BS 3763:1970
Withdrawn
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
View Superseded by
The International System of units (SI)
Available format(s)
Hardcopy
Withdrawn date
23-07-2013
Superseded by
Language(s)
English
Published date
22-12-1970
Publisher
Important note : All end users must be registered with an Account prior to user licenses being assigned.| DocumentType |
Standard
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| Pages |
0
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| PublisherName |
British Standards Institution
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| Status |
Withdrawn
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| SupersededBy |
| BS TA 52:1973 | Specification for sheet and strip of titanium-copper alloy (tensile strength 690-920 N/mm<sup>2</sup>) |
| BS 2TA 4:1973 | Specification for forging stock of commercially pure titanium (tensile strength 390-540 N/mm<sup>2</sup>) |
| BS TA 54:1973 | Specification for forging stock of titanium-copper alloy (tensile strength 650-880 N/mm<sup>2</sup>) (limiting ruling section 75 mm) |
| BS 2L 98:1971 | Specification for plate of aluminium-copper-magnesium-manganese alloy (solution treated and aged at room temperature: not controlled stretched) (Cu 4.4, Mg 1.5, Mn 0.6) |
| BS 9074 N002:1974 | Detail specification for fixed polystyrene foil dielectric capacitors. Tubular insulated case, axial terminations. Full asessment level |
| BS TA 50:1973 | Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1000-1200 N/mm<sup>2</sup>) (limiting ruling section over 100 mm up to and including 150 mm) |
| BS 2HR 503:1973 | Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy wire for thread inserts (0.45 mm to 2 mm diameter) (nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5) |
| BS L 168:1978 | Specification for bars and extruded sections of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and artificially aged) (not exceeding 200 mm diameter or minor sectional dimension) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8) |
| BS TA 48:1973 | Specification for forgings of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1050-1200 N/mm<sup>2</sup>) (limiting ruling section 100 mm) |
| BS L 155:1977 | Specification for ingots and castings of aluminium-copper-silicon alloy (solution treated and artificially aged) (Cu 4, Si 1) |
| BS 2HR 201:1974 | Specification for nickel-chromium-titanium-aluminium heat-resisting alloy plate, sheet and strip (nickel base, Cr 19.5, Ti 2.2, Al 1.4) |
| BS TA 38:1971 | Specification for bar for machining of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1250-1420 N/mm<sup>2</sup>) (limiting ruling section 25 mm) |
| BS L 166:1978 | Specification for close toleranced sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8) |
| BS L 158:1978 | Specification for close toleranced sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8) |
| BS 2HR 1:1973 | Specification for nickel-chromium-titanium-aluminium heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 19.5, Ti 2.2, Al 1.4) |
| BS 3G 100-2.3.0:1972 | Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Standard test requirements |
| BS 3G 100-2.3.3:1972 | Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Mould growth |
| BS 2HR 501:1973 | Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy cold drawn wire for springs (nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5) |
| BS L 161:1976 | Specification. Hand and die forgings of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and artificially aged to an overaged condition) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.22) |
| BS 41:1973 | Specification for cast iron spigot and socket flue or smoke pipes and fittings |
| BS 3L 58:1971 | Specification for wire for solid, cold-forged rivets of aluminium-5% magnesium alloy (not exceeding 10 mm diameter) |
| BS 2HR 504:1973 | Specification for nickel-chromium-titanium heat-resisting alloy bar, wire and rivets (nickel base, Cr 19.5, Ti 0.4) |
| BS 2L 97:1971 | Specification for plate of aluminium-copper-magnesium-manganese alloy (solution treated, controlled stretched and aged at room temperature) (Cu 4.4, Mg 1.5, Mn 0.6) |
| BS T 64:1972 | Specification for carbon-manganese steel tube (550 N/mm<sup>2</sup>) (tube less than 12.5 mm outside diameter) (weldable) |
| BS 5T 2:1972 | Specification for 4/1 nickel-chromium steel tube (1300 N/mm<sup>2</sup>) |
| BS 2L 83:1971 | Specification for forging stock, bars, extruded sections and forgings of aluminium-copper-nickel-magnesium-iron-silicon alloy (solution treated and precipitation treated) (Cu 2, Ni 1, Mg 1, Si 0.9, Fe 0.9) |
| BS L 515:1973 | Specification for sheet and strip of magnesium-1¼% zinc-zirconium alloy (suitable for welding by inert-gas shielded arc techniques) (Zn 1.25, Zr 0.6) |
