Al2) - Filler metal for welding |
| EN 2087:2005 | Aerospace series - Aluminium alloy AL-P2014A - T6 or T62 - Clad sheet and strip - 0,4 mm |
| EN 3956:2001 | Aerospace series - Silver base alloy AG-B14001 (AgCu42Ni2) - Filler metal for brazing - Wire |
| 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 3892:2001 | Aerospace series - Titanium alloy TI-W64001 - Filler metal for welding |
| EN 2085 : 2004 | Aerospace series - Aluminium alloy AL-P2618A - T6 - Hand and die forgings - a |
| EN 4372:2009 | Aerospace series - Heat resisting nickel alloy with copper NI-PD9001 (NiCu31) - Wire for solid rivets - D ≤ 10 mm |
| EN 4465:2007 | Aerospace series - Steel FE-PM1506 (X5CrNiMoAl13-8-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D ≤ 150 mm - Rm ≥ 1 300 MPa |
| EN 2032-001:2014 | Aerospace series - Metallic materials - Part 001: Conventional designation |
| EN 2543 : 2009 | AEROSPACE SERIES - STEEL FE-PL1502 (25CRMO4) - ANNEALED - SHEET AND STRIP - 0,3 MM <= A <= 2 MM - FOR PREVAILING TORQUE NUTS |
| EN 4384:2007 | Aerospace series - Heat resisting alloy NI-CH1303 (NiCo20Cr20Mo5Ti2Al) - Non heat treated - Remelting stock |
| EN 2209 : 2008 | AEROSPACE SERIES - STEEL FE-PL1502 (25CRMO4) - 900 MPA <= R[M] <= 1100 MPA - SHEETS, STRIPS AND PLATES - 0,5 MM <= A <= 20 MM |
| EN 4449:2005 | Aerospace series - Aluminium alloy AL-P7050 - T76 - Sheet - 0,8 mm |
| EN 2395:2005 | Aerospace series - Aluminium alloy AL-P2014A-T4 or T42 - Sheet and strip - 0,4 mm |
| EN 4000:2001 | Aerospace series - Metallic materials - Rules for the drafting and presentation of dimensional standards for metallic semi-finished products |
| EN 4340:2002 | Aerospace series - Magnesium alloy MG-W68001 - Filler metal for welding - Wire and rod |
| EN 2032-1 : 2001 | AEROSPACE SERIES - METALLIC MATERIALS - PART 1: CONVENTIONAL DESIGNATION |
| EN 3935:2001 | Aerospace series - Nickel base alloy NI-B21001 (NiCr15B4) - Filler metal for brazing - Borided foil |
| EN 4379:2007 | Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Solution treated, forging De ≤ 200 mm |
| EN 3954:2001 | Aerospace series - Silver base alloy AG-B12401 (AgCu40Zn5Ni) - Filler metal for brazing - Powder or paste |
| EN 4344:2001 | Aerospace series - Steel FE-WM1002 (X13Cr13) - Filler metal for welding - Wire and rod |
| EN 3965:2001 | Aerospace series - Titanium alloy TI-B17001 - Filler metal for brazing - Rolled foil |
| EN 4700-005:2010 | Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 005: Forging stock |
| EN 4007:2005 | Aerospace series - Aluminium alloy AL-P6082-T6 or T62 - Sheet and strip - 0,4 mm |
| EN 4725:2014 | Aerospace series - Aluminium alloy AL-P2024- Al Cu4Mg1 - T351 - Plate - 6 mm < a ≤ 150 mm |
| EN 2694:2005 | Aerospace series - Aluminium alloy AL-P6061-T6 or T62 - Sheet and strip - 0,4 mm |
| EN 3997:2015 | Aerospace series - Aluminium alloy AL-P2024- Al Cu4Mg1 - T3 - Sheet and strip - 0,4 mm ≤ a ≤ 6 mm |
| EN 3896:2001 | Aerospace series - Steel FE-WM1501 (X13CrNiMoCo12-3-2-2) - Filler metal for welding |
| 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 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 2086 : 2004 | Aerospace series - Aluminium alloy AL-P2618A - T851 - Hand and die forgings - a |
| EN 2448 : 2008 | Aerospace series - Steel FE-PL1503 (35CrMo4) - 900 MPa ≤ Rm ≤ 1 100 MPa - Bars - De ≤ 40 mm |
| EN 2480 : 2008 | AEROSPACE SERIES - STEEL FE-PL2108 (36NICRMO16) - 1250 MPA <= R[M] <= 1400 MPA - BARS - D[E] <= 75 MM |
| EN 2803:2005 | Aerospace series - Aluminium alloy AL-P7475-T761 - Clad sheet and strip - 1,0 mm |
| EN 4615:2005 | Aerospace series - Magnesium alloy MG-C18002 - T4 - Sand casting |
| EN 3893:2001 | Aerospace series - Titanium alloy TI-W19001 - Filler metal for welding |
| EN 3919:1998 | Aerospace series - Nickel base alloy NI-B41202 (NiCr14Si5B3) - Filler metal for brazing - Amorphous foil |
| EN 4214:2005 | Aerospace series - Aluminium alloy AL-P7010-T651 - Plate - 6 mm |
| EN 3922:1998 | Aerospace series - Nickel base alloy Ni-B41203 (NiCr7Si5B3) - Filler metal for brazing - Borided foil |
| EN 3930:2001 | Aerospace series - Nickel base alloy NI-B31001 (NiCr19Si10) - Filler metal for brazing - Powder or paste |
| EN 3924:1998 | Aerospace series - Nickel base alloy NI-B41203 (NiCr7Si5B3) - Filler metal for brazing - Tape |
| EN 3359:2007 | Aerospace series - Steel FE-PM1503 (X3CrNiMoAl13-8-2) - Vacuum induction melted and consumable electrode remelted, softened, forging stock a or D ≤ 300 mm |
| EN 2632:2005 | Aerospace series - Aluminium alloy AL-P7075 - T73511 - Extruded bar and section - a or D |
| EN 2460 : 2009 | AEROSPACE SERIES - STEEL FE-PM1901 (X12CRNI13) - 600 MPA <= R[M] <= 800 MPA - BARS - D[E] <= 70 MM |
| EN 4213:2005 | Aerospace series - Aluminium alloy AL-P6061-T651 - Plate - 6 mm |
| EN 3469 : 2009 | AEROSPACE SERIES - STEEL FE-PM1802 (X5CRNICU15-5) - CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 200 MM - R[M] >= 1310 MPA |
| EN 2399 : 2008 | AEROSPACE SERIES - HEAT RESISTING STEEL FE-PA2601 (X4NICRTIMOV26-15) - R[M] >= 900 MPA - BARS FOR FORGED BOLTS - D <= 25 MM |
| EN 4002:2007 | Aerospace series - Aluminium alloy AL-P2219-T81 - Sheet and strip 0,5 mm ≤ a ≤ 6 mm |
| EN 4333:2002 | Aerospace series - Steel FE-WA4902 (X5CrNiCoMoWMn21-20-20-3-3-2) - Filler metal for welding - Wire and rod |
| EN 2002-001:2005 | Aerospace series - Metallic materials - Test methods - Part 1: Tensile testing at ambient temperature |
| EN 2622 : 2001 | AEROSPACE SERIES - CIRCULAR TUBES, FOR FLUIDS IN HEAT RESISTING ALLOYS - DIAMETER 3,2 MM <= D <= 100 MM - DIMENSIONS |
| EN 2461 : 2009 | AEROSPACE SERIES - STEEL FE-PM1901 (X12CRNI13) - 600 MPA <= R[M] <= 800 MPA - FORGINGS - D[E] <= 70 MM |
| EN 4338:2001 | Aerospace series - Heat resisting alloy NI-WH3902 (NiCr25Mo10C) - Filler metal for welding - Wire and rod |
| EN 4099:2005 | Aerospace series - Aluminium alloy AL-P2219-T6 or T62 - Clad sheet and strip - 0,5 mm |
| EN 4202:2005 | Aerospace series - Aluminium alloy AL-P6082-T651 - Plate - 6 mm |
| EN 3163:2007 | Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted, softened, forging stock a or D ≤ 300 mm |
| EN 3120 : 2012 | Aerospace series - Titanium alloy TI-P64003 - Cold worked and stress relieved - Seamless tube for pressure systems - 4 mm ≤ D ≤ 51 mm - 690 MPa ≤ Rm ≤ 1 030 MPa |
| EN 2693:2005 | Aerospace series - Aluminium alloy AL-P5086-H111 - Sheet and strip - 0,3 mm |
| EN 4003:2006 | Aerospace series - Aluminium alloy AL-P2219-T87 - Sheet and strip 0,5 mm ≤ a ≤ 6 mm |
| EN 3887:2001 | Aerospace series - Heat resisting alloy CO-WH4101 (CoCr20W15Ni) - Filler metal for welding |
| EN 4180:2001 | Aerospace series - Circular tubes, for fluids in titanium and titanium alloys - Wide tolerances<br /><br />Diameter 4 mm < D < 40 mm - Dimensions |
| EN 2050 : 2001 | AEROSPACE SERIES - EXTRUDED T-SECTION, IN ALUMINIUM ALLOYS - DIMENSIONS |
| EN 4700-003:2010 | Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 003: Tube |
| EN 3114-001:2006 | Aerospace series - Test method - Microstructure of (α + β) titanium alloy wrought products - Part 001: General requirements |
| EN 3146:2001 | Aerospace series - Round bars, hot rolled in steel - Close tolerances - Diameter 6 mm < = D < = 250 mm - Dimensions |
| EN 3344 : 2005 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7050 - T76511 - EXTRUDED BAR AND SECTION - A OR D <= 150 MM WITH PERIPHERAL COARSE GRAIN CONTROL |
| EN 3884:2001 | Aerospace series - Heat resisting alloy NI-WH2601 (NiCr19Nb5Mo3Ti) - Filler metal for welding |
| 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 3476 : 2006 | AEROSPACE SERIES - STEEL FE-PL1501 (30CRMO12) - AIR MELTED - SOFTENED - FORGING STOCK - A OR D <= 300 MM |
| EN 4215:2005 | Aerospace series - Aluminium alloy AL-P7175-T651 - Plate - 6 mm |
| EN 3931:1998 | Aerospace series - Nickel base alloy NI-B31001 (NiCr19Si10) - Filler metal for brazing - Tape |
| EN 4382:2006 | Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Solution treated - Seamless tubes - For hydraulic application - D ≤ 50 mm, a ≤ 3 mm |
| EN 2048 : 2001 | AEROSPACE SERIES - EXTRUDED L-SECTION, IN ALUMINIUM ALLOYS - DIMENSIONS |
| EN 3342 : 2005 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6061 - T4 OR T42 - DRAWN OR EXTRUDED BAR AND SECTION - A OR D <= 150 MM |
