Aerospace series | State Library of NSW Content Lists

Call number: TQ081572

Box number	Standard number	Title	YEAR	PUBLISHER
Box 239	A. 14 : 1939	Hexagonal brass nuts for aircraft purposes	1939	British Standards Institution
Box 239	A. 22 : 1947	British standard for units of measurement in civil aviation	1947	British Standards Institution
Box 239	A. 24 : 1949	High tensile stainless steel hexagonal nuts (ordinary, thin, slotted and castle) for aircraft purposes	1947	British Standards Institution
Box 239	A. 25 : 1950	High tensile steel hexagonal-headed nuts (machined from bar or cold- or hot-forged) for aircraft purposes	1950	British Standards Institution
Box 239	A. 26 : 1949	High tensile stainless steel hexagonal-headed nuts (machined from bar) for aircraft purposes	1949	British Standards Institution
Box 239	A. 27 : 1950	Medium tensile steel hexagonal nuts (ordinary, thin, slotted and castle) for aircraft purposes	1950	British Standards Institution
Box 239	A. 29 : 1950	Aluminium alloy hexagonal nuts (ordinary and slotted) for aircraft purposes	1950	British Standards Institution
Box 239	A. 30 : 1950	Close tolerance hexagonal-headed bolts in high tensile steel for aircraft	1950	British Standards Institution
Box 239	A. 31 - 54 : 1951	British association (ba) low tensile screws and nuts for aeronautical purposes	1951	British Standards Institution
Box 239	A. 55 and 56 : 1951	Grub screws for aeronautical purposes	1951	British Standards Institution
Box 239	A. 57 and A. 58 : 1952	Shear bolts and nuts for aircraft	1952	British Standards Institution
Box 239	A. 59 : 1954	Cadmium plated hexagonal-headed steel bolts (b.a. And b.s.f. Threads and close tolerance shanks) for aircraft	1954	British Standards Institution
Box 239	A. 60 : 1954	Cadmium plated shear bolts (b.s.f. Threads) for aircraft	1954	British Standards Institution
Box 239	A. 61 : 1955	Aluminium alloy (b.s. L.65) hexagonal-headed bolts for aircraft	1955	British Standards Institution
Box 239	A. 100 : 1960	Bolts and nuts for aircraft (general clauses)	1960	British Standards Institution
Box 239	A. 101 : 1969	Aerospace series (metric and inch units) general requirements for titanium bolts	1969	British Standards Institution
Box 239	A. 120, March, 1954	British standard specification for 90 degree countersunk head corrosion- resisting steel bolts (unf threads) for aircraft	1954	British Standards Institution
Box 239	A. 172, August, 1955	British standard specification for 90 degree countersunk head aluminium alloy (b.s. L.65) bolts (unified threads) for aircraft	1955	British Standards Institution
Box 239	A. 174, April, 1956	British standard specification for 100 degree countersunk head corrosion- resisting steel bolts (unified threads) for aircraft	1956	British Standards Institution
Box 239	A. 175, April, 1956	British standard specification for 100 degree countersunk head aluminium alloy bolts (unified threads) for aircraft	1956	British Standards Institution
Box 239	A. 211 : October, 1961	British standard specification for 100 degree countersunk head steel bolts (unified threads and cruciform recesses) for aircraft	1961	British Standards Institution
Box 239	A. 212, September, 1961	British standard specification for cadmium plated steel bolts of high metallurgical quality (unified hexagons, unified threads and close tolerance shanks) for aircraft	1961	British Standards Institution
Box 239	A. 226, December, 1965	British standard specification for steel hexagon head bolts (short thread: class 3a)	1965	British Standards Institution
Box 239	A. 227, December, 1965	British standard specification for steel pan head bolts (short thread: class 3a)	1965	British Standards Institution
Box 239	A. 228, January, 1966	British standard specification for steel double hexagon head bolts (180 000 lbf/in2) for aircraft	1966	British Standards Institution
Box 239	A. 229, April, 1968	British standard: aerospace series specification for steel hexagonal head steel bolts 160 000 lbf/in2 (110hbar)	1968	British Standards Institution
Box 239	A. 230, February, 1968	British standard: aerospace series specification for 100 degree countersunk head steel bolts (160 000 lbf/in2 (110 hbar) with hi-torque recesses)	1968	British Standards Institution
Box 239	A. 231 : 1982 ISO 3353-1976	British standard: aerospace series specification for runout and lead threads	1982	British Standards Institution
Box 239	A. 232, February, 1968	British standard: aerospace series specification for 100 degree countersunk head steel bolts (160 000 lbf/in2 (110 hbar) with torq-set recesses)	1968	British Standards Institution
Box 239	A. 233-236, March, 1971	British standard: aerospace series specification for plain hexagonal thin nut (of class 3b unj thread)	1971	British Standards Institution
Box 239	A. 241 : October, 1973	British standard: aerospace series general requirements for steel protruding-head bolts of tensile strength 1250 mpa (180 000 lbf/in2) or greater	1973	British Standards Institution
Box 239	A 242-245 : June : 1974	British standard: aerospace series specification for hexagonal castle nuts (of class 3b unj thread)	1974	British Standards Institution
Box 239	A 246-249 : June : 1974	British standard: aerospace series specification for slotted hexagonal thick nuts (of class 3b unj thread)	1974	British Standards Institution
Box 239	A 250-253 : June : 1974	British standard: aerospace series specification for slotted hexagonal shear nuts (of class 3b unj thread)	1974	British Standards Institution
