| BS 2B 25:2001 | Copper-nickel-silicon alloy rods, sections, forging stock, forgings and parts (heat treated) |
| BS 2B 26:2001 | Copper-nickel-silicon alloy rods, sections and parts (solution treated, cold worked and precipitation treated) |
| BS 2B 28:2001 | Copper-beryllium alloy strip, foil and parts (solution treated and precipitation treated) |
| BS 2B 29:2001 | Copper-beryllium alloy strip, foil and parts (solution treated, cold rolled: quarter hard and precipitation treated) |
| BS 2B 30:2001 | Copper-beryllium alloy strip, foil and parts (solution treated, cold rolled: half hard and precipitation treated) |
| BS 2B 31:2001 | Copper-beryllium alloy strip, foil and parts (solution treated, cold rolled: full hard and precipitation treated) |
| BS 2B 32:2001 | Copper-beryllium alloy rods, sections and parts (solution treated and precipitation treated) |
| BS 2B 33:2001 | Copper-beryllium alloy wire and springs (solution treated and precipitation treated) |
| BS 2F 67:1980 | Specification for hose for aviation fuel and engine lubricating oil for aeronautical purposes |
| 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 2L 116:1985 | Specification for tube of 99% aluminium (cold drawn: seamless, not tested hydraulically) (not exceeding 12 mm wall thickness) |
| BS 2L 503:1973 | Specification for tube of magnesium-6% aluminium-zinc alloy (Al 6.0, Zn 1.0) |
| BS 2M 45:Part 2:1986 | Aircraft tyres and rims. Methods of test for tyres |
| BS 2M 46:1986* ISO 2964-1985 | Specification for outside diameters and thicknesses of tubing |
| BS 2M 47:1990 | Specification for retreading of cross ply tyres for aircraft |
| BS 2SP 101-104:1956 | Specifications for turnbarrels, tension rods and swaged cable-end connections (Unified threads) for aircraft |
| BS 2SP 105:1955 | Specification for swaged cable-end assemblies (Unified threads) for preformed steel wire rope (W.9) for aircraft |
| BS 2SP 106:1955 | Specification for swaged cable-end assemblies (Unified threads) for preformed non-corrodible steel wire rope (W.11) for aircraft |
| BS 2SP 168-169:1985 | Specification for ferrules and assembly wires for braided rubber cord assemblies for aerospace use |
| BS 2SP 170-171:1985 | Specification for braided rubber cord assemblies for aerospace use |
| BS 2SP 91-92:1973 | Specification for carbon steel worm drive clamps for aircraft |
| BS 2SP 93:1974 | Specification for elastomeric grommets (acrylonitrile-butadiene) for aerospace use |
| BS 2SP 95:1974 | Specification for elastomeric grommets (polychloroprene) for aerospace use |
| BS 2SP 96:1982 | Specification for internal retaining rings (imperial sizes) |
| BS 2T 57:1972 | Specification for 4/1 nickel-chromium steel tube (1150 N/mm˛) |
| BS 2T 66:1980 | Specification for 18/10 chromium-nickel corrosion-resisting steel tube (niobium stabilized: 550 MPa) (weldable) |
| BS 2T 68:1980 | Specification for cold drawn 18/10 chromium-nickel corrosion-resisting steel tube (niobium stabilized: 800 MPa) (weldable) |
| BS 2W 11:1967 | Specification for aircraft material. Preformed corrosion-resisting steel wire rope |
| BS 2W 12:1989 | Specification for preformed zinc coated carbon steel wire rope (metric and inch series) |
| BS 3F 63:1981 | Specification for low pressure oxygen hose for aeronautical purposes |
| BS 3F 65:1991 | Specification for flexible corrugated oxygen and air tubes for aircraft (natural or synthetic polyisoprene) |
| BS 3M 45-2:1998* ISO 3324-2:1998 | Aircraft tyres and rims. Test methods for tyres |
| BS 3M 45:Part 1:1994* ISO 3324-1:1993 | Aircraft tyres and rims. Specifications |
| BS 3SP 168-169:2002 | Ferrules and assembly wires for braided rubber cord assemblies for aerospace use |