| EN 2117 : 2009 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P5056A (5056A)-H32 - WIRE FOR SOLID RIVETS - D <= 10 MM |
| EN 4325:2001 | Aerospace series - Heat resisting alloy NI-WH1302 (NiCr20Co13Mo4Ti3AI) - Filler metal for welding - Wire and rod |
| EN 4317:2007 | Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Non heat treated, forging stock a or D ≤ 200 mm |
| EN 4464:2007 | Aerospace series - Steel FE-PM1506 (X5CrNiMoAl13-8-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D ≤ 150 mm - Rm ≥ 1 200 MPa |
| EN 2635 : 2005 | Aerospace series - Aluminium alloy AL-P2014A - T6511 - Extruded bar and section - a or D |
| EN 2257 : 1997 | AEROSPACE SERIES - CIRCULAR TUBES FOR STRUCTURES IN ALUMINIUM AND ALUMINIUM ALLOYS - DIAMETER 6 MM <= D <= 100 MM - THICKNESS 1 MM <= A <= 6 MM - DIMENSIONS |
| EN 3938:2001 | Aerospace series - Nickel base alloy NI-B46001 (NiCo20Si5B3) - Filler metal for brazing - Amorphous foil |
| EN 4341:2001 | Aerospace series - Aluminium alloy AL-W46431 - Filler metal for welding - Wire and rod |
| EN 2278 : 2014 | AEROSPACE SERIES - STEEL X12CRNIMOV12-3 (1.4933) - 900 MPA <= R[M] <= 1100 MPA - BARS - D[E] <= 150 MM |
| 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 2115:2009 | Aerospace series - Aluminium alloy 2117-T42 - Wire for solid rivets - D ≤ 10 mm |
| EN 3982:2015 | Aerospace series - Aluminium alloy AL-P7050 - AlZn6CuMgZr - T7451 - Plates - 6 mm < a ≤ 160 mm |
| EN 3532:2007 | Aerospace series - Steel FE-PM2701 (X2NiCoMo18-8-5) - Vacuum induction melted and vacuum arc remelted - Solution treated and precipitation treated - Plate - 6 mm < a ≤ 40 mm - 1 750 MPa ≤ Rm ≤ 2 000 MPa |
| EN 2478:2008 | Aerospace series - Steel FE-PL2107 (30NiCrMo16) - 1 220 MPa ≤ Rm ≤ 1 370 MPa - Bars - De ≤ 40 mm |
| EN 2687:2004 | Aerospace series - Aluminium alloy AL-P7010- - T7451 - Plate - 6 mm < a |
| EN 3964:2001 | Aerospace series - Copper CU-BU9001 - Filler metal for brazing - Wire |
| 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 3890:2001 | Aerospace series - Steel FE-WM1502 (X11CrNiMoVN12-3) - Filler metal for welding |
| 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 3145:2001 | Aerospace series - Round bars, hot rolled in steel - Normal tolerances - Diameter 6 mm < D < 250 mm - Dimensions |
| EN 2066 : 2001 | AEROSPACE SERIES - EXTRUDED SECTION IN ALUMINIUM ALLOYS - GENERAL TOLERANCES |
| EN 2134 : 2001 | AEROSPACE SERIES - ROUND BARS, EXTRUDED IN ALUMINIUM AND ALUMINIUM ALLOYS - DIAMETER 10 MM <= D <= 220 MM DIMENSIONS |
| EN 4343:2002 | Aerospace series - Steel FE-WM1001 (X13Cr12) - Filler metal for welding - Wire and rod |
| EN 2467:2007 | AEROSPACE SERIES - STEEL FE-PA3901 (X2CRNI18-9) - AIR MELTED - SOFTENED - PLATE, SHEET AND STRIP - 0,4 MM <= A <= 20 MM - 520 MPA <= R[M] <= 670 MPA |
| EN 2226 : 2014 | AEROSPACE SERIES - STEEL X105CRMO17 (1.4125) - HARDENED AND TEMPERED - HAND AND DIE FORGINGS - D[E] <= 150 MM |
| EN 3927:2001 | Aerospace series - Nickel base alloy NI-B40001 (NiSi5B3) - Filler metal for brazing - Powder or paste |
| EN 3361:2007 | Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted, solution treated and precipitation treated, sheet and strip a ≤ 6mm, 1 070 MPa ≤ Rm ≤ 1 220 MPa |
| EN 2702:2005 | Aerospace series - Aluminium alloy AL-P6061 - T6 or T62 - Drawn or extruded bar and section - a or D |
| EN 2599:2001 | Aerospace series - Strips in aluminium and aluminium alloys - Thickness 0,25 mm < a < 3,2 mm - Dimensions |
| EN 2030:2013 | Aerospace series - Steel X105CrMo17 (1.3544) - Hardened and tempered - Bars - De ≤ 150 mm |
| EN 4247:2005 | Aerospace series - Aluminium alloy AL-P2024-T42 - Plate - 6 mm |
| EN 4383:2006 | Aerospace series - Heat resisting alloy NI-CH2601 (NiCr19Fe19Nb5Mo3) - Non heat treated - Remelting stock |
| EN 2573:2007 | Aerospace series - Steel FE-PA3601 (X6CrNiTi18-10) - Softened - Rm ≤ 780 MPa - Wire - 0,25 mm ≤ De ≤ 3 mm |
| EN 3351 : 2012 | AEROSPACE SERIES - TITANIUM ALLOY TI-4AL-4MO-2SN - SOLUTION TREATED AND AGED - FORGINGS - D[E] <= 150 MM |
| EN 2617 : 2001 | AEROSPACE SERIES - PLATES IN TITANIUM AND TITANIUM ALLOYS - THICKNESS 6 MM < A <= 100 MM - DIMENSIONS |
| EN 3937:2001 | Aerospace series - Nickel base alloy NI-B44101 (NiW12Cr10Si4Fe3B3) - Filler metal for brazing - Powder or paste |
| EN 3941:2001 | Aerospace series - Nickel base alloy NI-B41204 (NiCr13Si4B3) - Filler metal for brazing - Amorphous foil |
| EN 4291:2005 | Aerospace series - Aluminium alloy AL-P8090 - Forging stock |
| EN 4331:2002 | Aerospace series - Steel FE-WL1804 (25CrMnMo4-2-2) - Filler metal for welding - Wire and rod |
| EN 3895:2001 | Aerospace series - Heat resisting alloy NI-WH3901 (NiCr16Mo15) - Filler metal for welding |
| EN 4328:2002 | Aerospace series - Steel FE-WM1601 (X18CrWNi13-3-2) - Filler metal for welding - Wire and rod |
| EN 3885:2001 | Aerospace series - Heat resisting alloy NI-WH3601 (NiCr22Mo9Nb4) - Filler metal for welding |
| EN 4045:2001 | Aerospace series - Capillary tubes, seamless in heat resisting alloys - Diameter 0,6 mm |
| EN 4342:2001 | Aerospace series - Titanium TI-W99001 - Filler metal for welding - Wire and rod |
| EN 3917:1998 | Aerospace series - Nickel base alloy NI-B41201 (NiCr14Si5B3C) - Filler metal for brazing - Powder or paste |
| 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 4528:2009 | Aerospace series - Steel FE-PA3903 (X10CrNi18-8) - Cold rolled - Strip for springs - a ≤ 3 mm - 1 250 MPa ≤ Rm ≤ 1 640 MPa |
| EN 3528 : 2013 | AEROSPACE SERIES - STEEL X2NICOMO18-8-5 (1.6359) - VACUUM INDUCTION MELTED AND VACUUM ARC REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BAR - A OR D <= 150 MM - 1750 MPA <= R[M] <= 2000 MPA |
| EN 4670:2010 | Aerospace series - Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) - Vacuum induction melted and consumable electrode remelted - Softened - Forging stock - a or D ≤ 300 mm |
| EN 4500-004:2012 | Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 004: Specific rules for titanium and titanium alloys |
| EN 3668:2006 | Aerospace series - Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9) - Non heat treated - Forging stock - a or D ≤ 250 mm |
| EN 3553 : 2004 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2618A - T6511 - EXTRUDED BAR AND SECTION - A OR D <= 160 MM |
| 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 <= 150 MM - 1750 MPA <= R[M] <= 2000 MPA |
| EN 4263:2013 | Aerospace series - Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20) - As forged - Forging stock - a or D ≤ 200 mm - 690 MPa ≤ Rm ≤ 960MPa |
| EN 3888:2001 | Aerospace series - Heat resisting alloy CO-WH1402 (CoCr22Ni22W15) - Filler metal for welding |
| EN 4500-001:2012 | Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 001: General rules |
| EN 2047 : 2001 | AEROSPACE SERIES - BEADED L-SECTION EXTRUDED, IN ALUMINIUM ALLOYS - DIMENSIONS |
| EN 4450:2005 | Aerospace series - Aluminium alloy AL-P7050-T762 - Sheet - 0,8 mm |
| 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 4267:2001 | Aerospace series - Round bars in titanium and titanium alloys - Diameter 6 mm < = D < = 160 mm - <br /><br />Dimensions |
| EN 3983:2013 | Aerospace series - Aluminium alloy AL-P7050- - T7651 - Plate - 6 mm < a ≤ 160 mm |
| EN 4500-003:2012 | Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 003: Specific rules for heat resisting alloys |
| EN 4250:2001 | Aerospace series - Nickel base alloys NI-B41001 (NiCr19Si7B) - Filler metal for brazing - Amorphous foil |
| EN 4700-007:2010 | Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 007: Remelting stock |
| EN 2402:2014 | Aerospace series - Heat resisting nickel base alloy NiCr20Co3Fe3 - Annealed - Wire - D ≤ 10 mm |
| EN 3920:2001 | Aerospace series - Nickel base alloy NI-B41202 (NiCr14Fe5Si5B3) - Filler metal for brazing - Powder or paste |
| EN 4471:2007 | Aerospace series - Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D ≤ 150 mm - Rm ≥ 1 300 MPa |
| EN 2078:2001 | Aerospace series - Metallic materials - Manufacturing schedule, inspection schedule, inspection and test report - Definition, general principles, preparation and approval |
| EN 3341 : 2005 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6061 - T4 OR T42 - SHEET AND STRIP - 0.4 MM <= A <= 6 MM |