Box 239	A 254-259 : 1976	British standard: aerospace series specification for hexagonal head titanium alloy bolts 160 000 lbf/in2 (1100 mpa)	1976	British Standards Institution
Box 239	A 260-265 : 1976	British standard: aerospace series specification for metric screws	1976	British Standards Institution
Box 239	A 266-271 : 1977	British standard specification for 100 degree countersunk head titanium alloy bolts 160 000 lbf/in2 (1100 mpa) with hi-torque speed drive recesses	1977	British Standards Institution
Box 239	A 272 : 1977	British standard: aerospace series specification for hi-torque recesses: dimensions and gauging for countersunk head fasteners	1977	British Standards Institution
Box 239	A 273 : 1978	British standard specification for gauging practice for 100 degree countersunk head fasteners for flushness control	1978	British Standards Institution
Box 239	A 274 : 1981	British standard: aerospace series specification for procurement of alloy steel bolts, metric, with a minimum tensile strength of 1100mpa	1981	British Standards Institution
Box 239	A 275-280 : 1981	British standard: aerospace series specification hexagon self-locking nuts with non-metallic locking inserts. Metric series	1981	British Standards Institution
Box 239	A 281-286 : 1981	British standard: aerospace series specification hexagon (thin) self-locking nuts with non-metallic locking inserts. Metric series	1981	British Standards Institution
Box 239	2 A. 24, May, 1962	British standard specification for corrosion-resisting steel hexagonal nuts (b.a. And b.s.f. Threads) (ordinary, thin, slotted and castle) for aircraft	1962	British Standards Institution
Box 239	2 A. 25, May, 1962	British standard specification for steel hexagonal-headed bolts (b.a. And b.s.f. Threads) for aircraft	1962	British Standards Institution
Box 239	2 A. 26, May, 1962	British standard specification for corrosion-resisting steel hexagonal-headed bolts (b.a. And b.s.f. Threads) for aircraft	1962	British Standards Institution
Box 239	2 A. 27, May, 1962	British standard specification for steel hexagonal nuts (b.a. And b.s.f. Threads) (ordinary, thin, slotted and castle) for aircraft	1962	British Standards Institution
Box 239	2 A. 29, November, 1962	British standard specification for aluminium alloy hexagonal nuts (b.a. And b.s.f. Threads) (ordinary, thin, slotted) for aircraft	1962	British Standards Institution
Box 239	2 A. 30, May, 1962	British standard specification for steel hexagonal-headed bolts (b.a. And b.s.f. Threads) with close tolerance shanks for aircraft	1962	British Standards Institution
Box 239	2 A. 57, May, 1962	British standard specification for steel hexagonal-headed shear bolts (b.s.f. Threads) for aircraft	1962	British Standards Institution
Box 239	2 A. 58, May, 1962	British standard specification for steel hexagonal-headed nuts (b.s.f. Threads) for shear bolts for aircraft	1962	British Standards Institution
Box 239	2 A. 59, May, 1962	British standard specification for cadmium plated steel hexagonal bolts (b.a. And b.s.f. Threads) with close tolerance shanks for aircraft	1962	British Standards Institution
Box 239	2 A. 60, May, 1962	British standard specification for cadmium plated steel hexagonal shear bolts (b.s.f. Threads) for aircraft	1962	British Standards Institution
Box 239	2 A. 61, November, 1962	British standard specification for aluminium alloy hexagonal nuts (b.a. And b.s.f. Threads) for aircraft	1962	British Standards Institution
Box 239	2 A. 100 : 1968	General requirements for bolts and nuts of tensile strength not exceeding 180000 1bf/in2 (125 hbar)	1968	British Standards Institution
Box 239	2 A. 104, January, 1956	British standard specification for corrosion-resisting steel bolts (unified hexagons and unified threads) for aircraft	1956	British Standards Institution
Box 239	2 A. 105, January, 1956	British standard specification for corrosion-resisting steel nuts (unified hexagons and unified threads) (ordinary, thin, slotted and castle) for aircraft	1956	British Standards Institution
Box 239	2 A. 107, January, 1956	British standard specification for aluminium alloy nuts (unified hexagons and unified threads) (ordinary and slotted) for aircraft	1956	British Standards Institution
Box 239	2 A. 109, June, 1962	British standard specification for steel shear bolts (unified hexagons and unified threads) for aircraft	1962	British Standards Institution
Box 239	2 A. 110, June, 1962	British standard specification for steel nuts (unified hexagons and unified threads) for shear bolts for aircraft	1962	British Standards Institution
Box 239	2 A. 112, June, 1962	British standard specification for cadmium plated steel hexagonal shear bolts (unified hexagons and unified threads) for aircraft	1962	British Standards Institution
Box 239	2 A. 114, March, 1956	British standard specification for corrosion-resisting steel mushroom head bolts (unified threads) for aircraft	1956	British Standards Institution
Box 239	2 A. 117, July, 1956	British standard specification for corrosion-resisting steel pan head bolts (unified threads) for aircraft	1956	British Standards Institution
Box 239	2 A. 119, March, 1954	British standard specification for 90 degree countersunk head steel bolts (unf threads) for aircraft	1954	British Standards Institution
Box 239	2 A 122-124 : 1981	British standard: aerospace series specification clinch nuts (unified threads) for aircraft	1981	British Standards Institution
