Specification for plate of titanium-aluminium-vanadium alloy (tensile strength 895-1150 MPa) (maximum thickness 100 mm)
Document status: Active
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)
Document status: Active
Specification for plate of titanium-copper alloy (tensile strength 520-640 MPa) (maximum thickness 10 mm)
Document status: Active
Specification for sheet of titanium-aluminium-vanadium alloy (tensile strength 920-1180 MPa)
Document status: Active
Specification for sheet and strip of commercially pure titanium (tensile strength 570-730 N/mm2)
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Specification for forgings of commercially pure titanium (tensile strength 540-740 N/mm2)
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Specification for aircraft material. Preformed corrosion-resisting steel wire rope
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Specification for aircraft material. Preformed galvanized carbon steel wire rope
Document status: Active
Specification for shellac varnish for aeronautical purposes
Document status: Active
Specification for pre-treatment etch primer for aerospace purposes
Document status: Active
