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 TA 49:1973

BS TA 49:1973

Superseded Historical

Specification for bar and section for machining of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1000-1200 N/mm2) (limiting ruling section over 100 mm up to and including 150 mm)

€165.00

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BS TA 50:1973

BS TA 50:1973

Superseded Historical

Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1000-1200 N/mm2) (limiting ruling section over 100 mm up to and including 150 mm)

€165.00

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BS TA 51:1973

BS TA 51:1973

Superseded Historical

Specification for forgings of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1000-1200 N/mm2) (limiting ruling section over 100 mm up to and including 150 mm)

€165.00

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BS TA 52:1973

BS TA 52:1973

Superseded Historical

Specification for sheet and strip of titanium-copper alloy (tensile strength 690-920 N/mm2)

€165.00

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BS TA 53:1973

BS TA 53:1973

Withdrawn Most Recent

Specification for bar and section for machining of titanium-copper alloy (tensile strength 650-880 N/mm2) (limiting ruling section 75 mm)

€165.00

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BS TA 54:1973

BS TA 54:1973

Withdrawn Most Recent

Specification for forging stock of titanium-copper alloy (tensile strength 650-880 N/mm2) (limiting ruling section 75 mm)

€165.00

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BS TA 55:1973

BS TA 55:1973

Withdrawn Most Recent

Specification for forgings of titanium-copper alloy (tensile strength 650-880 N/mm2) (limiting ruling section 75 mm)

€165.00

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BS TA 56:1974

BS TA 56:1974

Superseded Historical

Specification for plate of titanium-aluminium-vanadium alloy (tensile strength 895-1150 MPa) (maximum thickness 100 mm)

€165.00

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BS TA 57:1974

BS TA 57:1974

Superseded Historical

Specification for plate of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1030-1220 MPa) (maximum thickness 65 mm)

€165.00

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BS 6V 3:1943

BS 6V 3:1943

Withdrawn Most Recent

Specification for aircraft material. High strength plywood for aircraft

€269.00

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BS 3V 4:1929

BS 3V 4:1929

Withdrawn Most Recent

Specification for aircraft material. Ash

€95.00

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BS 5V 7:1952

BS 5V 7:1952

Withdrawn Most Recent

Specification for mahogany for use in airscrews

€165.00

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BS 2V 35:1966

BS 2V 35:1966

Withdrawn Most Recent

Specification for plywood for aeronautical purposes

€95.00

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BS 2V 37:1968

BS 2V 37:1968

Withdrawn Most Recent

Specification for Sitka spruce as finished timber

€165.00

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BS V 38:1967

BS V 38:1967

Withdrawn Most Recent

Specification for Sitka spruce as rough timber

€165.00

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