| BS 3SP 170-171:2002 | Braided rubber cord assemblies for aerospace use |
| BS 3SP 3:1943 | Specification for aircraft material. Fork joints (low tensile type) (for sizes No. 4 B.A. to 1/2 inch B.S.F. inclusive) |
| BS 3SP 89:1983* ISO 1002-1983 | Specification for characteristics, boundary dimensions, tolerances and static load ratings of airframe bearings |
| BS 3T 100:1978 | Procedure for inspection and testing of steel tubes |
| BS 3T 51:1945 | Specification for aircraft material. High pressure seamless copper tubes |
| BS 3T 53:1980 | Specification for chromium-molybdenum steel tube (700 MPa) (outside diameter not less than 12.5 mm) (weldable) |
| BS 3T 60:1980 | Specification for chromium-molybdenum steel tube (1150 MPa) (maximum thickness 8 mm) |
| BS 4K 6:1928 | Specification for aircraft material. Cast iron piston ring pots (sand cast and chill cast) |
| BS 4L 54:1986 | Specification for tube of 99% aluminium (cold drawn: seamless: tested hydraulically) (not exceeding 12 mm wall thickness) |
| BS 4L 56:1986 | Specification for tube of aluminium-2 1/4% magnesium alloy (temper designation-O) (seamless: tested hydraulically) (not exceeding 12 mm wall thickness) |
| BS 4M 45-1:1998* ISO 3324-1:1997 | Aircraft tyres and rims. Specifications |
| BS 4T 100:1997 | Procedure for inspection, testing and acceptance of seamless steel tubes and tubestock |
| BS 4T 45:1972 | Specification for carbon-manganese steel tube (700 N/mm˛) (tube 12.5 mm outside diameter and greater) (weldable) |
| BS 5T 2:1972 | Specification for 4/1 nickel-chromium steel tube (1300 N/mm˛) |
| BS 6W 8:1938 | Tie rods (swaged) (No. 4 B.A. to 1/2 inch B.S.F. inclusive) for aircraft purposes |
| BS A 328-2:1999* ISO 8399-2:1998 | Accessory drives and mounting flanges (Metric sizes). Dimensions |
| BS EN 2009:1992 | Bearings. Airframe rolling rigid, single row ball bearings in steel diameter series 8 and 9. Dimensions and loads |
| BS EN 2011:1989 | Specification for bearings - airframe rolling rigid single row ball bearings in corrosion resisting steel diameter series 8 and 9. Dimensions and loads |
| BS EN 2012:1989 | Specification for bearings - airframe rolling rigid, single row ball bearings in steel diameter series 0 and 2. Dimensions and loads |
| BS EN 2014:1989 | Specification for bearings - airframe rolling rigid single row ball bearings in corrosion resisting steel diameter series 0 and 2. Dimensions and loads |
| BS EN 2015:1989 | Specification for bearings - airframe rolling double row, self aligning ball bearings in steel diameter series 2. Dimensions and loads |
| BS EN 2017:1989 | Specification for bearings - airframe rolling double row self aligning ball bearings in corrosion resisting steel diameter series 2. Dimensions and loads |
| BS EN 2018:1989 | Specification for bearings - airframe rolling single row, self aligning roller bearings in steel diameter series 3 and 4. Dimensions and loads |
| BS EN 2020:1989 | Specification for bearings - airframe rolling single row self aligning roller bearings in corrosion resisting steel diameter series 3 and 4. Dimensions and loads |
| BS EN 2022:1990 | Specification for bearings, spherical plain in corrosion resisting steel with self-lubricating liner. Light series. Dimensions and loads |
| BS EN 2023:1989 | Specification for bearings - spherical plain in corrosion resisting steel with self-lubricating liner. Normal series. Dimensions and loads |
| BS EN 2044:2001 | Aerospace series. Round bars, drawn, in aluminium and aluminium alloys. Tolerance class h 11. Diameter 4 mm ≤ D ≤ 63 mm. Dimensions |