Box 239	2 A. 125-168, 2 A. 180-181, 2A. 186-187, 2 A. 192-193, 2 A. 200-201 January, 1958	British standards for stiffnuts (unified threads) for aircraft	1958	British Standards Institution
Box 239	2 A. 169, January, 1956	British standard specification for aluminium alloy bolts (unified hexagons and unified threads) for aircraft	1956	British Standards Institution
Box 239	2 A. 170, March,1956	British standard specification for aluminium alloy mushroom head bolts (unified threads) for aircraft	1956	British Standards Institution
Box 239	2 A. 171, July, 1956	British standard specification for aluminium alloy pan head bolts (unified thread) for aircraft	1956	British Standards Institution
Box 239	2 A. 173, June, 1962	British standard specification for 100 degree countersunk head steel bolts (unified threads) for aircraft	1962	British Standards Institution
Box 239	2 A. 174, May, 1962	British standard specification for 100 degree countersunk head corrosion- resisting steel bolts (unified threads) for aircraft	1962	British Standards Institution
Box 239	2 A. 175, November, 1962	British standard specification for 100 degree countersunk head aluminium alloy bolts (unified threads) for aircraft	1962	British Standards Institution
Box 239	A. 204-209, November, 1962	British standard specification for machine screws (unified threads) for aeronautical purposes	1962	British Standards Institution
Box 239	2 A. 204, 2 A. 206, 2 A. 208 and A. 217-225, April, 1963	British standard specification for machine screws and nuts (unified threads) below one quarter inch for aeronautical purposes	1963	British Standards Institution
Box 239	2 A. 210, , November, 1962	British standard specification for brass nuts (unified hexagons and unified threads) for aircraft	1962	British Standards Institution
Box 239	2 A. 212, June, 1973	British standard specification for cadmium plated steel bolts, 55/65 ton/in2 (unified hexagons, 3a unified threads and close tolerance shanks) for aerospace use	1973	British Standards Institution
Box 239	2 A. 228, July,1971	British standard specification for steel double hexagon bolts (180 000lbf/in2) for aircraft	1971	British Standards Institution
Box 239	2 A. 229, September,1972	British standard: aerospace series specification for hexagonal head steel bolts 160 000 lbf/in2 (1100 mpa) for aircraft	1972	British Standards Institution
Box 239	2 A. 230, June, 1974	British standard: aerospace series specification for 100 degree countersunk head steel bolts (160 000 lbf/in2 (1100 mpa) with hi-torque speed drive recesses)	1974	British Standards Institution
Box 239	3 A. 102, June, 1962	British standard specification for steel bolts (unified hexagons and unified threads) for aircraft	1962	British Standards Institution
Box 239	3 A. 103, June, 1962	British standard specification for steel nuts (unified hexagons and unified threads) (ordinary, thin, slotted and castle) for aircraft	1962	British Standards Institution
Box 239	3 A. 104, May, 1962	British standard specification for corrosion-resisting steel bolts (unified hexagons and unified threads) for aircraft	1962	British Standards Institution
Box 239	3 A. 105, May, 1962	British standard specification for corrosion-resisting steel bolts (unified hexagons and unified threads) (ordinary, thin, slotted and castle) for aircraft	1962	British Standards Institution
Box 239	3 A 107, November, 1962	British standard specification for aluminium alloy nuts (unified hexagons and unified threads) (ordinary and slotted) for aircraft	1962	British Standards Institution
Box 239	3 A 108, June, 1962	British standard specification for steel bolts with close tolerance shanks for aircraft	1962	British Standards Institution
Box 239	3 A. 111, June, 1962	British standard specification for cadmium plated steel bolts (unified hexagons and unified threads) with close tolerance shanks) for aircraft	1962	British Standards Institution
Box 239	3 A. 113, June, 1962	British standard specification for steel mushroom head bolts (unified threads) for aircraft	1962	British Standards Institution
Box 239	3 A. 114, May, 1962	British standard specification for corrosion-resisting steel mushroom head bolts (unified threads) for aircraft	1962	British Standards Institution
Box 239	3 A. 116, June,1962	British standard specification for steel pan head bolts (unified thread) for aircraft	1962	British Standards Institution
Box 239	3 A. 117, May,1962	British standard specification for corrosion-resisting steel pan head bolts (unified threads) for aircraft	1962	British Standards Institution
Box 239	3 A. 125-132, 136-143, 147-168, 180, 181, 186, 187, 192, 193, 200, 201, 213-216 : 1981	British standard specification for stiffnuts (unified threads) for aircraft	1981	British Standards Institution
Box 239	3 A. 169, November, 1962	British standard specification aluminium alloy bolts (unified hexagons and unified threads) for aircraft	1962	British Standards Institution
Box 239	3 A. 170, November, 1962	British standard specification for aluminium alloy mushroom head bolts (unified threads) for aircraft	1962	British Standards Institution
Box 239	3 A 171, November, 1962	British standard specification for aluminium allow pan head bolts for aircraft	1962	British Standards Institution
Box 239	3 A. 228 : 1979	British standard: aerospace series specification for steel double hexagon bolts 1250 mpa (180 000 lbf/in2) for aircraft	1979	British Standards Institution
