| Standard |
Official Title of Standard |
|
| BS 2G 223:1989 |
Specification for screen terminating devices for aircraft electric cables |
| BS 2G 232:1987 |
Specification for electric cables for general airframe or equipment interconnect use (135$0DC), wrapped insulation |
| BS 2G 238:1996 |
Specification for electric cables for general airframe or equipment interconnect use (260$0DC), nickel plated copper and copper alloy conductors, with wrapped insulation |
| BS 2G 239:1992 |
Specification for primary active lithium batteries for use in aircraft |
| BS 2HC 101:1989 |
Specification for precipitation hardening chromium-nickel-copper-molybdenum steel castings (950 MPa) (Cr 14.0, Ni 4.5, Cu 2.5, Mo 1.5) |
| BS 2HC 102:1989 |
Specification for precipitation hardening chromium-nickel-copper-molybdenum steel castings (1250 MPa) (Cr 14.0, Ni 4.5, Cu 2.5, Mo 1.5) |
| BS 2HC 203:1989 |
Specification for nickel-chromium-aluminium-molybdenum-niobium alloy castings (Nickel base Cr 13.0, Al 6.0, Mo 4.5, Nb 2.3) |
| BS 2HC 204:1989 |
Specification for nickel-cobalt-chromium-aluminium-titanium-molybdenum alloy castings (Nickel base Co 15.0, Cr 10.0, Al 5.5, Ti 4.8, Mo 3.0) |
| BS 2HC 207:1989 |
Specification for nickel-cobalt-tungsten-chromium-aluminium-tantalum-hafnium-titanium alloy castings (Nickel base Co 10.0, W 10.0, Cr 9.0, Al 5.5, Ta 2.5, Hf 1.5, Ti 1.5) |
| BS 2HC 208:1989 |
Specification for nickel-cobalt-tungsten-chromium-aluminium-molybdenum-titanium-tantalum alloy castings (nickel base Co 10.0, W 10.0, Cr 9.0, Al 5.5, Mo 2.5, Ti 1.5, Ta 1.5) |
| BS 2HC 209:1989 |
Specification for low carbon, precipitation hardening nickel-chromium-aluminium-molybdenum-niobium alloy castings (Nickel base Cr 11.5, Al 6.0, Mo 4.0, Nb 2.0) |
| BS 2HC 210:1989 |
Specification for nickel-tungsten-aluminium-chromium-molybdenum alloy castings (Nickel base W 10.5, Al 6.0, Cr 6.0, Mo 2.0) |
| BS 2HC 211:1989 |
Specification for nickel-chromium-cobalt-molybdenum-aluminium-titanium alloy castings (Nickel base Cr 15.5, Co 10.0, Mo 8,3, Al 4.2, Ti 3.6) |
| 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 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 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 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 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 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 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 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 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 126:1970 |
Specification for ingots and castings of magnesium-cerium-zinc-zirconium alloy (precipitation treated) (rare earth metals 3.0, Zn 2.3, Zr 0.6) |
| BS 2L 127:1970 |
Specification for ingots and castings of magnesium-zinc-zirconium alloy (precipitation treated) (Zn 4.5, Zr 0.7) |
| BS 2L 128:1970 |
Specification for ingots and castings of magnesium-zinc-cerium-zirconium alloy (precipitation treated) (Zn 4.5, rare earth metals 1.2, Zr 0.7) |
| BS 2L 169:2002 |
Ingots (as cast) and castings (solution treated and artificially aged) of aluminium-silicon-magnesium alloy (Si 7, Mg 0.6) |
| BS 2L 500:1973 |
Procedure for inspection and testing of wrought magnesium-base alloys |
| BS 2L 503:1973 |
Specification for tube of magnesium-6% aluminium-zinc alloy (Al 6.0, Zn 1.0) |
| BS 2L 504:1973 |
Specification for sheet and strip of magnesium-3% zinc-zirconium alloy (Zn 3.0, Zr 0.6) |
| BS 2L 505:1973 |
Specification for bars and extruded sections of magnesium-3% zinc-zirconium alloy (not exceeding 100 mm diameter or minor sectional dimension) (Zn 3.0, Zr 0.6) |
| BS 2L 508:1973 |
Specification for bars and extruded sections of magnesium-1$9D% zinc-zirconium alloy |
| BS 2L 509:1973 |
Specification for tube of magnesium-1$9D% zinc-zirconium alloy (suitable for welding by inert-gas shielded arc techniques) (Zn 1.25, Zr 0.6) |
| BS 2L 77:1971 |
Specification for forging stock and forgings of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and precipitation treated) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8) |
| 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 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 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) |
| 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 2L 95:1971 |
Specification for plate of aluminium-zinc-magnesium-copper-chromium alloy (solution treated, controlled stretched and precipitation treated) (Zn 5.8, Mg 2.5, Cu 1.6, Cr 0.15) |
| 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 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 2L 99:1972 |
Specification for ingots and castings of aluminium-silicon-magnesium alloy (solution treated and precipitation treated) (Si 7, Mg 0.3) |