| EN 4059:2001 | Aerospace series - Filler rods and filler wires for welding in steel - Diameter 0,5 mm < D < 5,0 mm - Dimensions |
| EN 4334:2002 | Aerospace series - Steel FE-WL1806 (15CrMnMoV5-4-9-3) - Filler metal for welding - Wire and rod |
| EN 3813:2013 | Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bar and wire for forged fasteners - De ≤ 50 mm |
| EN 3364:2007 | Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted, softened, forging stock a or D ≤ 300 mm |
| EN 3976:2006 | Aerospace series - Titanium and titanium alloys - Test method - Chemical analysis for the determination of hydrogen content |
| EN 4629:2013 | Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Softened - Forging stock - De ≤ 300 mm |
| EN 2043:2013 | Aerospace series - Metallic materials - General requirements for semi-finished product qualification (excluding forgings and castings) |
| EN 2206 : 2008 | AEROSPACE SERIES - STEEL FE-PL1502 (25CRMO4) - 650 MPA <= R[M] <= 850 MPA - BARS - D[E] <= 150 MM |
| 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 3333 : 2005 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7475 - T762 - SHEET AND STRIP - 0,6 MM <= A <= 6 MM |
| EN 3894:2001 | Aerospace series - Heat resisting alloy NI-WD3201 (NiMo25Fe6Cr5) - Filler metal for welding |
| EN 3329 : 2009 | Aerospace series - Strips in aluminium and aluminium alloys - Thickness 0,25 mm < a < 3,2 mm - Dimensions |
| EN 3957:2001 | Aerospace series - Silver base alloy AG-B14001 (AgCu42Ni2) - Filler metal for brazing - Powder or paste |
| 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 4327:2001 | Aerospace series - Heat resisting alloy CO-WH1401 (CoCr26Ni11W8) - Filler metal for welding - Wire and rod |
| EN 2049 : 2001 | AEROSPACE SERIES - EXTRUDED CHANNEL SECTION, IN ALUMINIUM ALLOYS - DIMENSIONS |
| EN 3933:2001 | Aerospace series - Nickel base alloy NI-B13001 (NiP11) - Filler metal for brazing - Powder or paste |
| EN 3947:1998 | Aerospace series - Nickel base alloy NI-B15701 (NiPd34Au30) - Filler metal for brazing - Rolled foil |
| EN 2071 : 2001 | AEROSPACE SERIES - SHEETS IN ALUMINIUM AND ALUMINIUM ALLOYS - THICKNESS 0,25 MM <= A <= 6 MM - DIMENSIONS |
| EN 2003-010 : 2007 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TEST METHODS - PART 010: SAMPLING FOR DETERMINATION OF HYDROGEN CONTENT |
| EN 3330 : 2009 | AEROSPACE SERIES - STEEL FE-PL1503 (35CRMO4) - ANNEALED - BAR AND WIRE - D[E] <= 40 MM - FOR PREVAILING TORQUE NUTS |
| EN 2732:2005 | Aerospace series - Magnesium alloy MG-C46001-T6 - Chill casting |
| EN 3918:1998 | Aerospace series - Nickel base alloy NI-B41201 (NiCr14Si5B3C) - Filler metal for brazing - Tape |
| EN 2398 : 2008 | Aerospace series - Heat resisting steel FE-PA2601 (X6NiCrTiMoV26-15) - Rm ≥ 900 MPa - Bars for machined bolts - D ≤ 25 mm |
| 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 4216:2007 | Aerospace series - Steel FE-CM3801 (GX5CrNiCuNb16-4) - Homogenized, solution treated and precipitation hardened, investment casting De ≤ 50 mm, Rm ≥ 900 MPa |
| EN 3959:2001 | Aerospace series - Cobalt base alloy CO-B41601 (CoCr19Ni17Si8W4) - Filler metal for brazing - Powder or paste |
| EN 3347 : 2005 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024 - T8511 - EXTRUDED BAR AND SECTION - A OR D <= 150 MM WITH PERIPHERAL COARSE GRAIN CONTROL |
| EN 4336:2002 | Aerospace series - Steel FE-WA3801 (X4CrNiMn20-10-2) - Filler metal for welding - Wire and rod |
| EN 4102:2005 | Aerospace series - Aluminium alloy AL-P2219-T81 - Clad sheet and strip - 0,5 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 3339 : 2006 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7010- - T76 - DIE FORGINGS - A <= 200 MM |
| EN 3969:2006 | Aerospace series - Steel FE-PL1507 (40CrMoV12) - Air melted - Annealed - Forging stock - a or D ≤ 350 mm |
| EN 4800-004:2010 | Aerospace series - Titanium and titanium alloys - Technical specification - Part 004: Wire |
| EN 2258 : 1997 | AEROSPACE SERIES - CIRCULAR TUBES FOR FLUIDS IN ALUMINIUM AND ALUMINIUM ALLOYS - DIAMETER 3,2 MM <= D <= 100 MM - THICKNESS 0,6 MM <= A <= 2,5 MM - DIMENSIONS |
| EN 4683:2011 | Aerospace series - Steel FE-WM 3504 (X4CrNiMo16-5-1) - Air melted - Filler metal for welding - Wire and rod |
| EN 4060:2001 | Aerospace series - Filler rods and filler wires for welding in heat resisting alloys - Diameter 0,5 mm < = D < = 5,0 mm - Dimensions |
| EN 3491:2006 | Aerospace series - Steel FE-PM3901 (X15CrNi17-3) - Air melted - Hardened and tempered - Forgings - De ≤ 100 mm - 900 MPa ≤ Rm ≤ 1 100 MPa |
| EN 2116 : 2009 | AEROSPACE SERIES - ALUMINIUM ALLOY 2017A-T42 - WIRE FOR SOLID RIVETS - D <= 10 MM |
| EN 3115:2009 | Aerospace series - Aluminium alloy 7050-T73 - Wire for solid rivets — D ≤ 10 mm |
| EN 2072:2005 | Aerospace series - Aluminium AL-P1050A - H14 - Sheet and strip - 0,4 mm |
| EN 3354 : 2013 | AEROSPACE SERIES - TITANIUM ALLOY TI-6AL-4V - ANNEALED - SHEET FOR SUPERPLASTIC FORMING - A <= 6 MM |
| EN 3889:2001 | Aerospace series - Steel FE-WM3801 (X5CrNiCu17-4) - Filler metal for welding |
| 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 |
| 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 3332 : 2005 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7475 - T762 - CLAD SHEET AND STRIP - 1,0 MM <= A <= 6 MM |
| EN 2131 : 2001 | AEROSPACE SERIES - PLATES IN ALUMINIUM ALLOYS - THICKNESS 6 MM < A <= 160 MM DIMENSIONS |
| 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 |
| EN 2486 : 2005 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2618A - FORGING STOCK |
| EN 3552 : 2005 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2681A - T6 OR T62 - CLAD SHEET AND STRIP - 0.4 MM <= A <= 6 MM |
| 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 2092:2005 | Aerospace series - Aluminium alloy AL-P7075-T6 or T62 - Clad sheet and strip - 0,4 mm |
| EN 2088 : 2005 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2014A - T4 OR T42 - CLAD SHEET AND STRIP - 0,4 MM <= A <= 6 MM |
| EN 4628:2013 | Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bar - De ≤ 200 mm — 1 150 MPa ≤ Rm ≤ 1 300 MPa |
| EN 2542:2008 | Aerospace series - Steel FE-PL1502 (25CrMo4) - Annealed - Bar and wire - De ≤ 40 mm - For prevailing torque nuts |
| EN 3451 : 2017 | AEROSPACE SERIES - TITANIUM TI-P99002 - NOT HEAT TREATED - GRADE 2 FORGING STOCK, FOR ANNEALED FORGINGS - A OR D <= 300 MM |
| EN 3939:2001 | Aerospace series - Nickel base alloy NI-B46001 (NiCo20Si5B3) - Filler metal for brazing - Powder or paste |
| EN 2466 : 2009 | AEROSPACE SERIES - STEEL FE-PA3901 (X2CRNI19-11) - SOFTENED - FORGINGS - D[E] <= 100 MM |
| EN 2002-002 : 2005 | AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - PART 2: TENSILE TESTING AT ELEVATED TEMPERATURE |
| EN 3955:2001 | Aerospace series - Silver base alloy AG-B12401 (AgCu40Zn5Ni) - Filler metal for brazing - Rolled foil |
| EN 4377:2015 | Aerospace series - Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) - Non heat treated - Forging stock - a or D ≤ 300 mm |
| EN 3934:2001 | Aerospace series - Nickel base alloy NI-B21001 (NiCr15B4) - Filler metal for brazing - Amorphous foil |
| EN 4339:2001 | Aerospace series - Heat resisting alloy CO-WH4001 (CoCr29W9) - Filler metal for welding - Wire and rod |
| EN 4314:2007 | Aerospace series - Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) - Non heat treated, forging stock a or D ≤ 250 mm |
| EN 4058:2001 | Aerospace series - Filler rods and filler wires for welding in titanium and titanium alloys - Diameter 0,5 mm < = D < = 5,0 mm - Dimensions |
| EN 4209:2005 | Aerospace series - Aluminium alloy AL-P2219-T851 - Plate - 6 mm |
| EN 4001:2007 | Aerospace series - Aluminium alloy AL-P2024-T351 - Clad sheet and strip with improved chemical milling capability 1,6 mm ≤ a ≤ 6 mm |
| 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 2704:2015 | Aerospace series - Aluminium alloy AL-P2024 - AlCu4Mg1 - T3511 - Drawn bars - De ≤ 75 mm |
| EN 2483 : 2010 | AEROSPACE SERIES - STEEL FE-PL2108 (36NICRMO16) - 1100 MPA <= R[M] <= 1300 MPA - FORGINGS - D[E] <= 100 MM |
| EN 2344:2001 | Aerospace series - Round bars, machined in heat resisting alloys - Diameter 10 mm < = D < = 180 mm - Dimensions |
| EN 4657:2010 | Aerospace series - Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bars - a or D ≤ 200 mm - Rm ≥ 1 650 MPa |