| BS EN 2045:2001 | Aerospace series. Square bars, drawn, in aluminium and aluminium alloys. Tolerance class h 11. Thickness 6 mm ≤ a ≤ 50 mm. Dimensions |
| BS EN 2046:2001 | Hexagonal bars, drawn, in aluminium and aluminium alloys. Tolerance class h 11. Width across flats 7 mm ≤ a ≤ 50 mm. Dimensions |
| BS EN 2063:1992 | Airframe rolling bearings. Technical specification |
| BS EN 2064:1992 | Bearings, spherical plain in corrosion resisting steel with self lubricating liner. Technical specification |
| BS EN 2067:1996 | Rod ends with self-aligning ball bearings. Technical specification |
| BS EN 2068:1996 | Rod ends with self-lubricating self-aligning bearings. Technical specification |
| BS EN 2079:1995 | Bearings, precision ball with flange in corrosion resisting steel, for instruments and equipment. Dimensions and loads |
| BS EN 2130:2001 | Aerospace Series. Bearings, precision ball in corrosion resisting steel for instruments and equipment. Technical specification |
| BS EN 2134:2002 | Aerospace series. Round bars, extruded in aluminium and aluminium alloys. Diameter 10 mm ≤ D ≤ 220 mm. Dimensions |
| BS EN 2289:1996 | Rod bodies in aluminium alloy for flight controls. Technical specification |
| BS EN 2290-1:1998 | Rod bodies, flight control in aluminium alloy, for adjustable end fittings. Dimensions and loads |
| BS EN 2335:1990 | Specification for bearings-spherical plain in corrosion resisting steel without assembly slot. Dimensions and loads |
| BS EN 2335:2005 | Aerospace series. Bearings, spherical plain in corrosion resisting steel without assembly slot. Dimensions and loads |
| BS EN 2336:1990 | Specification for bearings-spherical plain in steel with assembly slots. Dimensions and loads |
| BS EN 2336:2005 | Aerospace series. Bearings, spherical plain in steel with assembly slots. Dimensions and loads |
| BS EN 2337:1996 | Spherical plain bearings. Technical specification |
| BS EN 2337:2006 | Aerospace series. Spherical plain bearings. Technical specification |
| BS EN 2424:2008 | Aerospace series. Marking of aerospace products |
| BS EN 2498:1990 | Specification for rod ends, adjustable self-aligning plain bearing, with self-lubricating liner and threaded shank. Dimensions and loads |
| BS EN 2501:1992 | Bearings, spherical plain in corrosion resisting steel with self-lubricating liner and wide inner ring. Dimensions and loads |
| BS EN 2515:1990 | Specification for rod ends, adjustable single fork and threaded shank. Dimensions and loads |
| BS EN 2584:1992 | Bearings, spherical plain in corrosion resisting steel with self-lubricating liner. Narrow series. Elevated loads at ambient temperature. Dimensions and loads |
| BS EN 2584:2001 | Aerospace series. Bearings, spherical plain in corrosion resisting steel with self-lubricating liner. Narrow series. Elevated load at ambient temperature. Dimensions and loads |
| BS EN 2585:1992 | Bearings, spherical plain in corrosion resisting steel with self-lubricating liner. Wide series. Elevated loads at ambient temperature. Dimensions and loads |
| BS EN 2585:2001 | Aerospace series. Bearings, spherical plain in corrosion-resisting steel with self-lubricating liner. Elevated load at ambient temperature. Dimensions and loads |
| BS EN 2587:1990 | Specification for rod ends, adjustable double fork and threaded shank. Dimensions and loads |
| BS EN 2588:1992 | Bearings. Spherical plain in corrosion resisting steel with assembly slots. Dimensions and loads |
| BS EN 2588:2006 | Aerospace series. Bearings, spherical plain in corrosion resisting steel with assembly slots. Dimensions and loads |
| BS EN 2601:1996 | Fork ends, adjustable. Technical specification |
| BS EN 2644:1998 | Rod assemblies for flight controls. Technical specification |
