BS 4A 169:2002
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Specification for aluminium alloy bolts (Unified hexagons and Unified threads) for aircraft
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BS 7S 80:2002
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High chromium-nickel corrosion resisting steel forging stock, bars, forgings and parts (880 to 1080 MPa: limiting ruling section 100 mm)
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BS 2S 511:1970
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Specification for deep drawing carbon steel sheet and strip (280/400 MPa) (suitable for welding)
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BS 3S95(1967) : 1967
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SPECIFICATION FOR 1[1/2] PER CENT NICKEL-CHROMIUM-MOLYBDENUM STEEL - (880/1080 MPA: LIMITING RULING SECTION 150 MM)
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BS 2S 114:1964
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Specification for aircraft material. Manganese-molybdenum steel (55/65 tonf/sq in: limiting ruling section 2½ inches)
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BS S526(1969) : 1969
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AEROSPACE SERIES - SPECIFICATION FOR SOFTENED 18/10 CHROMIUM-NICKEL CORROSION-RESISTING STEEL SHEET AND STRIP (TITANIUM STABILIZED: 540 MPA)
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DEFSTAN 91-114/1(2003) : 2003
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LUBRICATING OIL, AIRCRAFT CONTROLS: ANTIFREEZING JOINT SERVICE DESIGNATION: OM-150
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BS 2S 113:1964
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Specification for aircraft material. \'40\' carbon steel bright bars for machining (45-55 tonf/sq in: limiting ruling section 1 inch) (primarily intended for the manufacture of nuts)
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BS 4A102(2002) : 2002
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AEROSPACE SERIES - SPECIFICATION FOR STEEL BOLTS (UNIFIED HEXAGONS AND UNIFIED THREADS) FOR AIRCRAFT
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BS 2HR 205:2009
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Specification for nickel-copper alloy sheet and strip: annealed (nickel base, Cu 31)
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DEFSTAN 03-9/3(2007) : 2007
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ELECTRO-DEPOSITION OF SILVER
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BS S 154:1976
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Specification. 2½% nickel-chromium-molybdenum steel billets, bars, forgings and parts (880-1080 MPa: limiting ruling section 150 mm)
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BS 3L 80:1985
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Specification for sheet and strip of aluminium-2¼% magnesium alloy (temper designation-O)
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BS 1580-1:2007
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Unified screw threads Screw threads with diameters ¼ in and larger. Requirements
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BS 2S 92:1964
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Specification for aircraft material. Carbon-manganese steel (suitable for welding) (40/55 tonf/sq in: limiting ruling section 4 in)
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DEFSTAN 03-25/5(2008) : 2008
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SULFURIC ACID ANODIZING OF ALUMINIUM AND ALUMINIUM ALLOYS
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BS EN 2133:2010
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Aerospace series. Cadmium plating of steels with specified tensile strength ≤ 1450 MPa, copper, copper alloys and nickel alloys
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BS 2S 137:1976
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Specification for high chromium-nickel corrosion-resisting steel bright bars (free machining) (880-1080 MPa: limiting ruling section 70 mm)
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BS L 163:1978
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Specification for sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy (solution treated, cold worked for flattening and aged at room temperature) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8)
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BS 2S 112:1964
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Specification for aircraft material. Semi-free cutting carbon steel, bright bars for machining (40-50 tonf/sq in: maximum size ½ inch diameter or minor sectional dimension) (primarily intended for the manufacture of nuts)
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BS 2S 117:1964
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Specification for aircraft material. 1 per cent chromium steel (55/65 tonf/sq in: limiting ruling section 1⅛ inch)
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BS L 168:1978
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Specification for bars and extruded sections of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and artificially aged) (not exceeding 200 mm diameter or minor sectional dimension) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8)
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BS 4A104(2002) : 2002
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AEROSPACE SERIES - SPECIFICATION FOR CORROSION-RESISTING STEEL BOLTS (UNIFIED HEXAGONS AND UNIFIED THREADS), STRENGTH CLASS 880 MPA, FOR AIRCRAFT
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BS 3L 81:1985
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Specification for sheet and strip of aluminium-2¼% magnesium alloy (temper designation H16 or H26)
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BS 2S 510:1970
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Specification for carbon steel sheet and strip (430/540 MPa) (suitable for welding)
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BS S527(1969) : 1969
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AEROSPACE SERIES - SPECIFICATION FOR SOFTENED 18/10 CHROMIUM-NICKEL CORROSION-RESISTING STEEL SHEET AND STRIP (NIOBIUM STABILIZED: 540 MPA)
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DEFSTAN 03-19/4(2010) : 2010
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ELECTRO-DEPOSITION OF CADMIUM
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DEFSTAN 80-217/1(2002) : 2002
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CORROSION PREVENTIVE COMPOUND: SOFT FILM, COLD APPLICATION NATO CODE: C-614 JOINT SERVICES DESIGNATION: PX-1
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