EN 4258:1998
Withdrawn
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
Aerospace series - Metallic materials - General organization of standardization - Links between types of EN standards and their use
Withdrawn date
30-11-1998
Published date
20-05-1998
Publisher
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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 |
Withdrawn
|
| 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 |
| ONORM EN 4258 : 1998 | Identical |
| DS EN 4258 : 1998 | Identical |
| EN 2306:2017 | Aerospace series - Heat resisting - Nickel base alloy Ni-Cr20Co3Fe3 - 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 ≤ Rm ≤ 650 MPa |
| EN 3507:2006 | Aerospace series - Steel FE-PL1501 (30CrMo12) - Air melted - Hardened and tempered - Forgings - De ≤ 100 mm - 930 MPa ≤ Rm ≤ 1 080 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 - De ≤ 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 |
| 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) - 1 100 MPa ≤ Rm ≤ 1 300 MPa - Bars - De ≤ 100 mm |
| EN 2512:2014 | Aerospace series - Aluminium alloy AL-P7175 - T7351 - Plate - 6mm < 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 ≤ Rm ≤ 1 100 MPa - Forgings - De ≤ 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) - 1 100 MPa ≤ Rm ≤ 1 300 MPa - Bars - De ≤ 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 ≤ Rm ≤ 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 |
| 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 ≤ Rm ≤ 1 100 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) - 1 250 MPa ≤ Rm ≤ 1 400 MPa - Bars - De ≤ 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 ≤ Rm ≤ 800 MPa - Bars - De ≤ 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 - Rm ≥ 1 310 MPa |
| EN 2399:2008 | Aerospace series - Heat resisting steel FE-PA2601 (X4NiCrTiMoV26-15) - Rm ≥ 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 ≤ Rm ≤ 800 MPa - Forgings - De ≤ 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 |
| 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 |
| 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 |
| 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 ≤ Rm ≤ 1 100 MPa - Bars - De ≤ 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 ≤ Rm ≤ 670 MPa |
| EN 2226:2014 | Aerospace series - Steel X105CrMo17 (1.4125) - Hardened and tempered - Hand and die forgings - De ≤ 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 - De ≤ 150 mm |
| EN 2617:2001 | Aerospace series - Plates in titanium and titanium alloys - Thickness 6 mm < = a < = 100 mm - <br /><br />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 - 1 750 MPa ≤ Rm ≤ 2 000 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 |
| 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 - 1 750 MPa ≤ Rm ≤ 2 000 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 |
| 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 ≤ Rm ≤ 850 MPa - Bars - De ≤ 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 |
| EN 3894:2001 | Aerospace series - Heat resisting alloy NI-WD3201 (NiMo25Fe6Cr5) - Filler metal for welding |
| EN 3329:2009 | Aerospace series |
| 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) - Annealead - Bar and wire - De ≤ 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 |
| 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 |
| 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 ≤ Rm ≤ 680 MPa - Bar for machining - 4 mm ≤ De ≤ 100 mm |
| EN 3161:2007 | Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted, solution treated and precipitation treated, bar a or D ≤ 200 mm, Rm ≥ 930 MPa |
| EN 3332:2005 | Aerospace series - Aluminium alloy AL-P7475-T762 - Clad sheet and strip - 1,0 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 - De ≤ 16 mm - 980 MPa ≤ Rm ≤ 1 180 MPa |
| EN 2486:2005 | Aerospace series - Aluminium alloy AL-P2618A - Forging stock |
| EN 3552:2005 | Aerospace series - Aluminium alloy AL-P2618A-T6 or T62 - Clad sheet and strip - 0,4 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 |
| 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 - De ≤ 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) - 1 100 MPa ≤ Rm ≤ 1 300 MPa - Forgings - De ≤ 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 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 |
| 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 ≤ Rm ≤ 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 |
| 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) - 1 250 MPa ≤ Rm ≤ 1 400 MPa - Forgings - De ≤ 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 |
| ONORM 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 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 |
| ONORM 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 2821:2007 | |
| 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 |
| ASD-STAN prEN 4500-003 P3:2023 | Aerospace series Metallic materials — Rules for drafting and presentation of material standards — Part 003: Specific rules for heat-resisting alloys |
| ONORM 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 |
| TR 2410 : 2 | AEROSPACE SERIES - METALLIC MATERIALS - RELATIONSHIP BETWEEN DIMENSIONAL STANDARDS AND MATERIAL STANDARDS |
| EN 2032-2:1994 | Aerospace series - Metallic materials - Part 2: Coding of metallurgical condition in delivery condition |
| EN 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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