Box 239	4 A.4 : Part 1 : Section Two, June, 1967	British standard test pieces and test methods for metallic materials for aircraft	1967	British Standards Institution
Box 239	4 A.4 : Part 1 : Section Three, June, 1967	British standard test pieces and test methods for metallic materials	1967	British Standards Institution
Box 239	4 A.4, February, 1966	British standard test pieces and test methods for metallic materials for aircraft	1966	British Standards Institution
Box 239	2 B. 8. August,1930	British standard specification for aircraft material. Phosphor bronze castings for bearings. (Including solid and cored sticks)	1930	British Standards Institution
Box 239	2 B. 21. July, 1933	British standard specification for aircraft material. White metal (88/8/4) ingots. (Suitable for bearings).	1933	British Standards Institution
Box 239	2 B. 22. July, 1933	British standard specification for aircraft material. White metal (92/4/4) ingots. (Suitable for bearings).	1933	British Standards Institution
Box 239	3 B. 11. April, 1933	British standard specification for aircraft material. Brass bars suitable to be brazed or silver soldered	1933	British Standards Institution
Box 239	C. 1, October, 1961	British standard specification for coupling dimensions for aircraft toilet flushing, chemical recharging and draining connections	1961	British Standards Institution
Box 239	C. 2, October, 1962	British standard specification for coupling dimensions for aircraft connections for water of drinkable quality	1962	British Standards Institution
Box 239	C. 3, May, 1964	British standard specification for aircraft material coupling dimensions for aircraft pressure re-oiling connection	1964	British Standards Institution
Box 239	C. 4, June , 1966	British standard specification for coupling dimensions for aircraft methanol-water pressure connections	1966	British Standards Institution
Box 239	C. 5 May, 1965	British standard specification for mating dimensions for liquid oxygen replenishment couplings for aircraft	1965	British Standards Institution
Box 239	C. 6 June, 1966	British standard specification for aircraft engine nacelle fire extinguisher doors	1966	British Standards Institution
Box 239	C. 7, December, 1967	British standard: aerospace series specification for interconnectability of aircraft tyre values	1967	British Standards Institution
Box 239	C. 8 February, 1969	British standards: aerospace series specification for the dimensions of seat rails and pins (metric and inch units)	1969	British Standards Institution
Box 239	C. 9, March, 1970	British standard: aerospace series specification for coupling dimensions for high pressure air charging valves for aircraft	1970	British Standards Institution
Box 239	C. 10, February, 1958	British standard for coupling dimensions for aircraft ground air-conditioning connections	1958	British Standards Institution
Box 239	C. 11, February, 1958	British standard for coupling dimensions for aircraft pressure cabin ground test connections	1958	British Standards Institution
Box 239	C. 12, May, 1958	British standard for form of contact surface of aircraft jacking pads	1958	British Standards Institution
Box 239	C. 15, October, 1960	British standard specification for coupling dimensions for aircraft-to-tractor tow bar connections	1960	British Standards Institution
Box 239	C 16 : October 1973	British standard: aerospace series specification for dimensions for gaseous oxygen replenishment couplings for aircraft	1973	British Standards Institution
Box 239	C 17 : October 1973	British standard: aerospace series specification for coupling dimensions for low pressure air connections for engine starting	1973	British Standards Institution
Box 239	C 18 : 1976	British standard aerospace series: specification for v-flange couplings for aircraft piping and ducting - metric series	1976	British Standards Institution
Box 239	2C 2 : November 1973	British standard: aerospace series specification for coupling dimensions for aircraft connections for water of a drinkable quality	1973	British Standards Institution
Box 239	2C 4 : October 1973	British standard: aerospace series specification for coupling dimensions for aero-engine refrigerant pressure replenishment connections	1973	British Standards Institution
Box 239	2C 5 : 1976	British standard aerospace series: specification for mating dimensions for liquid oxygen replenishment couplings	1976	British Standards Institution
Box 239	2C 12 : 1980	British standard aerospace series: specification for jacking pads for aircraft	1980	British Standards Institution
Box 239	2C. 14, March, 1970	British standard: aerospace series specification for coupling dimensions for aircraft pressure-refuelling connection	1970	British Standards Institution
Box 239	3C 14 : 1982	British standard aerospace series: specification for coupling requirements for aircraft pressure fuelling connection	1982	British Standards Institution
Box 239	D. 26. November, 1921	British standard specification for aircraft material. Yellow ochre	1921	British Standards Institution
Box 239	2 D. 27. October, 1929	British standard specification for aircraft material. Zinc oxide	1929	British Standards Institution
Box 239	2 D. 28. October, 1929	British standard specification for aircraft materials. Red oxide of iron	1929	British Standards Institution
Box 239	2 D. 29. October, 1929	British standard specification for aircraft materials. Identification red	1929	British Standards Institution