| BS L 513:1973 | Specification for forging stock and forgings of magnesium-6% aluminium-zinc alloy (Al 6.0, Zn 1.0) |
| BS 3G 100-2.2:1972 | Specification for general requirements for equipment for use in aircraft. All equipment Magnetic influence |
| BS TA 46:1973 | Specification for bar and section for machining of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1050-1220 N/mm<sup>2</sup>) (limiting ruling section over 25 mm up to and including 100 mm) |
| BS 2A 229:1972 | Specification for hexagonal head steel bolts 160000 lbf/in<sup>2</sup> (1100/MPa) |
| BS 2L 93:1971 | Specification for plate of aluminium-copper-magnesium-silicon-manganese alloy (solution treated, controlled stretched and precipitation treated) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8) |
| BS L 111:1971 | Specification for bars and extruded sections of aluminium-magnesium-silicon-manganese alloy (solution treated and precipitation treated) (suitable for welding) (Mg 0.8, Si 1, Mn 0.7) |
| BS L 159:1978 | Specification for close toleranced sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and artificially aged) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8) |
| BS TA 39:1971 | Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1250-1420 N/mm<sup>2</sup>) (limiting ruling section 25 mm) |
| BS 4315-2:1970 | Methods of test for resistance to air and water penetration Permeable walling constructions (water penetration) |
| BS L 163:1978 | Specification for sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy (solution treated, cold worked for flattening and aged at room temperature) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8) |
| BS TA 56:1974 | Specification for plate of titanium-aluminium-vanadium alloy (tensile strength 895-1150 MPa) (maximum thickness 100 mm) |
| BS 2L 87:1971 | Specification for hexagonal bars for nuts, couplings and hollow machined parts of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and precipitation treated) (free from peripheral and asymmetric coarse grain) (not less than 14 mm nor more than 36 mm across flats) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8) |
| BS L 117:1975 | Specification for tube of aluminium-magnesium-silicon-copper-chromium alloy (solution treated and artificially aged: not tested hydraulically) (not exceeding 10 mm thickness) (Mg 1.0, Si 0.6, Cu 0.28, Cr 0.2) |
| BS 3G 100-2.3.6:1972 | Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Acceleration requirements |
| BS 3G 100-2.3.8:1972 | Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Salt mist |
| BS 2HR 502:1973 | Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy cold drawn and solution heat treated wire for springs (nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5) |
| BS L 119:1975 | Specification for ingots and castings of aluminium-copper-nickel-manganese-titanium-zirconium-cobalt-antimony alloy (solution treated and artificially aged) (Cu 5.0, Ni 1.5, Mn 0.25, Ti 0.2, Zr 0.2, Co 0.2, Sb 0.2) |
| BS TA 51:1973 | Specification for forgings of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1000-1200 N/mm<sup>2</sup>) (limiting ruling section over 100 mm up to and including 150 mm) |
| BS 2HR 401:1973 | Specification for nickel-chromium-titanium-aluminium heat-resisting alloy cold worked and softened seamless tubes (nickel base, Cr 19.5, Ti 2.2, Al 1.4) |
| BS TA 57:1974 | Specification for plate of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1030-1220 MPa) (maximum thickness 65 mm) |
| BS 2L 85:1971 | Specification for forging stock, bars, extruded sections and forgings of aluminium-copper-silicon-magnesium alloy (solution treated and precipitation treated) (Cu 1.5, Si 1, Mg 0.8) |
| BS L 514:1973 | Specification for forging stock and forgings of magnesium-3% zinc-zirconium alloy (Zn 3.0, Zr 0.6) |
| BS 3170:1972 | Specification for flexible couplings for power transmission |
| BS TA 55:1973 | Specification for forgings of titanium-copper alloy (tensile strength 650-880 N/mm<sup>2</sup>) (limiting ruling section 75 mm) |
| BS 2TA 5:1973 | Specification for forgings of commercially pure titanium (tensile strength 390-540 N/mm<sup>2</sup>) |
| BS TA 44:1972 | Specification for forgings of titanium-aluminium-zirconium-molybdenum-silicon alloy (tensile strength 990-1140 N/mm<sup>2</sup>) (limiting ruling section 65 mm) |
| BS L 109:1971 | Specification for aluminium-coated sheet and strip of aluminium-copper-magnesium-manganese alloy (solution treated and aged at room temperature) (Cu 4.4, Mg 1.5, Mn 0.6) |
| BS L 115:1971 | Specification for plate of aluminium-magnesium-silicon-manganese alloy (solution treated, controlled stretched and precipitation treated) (not exceeding 25 mm thickness) (suitable for welding) (Mg 0.8, Si 1, Mn 0.7) |