| BS EN 2755:2009 | Aerospace series. Bearings, spherical plain in corrosion resisting steel with self-lubricating liner. Elevated load at ambient temperature. Technical specification |
| BS EN 2790:1991 | Rod ends, adjustable, self-aligning plain bearing with self-lubricating liner and threaded shank with engagement: 1.5 thread. Dimensions and loads |
| BS EN 2791:1991 | Rod ends, adjustable, single fork and threaded shank with engagement: 1.5 thread diameter. Dimensions and loads |
| BS EN 2792:1991 | Rod ends, adjustable, double fork and threaded shank with engagement: 1.5 thread diameter. Dimensions and loads |
| BS EN 3045:1994 | Bearings, airframe rolling. Rigid single row ball bearings in steel. Diameter series 0 and 2. Reduced clearance category. Dimensions and loads |
| BS EN 3046:1994 | Bearings, airframe rolling. Rigid single row ball bearings in steel, cadmium plated. Diameter series 0 and 2. Reduced clearance category. Dimensions and loads |
| BS EN 3047:1994 | Bearings, airframe rolling. Rigid single row ball bearings in corrosion resisting steel. Diameter series 0 and 2. Reduced clearance category. Dimensions and loads |
| BS EN 3048:1992 | Bearings, spherical plain in corrosion resisting steel with self-lubricating liner. Light series. Elevated loads at ambient temperature. Dimensions and loads |
| BS EN 3048:2001 | Bearings, spherical plain in corrosion resisting steel with self-lubricating liner. Light series. Elevated load at ambient temperature. Dimensions and loads |
| BS EN 3053:1994 | Bearings, airframe rolling. Single row self-aligning roller bearings in steel. Dimensions and loads |
| BS EN 3054:1994 | Bearings, airframe rolling. Single row self-aligning roller bearings in steel, cadmium plated. Dimensions and loads |
| BS EN 3055:1994 | Bearings, airframe rolling. Single row self-aligning roller bearings in corrosion resisting steel. Dimensions and loads |
| BS EN 3056:1994 | Bearings, airframe rolling. Rigid double row ball bearings in steel. Dimensions and loads |
| BS EN 3057:1994 | Bearings, airframe rolling. Rigid double row ball bearings in steel, cadmium plated. Dimensions and loads |
| BS EN 3058:1994 | Bearings, airframe rolling. Rigid double row ball bearings in corrosion resisting steel. Dimensions and loads |
| BS EN 3059:2007 | Aerospace series. Bearings, airframe rolling. Rigid single row ball bearings in steel with flanged alignment housing, cadmium plated. Dimensions and loads |
| BS EN 3060:2007 | Aerospace series. Bearings, airframe rolling. Rigid single row ball bearings in steel, cadmium plated, with flanged alignment housing, cadmium plated. Dimensions and loads |
| BS EN 3061:2007 | Aerospace series. Bearings, airframe rolling. Rigid single row ball bearings in corrosion resisting steel, with flanged alignment housing. Dimensions and loads |
| BS EN 3280:1994 | Bearings, airframe rolling, rigid or self-aligning. Technical specification |
| BS EN 3281:1994 | Bearings, airframe rolling. Rigid single row ball bearings in steel. Diameter series 8 and 9. Dimensions and loads |
| BS EN 3282:1994 | Bearings, airframe rolling. Rigid single row ball bearings in steel, cadmium plated. Diameter series 8 and 9. Dimensions and loads |
| BS EN 3283:1994 | Bearings, airframe rolling. Rigid single row ball bearings in corrosion resisting steel. Diameter series 8 and 9. Dimensions and loads |
| BS EN 3284:1994 | Bearings, airframe rolling. Rigid single row ball bearings in steel. Diameter series 0 and 2. Normal clearance category. Dimensions and loads |
| BS EN 3285:1994 | Bearings; airframe rolling. Rigid single row ball bearings in steel, cadmium plated. Diameter series 0 and 2. Normal clearance category. Dimensions and loads |
