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BS 4L 56:1986 Specification for tube of aluminium-2ΒΌ% magnesium alloy (temper designation-O) (seamless: tested hydraulically) (not exceeding 12 mm wall thickness)
BS 4N 100-1:1999+A3:2018 Aircraft oxygen systems and equipment Design installation
BS 4N 100-3:1999 Aircraft oxygen systems and equipment Testing of
BS 4N 100-4:1999+A2:2018 Aircraft oxygen systems and equipment Guide to the physiological factors
BS 4N 100-6:1999+A1:2018 Aircraft oxygen systems and equipment Guidance recommendations on the selection of materials for use with
BS 4S 106:1976 Specification. 3% chromium-molybdenum steel billets, bars, forgings and parts (930-1080 MPa: limiting ruling section 150 mm) (suitable for nitriding)
BS 4S 14:1964+A2:2015 Specification for Carbon case-hardening steel
BS 4S 28:1964+A3:2015 Specification for 4 per cent nickel-chromium-molybdenum steel (Air hardening). (1545 MPa: limiting ruling section 63.5mm)
BS 4S 500:2010 Aerospace series. Procedure for inspection, testing and acceptance of steel sheet and strip
BS 4T 45:1972+A2:2015 Specification for carbon manganese steel tube (700 MPa) (Tube 12.5 mm outside diameter and greater) (Weldable)
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