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BSI Standards List

Standard
Year
Title
BS S 1
1964
Specification for aircraft material. Carbon steel bright bars for machining (35/45 tonf/sq in; maximum size, 4 inches diameter or minor sectional dimension)
BS S 15
1964
Specification for aircraft material. 3 per cent nickel case-hardening steel
BS S 21
1964
Specification for aircraft material. '20' carbon steel (suitable for welding) (25/35 tonf/sq in: maximum size 6 inches diameter or minor sectional dimension)
BS S 28
1964
Specification for aircraft material. 4 per cent nickel-chromium-molybdenum steel (air hardening) (100 tonf/sq in: limiting ruling section 21/2 in)
BS S 61
1964
Specification for aircraft material. 12 per cent chromium corrosion-resisting steel (35/45 tonf/sq in: limiting ruling section 6 in)
BS S 62
1964
Specification for aircraft material. 12 per cent chromium corrosion-resisting steel (45/55 tonf/sq in: limiting ruling section 6 in)
BS S 70
1964
Specification for aircraft material. '55' carbon steel (normalized) (45/55 tonf/sq in: limiting ruling section 4 in)
BS S 79
1964
Specification for aircraft material. '55' carbon steel (hardened and tempered) (55/65 tonf/sq in: limiting ruling section 11/8 in)
BS S 92
1964
Specification for aircraft material. Carbon-manganese steel (suitable for welding) (40/55 tonf/sq in: limiting ruling section 4 in)
BS S 93
1964
Specification for aircraft material. '40' carbon steel (normalized) (35/45 tonf/sq in: limiting ruling section 6 in)
BS S 95
1967
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))
BS S 96
1964
21/2 per cent nickel-chromium-molybdenum steel (55/65 tonf/sq in: limiting ruling section 6 in)
BS S 97
1964
Specification for aircraft material. 21/2 per cent nickel-chromium-molybdenum steel (65/75 tonf/sq in: limiting ruling section 6 in)
BS S 98
1964
Specification for aircraft material. 21/2 per cent nickel-chromium-molybdenum steel (high carbon) (75/85 tonf/sq in: limited ruling section 6 in)
BS S 102
1969
Specification for carbon-molybdenum steel (bar for the manufacture of forged bolts only)
BS S 105
1969
Specification for carbon steel (bar for the manufacture of forged bolts only)
BS S 107
1969
3 per cent nickel-chromium-molybdenum case-hardening steel
BS S 111
1964
Specification for aircraft material. Nickel-chromium-tungsten valve steel
BS S 112
1964
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)
BS S 113
1964
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)
BS S 114
1964
Specification for aircraft material. Manganese-molybdenum steel (55/65 tonf/sq in: limiting ruling section 21/2 inches)
BS S 116
1964
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)
BS S 117
1964
Specification for aircraft material. 1 per cent chromium steel (55/65 tonf/sq in: limiting ruling section 11/8 inch)
BS S 119
1964
Specification for aircraft material. 11/2 per cent nickel-chromium-molybdenum steel (65/75 tonf/sq in: limiting ruling section 21/2 in)
BS S 120
1964
Specification for aircraft material. 21/2 per cent nickel-chromium-molybdenum steel (oil hardening) (100 tonf/sq in: limiting ruling section 21/2 in)
BS S 124
1964
Specification for aircraft material. 12 per cent chromium corrosion-resisting steel (free machining) (45/55 tonf/sq in: limiting ruling section 6 in)
BS S 125
1964
Specification for aircraft material. 23/14 chromium-nickel heat-resisting steel (titanium stabilized) (35 tonf/sq in: limiting ruling section 6 in)
BS S 126
1964
Specification for aircraft material. 23/14 chromium-nickel heat-resisting steel (niobium stabilized) (35 tonf/sq in: limiting ruling section 6 in)
BS S 127
1964
Specification for aircraft material. 24/17 chromium-nickel heat-resisting steel (titanium stabilized) (35 tonf/sq in: limiting ruling section 6 in)
BS S 128
1964
Specification for aircraft material. 24/17 chromium-nickel heat-resisting steel (niobium stabilized) (35 tonf/sq in: limiting ruling section 6 in)
BS S 129
1976
Specification for 18/9 chromium-nickel corrosion-resisting steel (titanium stabilized) billets, bars, forgings and parts (540 MPa: limiting ruling section 150 mm)
BS S 133
1965
Specification for aircraft material. 3/4 per cent nickel-chromium case-hardening steel
BS S 134
1965
Specification for aircraft material. 3 per cent chromium-molybdenum-vanadium steel (air hardening) (100 tonf/sq in: limiting ruling section 11/8 inches)
BS S 138
1967
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))
BS S 139
1968
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))
BS S 141
1968
Specification for 12 per cent chromium corrosion-resisting steel (60/80 kgf/mm2 (38/51 tonf/in2): limiting ruling section 150 mm (6in))
