How Do I
BSI Standards List
Standard
Year
Title
Specification for aircraft material. Carbon steel bright bars for machining (35/45 tonf/sq in; maximum size, 4 inches diameter or minor sectional dimension)
Specification for aircraft material. 3 per cent nickel case-hardening steel
Specification for aircraft material. '20' carbon steel (suitable for welding) (25/35 tonf/sq in: maximum size 6 inches diameter or minor sectional dimension)
Specification for aircraft material. 4 per cent nickel-chromium-molybdenum steel (air hardening) (100 tonf/sq in: limiting ruling section 21/2 in)
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 11/8 in)
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)
Specification for 11/2 per cent nickel-chromium-molybdenum steel (90/110 kgf/mm2 (57/70 tonf/in2): limiting ruling section 150 mm (6 in))
21/2 per cent nickel-chromium-molybdenum steel (55/65 tonf/sq in: limiting ruling section 6 in)
Specification for aircraft material. 21/2 per cent nickel-chromium-molybdenum steel (65/75 tonf/sq in: limiting ruling section 6 in)
Specification for aircraft material. 21/2 per cent nickel-chromium-molybdenum steel (high carbon) (75/85 tonf/sq in: limited ruling section 6 in)
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 for aircraft material. Nickel-chromium-tungsten valve steel
Specification for aircraft material. Semi-free cutting carbon steel, bright bars for machining (40-50 tonf/sq in: maximum size 1/2 inch diameter or minor sectional dimension) (primarily intended for the manufacture of nuts)
Specification for aircraft material. '40' carbon steel bright bars for machining (45-55 tonf/sq in: limiting ruling section 1 inch) (primarily intended for the manufacture of nuts)
Specification for aircraft material. Manganese-molybdenum steel (55/65 tonf/sq in: limiting ruling section 21/2 inches)
Specification for aircraft material. '40' carbon steel bright bars for machining (55-65 tonf/sq in: limiting ruling section 3/4 inch) (primarily intended for the manufacture of machined bolts)
Specification for aircraft material. 1 per cent chromium steel (55/65 tonf/sq in: limiting ruling section 11/8 inch)
Specification for aircraft material. 11/2 per cent nickel-chromium-molybdenum steel (65/75 tonf/sq in: limiting ruling section 21/2 in)
Specification for aircraft material. 21/2 per cent nickel-chromium-molybdenum steel (oil hardening) (100 tonf/sq in: limiting ruling section 21/2 in)
Specification for aircraft material. 12 per cent chromium corrosion-resisting steel (free machining) (45/55 tonf/sq in: limiting ruling section 6 in)
Specification for aircraft material. 23/14 chromium-nickel heat-resisting steel (titanium stabilized) (35 tonf/sq in: limiting ruling section 6 in)
Specification for aircraft material. 23/14 chromium-nickel heat-resisting steel (niobium stabilized) (35 tonf/sq in: limiting ruling section 6 in)
Specification for aircraft material. 24/17 chromium-nickel heat-resisting steel (titanium stabilized) (35 tonf/sq in: limiting ruling section 6 in)
Specification for aircraft material. 24/17 chromium-nickel heat-resisting steel (niobium stabilized) (35 tonf/sq in: limiting ruling section 6 in)
Specification for 18/9 chromium-nickel corrosion-resisting steel (titanium stabilized) billets, bars, forgings and parts (540 MPa: limiting ruling section 150 mm)
Specification for aircraft material. 3/4 per cent nickel-chromium case-hardening steel
Specification for aircraft material. 3 per cent chromium-molybdenum-vanadium steel (air hardening) (100 tonf/sq in: limiting ruling section 11/8 inches)
Specification for 3 per cent chromium-molybdenum-vanadium steel (vacuum remelted - air hardening) (157 kgf/mm2 (100 tonf/in2): limiting ruling section 30 mm (11/8 in))
Specification for 11/2 per cent nickel-chromium-molybdenum steel (110/130 kgf/mm2 (70/83 tonf/in2): limiting ruling section 70 mm (23/4 in))
Specification for 12 per cent chromium corrosion-resisting steel (60/80 kgf/mm2 (38/51 tonf/in2): limiting ruling section 150 mm (6in))
Specification for low nickel-chromium steel (bar for the manufacture of forged bolts only)
Specification for chromium-molybdenum-vanadium-niobium heat-resisting steel billets, bars, forgings and parts (930-1080 MPa) (Cr 10.5, Mo 0.6, V 0.2, Nb 0.3)
