49.025 : Materials for aerospace construction

49.025.01

Materials for aerospace construction in general

49.025.05

Ferrous alloys in general

49.025.10

Steels

49.025.15

Non-ferrous alloys in general

49.025.20

Aluminium

49.025.30

Titanium

49.025.40

Rubber and plastics

49.025.50

Adhesives

49.025.60

Textiles

49.025.99

Other materials
SAE AMS 5937:2012-10-11

SAE AMS 5937:2012-10-11

Superseded Historical

Steel, Corrosion-Resistant, Bars, Wire, and Forgings 12Cr - 11Ni - 2Mo 1.5Al 0.3Ti Vacuum Induction Plus Vacuum Consumable Electrode Melted Solution Heat Treated, Precipitation Hardenable

€73.00

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SAE AMS 5383E:2012-10-11

SAE AMS 5383E:2012-10-11

Superseded Historical

Nickel Alloy, Corrosion and Heat-Resistant, Investment Castings 52.5Ni - 19Cr - 3.0Mo - 5.1Cb(Nb) - 0.90Ti - 0.60Al - 18Fe Vacuum Melted Homogenization and Solution Heat Treated

€73.00

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SAE AMS 2431/8B:2007-05-15

SAE AMS 2431/8B:2007-05-15

Superseded Historical

Peening Media (AWCH) Conditioned Carbon Steel Cut Wire Shot, High Hardness (55 to 62 HRC)

€68.00

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ASTM D3878-07

ASTM D3878-07

Superseded Historical

Standard Terminology for Composite Materials

This product is not for sale, please contact us for more information

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ASTM D3878-07(2013)

ASTM D3878-07(2013)

Superseded Historical

Standard Terminology for Composite Materials

This product is not for sale, please contact us for more information

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SAE ARP 1962A:2007-05-01

SAE ARP 1962A:2007-05-01

Superseded Historical

Training and Approval of Heat-Treating Personnel

€81.00

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SAE AS 5706:2007-05-01

SAE AS 5706:2007-05-01

Superseded Historical

Test Plan/Procedure for AS5643/1 S400 Copper Media Interface Characteristics Over Extended Distances

€124.00

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BS EN 3524:2007

BS EN 3524:2007

Superseded Historical

Aerospace series. Steel FE-PL1505 (15CrMoV6). Air melted. Hardened and tempered. Sheet and strip. 2 mm = a = 6 mm. 1080 MPa = Rm =1280 MPa

€165.00

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BS EN 3525:2007

BS EN 3525:2007

Superseded Historical

Aerospace series. Steel FE-PL1505 (15CrMoV6). Air melted. Hardened and tempered. Plate. 6 mm « a = 20 mm. 1080 MPa = Rm = 1280 MPa

€165.00

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BS EN 3526:2007

BS EN 3526:2007

Superseded Historical

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

€165.00

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BS EN 3479:2007

BS EN 3479:2007

Superseded Historical

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

€165.00

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BS EN 3531:2007

BS EN 3531:2007

Superseded Historical

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

€165.00

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BS EN 3532:2007

BS EN 3532:2007

Superseded Historical

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

€165.00

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BS EN 3677:2007

BS EN 3677:2007

Superseded Historical

Aerospace series. Steel FE-PM3801 (X5CrNiCu17-4). Air melted. Solution treated and precipitation treated. Forgings. a or D = 200 mm. Rm = 1310 MPa

€155.00

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BS EN 2821:2007

BS EN 2821:2007

Superseded Historical

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

€165.00

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