BS S 148
1969
Specification for low nickel-chromium steel (bar for the manufacture of forged bolts only)
BS S 150
1975
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)
BS S 152
1975
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)
BS S 153
1976
Specification. 21/2% nickel-chromium-molybdenum steel billets, bars, forgings and parts (1230-1430 MPa: limiting ruling section 40 mm)
BS S 154
1976
Specification. 21/2% nickel-chromium-molybdenum steel billets, bars, forgings and parts (880-1080 MPa: limiting ruling section 150 mm)
BS S 155
1976
Specification for nickel-silicon-chromium-molybdenum-vanadium steel (vacuum arc remelted) billets, bars, forgings and parts (1900-2100 MPa: limiting ruling section 75 mm)
BS S 156
1976
Specification for 4% nickel-chromium-molybdenum case-hardening steel (vacuum arc remelted) billets, bars, forgings and parts (1320-1520 MPa)
BS S 157
1976
Specification. 3% nickel-chromium-molybdenum case-hardening steel billets, bars, forgings and parts (1180-1380 MPa)
BS S 158
1977
Specification for 1% chromium-molybdenum steel bars for the manufacture of forged bolts and forged nuts
BS S 159
1981
Specification for 12% chromium-nickel-molybdenum-vanadium heat-resisting steel bars for the manufacture of fasteners (1100-1300 MPa: limiting ruling section 50 mm)
BS S 160
1990
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)
BS S 161
1990
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)
BS S 163
1990
Specification for nickel-chromium-molybdenum-vanadium steel forging stock, forgings, bars and parts (1900 MPa : limiting ruling section 100 mm)
BS S 201
1967
Specification for patented cold drawn carbon steel wire and springs (high duty unground wire)
BS S 202
1967
Specification for patented cold drawn carbon steel wire and springs (high duty ground wire)
BS S 203
1967
Specification for carbon steel wire and springs (high duty unground wire - hardened and tempered)
BS S 204
1967
Specification for chromium-vanadium steel wire and springs (high duty ground wire - hardened and tempered)
BS S 205
1969
Specification for austenitic chromium-nickel steel wire and springs
BS S 206
1999
Chromium-nickel-aluminium corrosion resisting steel (precipitation hardening) rod, cold drawn wire and springs
BS S 500
1996
Procedure for inspection, testing and acceptance of steel sheet and strip
BS S 512
1956
Tinned steel sheets and strips
BS S 516
1969
Specification for carbon-manganese steel sheet and strip (93/116 hbar)
BS S 517
1969
Specification for carbon-manganese steel sheet and strip (116/131 hbar)
BS S 524
1969
Specification for cold-rolled 18/10 chromium-nickel corrosion-resisting steel sheet and strip (titanium stabilized: 800 MPa)
BS S 525
1969
Specification for cold-rolled 18/10 chromium-nickel corrosion-resisting steel sheet and strip (niobium stabilized: 800 MPa)
BS S 526
1969
Specification for softened 18/10 chromium-nickel corrosion-resisting steel sheet and strip (titanium stabilized: 540 MPa)
BS S 527
1969
Specification for softened 18/10 chromium-nickel corrosion-resisting steel sheet and strip (niobium stabilized: 540 MPa)
BS S 528
1970
Specification for 23/14 chromium-nickel heat-resisting steel sheet and strip (titanium stabilized: 54 hbar) (elevated temperature properties not verified)
BS S 529
1970
Specification for 23/14 chromium-nickel heat-resisting steel sheet and strip (niobium stabilized: 54 hbar) (elevated temperature properties not verified)
BS S 530
1970
Specification for 24/17 chromium-nickel heat-resisting steel sheet and strip (titanium stabilized: 540 MPa) (elevated temperature properties not verified)
BS S 531
1970
Specification for 24/17 chromium-nickel heat-resisting steel sheet and strip (niobium stabilized: 54 hbar) (elevated temperature properties not verified)
BS S 532
1969
Specification for chromium-nickel-copper-molybdenum corrosion-resisting steel sheet and strip (precipitation hardening: 980/1180 MPa)
BS S 533
1969
Specification for chromium-nickel-copper-molybdenum corrosion-resisting steel sheet and strip (precipitation hardening: 1180/1370 MPa)
BS S 534
1969
Specification for chromium-molybdenum steel sheet and strip (880/1080 MPa (suitable for welding)
BS S 535
1969
Specification for chromium-molybdenum steel sheet and strip (1150/1300 Mpa) (suitable for welding)
BS S 536
1970
Specification for low carbon 18/10 chromium-nickel corrosion-resisting steel sheet and strip (500 MPa)
BS S 537
1970
Specification for low carbon 17/12 chromium-nickel-molybdenum corrosion-resisting steel sheet and strip (500 MPa)
BS S 538
1975
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)