| EN 2633:2015 | Aerospace series - Aluminium alloy AL-P2024 - AlCu4Mg1 - T3511 - Extruded bars and sections - 1,2 mm ≤ De ≤ 160 mm with peripheral coarse grain control |
| EN 4103:2001 | Aerospace series - Nickel base alloy NI-B40002 (NiSi4B2) - Filler metal for brazing - Borided foil |
| EN 2338 : 2001 | Aerospace series - Sheets, hot rolled in titanium and titanium alloys - Thickness 0,8 mm < = a < = 6 mm - Dimensions |
| 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 3979:2005 | Aerospace series - Aluminium alloy AL-P8090-O2 - Sheet for superplastic forming (SPF) - 0,8 mm < a < 6 mm |
| EN 3948:1998 | Aerospace series - Nickel base alloy NI-B15701 (NiPd34Au30) - Filler metal for brazing - Wire |
| 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 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 3365:2007 | Aerospace series - Steel FE-PM3901 (X15CrNi17-3) - Air melted, softened, forging stock a or D ≤ 300 mm |
| 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 2684:2004 | Aerospace series - Aluminium alloy AL-P7010- - T7651 - Plate - 6 mm < a |
| EN 3961:2001 | Aerospace series - Gold base alloy AU-B40001 - Filler metal for brazing - Rolled foil |
| EN 3962:2001 | Aerospace series - Gold base alloy AU-B40001 - Filler metal for brazing - Wire |
| EN 4800-008:2010 | Aerospace series - Titanium and titanium alloys - Technical specification - Part 008: Pre-production and production castings |
| EN 3940:1998 | Aerospace series - Nickel base alloy NI-B46001 (NiCoSi5B3) - Filler metal for brazing - Tape |
| EN 4332:2002 | Aerospace series - Steel FE-WL1805 (8CrMnMo12-4-9) - Filler metal for welding - Wire and rod |
| EN 3527:2007 | Aerospace series - Steel FE-PL1504 (33CrMoV12) - Air melted - Softened - Forging stock - a or D ≤ 300 mm |
| EN 4104:2001 | Aerospace series - Nickel base alloy NI-B40002 - Filler metal for brazing - Powder or paste |
| EN 4337:2001 | Aerospace series - Heat resisting alloy NI-WH8901 (NiCr16Ti3Mn3) - Filler metal for welding - Wire and rod |
| EN 3474:2005 | Aerospace series - Aluminium alloy AL-P2024-T81 - Sheet and strip - 0,25 mm |
| EN 4373:2007 | Aerospace series - Heat resisting alloy NI-PD9001 (NiCu31) - Annealed, seamless tube D ≤ 75 mm, a ≤ 3 mm |
| EN 4672:2011 | Aerospace series - Steel FE-PM1504 (X1CrNiMoAlTi12-10-2) - Vacuum induction melted and consumable electrode remelted - Softened - Forging stock - a or D ≤ 300 mm |
| EN 3971:2006 | Aerospace series - Steel FE-PL1507 (40CrMoV12) - Consumable electrode remelted - Annealed - Forging stock - a or D ≤ 350 mm |
| EN 2947:2006 | Aerospace series - Steel FE-PA3004 (X10CrNi18-09) - Air melted - Non heat treated - Cold drawn wire - a or D ≤ 2,3 mm |
| EN 4800-007:2010 | Aerospace series - Titanium and titanium alloys - Technical specification - Part 007: Remelting stock |
| EN 2681:2004 | Aerospace series - Aluminium alloy AL-P7010- - T74 - Hand and die forgings - a |
| 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 4656:2010 | Aerospace series - Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bars - a or D ≤ 200 mm - Rm ≥ 1520 MPa |
| EN 3816:2006 | Aerospace series - Steel FE-PA3601 (X6CrNiTi18-10) - Air melted - Softened and cold rolled - Sheet and strip a ≤ 3 mm - Rm ≥ 800 MPa |
| EN 4330:2002 | Aerospace series - Steel FE-WA4802 (X8CrNiMn27-22-2) - Filler metal for welding - Wire and rod |
| 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 4005:2007 | Aerospace series - Aluminium alloy AL-P5052-O - Sheet and strip 0,3 mm ≤ a ≤ 6 mm |
| EN 2205 : 2009 | Aerospace series - Steel FE-PL1502 (25CrMo4) - 900 MPa ≤ Rm ≤ 1 100 MPa - Bars - De ≤ 40 mm |
| EN 4212:2005 | Aerospace series - Aluminium alloy AL-P5086-H111 - Plate - 6 mm |
| EN 4100:2005 | Aerospace series - Aluminium alloy AL-P2219-T6 or T62 - Sheet and strip - 0,5 mm |
| EN 2339 : 2001 | AEROSPACE SERIES - SHEETS, COLD ROLLED IN TITANIUM AND TITANIUM ALLOYS - THICKNESS 0,2 MM <= A <= 6 MM - DIMENSIONS |
| EN 2044 : 2001 | AEROSPACE SERIES - ROUND BARS, DRAWN, IN ALUMINIUM AND ALUMINIUM ALLOYS - TOLERANCE CLASS H 11 - DIAMETER 4 MM <= D <= 63 MM - DIMENSIONS |
| EN 3162:2007 | Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted, solution treated and precipitation treated, sheet and strip a ≤ 6 mm, Rm ≥ 930 MPa |
| EN 4101:2005 | Aerospace series - Aluminium alloy AL-P2024-T4 - Sheet and strip with improved stretch forming capability - 0,4 mm |
| EN 4313:2005 | Aerospace series - Aluminium alloy AL-P6013-T6 - Sheet and strip - 0,5 mm |
| EN 3311:2009 | Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bar for machining - D < 110 mm |
| EN 2703:2005 | Aerospace series - Aluminium alloy AL-P2024-T4 or T42 - Clad sheet and strip - 0,3 mm |
| EN 3998:2007 | Aerospace series - Aluminium alloy AL-P2024-T4 or T42 - Sheet and strip 0,3 mm ≤ a ≤ 6 mm |
| EN 4800-005:2010 | Aerospace series - Titanium and titanium alloys - Technical specification - Part 005: Forging stock |
| EN 3952:2001 | Aerospace series - Silver base alloy AG-B10001 (AgCu28) - Filler metal for brazing - Wire |
| EN 4292:2005 | Aerospace series - Aluminium alloy AL-R39002 - Forging stock |
| EN 4700-004:2010 | Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 004: Wire |
| EN 3842:2001 | Aerospace series - Circular tubes for fluids in corrosion resistant steel - Diameter 3,2 mm < = D < = 100 mm - Thickness 0,32 mm < = a < = 2,5 mm - Dimensions |
| EN 4472:2007 | Aerospace series - Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D ≤ 150 mm - Rm ≥ 1 400 MPa |
| EN 3459 : 2010 | AEROSPACE SERIES - TITANIUM ALLOY TI-P63001 (TI-4AL-4MO-2SN) - SOLUTION TREATED AND AGED - PLATE - 6 MM < A <= 50 MM |
| EN 3963:2001 | Aerospace series - Copper CU-BU9001 - Filler metal for brazing - Rolled foil |
| EN 3946:2001 | Aerospace series - Nickel base alloy NI-B15701 (NiPd34Au30) - Filler metal for brazing - Powder or paste |
| EN 3973 : 2006 | Aerospace series - Steel FE-CM3801 (X5CrNiCuNb16-4) - Homogenized, solution treated and precipitation hardened - Investment casting - De ≤ 50 mm - Rm ≥ 1 030 MPa |
| EN 4700-001:2010 | Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 001: Plate, sheet and strip |
| EN 4203:2005 | Aerospace series - Aluminium alloy AL-P8090-T89 - Sheet - 0,6 mm |
| EN 4326:2001 | Aerospace series - Heat resisting alloy CO-WH4102 (CoCr28W20Ni5V1) - Filler metal for welding - Wire and rod |
| EN 3960:2001/AC:2002 | AEROSPACE SERIES - GOLD BASE ALLOY AU-B40001 (AUNI18) - FILLER METAL FOR BRAZING - POWDER OR PASTE |
| EN 3953:2001 | Aerospace series - Silver base alloy AG-B12401 (AgCu40Zn5Ni) - Filler metal for brazing - Wire |
| EN 3872:2005 | Aerospace series - Aluminium alloy AL-R39002-H112 - Die forgings - a |
| EN 4204:2005 | Aerospace series - Aluminium alloy AL-P8090 - T841 - Sheet - 0,6 mm |
| EN 4800-006:2010 | Aerospace series - Titanium and titanium alloys - Technical specification - Part 006: Pre-production and production forgings |
| EN 2422:2005 | Aerospace series - Aluminium alloy AL-P2124-T351 - Plate - 25 mm |
| EN 3506 : 2001 | Aerospace series - Hot rolled sheets and plates in heat resisting alloys - Thickness 2,0 mm < = a < = 100 mm - Dimensions |
| EN 4685:2011 | Aerospace series - Titanium Ti10V2Fe3Al - Bars - D < 110 mm - Rm ≥ 1 240 MPa |
| EN 4262:2013 | Aerospace series - Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20) - As forged - Forging stock - a or D ≤ 200 mm - 690 MPa ≤ Rm ≤ 880MPa |
| EN 2090 : 2005 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024 - T3 - CLAD SHEET AND STRIP 0,3 MM <= A <= 6 MM |
| EN 3942:2001 | Aerospace series - Nickel base alloy NI-B41204 (NiCr13Si4B3) - Filler metal for brazing - Borided foil |
| EN 4004:2007 | Aerospace series - Aluminium alloy AL-P3103-H16 - Sheet and strip 0,4 mm ≤ a ≤ 6 mm |
| EN 4616:2005 | Aerospace series - Magnesium alloy MG-C18002 - T4 - Chill casting |
| EN 2089:2005 | Aerospace series - Aluminium alloy AL-P2014A-T6 or T62 - Sheet and strip - 0,4 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 |
| EN 3480 : 2007 | AEROSPACE SERIES - STEEL FE-PA3601 (X6CRNITI18-10) - AIR MELTED - SOFTENED - PLATE - 6 MM < A <= 50 MM - 500 MPA <= R[M] <= 700 MPA |