| BS EN 3286:1994 | Bearings, airframe rolling. Rigid single row ball bearings in corrosion resisting steel. Diameter series 0 and 2. Normal clearance category. Dimensions and loads |
| BS EN 3287:1994 | Bearings, airframe rolling. Double row self-aligning ball bearings in steel. Diameter series 2. Dimensions and loads |
| BS EN 3288:1994 | Bearings, airframe rolling. Double row self-aligning ball bearings in steel, cadmium plated. Diameter series 2. Dimensions and loads |
| BS EN 3289:1994 | Bearings, airframe rolling. Double row self-aligning ball bearings in corrosion resisting steel. Diameter series 2. Dimensions and loads |
| BS EN 3290:1994 | Bearings, airframe rolling. Single row self-aligning roller bearings in steel. Diameter series 3 and 4. Dimensions and loads |
| BS EN 3291:1994 | Bearings, airframe rolling. Single row self-aligning roller bearings in steel, cadmium plated. Diameter series 3 and 4. Dimensions and loads |
| BS EN 3292:1994 | Bearings, airframe rolling. Single row self-aligning roller bearings in corrosion resisting steel. Diameter series 3 and 4. Dimensions and loads |
| BS EN 3446:1995 | Bearings, precision ball without flange in corrosion resisting steel, for instruments and equipment. Dimensions and loads |
| BS EN 3541:1992 | Rod ends, adjustable, self-aligning ball bearing with threaded shank. Dimensions, torques, clearances and loads |
| BS EN 3727:2006 | Aerospace series. Bearings, airframe rolling rigid with flanged alignment housing. Technical specification |
| BS EN 3848:2001 | Aerospace series. Semi-finished metallic products. Methods of measuring form deviations |
| BS EN 4033:2007 | Aerospace series. Bearings, airframe rolling. Rigid single row ball bearings in corrosion resisting steel. Diameter series 8 and 9, reduced internal radial clearance. Dimensions and loads |
| BS EN 4034:2007 | Aerospace series. Bearings, airframe rolling. Double row self-aligning ball bearings with flanged outer ring in corrosion resisting steel, reduced internal radial clearance. Dimensions and loads |
| BS EN 4035:2006 | Aerospace series. Rod ends, adjustable with self-aligning double row ball bearing in corrosion resisting steel, reduced internal radial clearance and threaded shank in titanium alloy. Dimensions and loads |
| BS EN 4036:2006 | Aerospace series. Rod ends, adjustable with self-aligning double row ball bearing and threaded shank in corrosion resisting steel, reduced internal radial clearance. Dimensions and loads |
| BS EN 4040:2006 | Aerospace series. Bearings, spherical plain in corrosion resisting steel with self-lubricating liner with wide inner ring. Elevated loads at ambient temperature. Dimensions and loads |
| BS EN 4041:2006 | Aerospace series. Bearings, airframe rolling. Rigid single row ball bearings in corrosion resisting steel, with extended inner ring and flanged alignment bush. Dimensions and loads |
| BS EN 4198:2006 | Aerospace series. Rod-ends, adjustable self-aligning plain bearing with self-lubricating liner and threaded shank in corrosion resisting steel. Dimensions and loads |
| BS EN 4424:2006 | Aerospace series. Rod-ends, adjustable single fork and threaded shank with engagement: 1,5 x thread diameter in titanium alloys. Dimensions and loads |
| BS EN 4534-2:2009 | Aerospace series. Bushes, plain in aluminium alloy with self-lubricating liner, elevated load. Dimensions and loads. Inch series |
| BS EN 4535-2:2009 | Aerospace series. Bushes, flanged in aluminium alloy with self-lubricating liner, elevated load. Dimensions and loads. Inch series |