| BS 2M 41:1977 |
Methods of numbering propulsion units and components and describing their direction of rotation |
| BS 2M 46:1986 |
Specification for outside diameters and thicknesses of tubing |
| BS 2M 47:1990 |
Specification for retreading of cross ply tyres for aircraft |
| BS 2M 49:1997 |
Aircraft. Hydraulic components. Marking to indicate fluid for which component is approved |
| BS 2M 50:1986 |
Specification for clearance dimensions for tripod jacks for aircraft |
| BS 2M 51:1989 |
Classification for pressure and temperature for fluid systems and components |
| BS 2M 52:1989 |
Method for impulse testing of hydraulic hose, tubing and fitting assemblies for aerospace fluid systems |
| BS 2M 53:1997 |
Aircraft. Fluid systems. Thermal shock testing of piping and fittings |
| BS 2M 54:1991 |
Specification for temperature control in the heat treatment of metals |
| BS 2M 59:1993 |
Specification for interface of metric couplings, 24$0D cone, for aerospace fluid systems |
| BS 2M 63:1993 |
Specification for dimensions of aerospace fluid system port connection, seal and fitting end |
| BS 2PL 1:1966 |
Specification for phenolic mouldings for aeronautical purposes |
| BS 2S 111:1964 |
Specification for aircraft material. Nickel-chromium-tungsten valve steel |
| BS 2S 112:1964 |
Specification for aircraft material. Semi-free cutting carbon steel, bright bars for machining |
| BS 2S 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 2S 114:1964 |
Specification for aircraft material. Manganese-molybdenum steel (55/65 tonf/sq in: limiting ruling section 2$9H inches) |
| BS 2S 116:1964 |
Specification for aircraft material. '40' carbon steel bright bars for machining (55-65 tonf/sq in: limiting ruling section $9L inch) (primarily intended for the manufacture of machined bolts) |
| BS 2S 117:1964 |
Specification for aircraft material. 1 per cent chromium steel (55/65 tonf/sq in: limiting ruling section 1$9B inch) |
| BS 2S 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 2S 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 2S 130:1976 |
Specification for 18/9 chromium-nickel corrosion-resisting steel (niobium stabilized) billets, bars, forgings and parts (540 MPa: limiting ruling section 150 mm) |
| BS 2S 131:1977 |
Specification for high thermal expansion steel billets, bars, forgings and parts (620 MPa: limiting ruling section 150 mm) |
| BS 2S 135:1977 |
Specification for 1% carbon-chromium steel billets, bars, forgings and parts (limiting ruling section 25 mm) |
| BS 2S 136:1977 |
Specification for 1% carbon-chromium steel (vacuum arc remelted) billets, bars, forgings and parts (limiting ruling section 25 mm) |
| BS 2S 137:1976 |
Specification for high chromium-nickel corrosion-resisting steel bright bars (free machining) (880-1080 MPa: limiting ruling section 70 mm) |
| BS 2S 140:1976 |
Specification for 2 1/2% nickel-chromium-molybdenum steel billets, bars, forgings and parts (1080-1280 MPa: limiting ruling section 150 mm) |
| BS 2S 142:1977 |
Specification for 1% chromium-molybdenum steel billets, bars, forgings and parts (900-1100 MPa: limiting ruling section 40 mm) |
| BS 2S 143:1976 |
Specification for chromium-nickel-copper-molybdenum corrosion-resisting steel (precipitation hardening) billets, bars, forgings and parts (930-1080 MPa) |
| BS 2S 146:1976 |
Specification for 4% nickel-chromium-molybdenum air-hardening steel (vacuum arc remelted) billets, bars, forgings and parts (1760-1960 MPa: limiting ruling section 100 mm) |
| BS 2S 147:1976 |
Specification for 0.5% nickel-chromium-molybdenum steel bars for the manufacture of forged bolts and forged nuts |
| BS 2S 149:1976 |
Specification for 1.75% nickel-chromium-molybdenum steel bars for the manufacture of forged bolts and forged nuts |
| BS 2S 201:2004 |
Carbon steel wire rod, patented cold drawn carbon steel wire and springs. High duty unground wire. Specifcation |
| BS 2S 202:2004 |
Carbon steel wire rod, patented cold drawn carbon steel wire and springs. High duty ground wire. Specification |
| BS 2S 203:2004 |
Carbon steel wire rod, wire and springs. High duty unground wire. Hardened and tempered. Specification |
| BS 2S 204:2004 |
Chromium-vanadium steel wire rod, wire and springs. High duty ground wire. Hardened and tempered. Specification |
| BS 2S 205:2004 |
Austenitic chromium-nickel steel wire rod, wire and springs. Specification |
| BS 2S 510:1970 |
Specification for carbon steel sheet and strip (430/540 MPa) (suitable for welding) |
| BS 2S 511:1970 |
Specification for deep drawing carbon steel sheet and strip (280/400 MPa) (suitable for welding) |
| BS 2S 513:1970 |
Specification for spring steel strip |