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BS 2SP 87 and 2SP 88:1973+A3:- 2015 ...
BS 2SP 77 to 2SP 80:1973+A4:- 2015 ...
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BS 2TA 49:2009 Specification for bar and section for machining of titanium-aluminium- molybdenum-tin-silicon-carbon alloy (Tensile strength 1000-1200 MPa) (Limiting ruling section over 100 mm up to and including 150 mm)
BS 2TA 50:2009 Specification for forging stock of titanium- aluminium-molybdenum-tin-silicon alloy (tensile strength 1000-1200 MPa) (limiting ruling section over 100 mm up to and including 150 mm)
BS 2TA 52:2009 Specification for sheet and strip of titanium- copper alloy (tensile strength 690-920 MPa)
BS 2TA 56:2009 Specification for plate of titanium-aluminium-vanadium alloy (tensile strength 895-1150 MPa) (maximum thickness 100 mm)
BS 2TA 57:2009 Specification for plate of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1030-1220 MPa) (thickness over 50 mm up to and including 65 mm)
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 2X 26:2001 Doping and finishing schemes for fabric covered aircraft
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