| BS 2TA 28:1974 | Specification for forging stock and wire of titanium-aluminium-vanadium alloy (tensile strength 1100-1300 MPa) (limiting ruling section 20 mm) (primarily intended for the manufacture of fasteners complying with the requirements of the \'A\' series of British Standards) |
| BS 4022:1970 | Specification for prefabricated gypsum wallboard panels |
| BS L 165:1978 | Specification for sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy (solution treated and artificially aged) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8) |
| BS L 154:1977 | Specification for ingots and castings of aluminium-copper-silicon alloy (solution treated and aged at room temperature) (Cu 4, Si 1) |
| BS TA 53:1973 | Specification for bar and section for machining of titanium-copper alloy (tensile strength 650-880 N/mm<sup>2</sup>) (limiting ruling section 75 mm) |
| BS 2L 99:1972 | Specification for ingots and castings of aluminium-silicon-magnesium alloy (solution treated and precipitation treated) (Si 7, Mg 0.3) |
| BS L 112:1971 | Specification for forging stock and forgings of aluminium-magnesium-silicon-manganese alloy (solution treated and precipitation treated) (suitable for welding) (Mg 0.8, Si 1, Mn 0.7) |
| BS 2T 57:1972 | Specification for 4/1 nickel-chromium steel tube (1150 N/mm<sup>2</sup>) |
| BS 3L 86:1971 | Specification for wire for solid, cold-forged rivets of aluminium-copper-magnesium alloy (not exceeding 10 mm diameter) (Cu 2.5, Mg 0.3) |
| BS T 74:1972 | Specification for low carbon 18/10 chromium-nickel corrosion-resisting steel tube (500 N/mm<sup>2</sup>) |
| BS TA 43:1972 | Specification for forging stock of titanium-aluminium-zirconium-molybdenum-silicon alloy (tensile strength 990-1140 N/mm<sup>2</sup>) (limiting ruling section 65 mm) |
| BS T 75:1972 | Specification for low carbon 17/12 chromium-nickel-molybdenum corrosion-resisting steel tube (500 N/mm<sup>2</sup>) |
| BS T 67:1972 | Specification for 18/10 chromium-nickel corrosion-resisting steel tube (titanium stabilized: 550 N/mm<sup>2</sup>) (weldable) |
| BS TA 41:1971 | Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 N/mm<sup>2</sup>) (limiting ruling section over 25 mm up to and including 75 mm) |
| BS TA 42:1971 | Specification for forgings of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 N/mm<sup>2</sup>) (limiting ruling section over 25 mm up to and including 75 mm) |
| BS 2HR 2:1973 | Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5) |
| BS TA 40:1971 | Specification for bar for machining of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 N/mm<sup>2</sup>) (limiting ruling section over 25 mm up to and including 75 mm) |
| BS L 167:1978 | Specification for close toleranced sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy (solution treated and artificially aged) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8) |
| BS L 164:1978 | Specification for sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8) |
| BS T 69:1972 | Specification for cold drawn 18/10 chromium-nickel corrosion-resisting steel tube (titanium stabilized: 800 N/mm<sup>2</sup>) (weldable) |
| BS TA 45:1973 | Specification for bar and section for machining of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1100-1280 N/mm<sup>2</sup>) (limiting ruling section 25 mm) |
| BS 2HR 202:1973 | Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy sheet and strip (nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5) |
| BS L 118:1975 | Specification for tube of aluminium-magnesium-silicon-copper-chromium alloy (solution treated and artificially aged: tested hydraulically) (not exceeding 10 mm thickness) (Mg 1.0, Si 0.6, Cu 0.28, Cr 0.2) |
| BS 3457:1973 | Specification for materials for water tap and stopvalve seat washers |
| BS 3470:1975 | Specification for field gates and posts |
| BS TA 47:1973 | Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1050-1220 N/mm<sup>2</sup>) (limiting ruling section 100 mm) |
| BS L 162:1976 | Specification. Cold compressed hand forgings of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and artificially aged to an overaged condition) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.22) |
| BS 835:1973 | Specification for asbestos-cement flue pipes and fittings, heavy quality |
| BS N 4:1974 | SPECIFICATION FOR FULL FACE MASK ASSEMBLIES FOR USE IN CONTAMINATED ATMOSPHERES |
| BS 2TA 3:1973 | SPECIFICATION FOR BAR AND SECTION FOR MACHINING OF COMMERCIALLY PURE TITANIUM (TENSILE STRENGTH 390-540 N/MM[2]) |
| BS 4604-2:1970 | SPECIFICATION FOR THE USE OF HIGH STRENGTH FRICTION GRIP BOLTS IN STRUCTURAL STEELWORK - METRIC SERIES - HIGHER GRADE (PARALLEL SHANK) |
| BS 4604-1:1970 | SPECIFICATION FOR THE USE OF HIGH STRENGTH FRICTION GRIP BOLTS IN STRUCTURAL STEELWORK METRIC SERIES - PART 1: GENERAL GRADE |
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