Specification for chromium-cobalt-molybdenum-vanadium-niobium heat-resisting steel billets, bars, forgings and parts (consumable electrode remelted) (1000-1140 MPa) (Cr 10.5, Co 6, Mo 0.8, V 0.2, Nb 0.3)
Specification. 21/2% nickel-chromium-molybdenum steel billets, bars, forgings and parts (1230-1430 MPa: limiting ruling section 40 mm)
Specification. 21/2% nickel-chromium-molybdenum steel billets, bars, forgings and parts (880-1080 MPa: limiting ruling section 150 mm)
Specification for nickel-silicon-chromium-molybdenum-vanadium steel (vacuum arc remelted) billets, bars, forgings and parts (1900-2100 MPa: limiting ruling section 75 mm)
Specification for 4% nickel-chromium-molybdenum case-hardening steel (vacuum arc remelted) billets, bars, forgings and parts (1320-1520 MPa)
Specification. 3% nickel-chromium-molybdenum case-hardening steel billets, bars, forgings and parts (1180-1380 MPa)
Specification for 1% chromium-molybdenum steel bars for the manufacture of forged bolts and forged nuts
Specification for 12% chromium-nickel-molybdenum-vanadium heat-resisting steel bars for the manufacture of fasteners (1100-1300 MPa: limiting ruling section 50 mm)
Specification for chromium-nickel corrosion-resisting steel - bright bars and parts (540 MPa, limiting ruling section 160 mm) (Cr 18, Ni 10.5, controlled nitrogen content)
Specification for chromium-nickel-molybdenum corrosion-resisting steel. Bright bars and parts (540 MPa, limiting ruling section 160 mm) (Cr 17.5, Ni 12.5, Mo 2.25, controlled nitrogen content)
Specification for nickel-chromium-molybdenum-vanadium steel forging stock, forgings, bars and parts (1900 MPa : limiting ruling section 100 mm)
Specification for patented cold drawn carbon steel wire and springs (high duty unground wire)
Specification for patented cold drawn carbon steel wire and springs (high duty ground wire)
Specification for carbon steel wire and springs (high duty unground wire - hardened and tempered)
Specification for chromium-vanadium steel wire and springs (high duty ground wire - hardened and tempered)
Specification for austenitic chromium-nickel steel wire and springs
Chromium-nickel-aluminium corrosion resisting steel (precipitation hardening) rod, cold drawn wire and springs
Procedure for inspection, testing and acceptance of steel sheet and strip
Tinned steel sheets and strips
Specification for carbon-manganese steel sheet and strip (93/116 hbar)
Specification for carbon-manganese steel sheet and strip (116/131 hbar)
Specification for cold-rolled 18/10 chromium-nickel corrosion-resisting steel sheet and strip (titanium stabilized: 800 MPa)
Specification for cold-rolled 18/10 chromium-nickel corrosion-resisting steel sheet and strip (niobium stabilized: 800 MPa)
Specification for softened 18/10 chromium-nickel corrosion-resisting steel sheet and strip (titanium stabilized: 540 MPa)
Specification for softened 18/10 chromium-nickel corrosion-resisting steel sheet and strip (niobium stabilized: 540 MPa)
Specification for 23/14 chromium-nickel heat-resisting steel sheet and strip (titanium stabilized: 54 hbar) (elevated temperature properties not verified)
Specification for 23/14 chromium-nickel heat-resisting steel sheet and strip (niobium stabilized: 54 hbar) (elevated temperature properties not verified)
Specification for 24/17 chromium-nickel heat-resisting steel sheet and strip (titanium stabilized: 540 MPa) (elevated temperature properties not verified)
Specification for 24/17 chromium-nickel heat-resisting steel sheet and strip (niobium stabilized: 54 hbar) (elevated temperature properties not verified)
Specification for chromium-nickel-copper-molybdenum corrosion-resisting steel sheet and strip (precipitation hardening: 980/1180 MPa)
Specification for chromium-nickel-copper-molybdenum corrosion-resisting steel sheet and strip (precipitation hardening: 1180/1370 MPa)
Specification for chromium-molybdenum steel sheet and strip (880/1080 MPa (suitable for welding)
Specification for chromium-molybdenum steel sheet and strip (1150/1300 Mpa) (suitable for welding)
Specification for low carbon 18/10 chromium-nickel corrosion-resisting steel sheet and strip (500 MPa)
Specification for low carbon 17/12 chromium-nickel-molybdenum corrosion-resisting steel sheet and strip (500 MPa)
Specification for chromium-nickel-molybdenum-vanadium heat-resisting steel sheet and strip (930-1130 MPa: maximum thickness 6 mm) (Cr 12, Ni 2.5, Mo 1.7, V 0.3)
