Aircraft And Space Vehicle Engineering Standards
BS 2TA 58:2009
Specification for plate of titanium-copper alloy (tensile strength 520-640 MPa) (maximum thickness 10 mm)...
BS 2TA 59:2009
Specification for sheet of titanium-aluminium-vanadium alloy (tensile strength 920-1180 MPa)...
BS 2W 11:1967
Specification for aircraft material. Preformed corrosion-resisting steel wire rope...
BS 2W 12:1989
Specification for preformed zinc coated carbon steel wire rope (metric and inch series)...
BS 3224-1:1988
Lighting fittings for civil land aerodromes - Specification for lighting units for use in precision approach path indica...
BS 3224-4:1988
Lighting fittings for civil land aerodromes - Specification for elevated lighting units...
BS 3224-6:1988
Lighting fittings for civil land aerodromes - Specification for obstacle lighting units...
BS 3A 103:1962
Specification for steel nuts (Unified hexagons and Unified threads) (ordinary, thin, slotted and castle) for aircraft...
BS 3A 105:1962
Specification for corrosion-resisting steel nuts (Unified hexagons and Unified threads) (ordinary, thin, slotted and cas...
BS 3A 107:1962+A2:2018
Aerospace series. Specification for aluminium alloy nuts (Unified hexagons and Unified threads) (ordinary and slotted) f...
BS 3A 108:1962
Specification for steel bolts (Unified hexagons and Unified threads) with close tolerance shanks for aircraft...
BS 3A 117:1962+A2:2016
Aerospace Series. Bolts, Pan Head, Slotted Drive, Unified Threads, Corrosion Resisting Steel, Strength Class 880 MPa, fo...
BS 3A 171:1962
Specification for aluminium alloy pan head bolts (Unified threads) for aircraft...