| BS EN 4536-2:2009 | Aerospace series. Bushes, plain in corrosion-resisting steel with self-lubricating liner, elevated load. Dimensions and loads. Inch series |
| BS EN 4537-2:2009 | Aerospace series. Bushes, flanged in corrosion-resisting steel with self-lubricating liner, elevated load. Dimensions and loads. Inch series |
| BS EN 4613:2009 | Aerospace series. Spherical plain bearings in corrosion resisting steel with self-lubricating liner, narrow series. Dimensions and loads. Inch series |
| BS EN 4614:2009 | Aerospace series. Spherical plain bearings in corrosion resisting steel with self-lubricating liner, wide series. Dimensions and loads. Inch series |
| BS HC 402:1977 | Specification for cast iron ring pots (centrifugally cast) (suitable for piston rings up to 200 mm in diameter) |
| BS HC 403:1977 | Specification for high chromium alloy cast iron ring pots (centrifugally cast) (suitable for piston rings up to 400 mm in diameter) |
| BS HC 404:1977 | Specification for chromium-molybdenum alloy cast iron ring pots (suitable for centrifugally cast and sand cast sealing rings, piston rings and cylinder liners) |
| BS HR 402:1973 | Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy cold worked and softened seamless tubes (nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5) |
| BS HR 403:1973 | Specification for nickel-chromium-titanium heat-resisting alloy cold-worked and softened seamless tubes (nickel base, Cr 19.5 Ti 0.4) |
| BS HR 404:1973 | Specification for nickel-cobalt-chromium-molybdenum-titanium-aluminium heat-resisting alloy cold worked solution treated seamless tubes (nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.1, Al 0.5) |
| BS ISO 10792-1:1995 | Aerospace. Airframe spherical plain bearings in corrosion-resisting steel with self-lubricating liner. Metric series |
| BS ISO 10792-2:1995 | Aerospace. Airframe spherical plain bearings in corrosion-resisting steel with self-lubricating liner. Inch series |
| BS ISO 10792-3:1995 | Aerospace. Airframe spherical plain bearings in corrosion-resisting steel with self-lubricating liner. Technical specification |
| BS ISO 10955:1999 | End-fittings and turnbarrels for aircraft control wire rope. Technical specification |
| BS ISO 2020-1:1997 | Aerospace. Preformed flexible steel wire rope for aircraft controls. Dimensions and loads |
| BS ISO 2020-2:1997 | Aerospace. Preformed flexible steel wire rope for aircraft controls. Technical specification |
| BS ISO 9736:2000 | Eye-ends, in corrosion-resistant steel, threaded, for aircraft control wire rope. Dimensions and loads |
| BS ISO 9737:2000 | Eye-ends, in corrosion resisting steel, swaged on aircraft control wire rope. Dimensions and loads |
| BS ISO 9738:2000 | Turnbarrels, for aircraft control wire rope. Dimensions and loads |
| BS ISO 9747:2000 | Double shank ball-ends, in corrosion-resistant steel, swaged on aircraft control wire rope. Dimensions and loads |
| BS ISO 9748:2000 | Ball-ends, in corrosion-resistant steel, swaged on aircraft control wire rope. Dimensions and loads |
| BS ISO 9749:2000 | Stud-ends, in corrosion-resistant steel, swaged on aircraft control wire rope. Dimensions and loads |
| BS ISO 9757:2000 | Fork-ends, in corrosion-resistant steel, threaded, for aircraft control wire rope turnbarrels. Dimensions and loads |
| BS ISO 9758:2000 | Fork-ends, in corrosion-resistant steel, threaded, for rolling bearings, for aircraft control wire rope. Dimensions and loads |
| BS ISO 9759:2000 | Fork ends, in corrosion-resistant steel, swaged on aircraft control wire rope. Dimensions and loads |
| BS ISO 9760:2000 | Aerospace. Fork-ends, in corrosion-resistant steel, swaged on aircraft control wire rope, for rolling bearings. Dimensions and loads |
