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
BS EN 2818:2009

BS EN 2818:2009

Active Most Recent

Aerospace series. Steel FE-PM1802 (X5CrNiCu15-5). Consumable electrode remelted. Solution treated and precipitation treated. Forgings. a or D = 200 mm. Rm = 1070 MPa

€165.00

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BS EN 3469:2009

BS EN 3469:2009

Active Most Recent

Aerospace series. Steel FE-PM1802 (X5CrNiCu15-5). Consumable electrode remelted. Solution treated and precipitation treated. Forgings. a or D = 200 mm. Rm = 1310 MPa

€165.00

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BS 3F 128:2010

BS 3F 128:2010

Active Most Recent

Specification for cotton webbing suitable for aerospace purposes (warp yarn nominally R 310 tex)

€193.00

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BS EN 6072:2010

BS EN 6072:2010

Active Most Recent

Aerospace series. Metallic materials. Test methods. Constant amplitude fatigue testing

€316.00

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BS EN 3529:2010

BS EN 3529:2010

Active Most Recent

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

€165.00

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BS EN 3329:2009

BS EN 3329:2009

Active Most Recent

Aerospace series. Steel FE-PL1503 (35CrMo4). Annealed Sheet and strip. 0,3 mm = a = 2 mm. For prevailing torque nuts

€165.00

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BS EN 4469:2007

BS EN 4469:2007

Active Most Recent

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

€165.00

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BS EN 4800-001:2010

BS EN 4800-001:2010

Superseded Historical

Aerospace series. Titanium and titanium alloys. Technical specification Plate, sheet strip

€269.00

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BS EN 2954-002:2010

BS EN 2954-002:2010

Active Most Recent

Aerospace series. Macrostructure of titanium and alloy wrought products bar, section, forging stock forgings

€269.00

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BS 2HR 209:2011

BS 2HR 209:2011

Active Most Recent

Specification for nickel-chromium-cobalt-molybdenum- titanium-aluminium heat-resisting alloy plate, sheet and strip (Nickel base, Cr 18, Co 14, Mo 7, Ti 2.2, Al 2.1)

€165.00

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BS 2HR 240:2011

BS 2HR 240:2011

Active Most Recent

Specification for cobalt-chromium-tungsten-nickel-manganese heat-resisting alloy plate, sheet and strip (Cobalt base, Cr 20, W 15, Ni 10, Mn 1.5)

€165.00

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BS 3HR 501:2011 (R2016)

BS 3HR 501:2011 (R2016)

Active Most Recent

Specification for nickel-chromium-cobalt-titanium- aluminium heat-resisting alloy cold drawn wire for springs and springs (Nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)

€165.00

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BS 3HR 502:2011 (R2016)

BS 3HR 502:2011 (R2016)

Active Most Recent

Specification for nickel-chromium-cobalt-titanium- aluminium heat-resisting alloy cold drawn and solution treated wire for springs and springs (Nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)

€165.00

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BS 3HR 503:2011

BS 3HR 503:2011

Active Most Recent

Specification for nickel-chromium-cobalt-titanium- aluminium heat-resisting alloy wire for thread inserts (Nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5) (0.45 mm to 2 mm diameter)

€165.00

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BS 3HR 504:2011

BS 3HR 504:2011

Active Most Recent

Specification for nickel-chromium-titanium heat-resisting alloy bar and wire for rivets and rivets (Maximum diameter or minor sectional dimension 20 mm) (Nickel base, Cr 19.5, Ti 0.4)

€165.00

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