| EN 4720:2014 | Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electroslag remelted (ESR) - Hardened and tempered - Bar - De ≤ 200 mm - 1 150 MPa ≤ Rm ≤ 1 300 MPa |
| EN 3886:2001 | Aerospace series - Heat resisting alloy NI-WH1303 (NiCo20Cr20Mo5Ti2Al) - Filler metal for welding |
| EN 2256 : 2004 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2618A - T852 - HAND AND DIE FORGINGS - A <= 150 MM |
| EN 4085:2001 | Aerospace series - Nickel base alloy NI-B40002 (NiSi4B2) - Filler metal for brazing - Amorphous foil |
| EN 4346:2007 | Aerospace series - Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) - Vacuum induction melted and consumable electrode remelted, softended, forging stock a or D ≤ 300 mm |
| EN 2481 : 2010 | AEROSPACE SERIES - STEEL FE-PL2108 (36NICRMO16) - 1250 MPA <= R[M] <= 1400 MPA - FORGINGS - D[E] <= 75 MM |
| 96/716592 DC : 0 | PREN 2304 - AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2601 (X6NICRTIMOV26-15) SOLUTION AND PRECIPITATION TREATED - FORGINGS D[E] <= 100 MM R[M] => 960 MPA |
| 06/30146149 DC : 0 | EN 4629 - AEROSPACE SERIES - STEEL FE-PM 3504 (X4CRNIMO16-5-1) - AIR MELTED HARDENED AND TEMPERED FORGING STOCK - DE = 300 MM |
| 07/30157997 DC : 0 | EN 2116 - AEROSPACE SERIES - ALUMINIUM ALLOY 2017A-T42 - WIRE FOR SOLID RIVETS - D <= 10 MM |
| BS EN 2002-1:2005 | Aerospace series. Metallic materials. Test methods Tensile testing at ambient temperature |
| 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 |
| 97/719257 DC : 0 | PREN 4294 - AEROSPACE SERIES - ALUMINIUM AL-P7175-T7354 - DIE FORGINGS - A <= 150 MM |
| BS EN 4800-008:2010 | Aerospace series. Titanium and titanium alloys. Technical specification Pre-production and production castings |
| 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 |
| BS EN 4293:2014 | Aerospace series. Aluminium alloy AL-P7175. T73511. Extruded bar and section. a or D ≤ 150 mm |
| NF EN 4346 : 2008 | AEROSPACE SERIES - STEEL FE-PM1505 (X1CRNIMOALTI12-9-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED, SOFTENDED, FORGING STOCK A OR D <= 300 MM |
| 17/30364761 DC : 0 | BS EN 2951 - AEROSPACE SERIES - METALLIC MATERIALS - TEST METHOD - MICROGRAPHIC DETERMINATION OF CONTENT OF NON-METALLIC INCLUSIONS |
| BS EN 2398:2008 | Aerospace series. Heat resisting steel FE-PA2601(X6NiCrTiMoV26-15). Rm ≥ 900 MPa. Bars for machined bolts. D ≤ 25 mm |
| 96/716603 DC : 0 | PREN 4368 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-CD1701 (NICO15CR10A16TI5MO3) AS CAST - REMELTING STOCK |
| UNI EN 3459 : 2011 | AEROSPACE SERIES - TITANIUM ALLOY TI-P63001 (TI-4AL-4MO-2SN) - SOLUTION TREATED AND AGED - PLATE - 6 MM < A <= 50 MM |
| 97/717254 DC : DRAFT OCT 1997 | PREN 4216 - AEROSPACE SERIES - STEEL FE-CM3801 (X5CRNICUNB16-4) - HOMOGENIZED, SOLUTION TREATED AND PRECIPITATION HARDENED - INVESTMENT CASTING D[E] <= 50 MM R[M] => 900 MPA |
| I.S. EN 3480:2007 | AEROSPACE SERIES - STEEL FE-PA3601 (X6CRNITI18-10) - AIR MELTED - SOFTENED - PLATE - 6 MM < A <= 50 MM - 500 MPA <= R[M] <= 700 MPA |
| BS EN 2115:2009 | Aerospace series. Aluminium alloy 2117-T42. Wire for solid rivets. D ≤ 10 mm |
| 98/712166 DC : DRAFT JULY 1998 | PREN 2702 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6061-T6 OR T62 - EXTRUDED BAR AND SECTION A OR D <= 150 MM |
| 97/719249 DC : DRAFT NOV 1997 | PREN 4282 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2219-T37 - PLATE - 6 MM <= A <= 40 MM |
| 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 3982:2015 | Aerospace series. Aluminium alloy AL-P7050. AlZn6CuMgZr. T7451. Plates. 6 mm < a ≤ 160 mm |
| I.S. EN 3310:2011 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - NOT HEAT TREATED - FORGING STOCK, FOR ANNEALED FORGINGS - D[E] <= 360 MM |
| I.S. EN 4500-005:2012 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 005: SPECIFIC RULES FOR STEELS |
| BS EN 4263:2013 | Aerospace series. Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20). As forged. Forging stock. a or D ≤ 200 mm - 690 MPa ≤ Rm ≤ 960MPa |
| 02/702972 DC : DRAFT FEB 2002 | EN 4203 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P8090-T89 - SHEET - 0,6 MM <= A <= 6 MM |
| BS EN 3354:2013 | Aerospace series. Titanium alloy Ti-6Al-4V. Annealed. Sheet for superplastic forming. a ≤ 6 mm |
| I.S. EN 4700-003:2010 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 003: TUBE |
| 97/700684 DC : DRAFT JAN 1997 | PREN 3018 - HEAT RESISTING ALLOY NI-PH2801 (NICR16FE7TI3NB1AL1) - CONSUMABLE ELECTRODE REMELTED - COLD DRAWN WIRE FOR THE MANUFACTURE OF THREAD INSERTS D <= 3 MM |
| BS EN 2467:2007 | Aerospace series. Steel FE-PA3901 (X2CrNi18-9). Air melted. Softened. Plate, sheet and strip. 0,4 mm ≤ a ≤ 20 mm. 520 MPa ≤ Rm ≤ 670 MPa |
| 06/30146674 DC : 0 | EN 3480 - AEROSPACE SERIES - STEEL FE-PA3601 (X6CRNITI18.10) AIR MELTED SOFTENED PLATE 6 |
| BS EN 2466:2009 | Aerospace series. Steel FE-PA3901 (X2CrNi19-11). Softened. Forgings. De ≤ 100 mm |
| BS EN 2117:2009 | Aerospace series. Aluminium alloy AL-P5056A (5056A)-H32. Wire for solid rivets. D ≤ 10 mm |
| BS EN 4376:2016 | Aerospace series. Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) solution treated and precipitation treated. Bar and section, De ≤ 200 mm |
| BS EN 4528:2009 | Aerospace series. Steel FE-PA 3903 (X10CrNi18-8). Cold rolled. Strip for springs. a ≤ 3 mm. 1250 MPa ≤ Rm ≤ 1640 MPa |
| 01/716454 DC : DRAFT JAN 2002 | PREN 2695 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6081 - T6 - SHEET AND STRIP - 0,3 MM < A < 6 MM |
| BS EN 4700-007:2010 | Aerospace series. Steel and heat resisting alloys. Wrought products. Technical specification Remelting stock |
| 11/30243873 DC : 0 | BS EN 8.4554 - AEROSPACE SERIES - COPPER ALLOY CUBE 1.9 - SHEET AND STRIP |
| 11/30243861 DC : 0 | BS EN 4627 - AEROSPACE SERIES - STEEL FE-PM 3504 (X4CRNIMO16-5-1) - AIR MELTED - HARDENED AND TEMPERED - FORGINGS - D[E] <= 200 MM - 1150 MPA <= R[M] <= 1300 MPA |
| I.S. EN 4800-003:2010 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 003: TUBE |
| NF EN 4372 : 2009 | AEROSPACE SERIES - HEAT RESISTING NICKEL ALLOY WITH COPPER NI-PD9001 (NICU31) - WIRE FOR SOLID RIVETS - D <= 10 MM |
| UNI EN 2032-001 : 2014 | AEROSPACE SERIES - METALLIC MATERIALS - PART 001: CONVENTIONAL DESIGNATION |
| 95/715396 DC : 0 | PREN 4261-5 - AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF TEST METHOD STANDARDS - PART 5: SPECIFIC REQUIREMENTS FOR MACROGRAPHIC AND MICROGRAPHIC EXAMINATION METHOD STANDARD |
| NF EN 4657 : 2011 | AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION REMELTED - BARS - A OR D < OR = 200 MM - R[M] > OR = 1650 MPA |
| BS EN 4683:2011 | Aerospace series. Steel FE-WM 3504 (X4CrNiMo16-5-1). Air melted. Filler metal for welding. Wire and rod |
| 96/716594 DC : 0 | PREN 2405 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2601 (NICR19FE19NB5MO3) SOLUTION AND PRECIPITATION TREATED - FORGINGS D[E] <= 200 MM |
| UNI EN 4672 : 2012 | AEROSPACE SERIES - STEEL FE-PM1504 (X1CRNIMOALTI12-10-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOFTENED - FORGING STOCK - A OR D <= 300 MM |
| 02/702913 DC : 0 | PREN 3980 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P8090-T62 - SHEET - 0,6 MM <= A <= 6 MM |
| 06/30146152 DC : 0 | EN 4630 - AEROSPACE SERIES - STEEL FE-PM 3504 (X4CRNIMO16-5-1) - AIR MELTED HARDENED AND TEMPERED FORGINGS - DE = 200 MM 900 MPA = RM = 1 050 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 |
| 11/30243872 DC : 0 | BS EN 8.4553 - AEROSPACE SERIES - COPPER ALLOY CUBE 1.9 - BARS |
| BS EN 2461:2009 | Aerospace series. Steel FE-PM1901 (X12CrNi13). 600 MPa ≤ Rm ≤ 800 MPa. Forgings. De ≤ 70 mm |
| BS EN 2278:2014 | Aerospace series. Steel X12CrNiMoV12-3 (1.4933). 900 MPa ≤ Rm ≤ 1 100 MPa. Bars. De ≤ 150 mm |
| 09/30211106 DC : 0 | BS EN 2030 - AEROSPACE SERIES - STEEL FE-PM3501 (X105CRMO17) - HARDENED AND TEMPERED - BARS D <= 150 MM |
| BS EN 4800-007:2010 | Aerospace series. Titanium and titanium alloys Remelting stock |
| BS EN 2481:2010 | Aerospace series. Steel FE-PL2108 (36NiCrMo16). 1250 MPa ≤ Rm ≤ 1400 MPa. Forgings. De ≤ 75 mm |
| 97/719248 DC : DRAFT NOV 1997 | PREN 4278 - AEROSPACE SERIES - ALUMINIUM AL-P7175-T7352 - HAND AND DIE FORGINGS - A <= 150 MM |
| 97/719250 DC : DRAFT NOV 1997 | PREN 4283 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2219-T87 - PLATE - 6 MM <= A <= 40 MM |