| BS ISO 9761:2000 | Locking clips, in corrosion-resistant steel, for aircraft control wire rope turnbuckles. Dimensions |
| BS ISO 9762:2000 | Aircraft control wire rope assemblies. Dimensions and end-fitting combinations |
| BS L 114:1971 | Specification for tube of aluminium-magnesium-silicon-manganese alloy (solution treated and precipitation treated) (not exceeding 10 mm wall thickness) (suitable for welding) (Mg 0.8, Si 1, Mn 0.7) |
| 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 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 M 33:1970 | Specification for dimensions of elastomeric toroidal sealing rings (inch series) to Class 1 tolerances for aircraft |
| BS M 37:1970 | Method for the etch inspection of metallic materials and components |
| BS M 39:1972 | Method for penetrant inspection of aerospace materials and components |
| BS M 48:1975 | Specification for dimensions of elastomeric toroidal sealing rings for aerospace use - inch series |
| BS SP 115 to 117:1956 | Specifications for hydraulic surface-check type lubricating nipples for aircraft |
| BS SP 119 and SP 120:1957 | High tensile steel fork joints (Unified threads) for aircraft |
| BS SP 121:1958 | Collars for shear pins for aircraft |
| BS SP 144-147:1971 | Specification for corrosion resisting worm drive clamps for aircraft |
| BS SP 166:1982 | Specification for spring retaining rings for aerospace application: carbon steel circlips (metric series) |
| BS SP 21:1950 | Specification for lubricating nipples for aircraft purposes |
| BS SP 33-39:1951 | Specifications for turnbarrels, tension rods and swaged cable-end connections for aircraft |
| BS SP 49 and 50:1953 | Specifications for ball ends for swaging on cable for aircraft (suitable for 5 cwt. cable) |
| BS SP 51 and 52:1953 | Specifications for identification tags for swaged cable-end assemblies for aircraft |
| BS SP 53:1953 | Specification for swaged cable-end assemblies (B.A. and B. S.F. threads) for preformed steel wire rope for aircraft (suitable for use with British Standard W.9 wire rope) |
| BS SP 54:1953 | Specification for swaged cable-end assemblies (B.A. and B. S.F. threads) for preformed non-corrodible steel wire rope for aircraft (suitable for use with British Standard W.11 wire rope) |
| BS SP 94:1964 | Specification for bronze oil-retaining bushes and thrust washers for aircraft |
| BS T 64:1972 | Specification for carbon-manganese steel tube (550 N/mm˛) (tube less than 12.5 mm outside diameter) (weldable) |
| BS T 67:1972 | Specification for 18/10 chromium-nickel corrosion-resisting steel tube (titanium stabilized: 550 N/mm˛) (weldable) |
| BS T 69:1972 | Specification for cold drawn 18/10 chromium-nickel corrosion-resisting steel tube (titanium stabilized: 800 N/mm˛) (weldable) |
| BS T 74:1972 | Specification for low carbon 18/10 chromium-nickel corrosion-resisting steel tube (500 N/mm˛) |
| BS T 75:1972 | Specification for low carbon 17/12 chromium-nickel-molybdenum corrosion-resisting steel tube (500 N/mm˛) |
| BS T 76:1978 | Specification for chromium-molybdenum steel tube (770 MPa) (weldable) |
| BS T 77:1980 | Specification for chromium-molybdenum steel tube (900 MPa) (weldable) |
| BS T 78:1997 | Specification for 2 1/2% nickel-chromium-molybdenum steel tubes (1390 Mpa) |
| BS T 79:1997 | Specification for 2 1/2% nickel-chromium-molybdenum steel tubes (1160 MPa) |
| BS T 80:1997 | Specification for 12% chromium corrosion-resisting steel tubes (770 MPa) |
| BS W 13:1973 | Specification for preformed corrosion-resisting steel wire rope (ISO diameters and strengths) |
| BS W 14:1999* ISO 9763:1999 | Aircraft control wire rope assemblies. Technical specification |