Box 239	2 D. 30. March, 1930	British standard specification for aircraft materials. Carbon black	1930	British Standards Institution
Box 239	2 D. 31. October, 1929	British standard specification for aircraft materials. Ultramarine blue	1929	British Standards Institution
Box 239	2 D. 32 March, 1930	British standard specification for aircraft materials. Aluminium powder	1930	British Standards Institution
Box 239	3 D. 7. October, 1929	British standard specification for aircraft material. Benzyl alcohol	1929	British Standards Institution
Box 239	E. 19. September, 1948	British standard specification for aircraft material. Aircraft lamps	1948	British Standards Institution
Box 239	E. 20. February, 1949	British standard specification for high tension ignition cables for aircraft engines	1949	British Standards Institution
Box 239	E. 22, March, 1955	British standard specification for dummy sparking plug for aircraft	1955	British Standards Institution
Box 239	E. 23, April, 1957	British standard for guards for feathering switches for aircraft	1957	British Standards Institution
Box 239	E. 25, December, 1957	British standard for spring covers for push-button switches for aircraft	1957	British Standards Institution
Box 239	2 E. 21, December, 1957	British standard for pren type electric cables for aircraft	1957	British Standards Institution
Box 240	F. 57. June, 1934	British standard specification for aircraft material. Scoured cotton fabrics	1934	British Standards Institution
Box 240	F. 60. November, 1934	British standard specification for hard vulcanized fibre sheets for jointing for aircraft purposes	1934	British Standards Institution
Box 240	F. 61, March, 1935	British standard specification for vulcanized rubber sheet for aircraft	1935	British Standards Institution
Box 240	F. 62, November, 1951	British standard specification for cellular rubber sheet for aircraft	1951	British Standards Institution
Box 240	F. 63, August, 1957	British standard for low pressure oxygen hose for aircraft	1957	British Standards Institution
Box 240	F. 64, August, 1957	British standard for flexible vulcanized fibre sheets for aeronautical purposes	1957	British Standards Institution
Box 240	F. 65, July, 1958	British standard for flexible corrugated oxygen tubes for aircraft	1958	British Standards Institution
Box 240	F. 66, February, 1965	British standard specification for rubber boned cork sheets for aeronautical purposes	1965	British Standards Institution
Box 240	F. 67, February, 1966	British standard specification for hose for aviation fuel and engine lubricating oil for aeronautical purposes	1966	British Standards Institution
Box 240	F. 68, February, 1968	British standard: aerospace series recommendations for the storage and inspection in store of vulcanized rubber items	1968	British Standards Institution
Box 240	F. 69, February, 1968	British standard: aerospace series specification for packing and identification of vulcanized rubber items	1968	British Standards Institution
Box 240	F. 70: February, 1973	British standard: aerospace series specification for heavy duty braided rubber cord	1973	British Standards Institution
Box 240	F. 71: February, 1973	British standard: aerospace series specification for light duty braided rubber cord	1973	British Standards Institution
Box 240	F. 100, August, 1957	British standard for inspection and testing procedures for textiles for aeronautical purposes	1957	British Standards Institution
Box 240	F. 110, October, 1959	British standard for medium weight flax fabric for aeronautical purposes	1959	British Standards Institution
Box 240	F. 111, October, 1959	British standard for flax harness webbing for aeronautical purposes	1959	British Standards Institution
Box 240	F. 112, December, 1960	British standard for twisted and cabled flat cords for aeronautical purposes	1960	British Standards Institution
Box 240	F. 113, December, 1960	British standard for buoyant cotton cord for aeronautical purposes	1960	British Standards Institution
Box 240	F. 114, June, 1963	British standard specification for light cotton fabric for aeronautical purposes	1963	British Standards Institution
Box 240	F. 115, June, 1963	British standard specification for 1 and 1/2 oz cotton fabric for aeronautical purposes	1963	British Standards Institution
Box 240	F. 116, June, 1963	British standard specification for mercerised cotton fabrics for aeronautical purposes	1963	British Standards Institution
Box 240	F. 117, June, 1963	British standard specification for 7 oz cotton fabric for aeronautical purposes	1963	British Standards Institution
Box 240	F. 118, February, 1964	British standard specification for medium-weight nylon fabrics for aeronautical purposes	1964	British Standards Institution
Box 240	F. 119, February, 1964	British standard specification for medium-weight nylon fabrics for aeronautical purposes	1964	British Standards Institution
Box 240	F. 120, September, 1964	British standard specification for nylon sewing threads for aeronautical purposes	1964	British Standards Institution
Box 240	F. 121, December, 1964	British standard specification for metallic slide fasteners for aeronautical purposes	1964	British Standards Institution
Box 240	F. 122, September, 1967	British standard: aerospace series specification for two ply fabric for liferaft packs	1967	British Standards Institution
Box 240	F. 123, April, 1968	British standard: aerospace series specification for medium-strength woven nylon tape and webbing	1968	British Standards Institution