| 01/716448 DC : DRAFT JAN 2002 | PREN 2092 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7075 - T6 OR T62 - CLAD SHEET AND STRIP - 0,4 MM < A < 6 MM |
| UNI EN 4629 : 2013 | AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED - SOFTENED - FORGING STOCK - D[E] <= 300 MM |
| XP PREN 4347 : 1996 XP | AEROSPACE SERIES - STEEL FE-PM1506 (X3CRNIMOAL13-8-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOFTENED - FORGING STOCK - A OR D =< 300 MM |
| UNI EN 4670 : 2011 | AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOFTENED - FORGING STOCK - A OR D <= 300 MM |
| I.S. EN 3365:2007 | AEROSPACE SERIES - STEEL FE-PM3901 (X15CRNI17-3) - AIR MELTED - SOFTENED - FORGING STOCK - A OR D <= 300 MM |
| UNI EN 4628 : 2013 | AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED - HARDENED AND TEMPERED - BAR - D[E] <= 200 MM - 1150 MPA <= R[M] <= 1300 MPA |
| 97/718316 DC : OCT 97 | EN 3678 - AEROSPACE SERIES - STEEL FE-PM3081 (X5CRNICU17-4) - AIR MELTED - SOLUTION TREATED AND PRECIPITATION HARDENED - FORGINGS A OR D LESS THAN OR EQUAL TO 150 MM RM LESS THAN OR EQUAL TO 930 MPA |
| 97/718300 DC : DRAFT OCT 1997 | PREN 2772 - AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - AIR MELTED SOLUTION TREATED AND PRECIPATION HARDENED FORGINGS A OR D <= 150 MM - RM => 965 MPA |
| BS EN 4472:2007 | Aerospace series. Steel FE-PM1505 (X1CrNiMoAlTi12-9-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Forgings. a or D ≤ 150 mm. Rm ≥ 1400 MPa |
| I.S. EN 4800-007:2010 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 007: REMELTING STOCK |
| 07/30162489 DC : 0 | BS EN 4528 - AEROSPACE SERIES - STEEL FE-PA3903 (X12CRNI18-10) - AS COLD ROLLED - STRIP FOR SPRING - A <= 3 MM 1250 MPA <= R[M] <= 1640 MPA |
| 03/310514 DC : 0 | BS EN 4400-4 - AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM- AND MAGNESIUM-ALLOYS - TECHNICAL SPECIFICATION - PART 4: ALUMINIUM AND ALUMINIUM ALLOY TUBE |
| 04/30111424 DC : DRAFT MAR 2004 | PREN 2085 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2618A-T6 - HAND AND DIE FORGINGS - A LESS THAN OR EQUAL TO 150 MM |
| NF EN 2002-001 : 2006 | AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - PART 001: TENSILE TESTING AT AMBIENT TEMPERATURE |
| PREN 4573 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA4901 (X12CRNICOMOW21-20) - SOLUTION TREATED AND PRECIPITATION TREATED - BAR AND SECTION - D[E] <= 100 MM |
| 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 |
| BS EN 4629:2013 | Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Softened. Forging stock. De ≤ 300 mm |
| PREN 4800-001 : 200P2 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 1: PLATE, SHEET AND STRIP |
| 96/716616 DC : 0 | PREN 4381 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH3601 (NICR22MO9NB) SOLUTION TREATED - SEAMLESS TUBES - FOR STRUCTURAL APPLICATION D <= 50 MM, A <= 3 MM |
| I.S. EN 4700-002:2016 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 002: BAR AND SECTION |
| 96/717410 DC : 0 | PREN 3510 - AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2602 (X4NICRTIMOV26-15) SOLUTION AND PRECIPITATION TREATED - BAR AND SECTION A OR D <= 100 MM |
| 96/716591 DC : 0 | PREN 2233 - AEROSPACE SERIES - HEAT RESISTING ALLOY NI-CD1701 (NICO15CR10A16TI5MO3) - AS CAST - PRECISION CASTING D[E] <= 50 MM |
| PREN 2405 : 200P1 | AEROSPACE SERIES - HEAT RESISTING NICKEL BASE ALLOY NI-PH2601 (NICR19FE19NB5MO3) - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - D[E] <= 200 MM |
| PREN 2481 : 200P1 | AEROSPACE SERIES - STEEL FE-PL2108 (36NICRMO16) - 1250 MPA <= R[M] <= 1400 MPA - FORGINGS - D[E] <= 75 MM |
| PREN 2469 : 200P1 | AEROSPACE SERIES - STEEL FE-PA3901 (X1CRNI18-10) - AIR MELTED - SOFTENED - WIRES - 0,4 <= D <= 12,5 MM - 450 MPA <= R[M] <= 650 MPA |
| PREN 2687 : 200P1 | ALUMINIUM ALLOY AL-P7010-T7451 - PLATE - 6 MM <= 160 MM |
| PREN 2694 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6061-T6 OR T62 - SHEET AND STRIP - 0,4 MM <= A <= 6 MM |
| PREN 2732 : 200P2 | AEROSPACE SERIES - MAGNESIUM ALLOY MG-C46001 - T6 - CHILL CASTINGS |
| PREN 2511 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7075-T7351 - PLATE - 6 MM < A <= 100 MM |
| PREN 2773 : 200P2 | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU 17-4) - CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - SHEET AND STRIP - A <= 6 MM - R[M] >= 1310 MPA |
| PREN 2803 : 200P3 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7475-T761 - CLAD SHEET AND STRIP - 1,0 MM <= A <= 6 MM |
| PREN 2813 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6061-T6 - DRAWN TUBE FOR PRESSURE APPLICATIONS - 0,6 MM <= A <= 12,5 MM |
| PREN 2197 : 200P2 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1701 (NICR15CO14AL5TI4MO4) - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - D[E] <= 200 MM - R[M] >= 1 250 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 2445 : 200P2 | AEROSPACE SERIES - STEEL FE-PL8201 (41NICRMO2) - AIR MELTED - HARDENED AND TEMPERED - FORGINGS D[E] <= 45 MM - 900 MPA <= R[M] <= 1100 MPA |
| PREN 2185 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2301 (NICR21FE18MO9) - SOLUTION TREATED - SHEET, STRIP AND PLATE - 0,2 MM <= A <= 10 MM |
| I.S. EN 3364:2007 | AEROSPACE SERIES - STEEL FE-PM1802 (X5CRNICU15-5) - CONSUMABLE ELECTRODE REMELTED - SOFTENED - FORGING STOCK A OR D <= 300 MM |
| PREN 4842 : DRAFT 2016 | AEROSPACE SERIES - X5CRNICU15-5 (1.4545) CONSUMABLE ELECTRODE REMELTED (ESR OR VAR) - SOLUTION TREATED AND PRECIPITATION TREATED (H1025) BAR FOR MACHINING A OR D <= 250 MM 1070 MPA <= R[M] <= 1200 MPA PREMIUM QUALITY (PQ) |
| NF EN 3310 : 2012 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AI-4V) - NOT HEAT TREATED - FORGING STOCK, FOR ANNEALED FORGINGS - D[E] < OR = 360 MM |
| NF EN 3488 : 2008 | AEROSPACE SERIES - STEEL FE-PA3601 (X6CRNITI18-10) - AIR MELTED - SOFTENED - SHEET AND STRIP - A <= 6 MM - 500 MPA <= R[M] <= 700 MPA |
| PREN 2704 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024 - T3511 - DRAWN BAR D[E] <= 75 MM |
| PREN 2512 : 200P3 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7175-T7351 - PLATE - 6 MM < A <= 100 MMM |
| PREN 2465 : 200P1 | AEROSPACE SERIES - STEEL X2CRNI18-9 (1.4307) - SOFTENED 450 MPA <= R[M] <= 680 MPA BAR FOR MACHINING 4 MM <= D[E] <= 100 MM |
| PREN 2816 : 200P3 | AEROSPACE SERIES - STEEL FE-PM1802 (X5CRNICU15-5) - CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED FORGINGS - A OR D <= 200 MM - R[M] >= 965 MPA |
| DIN EN 2804:2000-04 (Draft) | Aerospace series - Aluminium alloy AL-P7075-T7651 - Plate, 6 mm < a <kleiner |
| PREN 2684 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7010-T7651 - PLATE - 6 MM < A <= 140 MM |
| PREN 2728 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-C42101 - T6 - SAND CASTING - A <= 20 MM |
| PREN 2775 : 200P2 | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU 17-4) - CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 200 MM - R[M] >= 1310 MPA |
| NF EN 2446 : 2009 | AEROSPACE SERIES - STEEL FE-PL1503 (35CRMO4) - 1100 MPA <= R[M] <= 1300 MPA - BARS - D[E] <= 25 MM |
| PREN 2693 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P5086-H111 - SHEET AND STRIP - 0,3 MM <= A <= 6 MM |
| PREN 3163 : 200P1 | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - AIR MELTED - SOFTENED - FORGING STOCK - A OR D <= 300 MM |
| PREN 2772 : 200P2 | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU 17-4) - AIR MELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 200 MM - R[M] >= 965 MPA |
| PREN 2802 : 200P3 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7475-T761 - SHEET AND STRIP - 0,6 MM <= A <= 6 MM |
| PREN 2821 : 200P2 | |
| PREN 3124 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-C42201 - T6 - HIGH STRENGTH CASTING - A <= 20 MM |
| PREN 4400-1 : 200P1 | AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM ALLOY WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 1: PLATE |
| PREN 4574 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA4901 (X12CRNICOMOW21-20) - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - D[E] <= 100 MM |
| PREN 4500-005 : 200P2 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 005: SPECIFIC RULES FOR STEELS |
| PREN 3527 : 200P2 | AEROSPACE SERIES - STEEL FE-PL1504 (33CRMOV12) - AIR MELTED - SOFTENED - FORGING STOCK - A OR D <= 300 MM |
