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 3G 100-2.3.7:1972
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Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Tropical exposure
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BS 3G 100-2.3.13:1973
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Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Resistance to fire in designated fire zones
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BS 3G 100-2.3.10:1974
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Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Impact icing
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BS 2TA 23:1973
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Specification for forging stock of titanium-copper alloy (tensile strength 540-770 N/mm<sup>2</sup>)
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BS 3G 100-2.3.9:1972
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Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Ice formation
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BS 2TA 8:1973
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Specification for forging stock of commercially pure titanium (tensile strength 540-740 N/mm<sup>2</sup>)
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BS 3G 100-2.3.4:1972
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Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Differential pressure requirements
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BS 2L 503:1973
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Specification for tube of magnesium-6% aluminium-zinc alloy (Al 6.0, Zn 1.0)
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BS 3A 105:1962
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Specification for corrosion-resisting steel nuts (Unified hexagons and Unified threads) (ordinary, thin, slotted and castle) for aircraft
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BS 2TA 24:1973
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Specification for forgings of titanium-copper alloy (tensile strength 540-770 N/mm<sup>2</sup>)
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BS 3129:1959
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Specification for latex foam rubber components for furniture
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BS 3348:1961
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Specification for antral trocars and cannulae
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BS 2TA 11:1974
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Specification for bar and section for machining of titanium-aluminium-vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm)
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BS 2T 68:1980
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Specification for cold drawn 18/10 chromium-nickel corrosion-resisting steel tube (niobium stabilized: 800 MPa) (weldable)
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BS 2TA 7:1973
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Specification for bar and section for machining of commercially pure titanium (tensile strength 540-740 N/mm<sup>2</sup>)
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BS 3G 100-2.3.14:1973
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Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Acoustic vibration
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PD 6430:1969
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The adoption of the metric system in the marine industry: report, basic programme and guide
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BS 2L 504:1973
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Specification for sheet and strip of magnesium-3% zinc-zirconium alloy (Zn 3.0, Zr 0.6)
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BS 2TA 9:1973
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Specification for forgings of commercially pure titanium (tensile strength 540-740 N/mm<sup>2</sup>)
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BS 2TA 13:1974
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Specification for forgings of titanium-aluminium-vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm)
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BS CP118(1969) : 1969 AMD 1129
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THE STRUCTURAL USE OF ALUMINIUM
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BS 2L 509:1973
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Specification for tube of magnesium-1¼% zinc-zirconium alloy (suitable for welding by inert-gas shielded arc techniques) (Zn 1.25, Zr 0.6)
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BS 2TA 22:1973
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Specification for bar and section for machining of titanium-copper alloy (tensile strength 540-770 N/mm<sup>2</sup>)
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BS 2L 508:1973
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Specification for bars and extruded sections of magnesium-1¼% zinc-zirconium alloy (suitable for welding by inert-gas shielded arc techniques) (not exceeding 50 mm diameter or minor sectional dimension) (Zn 1.25, Zr 0.6)
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BS 2TA 12:1974
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Specification for forging stock of titanium-aluminium-vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm)
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BS 350-2:SUPP1(1967) : 1967
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CONVERSION FACTORS AND TABLES - DETAILED CONVERSION TABLES - ADDITIONAL TABLES FOR SI CONVERSIONS
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BS 2L 505:1973
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Specification for bars and extruded sections of magnesium-3% zinc-zirconium alloy (not exceeding 100 mm diameter or minor sectional dimension) (Zn 3.0, Zr 0.6)
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BS 2W 11:1967
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Specification for aircraft material. Preformed corrosion-resisting steel wire rope
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BS 2A204,2A206,2A208,A217-A225(1963) : 1963 PD 6167
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SPECIFICATIONS FOR MACHINE SCREWS AND NUTS (UNIFIED THREADS) BELOW 1/4 INCH FOR AERONAUTICAL PURPOSES
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BS 3G 100-2.3.5:1972
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Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Explosion-proofness
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BS 2V 35:1966
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Specification for plywood for aeronautical purposes
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BS CP1018(1971) : 1971
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ELECTRIC FLOOR WARMING SYSTEMS FOR USE WITH OFF-PEAK AND SIMILAR SUPPLIES OF ELECTRICITY
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BS 3G 100-2.3.11:1973
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Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Water-proofness
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