Box 240	F. 124, April, 1968	British standard: aerospace series specification for high-strength woven nylon tape and webbing	1968	British Standards Institution
Box 240	F. 125: November 1973	British standard: aerospace series specification for rubber bonded compressed asbestos fibre jointing	1973	British Standards Institution
Box 240	F. 126: 1980	British standard: aerospace series specification for 35 g/m square nylon parachute fabric	1980	British Standards Institution
Box 240	2F. 30. october, 1930	British standard specification for aircraft material. Cotton breaking cord for supplies droppers	1930	British Standards Institution
Box 240	2F. 38. october, 1930	British standard specification for aircraft material. 18 oz. Flax canvas	1930	British Standards Institution
Box 240	2F. 41. August, 1930	British standard specification for aircraft material. Rubber-proofed fabric	1930	British Standards Institution
Box 240	2F. 49, October, 1959	British standard for cotton webbing for aeronautical purposes	1959	British Standards Institution
Box 240	2F. 52, October, 1959	British standard for flax reinforcement webbing for aeronautical purposes	1959	British Standards Institution
Box 240	2F. 54 December, 1960	British standard for flax sewing cord for aeronautical purposes	1960	British Standards Institution
Box 240	2F. 55. May, 1940	British standard specification for cotton duck (dyed) for cases and travelling bags for parachutes for aircraft purposes	1940	British Standards Institution
Box 240	2F. 57, June, 1963	British standard specification for scoured cotton fabrics for aeronautical purposes	1963	British Standards Institution
Box 240	2F. 58, December, 1960	British standard for cotton sewing thread for aeronautical purposes	1960	British Standards Institution
Box 240	2 F. 59 December, 1960	British standard for plaited cord for aeronautical purposes	1960	British Standards Institution
Box 240	2F. 63, January, 1967	British standard specification for low pressure oxygen hose for aeronautical purposes	1967	British Standards Institution
Box 240	2F. 65:1981	British standard aerospace series: specification for flexible corrugated oxygen and air tubes for aircraft (natural or synthetic polyisoprene)	1981	British Standards Institution
Box 240	2F. 66:1982	British standard aerospace series: specification for rubber bonded cork sheets	1982	British Standards Institution
Box 240	2F. 67: 1980	British standard aerospace series: specification for hose for aviation fuel and engine lubricating oil for aeronautical purposes	1980	British Standards Institution
Box 240	2F. 68: March 1973	British standard: aerospace series recommendations for the storage and inspection in store of vulcanized rubber items	1973	British Standards Institution
Box 240	2F. 69, October 1973	British standard: aerospace series specification for packaging and identification of vulcanized rubber items	1973	British Standards Institution
Box 240	2F. 100, September,1966	British standard for inspection and testing procedures and certain basic requirements for textiles for aeronautical purposes	1966	British Standards Institution
Box 240	2F. 111: April 1973	British standard: aerospace series specification for flax harness webbing	1973	British Standards Institution
Box 240	2F. 114: February 1975	British standard: aerospace series specification for 80g cotton madapolam fabric	1975	British Standards Institution
Box 240	2F. 115: February 1975	British standard: aerospace series specification for 50g cotton madapolam fabric	1975	British Standards Institution
Box 240	2F. 116: February 1975	British standard: aerospace series specification for mercerized cotton parachute fabric	1975	British Standards Institution
Box 240	2F. 118: 1978	British standard: aerospace series specification for 50g/m square nylon parachute fabric	1978	British Standards Institution
Box 240	2F. 119: 1982	British standard: aerospace series specification for 145g/m square to 210g/m square nylon fabrics	1982	British Standards Institution
Box 240	2F. 120: 1975	British standard: aerospace series specification for nylon sewing thread	1975	British Standards Institution
Box 240	2F. 122: 1978	British standard: aerospace series specification for two ply cotton fabric for liferaft packs	1978	British Standards Institution
Box 240	3F. 37, June, 1963	British standard specification for heavy cotton fabric for aeronautical purposes	1963	British Standards Institution
Box 240	3F. 45. November, 1936	British standard specification for aircraft material. Rubber hose for use with hot water for aircraft purposes	1936	British Standards Institution
Box 240	3F. 49, June, 1972	British standard: aerospace series specification for cotton webbing	1972	British Standards Institution
Box 240	3F. 50, May, 1939	British standard specification for eyeleted fuselage webbing for aircraft purposes	1939	British Standards Institution
Box 240	3F. 54: 1975	British standard specification for heavy duty linen (flax) sewing thread	1975	British Standards Institution
Box 240	3F. 55, June, 1963	British standard specification for medium weight cotton fabrics for aeronautical purposes	1963	British Standards Institution
Box 240	3F. 57: February 1975	British standard: aerospace series specification for scoured cotton fabric for inflatable equipments	1975	British Standards Institution
Box 240	3F. 58: 1975	British standard: aerospace series specification for cotton sewing thread	1975	British Standards Institution
