CTN ACE : Aerospace

BS T 64:1972

BS T 64:1972

Withdrawn Most Recent

Specification for carbon-manganese steel tube (550 N/mm2) (tube less than 12.5 mm outside diameter) (weldable)

€77.00

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BS 3G 173:1972

BS 3G 173:1972

Superseded Historical

Specification for performance and interchangeability requirements for plugs and sockets for ground electrical supply to aircraft

€269.00

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BS 3G 100-2.3.3:1972

BS 3G 100-2.3.3:1972

Withdrawn Most Recent

Specification for general requirements equipment use in aircraft. All equipment. Environmental conditions Mould growth

€165.00

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BS 3G 100-2.3.4:1972

BS 3G 100-2.3.4:1972

Withdrawn Most Recent

Specification for general requirements equipment use in aircraft. All equipment. Environmental conditions Differential pressure

€165.00

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BS HR 203:1972

BS HR 203:1972

Superseded Historical

Specification for nickel-chromium-titanium heat-resisting alloy plate, sheet and strip (nickel base, Cr 19.5, Ti 0.4)

€165.00

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BS HR 204:1972

BS HR 204:1972

Superseded Historical

Specification for nickel-chromium-iron-molybdenum-cobalt-tungsten heat-resisting alloy plate, sheet and strip (nickel base Cr 22, Fe 18.5, Mo 9, Co 1.5, W 0.6)

€81.00

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BS L 113:1971 (R2003)

BS L 113:1971 (R2003)

Superseded Historical

Specification for sheet and strip of aluminium-magnesium-silicon-manganese alloy (solution treated and precipitation treated) (suitable for welding) (Mg 0.8, Si 1, Mn 0.7)

€165.00

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BS TA 38:1971

BS TA 38:1971

Superseded Historical

Specification for bar for machining of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1250-1420 N/mm2) (limiting ruling section 25 mm)

€165.00

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BS TA 39:1971

BS TA 39:1971

Superseded Historical

Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1250-1420 N/mm2) (limiting ruling section 25 mm)

€165.00

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BS TA 40:1971

BS TA 40:1971

Superseded Historical

Specification for bar for machining of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 N/mm2) (limiting ruling section over 25 mm up to and including 75 mm)

€165.00

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BS TA 41:1971

BS TA 41:1971

Superseded Historical

Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 N/mm2) (limiting ruling section over 25 mm up to and including 75 mm)

€165.00

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BS TA 42:1971

BS TA 42:1971

Superseded Historical

Specification for forgings of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 N/mm2) (limiting ruling section over 25 mm up to and including 75 mm)

€165.00

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BS L 109:1971

BS L 109:1971

Superseded Historical

Specification for aluminium-coated sheet and strip of aluminium-copper-magnesium-manganese alloy (solution treated and aged at room temperature) (Cu 4.4, Mg 1.5, Mn 0.6)

€165.00

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BS L 110:1971

BS L 110:1971

Superseded Historical

Specification for aluminium-coated sheet and strip of aluminium-copper-magnesium-manganese alloy (supplied for solution treatment by the user) (Cu 4.4, Mg 1.5, Mn 0.6)

€81.00

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BS L 115:1971

BS L 115:1971

Superseded Historical

Specification for plate of aluminium-magnesium-silicon-manganese alloy (solution treated, controlled stretched and precipitation treated) (not exceeding 25 mm thickness) (suitable for welding) (Mg 0.8, Si 1, Mn 0.7)

€81.00

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