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 2HC 211:1989

BS 2HC 211:1989

Active Most Recent

Specification for nickel-chromium-cobalt-molybdenum-aluminium-titanium alloy castings (Nickel base Cr 15.5, Co 10.0, Mo 8,3, Al 4.2, Ti 3.6)

€165.00

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BS EN 2377:1989

BS EN 2377:1989

Active Most Recent

Specification for glass fibre reinforced plastics. Test method. Determination of apparent interlaminar shear strength

€165.00

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BS 7L 37:1989

BS 7L 37:1989

Active Most Recent

Specification for wire for solid cold-forged rivets of aluminium-copper-magnesium-silicon-manganese alloy (for use in the solution treated and naturally aged condition) (not exceeding 10 mm diameter) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8) (2014A)

€165.00

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BS L 172:1989

BS L 172:1989

Active Most Recent

Specification for extruded, rolled or cast forging stock of aluminium-zinc-magnesium-manganese-copper alloy (for manufacture of forgings to BS L 171) (Zn 5.7, Mg 2.7, Mn 0.5, Cu 0.5) (7014)

€165.00

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BS L 170:1989

BS L 170:1989

Active Most Recent

Specification for extruded bars and sections of aluminium-zinc-copper-chromium alloy (solution treated, controlled stretched and artificially aged) (not exceeding 150 mm diameter or minor sectional dimension) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.23) (7075)

€165.00

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BS F 137:1989

BS F 137:1989

Active Most Recent

Specification for warp knitted cotton polishing and polish application cloths for aircraft transparencies

€165.00

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BS L 171:1990

BS L 171:1990

Active Most Recent

Specification for forging of aluminium-zinc-magnesium-manganese-copper alloy (supplied as-forged or annealed for subsequent heat treatment) (not exceeding 150 mm diameter or minor sectional dimension) (Zn 5.7, Mg 2.7, Mn 0.5, Cu 0.5) (7014)

€165.00

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BS S 160:1990

BS S 160:1990

Active Most Recent

Specification for chromium-nickel corrosion-resisting steel - bright bars and parts (540 MPa, limiting ruling section 160 mm) (Cr 18, Ni 10.5, controlled nitrogen content)

€165.00

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BS S 161:1990

BS S 161:1990

Active Most Recent

Specification for chromium-nickel-molybdenum corrosion-resisting steel. Bright bars and parts (540 MPa, limiting ruling section 160 mm) (Cr 17.5, Ni 12.5, Mo 2.25, controlled nitrogen content)

€165.00

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BS 6F 37:1990

BS 6F 37:1990

Active Most Recent

Specification for 570 g/m2 and 640 g/m2 cotton canvas fabrics for aerospace purposes

€165.00

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BS S 163:1990

BS S 163:1990

Active Most Recent

Specification for nickel-chromium-molybdenum-vanadium steel forging stock, forgings, bars and parts (1900 MPa : limiting ruling section 100 mm)

€165.00

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SAE AMS 7849E:2018-11-21

SAE AMS 7849E:2018-11-21

Superseded Historical

Tantalum Sheet, Strip, and Plate Annealed

€71.00

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UNE 28017-1:1958

UNE 28017-1:1958

Active Most Recent

AIRCRAFT FABRIC. CLASSIFICATION, CHARACTERISTICS, RECEPTION AND MAINTENANCE.

€18.00

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UNE 28017-8:1961

UNE 28017-8:1961

Active Most Recent

TRACTION AND ELONGATION TESTS IN AIRCRAFT FABRICS.

€15.00

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ASTM D6465-99(2024)

ASTM D6465-99(2024)

Active Most Recent

Standard Guide for Selecting Aerospace and General Purpose Adhesives and Sealants

€65.00

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