Box 240	3F. 59: 1975	British standard: aerospace series specification for braided lned (flax) cord	1975	British Standards Institution
Box 240	3F. 63: 1981	British standard: aerospace series specification for low pressure oxygen hose for aeronautical purposes	1981	British Standards Institution
Box 240	3F. 68 :1977	British standard: aerospace series specification for controlled storage of vulcanized rubbers for use in aerospace applications	1977	British Standards Institution
Box 240	3F. 69: 1979	British standard: aerospace series specification for packaging and identification of vulcanized rubber items	1979	British Standards Institution
Box 240	3F. 100: Februeary 1975	British standard: aerospace series procedure for inspection and testing of textiles	1975	British Standards Institution
Box 240	3F. 118: 1980	British standard: aerospace series specification for 50g/m square nylon parachute fabric	1980	British Standards Institution
Box 240	4 F. 31 December, 1960	British standard for soft laid hemp cord for aeronautical purposes	1960	British Standards Institution
Box 240	4 F. 37: February 1975	British standard: aerospace series specification for heavy cotton fabric	1975	British Standards Institution
Box 240	4 F. 47, October, 1959	British standard for cotton tape for aeronautical purposes	1959	British Standards Institution
Box 240	4 F. 51, February, 1957	British standard for light duty braided rubber cord for aircraft	1957	British Standards Institution
Box 240	4 F. 55, February, 1957	British standard: aerospace series specification for medium-mass cotton fabric	1957	British Standards Institution
Box 240	4F 100: 1982	British standard aerospace series: procedure for inspection and testing of textiles	1982	British Standards Institution
Box 240	5F.8, January, 1965	British standard specification for 4 and 1/4 oz cotton fabric and serrated edge strip for aeronautical purposes	1965	British Standards Institution
Box 240	5F.15 December, 1960	British standard for hemp line and rope for aeronautical purposes	1960	British Standards Institution
Box 240	5F.32 December, 1960	British standard for hemp cord for aeronautical purposes	1960	British Standards Institution
Box 240	4F. 33 October, 1961	British standard specification for flexible cotton rope for aeronautical purposes	1961	British Standards Institution
Box 240	4F. 34 December, 1960	British standard for linen sewing thread for aeronautical purposes	1960	British Standards Institution
Box 240	5F. 34: 1975	British standard: aerospace series specification for light and medium dutylined (flax) sewing thread	1975	British Standards Institution
Box 240	5F. 35 December, 1960	British standard for braided (plaited) flax cord for aeronautical purposes	1960	British Standards Institution
Box 240	5F. 47, June, 1972	British standard: aerospace series specification for cotton tape	1972	British Standards Institution
Box 240	5F. 51, August, 1966	British standard specification light duty braided rubber cord for aeronautical purposes	1966	British Standards Institution
Box 240	5F. 55: 1982	British standard aerospace series: specification for 345g/m square and 415g/m square cotton fabrics	1982	British Standards Institution
Box 240	6F 8: February 1975	British standard: aerospace series specification for mercerized 140g cotton fabric and serrated edge strip	1975	British Standards Institution
Box 240	6F 16: February, 1957	British standard for heavy duty braided rubber cord for aircraft	1957	British Standards Institution
Box 240	6F 35: 1975	British standard: aerospace series specification for braided linen (flax) lacing cord	1975	British Standards Institution
Box 240	7F. 1, October, 1959	British standard for linen fabric and tape for aeronautical purposes	1959	British Standards Institution
Box 240	7F. 16, August, 1966	British standard specification for heavy duty braided rubber cord for aeronautical purposes	1966	British Standards Institution
Box 240	8F 1: February, 1975	British standard: aerospace series specification for 140g linen fabric and serrated edge strip	1975	British Standards Institution
Box 240	G 100	British standard specification for general requirements for electrical equipment and indicating instruments for aircraft	1952	British Standards Institution
Box 240	G 101	British standard specification for general requirements for aircraft indicators: presentation and case sizes	1963	British Standards Institution
Box 240	G 102	British standard: aerospace series specification for general requirements for rotating electrical machinery	1971	British Standards Institution
Box 240	G 116	Permanent magnet moving coil millivoltmeter for the indication of temperature in conjunction with thermocouples in aircraft	1949	British Standards Institution
Box 240	G 117	British standard specification for air speed indicator for aircraft	1949	British Standards Institution
Box 240	G 118	British standard specification for aircraft magnetic compass direct-reading	1949	British Standards Institution
Box 240	G 119	British standard specification for simple altimeters for aircraft	1949	British Standards Institution
Box 240	G 120	British standard specification for direct-reading pressure gauges for aircraft	1949	British Standards Institution
Box 240	G 122	British standard specification for aircraft compass remote-reading gyro-stabilized	1949	British Standards Institution
Box 240	G 123	British standard specification for aircraft magnetic compass remate-reading (non-stabilized)	1949	British Standards Institution