| PREN 4468 : 200P1 | |
| PREN 2175 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2602 (X4NICRTIMOV26-15) - SOLUTION TREATED AND PRECIPITATION TREATED - SHEET, STRIP AND PLATE - 0,5 MM <= A <= 10 MM - R[M] >= 850 MPA |
| PREN 4800-007 : 200P2 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 7: REMELTING STOCK |
| PREN 4211 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024 - T42 - CLAD PLATE - 6 MM < A <= 25 MM |
| PREN 4213 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6061-T651 - PLATE - 6 MM < A <= 80 MM |
| PREN 2092 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7075-T6 OR T62 - CLAD SHEET AND STRIP - 0,4 MM <= A <= 6 MM |
| PREN 4670 : 200P1 | AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOFTENED - FORGING STOCK - A OR D <= 300 MM |
| PREN 4672 : 200P1 | AEROSPACE SERIES - STEEL FE-PM1504 (X1CRNIMOALTI12-10-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOFTENED - FORGING STOCK - A OR D <= 300 MM |
| 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 2117 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P5056A (5056A)-H32 WIRE FOR SOLID RIVETS D <= 10 MM |
| PREN 4572 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA4901 (X12CRNICOMOW21-20) - SOLUTION TREATED - SHEET AND STRIP - A <= 3 MM |
| PREN 4101 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024-T4 - SHEET AND STRIP WITH IMPROVED STRETCH FORMING CAPABILITY - 0,4 MM <= A <= 6 MM |
| PREN 2030 : 200P1 | AEROSPACE SERIES - STEEL FE-PM3501 (X105CRMO17) - HARDENED AND TEMPERED - BARS D[E] <= 150 MM |
| PREN 2089 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2014A-T6 OR T62 - SHEET AND STRIP - 0,4 MM <= A <= 6 MM |
| PREN 2116 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY 2017A T42 WIRE FOR SOLID RIVETS D <= 10 MM |
| PREN 4700-007 : 200P2 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 007: REMELTING STOCK |
| I.S. EN 3329:2009 | AEROSPACE SERIES - STEEL FE-PL1503 (35CRMO4) - ANNEALED - SHEET AND STRIP - 0,3 MM <= A <= 2 MM - FOR PREVAILING TORQUE NUTS |
| PREN 4001 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024 - T351 - CLAD SHEET AND STRIP WITH IMPROVED CHEMICAL MILLING CAPABILITY - 1,6 MM <= A <= 6 MM |
| I.S. EN 3456:2012 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - SHEET AND STRIP, HOT ROLLED - A <= 6 MM |
| PREN 2177 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2501 (X4NICRMOTI43-13) - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - D[E] <= 100 MM |
| PREN 4800-004 : 200P2 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 4: WIRE |
| PREN 4675 : 200P1 | AEROSPACE SERIES - TITANIUM TI-P63002 (TI5AL5MO5V3CR0,4FE) - R[M] >= 1300 MPA - BARS - D[E] <= 100 MM |
| PREN 2124 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2214 - T651 - PLATE - 6 MM < A <= 140 MM |
| PREN 2172 : 200P2 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA2601 (X6NICRTIMOV26-15) - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - D[E] <= 100 MM - R[M] >= 900 MPA |
| PREN 4700-001 : 200P2 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 001: PLATE, SHEET AND STRIP |
| PREN 3491 : 200P2 | AEROSPACE SERIES - STEEL FE-PM3901 (X15CRNI17-3) - AIR MELTED - HARDENED AND TEMPERED - FORGINGS - D[E] <= 100 MM - 900 MPA <= R[M] <= 1100 MPA |
| PREN 3511 : 200P2 | AEROSPACE SERIES - STEEL FE-PL1801 (100CR6) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOFTENED - BAR FOR THE MANUFACTURE OF MACHINED BEARINGS - A OR D <= 130 MM |
| PREN 3557 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6061-T4 - DRAWN TUBE FOR PRESSURE APPLICATIONS - 0,6 MM <= A <= 3,0 MM |
| I.S. EN 4465:2007 | AEROSPACE SERIES - STEEL FE-PM1506 (X5CRNIMOAL13-8-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 150 MM - R[M] >= 1 300 MPA |
| PREN 3979 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P8090-O2 - SHEET FOR SUPERPLASTIC FORMING (SPF) - 0,8 MM <= A <= 6 MM |
| PREN 4006 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6082 - T4 OR T42 - SHEET AND STRIP - 0,4 MM <= A <= 6 MM |
| PREN 3980 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P8090-T6 - SUPERPLASTIC SHEET FORMINGS (SPF) - 0,8 MM <= A <= 6 MM |
| PREN 4004 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P3103 - H16 - SHEET AND STRIP - 0,4 MM <= A <= 6 MM |
| PREN 4700-002 : 200P3 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 002: BAR AND SECTION |
| PREN 2048 : 200P1 | AEROSPACE SERIES - EXTRUDED L-SECTION, IN ALUMINIUM ALLOYS - DIMENSIONS |
| PREN 4615 : 200P1 | AEROSPACE SERIES - MAGNESIUM ALLOY MG-C18002 - T4 - SAND CASTING |
| 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 |
| PREN 4500-001 : 200P2 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 001: GENERAL RULES |
| PREN 4500-003 : 200P2 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 003: SPECIFIC RULES FOR HEAT RESISTING SLLOYS |
| PREN 4457 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7475-T7351 - PLATE - 6 MM < A <= 100 MM |
| PREN 4466 : 200P1 | AEROSPACE SERIES - STEEL FE-PM1506 (X5CRNIMOAL13-8-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 150 MM - R[M] >= 1 400 MPA |
| I.S. EN 2135:2017 | AEROSPACE SERIES - STEEL FE-PL61 - CARBURIZED, HARDENED AND TEMPERED - BAR - DE <= 40 MM |
| I.S. EN 2542:2008 | AEROSPACE SERIES - STEEL FE-PL1502 (25CRMO4) - ANNEALED - BAR AND WIRE - D[E] <= 40 MM - FOR PREVAILING TORQUE NUTS |
| UNI EN 4800-002 : 2011 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 002: BAR AND SECTION |
| S.R. CWA 16762:2014 | CEN WORKSHOP AGREEMENT - CEN/WS SERES - ICT STANDARDS IN SUPPORT OF AN EREPORTING FRAMEWORK FOR THE ENGINEERING MATERIALS SECTOR |
| NF EN 2481 : 2011 | AEROSPACE SERIES - STEEL FE-PL2108 (35NICRMO16) - 1250 MPA < OR = R[M] < OR = 1400 MPA - FORGINGS - D[E] < OR = 75 MM |
| I.S. EN 4656:2010 | AEROSPACE SERIES - STEEL FE-PM1507 (X1CRNIMOALTI12-11-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BARS - A OR D <= 200 MM - R[M] >= 1520 MPA |
| I.S. EN 4628:2013 | AEROSPACE SERIES - STEEL X4CRNIMO16-5-1 (1.4418) - AIR MELTED - HARDENED AND TEMPERED - BAR - D[E] <= 200 MM - 1150 MPA <= R[M] <= 1300 MPA |
| I.S. EN 4470:2007 | AEROSPACE SERIES - STEEL FE-PM1505 (X1CRNIMOALTI12-9-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 150 MM - R[M] >= 1200 MPA |
| I.S. EN 4800-001:2010 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 001: PLATE, SHEET AND STRIP |
| 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 |
| I.S. EN 4631:2013 | 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 4700-004:2010 | AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 004: WIRE |
| I.S. EN 3813:2013 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - BAR AND WIRE FOR FORGED FASTENERS - D[E] <= 50 MM |
| NF EN 3163 : 2008 | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - AIR MELTED, SOFTENED, FORGING STOCK A OR D <= 300 MM |
| BS EN 2306:2017 | Aerospace series. Heat resisting. Nickel base alloy Ni-Cr20Co3Fe3. Annealed. Bars |
| I.S. EN 3351:2012 | AEROSPACE SERIES - TITANIUM ALLOY TI-4AL-4MO-2SN - SOLUTION TREATED AND AGED - FORGINGS - D[E] <= 150 MM |
| UNI EN 4262 : 2014 | AEROSPACE SERIES - HEAT RESISTING ALLOY FE-PA4901 (X12CRNICOMOW21-20) - AS FORGED - FORGING STOCK - A OR D <= 200 MM - 690 MPA <= R[M] <= 880 MPA |
| NF EN 3162 : 2008 | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - AIR MELTED, SOLUTION TREATED AND PRECIPITATION TREATED, SHEET AND STRIP A <= 6 MM, R[M] >= 930 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 4500-001:2012 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 001: GENERAL RULES |
| NF EN 4466 : 2008 | AEROSPACE SERIES - STEEL FE-PM1506 (X5CRNIMOAL13-8-2) - VACUUM INDUCTION MELTED AND CONSUMABLE ELECTRODE REMELTED - SOLUTION TREATED AND PRECIPITATION TREATED - FORGINGS - A OR D <= 150 MM - R[M] >= 1400 MPA |
| UNI EN 3312 : 2013 | AEROSPACE SERIES - TITANIUM ALLOY TI-6AL-4V - ANNEALED - FORGINGS D[E] <= 150 MM |
| 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 |
| I.S. EN 2573:2007 | AEROSPACE SERIES - STEEL FE-PA3601 (X6CRNITI18-10) - SOFTENED - R[M] <= 780 MPA - WIRE - 0,25 MM <= D[E] <= 3 MM |
| I.S. EN 2466:2009 | AEROSPACE SERIES - STEEL FE-PA3901 (X2CRNI19-11) - SOFTENED - FORGINGS - D[E] <= 100 MM |
| I.S. EN 4468:2007 | |
| 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 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 |
