49.035 : Components for aerospace construction

BS EN 2601:1996

BS EN 2601:1996

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Fork ends, adjustable. Technical specification

€165.00

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BS EN 2289:1996

BS EN 2289:1996

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Rod bodies in aluminium alloy for flight controls. Technical specification

€193.00

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BS 4T 100:1997

BS 4T 100:1997

Superseded Historical

Procedure for inspection, testing and acceptance of seamless steel tubes and tubestock

€193.00

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BS ISO 2020-2:1997

BS ISO 2020-2:1997

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Aerospace. Preformed flexible steel wire rope for aircraft controls Technical specification

€193.00

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BS EN 2644:1998

BS EN 2644:1998

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Rod assemblies for flight controls. Technical specification

€165.00

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BS A 328-2:1999

BS A 328-2:1999

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Accessory drives and mounting flanges (Metric sizes) Dimensions

€193.00

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BS EN 2290-1:1998

BS EN 2290-1:1998

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Rod bodies, flight control in aluminium alloy, for adjustable end fittings Dimensions and loads

€165.00

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BS ISO 2020-1:1997

BS ISO 2020-1:1997

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Aerospace. Preformed flexible steel wire rope for aircraft controls Dimensions and loads

€165.00

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BS 2W 12:1989

BS 2W 12:1989

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Specification for preformed zinc coated carbon steel wire rope (metric and inch series)

€193.00

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BS 3F 63:1981

BS 3F 63:1981

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Specification for low pressure oxygen hose for aeronautical purposes

€165.00

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BS 2F 67:1980

BS 2F 67:1980

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Specification for hose for aviation fuel and engine lubricating oil for aeronautical purposes

€165.00

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BS L 114:1971

BS L 114:1971

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Specification for tube of aluminium-magnesium-silicon-manganese alloy (solution treated and precipitation treated) (not exceeding 10 mm wall thickness) (suitable for welding) (Mg 0.8, Si 1, Mn 0.7)

€165.00

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BS L 117:1975

BS L 117:1975

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Specification for tube of aluminium-magnesium-silicon-copper-chromium alloy (solution treated and artificially aged: not tested hydraulically) (not exceeding 10 mm thickness) (Mg 1.0, Si 0.6, Cu 0.28, Cr 0.2)

€165.00

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BS L 118:1975

BS L 118:1975

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Specification for tube of aluminium-magnesium-silicon-copper-chromium alloy (solution treated and artificially aged: tested hydraulically) (not exceeding 10 mm thickness) (Mg 1.0, Si 0.6, Cu 0.28, Cr 0.2)

€165.00

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BS M 39:1972 (R2014)

BS M 39:1972 (R2014)

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Method for penetrant inspection of aerospace materials and components

€165.00

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