Chromium-vanadium steel wire rod, wire and springs. High duty ground wire. Hardened and tempered. Specification

Austenitic chromium-nickel steel wire rod, wire and springs. Specification

Inspection and testing procedure for steel sheet and strip

Specification for carbon steel sheet and strip (430/540 MPa) (suitable for welding)

Specification for deep drawing carbon steel sheet and strip (280/400 MPa) (suitable for welding)

Specification for spring steel strip

Specification for carbon-manganese steel sheet and strip (for use in the hardened and tempered condition: 770/1000 MPa) (suitable for welding)

Specification for carbon-manganese steel sheet and strip (softened) (for use in the softened condition: 460/600MPa) (suitable for welding)

Specification for carbon-manganese steel sheet and strip (93/116 hbar)

Specification for carbon-manganese steel sheet and strip (116/131 hbar)

Specification for aircraft material. Carbon-manganese steel (suitable for welding) (40/55 tonf/sq in: limiting ruling section 4 in)

Specification for aircraft material. '40' carbon steel (normalized) (35/45 tonf/sq in: limiting ruling section 6 in)

2½ per cent nickel-chromium-molybdenum steel (55/65 tonf/sq in: limiting ruling section 6 in)

Specification 2½ per cent nickel-chromium-molybdenum steel. (1000/1160 MPa: limiting ruling section 150 mm)

Specification for aircraft material. 2½ per cent nickel-chromium-molybdenum steel (high carbon) (75/85 tonf/sq in: limited ruling section 6 in)

Specification for aircraft material. Shackles

Specification for swaged cable-end assemblies (Unified threads) for preformed steel wire rope (W.9) for aircraft

Specification for swaged cable-end assemblies (Unified threads) for preformed non-corrodible steel wire rope (W.11) for aircraft

Single coil spring washers for aircraft

Specification for aircraft material. Fork joints (high tensile type) (for sizes No. 4 B.A. to ¾ inch B.S.F. inclusive)

Specification for corrosion-resisting steel split cotter pins for aircraft. Inch series

Specification for elastomeric grommets (acrylonitrile-butadiene) for aerospace use

Aerospace series. Bushes (plain and flanged), press-fit and thrust washers, oil‑retaining sintered bronze. Specification

Specification for internal retaining rings (imperial sizes)

Specification for 4/1 nickel-chromium steel tube (1150 N/mm²)