| 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 3936:2001 | Aerospace series. Nickel base alloy NI-B21001 (NiCr15B4). Filler metal for brazing. Powder or paste |
| BS EN 4003:2006 | Aerospace series. Aluminium alloy AL-P2219-T87. Sheet and strip 0,5 mm ≤ a ≤ 6 mm |
| BS EN 3969:2006 | Aerospace series. Steel FE-PL1507 (40CrMoV12). Air melted. Annealed. Forging stock. a or D ≤ 350 mm |
| BS EN 4332:2002 | Aerospace series. Steel FE-WL1805 (8CrMnMo12-4-9). Filler metal for welding. Wire and rod |
| BS EN 3963:2001 | Aerospace series. Copper CU-BU9001. Filler metal for brazing. Rolled foil |
| BS EN 3919:1998 | Nickel base alloy NI-B41202 (NiCr14Si5B3). Filler metal for brazing. Amorphous foil |
| BS EN 4214:2005 | Aerospace series. Aluminium alloy AL-P7010-T651. Plate. 6 mm |
| BS EN 3997:2015 | Aerospace series. Aluminium alloy AL-P2024-Al Cu4Mg1-T3. Sheet and strip. 0,4 mm ≤ a ≤ 6 mm |
| BS EN 2803:2005 | Aerospace series. Aluminium alloy AL-P7475-T761. Clad sheet and strip. 1,0 mm ≤ a ≤ 6 mm |
| 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 3527:2007 | Aerospace series. Steel FE-PL1504 (33CrMoV12). Air melted. Softened. Forging stock. a or D ≤ 300 mm |
| BS EN 3976:2006 | Aerospace series. Titanium and titanium alloys. Test method. Chemical analysis for the determination of hydrogen content |
| BS EN 3506:2001 | Aerospace series. Hot rolled sheets and plates in heat resisting alloys. Thickness 2,0 mm ≤ a ≤ 100 mm. Dimensions |
| BS EN 2702:2005 | Aerospace series. Aluminium alloy. AL-P6061. T6 or T62. Drawn or extruded bar and section. a or D ≤ 200 mm |
| BS EN 3943:2001 | Aerospace series. Nickel base alloy NI-B41204 (NiCr13Fe4Si4B3). Filler metal for brazing. Powder or paste |
| BS EN 2338:2001 | Aerospace series. Sheets, hot rolled in titanium and titanium alloys. Thickness 0,8 mm ≤ a ≤ 6 mm. Dimensions |
| BS EN 3114-001:2006 | Aerospace series. Test method. Microstructure of (α + β) titanium alloy wrought products General requirements |
| BS EN 3476:2006 | Aerospace series. Steel FE-PL1501 (30CrMo12). Air melted. Softened. Forging stock. a or D ≤ 300 mm |
| BS EN 2802:2005 | Aluminium alloy AL-P7475-T761. Sheet and strip. 0,6 mm ≤ a ≤ 6 mm |
| BS EN 3890:2002 | Aerospace series. Steel FE-WM1502 (X11CrNiMoVN12-3). Filler metal for welding |
| BS EN 4000:2002 | Aerospace series. Metallic materials. Rules for the drafting and presentation of dimensional standards for metallic semi-finished products |
| BS EN 2469:2007 | Aerospace series. Steel FE-PA3901 (X1CrNi18-10). Air melted. Softened. Wires. 0,4 mm ≤ D ≤ 12,5 mm. 450 MPa ≤ Rm ≤ 650 MPa |
| BS EN 2731:2005 | Aerospace series. Magnesium alloy MG-C46001. T6. Sand casting |
| 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 2695:2005 | Aerospace series. Aluminium alloy AL-P6081-T6. Sheet and strip. 0,3 mm ≤a ≤6 mm |
| BS EN 2071:2002 | Aerospace series. Sheets in aluminium and aluminium alloys. Thickness 0,25 mm ≤ a ≤ 6 mm. Dimensions |
| BS EN 4313:2005 | Aerospace series. Aluminium aloy AL-P6013-T6. Sheet and strip. 0,5 mm ≤a ≤6 mm |
| BS EN 3338:2005 | Aerospace series. Aluminim alloy AL-P7050. T74511. Extruded bar and section. a or D ≤ 150 mm with peripheral coarse grain control |
| BS EN 3973:2006 | Aerospace series. Steel FE-CM3801 (X5CrNiCuNb16-4). Homogenized, solution treated and precipitation hardened. Investment casting. De ≤ 50 mm. Rm ≥ 1030 MPa |
| BS EN 2339:2001 | Aerospace series. Sheets, cold rolled in titanium and titanium alloys. Thickness 0,2 mm ≤ a ≤ 6 mm. Dimensions |
| 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 |
| BS EN 4059:2001 | Aerospace series. Filler rods and filler wire for welding in steel. Diameter 0,5 mm ≤ D ≤ 5,0 mm. Dimensions |
| BS EN 3816:2006 | Aerospace series. Steel FE-PA3601 (X6CrNiTi18-10). Air melted. Softened and cold rolled. Sheet and strip. a ≤ 3 mm. Rm ≥ 800 MPa |
| BS EN 2256:2004 | Aerospace series. Aluminium alloy AL-P2618A-T852. Hand and die forgings. a ≤ 150 mm |
| BS EN 4085:2001 | Aerospace series. Nickel base alloy NI-B40002 (NiSi4B2). Filler metal for brazing. Amorphous foil |
| BS EN 3945:2001 | Aerospace series. Nickel base alloy NI-B48801 (NiMn19Si6Cu4B). Filler metal for brazing. Powder or paste |
| BS EN 3921:2001 | Aerospace series. Nickel base alloy NI-B41203 (NiCr7Si5B3). Filler metal for brazing. Amorphous foil |
| BS EN 2032-1:2002 | Metallic materials Conventional designation |
| BS EN 3894:2001 | Aerospace series. Heat resisting alloy NI-WD3201 (NiMo25Fe6Cr5). Filler metal for welding |
| BS EN 3935:2001 | Aerospace series. Nickel base alloy NI-B21001 (NiCr15B4). Filler metal for brazing. Borided foil |
| BS EN 3952:2001 | Aerospace series. Silver base alloy AG-B10001 (AgCu28). Filler metal for brazing. Wire |
| BS EN 4267:2001 | Aerospace series. Round bar in titanium and titanium alloys. Diameter 6 mm ≤ D ≤ 160 mm. Dimensions |
| BS EN 3947:1998 | Nickel base alloy NI-B15701 (NiPd34Au30). Filler metal for brazing. Rolled foil |
| BS EN 3979:2005 | Aerospace series. Aluminium alloy AL-P8090-O2. Sheet for superplastic forming (SPF). 0,8 mm ≤ a ≤ 6 mm |
| BS EN 4247:2005 | Aerospace series. Aluminium alloy AL-P2024-T42. Plate. 6 mm |
| BS EN 2050:2001 | Aerospace series. Extruded T-section, in aluminium alloys. Dimensions |
| BS EN 4317:2007 | Aerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Non heat treated, forging stock a or D ? 200 mm |
| BS EN 4209:2005 | Aerospace series. Aluminium alloy AL-P2219-T851. Plate. 6 mm |
| I.S. EN 3525:2007 | AEROSPACE SERIES - STEEL FE-PL1505 (15CRMOV6) - AIR MELTED - HARDENED AND TEMPERED - PLATE - 6 MM < A <= 20 MM - 1080 MPA <= R[M] <= 1280 MPA |
| I.S. EN 3526:2007 | AEROSPACE SERIES - STEEL FE-PL1505 (15CRMOV6) - AIR MELTED - HARDENED AND TEMPERED - SHEET AND STRIP - 0,5 MM <= A <= 6 MM - 980 MPA <= R[M] <= 1180 MPA |
| I.S. EN 3524:2007 | AEROSPACE SERIES - STEEL FE-PL1505 (15CRMOV6) - AIR MELTED - HARDENED AND TEMPERED - SHEET AND STRIP - 2 MM <= A <= 6 MM - 1080 MPA <= R[M] <= 1280 MPA |
| ASD-STAN prEN 3311 P3:2023 | Aerospace series Titanium alloy TI-P64001 (Ti-6Al-4V) — Annealed — Bars for machining — D < 300 mm — 900 MPa ≤ Rm ≤ 1 160 MPa |
| NS-EN 3525:2023 | Aerospace series - Steel 15CrMoV6 (1.7334) - Air melted - Hardened and tempered - Plates - 6 mm ≤ a ≤ 20 mm - 1 080 MPa ≤ Rm ≤ 1 280 MPa |
| ASD-STAN prEN 4500-004 P3:2023 | Aerospace series Metallic materials — Rules for drafting and presentation of material standards — Part 004: Specific rules for titanium and titanium alloys |
| NS-EN 3524:2023 | Aerospace series - Steel 15CrMoV6 (1.7334) - Air melted - Hardened and tempered - Sheets and strips - 2 mm ≤ a ≤ 6 mm - 1 080 MPa ≤ Rm ≤ 1 280 MPa |
| ASD-STAN prEN 4877-001 P2:2023 | Aerospace series — Filler metals for welding — Part 001: Technical specification |
| ASD-STAN prEN 2467 P2:2023 | Aerospace series Steel X2CrNi18-9 (1.4307) — Air melted — Softened — Plates, sheets and strips — 0,4 mm ≤ a ≤ 20 mm — 520 MPa ≤ Rm ≤ 670 MPa |
| ASD-STAN prEN 3488 P3:2023 | Aerospace series Steel X6CrNiTi18-10 (1.4541) — Air melted — Softened — Sheets and strips — a ≤ 6 mm — 500 MPa ≤ Rm ≤ 700 MPa |
| NS-EN 3311:2023 | Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bars for machining - D ≤ 300 mm - 900 MPa ≤ Rm ≤ 1 160 MPa |
| TR 2410 : 2 | AEROSPACE SERIES - METALLIC MATERIALS - RELATIONSHIP BETWEEN DIMENSIONAL STANDARDS AND MATERIAL STANDARDS |
| EN 2032-2 : 1994 | AEROSPACE SERIES - METALLIC MATERIALS - CODING OF METALLURGICAL CONDITION IN DELIVERY CONDITION |
| EN 4268 : 2012 | AEROSPACE SERIES - METALLIC MATERIALS - HEAT TREATMENT FACILITIES - GENERAL REQUIREMENTS |
| EN 2032-1 : 2001 | AEROSPACE SERIES - METALLIC MATERIALS - PART 1: CONVENTIONAL DESIGNATION |
| EN 2043:2013 | Aerospace series - Metallic materials - General requirements for semi-finished product qualification (excluding forgings and castings) |
| EN 4000:2001 | Aerospace series - Metallic materials - Rules for the drafting and presentation of dimensional standards for metallic semi-finished products |
| EN 4179:2017 | Aerospace series - Qualification and approval of personnel for non-destructive testing |
| 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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