Aluminium-coated sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8)

Specification for ingots and castings of aluminium-silicon-copper-magnesium alloy (solution treated and precipitation treated) (Si 5, Cu 1.2, Mg 0.5)

Specification for sheet and strip of aluminium-2¼% magnesium alloy (temper designation-O)

Specification for sheet and strip of aluminium-2¼% magnesium alloy (temper designation H16 or H26)

Specification for wire for solid, cold-forged rivets of aluminium-copper-magnesium alloy (not exceeding 10 mm diameter) (Cu 2.5, Mg 0.3)

Separable tube fittings for fluid systems, 24° cone. General specification

Specification for general design requirements for aircraft oxygen systems and equipment

Breathing oxygen for airborne applications

Specification for carbon-molybdenum steel (bar for the manufacture of forged bolts only)

Specification for Carbon steel. (Bar for the manufacture of forged bolts only)

3 per cent nickel-chromium-molybdenum case-hardening steel

Specification. 3% chromium-molybdenum-vanadium steel billets, bars, forgings and parts (1320-1470 MPa: limiting ruling section 70 mm) (suitable for nitriding)

Specification for chromium-nickel-copper-molybdenum corrosion resisting steel (precipitation hardening) billets, bars, forgings and parts (1130-1330 MPa)

Procedure for inspection, testing and acceptance of steel sheet and strip

Specification for aircraft material. 12 per cent chromium corrosion-resisting steel (35/45 tonf/sq in: limiting ruling section 6 in)

Specification for aircraft material. 12 per cent chromium corrosion-resisting steel (45/55 tonf/sq in: limiting ruling section 6 in)

Specification for aircraft material. '55' carbon steel (normalized) (45/55 tonf/sq in: limiting ruling section 4 in)

Specification for aircraft material. '55' carbon steel (hardened and tempered) (55/65 tonf/sq in: limiting ruling section 1⅛ in)

Specification for mild steel billets, bars, forgings and parts (suitable for bearing shells)

Specification for 1½ per cent nickel-chromium-molybdenum steel. (880/1080 MPa: limiting ruling section 150 mm)

Specification for 2.5% nickel-chromium-molybdenum (high carbon) steel billets, bars, forging and parts (1 160 - 1 310 MPa: limiting ruling section 155 mm)

Specification. Shackles, carbon steel, cadmium plated for aircraft

Specification for aircraft material. Fork joints (low tensile type) (for sizes No. 4 B.A. to ½ inch B.S.F. inclusive)

Specification for characteristics, boundary dimensions, tolerances and static load ratings of airframe bearings

Procedure for inspection and testing of steel tubes