Box 240	G 124	British standard specification for a.c generators for aircraft	1950	British Standards Institution
Box 240	G 125	Turn and slip indicators for aircraft purposes	1950	British Standards Institution
Box 240	G 126	British standard specification for electric power metal rectifiers for aircraft purposes	1950	British Standards Institution
Box 240	G 127	Power transformers for aircraft purposes	1950	British Standards Institution
Box 240	G 128	British standard specification for crossed pointer indicators for use instrument landing system receivers for aircraft purposes	1950	British Standards Institution
Box 240	G 129	British standard specification for extra-low voltage switches (hand-operated) for aircraft	1950	British Standards Institution
Box 240	G 130	Battery cut-outs (reserve current relays) for aircraft	1950	British Standards Institution
Box 240	G 132	British standard specification for electro-magnetically operated a.c contactors for aircraft	1951	British Standards Institution
Box 240	G133	British standard specification for electro-magnetic indicators for extra low voltage aircraft systems	1951	British Standards Institution
Box 240	G 135	British standard specification for electrically heated pitot and pitot static pressure heads for aircraft	1951	British Standards Institution
Box 240	G 136	British standard specification for extra-low voltage d.c cyclic switches for aircraft	1951	British Standards Institution
Box 240	G 137	British standard specification for extra-low voltage d.c flashing unit for aircraft navigation light systems	1952	British Standards Institution
Box 240	G 138	British standard specification for extra-low voltage and low voltage ram air pressure switches for aircraft	1952	British Standards Institution
Box 240	G 140	British standard specification for hand-operated a.c. Circuit-breakers for aircraft	1952	British Standards Institution
Box 240	G 141	British standard specification for flexibly mounted instrument panels for fixed wing aircraft	1953	British Standards Institution
Box 240	G 142	British standard specification for heavy duty, electro-magnetically operated, single-pole circuit-breakers for extra-low voltage d.c systems in aircraft	1953	British Standards Institution
Box 240	G 143	British standard specification for d.c. Linear and rotary actuators for aircraft	1953	British Standards Institution
Box 240	G 144	British standard specification for direct-reading storage pressure gauges for aircraft	1953	British Standards Institution
Box 240	G 145	British standard specification for extra-low voltage spring return non-latch switches for aircraft	1954	British Standards Institution
Box 240	G 146	British standard specification for d.c. Motors for aircraft	1955	British Standards Institution
Box 240	G 147	British standard specification for a.c motors for aircraft. Part 1: three-phase 400 c/s squirrel-cage induction motors	1955	British Standards Institution
Box 240	G 148	British standard specification for platinum wire thermometer bulbs and connectors for aircraft	1955	British Standards Institution
Box 240	G 149	British standard specification for nickel wire thermometer bulbs and connectors for liquid temperature measurement in aircraft	1955	British Standards Institution
Box 240	G 150	British standard specification for tachometer indicators (synchronous type) for aircraft	1955	British Standards Institution
Box 240	G 151	British standard specification for tachometer generators (synchronous type) for aircraft	1955	British Standards Institution
Box 240	G 152	British standard specification for a.c. Electrically-operated artificial horizons for aircraft	1956	British Standards Institution
Box 240	G 153	British standard specification for air-driven artificial horizons for aircraft	1956	British Standards Institution
Box 240	G 154	British standard for screws with captive washers for aircraft	1958	British Standards Institution
Box 240	G 155	British standard for single-entry gland assemblies for aircraft electrical cables	1958	British Standards Institution
Box 240	G 156	British standard for glands for aircraft electrical cables	1958	British Standards Institution
Box 240	G 157 to G 166	British standard for sealing sleeves and sealing cones for aircraft electrical cable gland assemblies	1958	British Standards Institution
Box 240	G 167 to 170	British standard for bonding sleeves for aircraft electrical cable gland assemblies	1958	British Standards Institution
Box 240	G 171	British standard for washers for aircraft electrical cable gland assemblies	1958	British Standards Institution
Box 240	G 172	British standard for union nuts for aircraft electrical cable gland assemblies	1958	British Standards Institution
Box 240	G 173	British standard for [?] for ground electrical supply to aircraft	1958	British Standards Institution
Box 240	G 174	British standard for invertors for secondary electrical supplies for aircraft	1959	British Standards Institution
Box 240	G 175	British standard for aircraft fuel nozzle grounding plugs and sockets	1959	British Standards Institution
Box 240	G 176 : Part 3	British standard specification for cartridge fuses for aircraft. Part 3. Cartridge fuse-links (type b)	1961	British Standards Institution
Box 240	G 176 : Part 4	British standard specification for cartridge fuses for aircraft. Part 4. Cartridge fuse-links (type c)	1962	British Standards Institution
Box 240	G 176 : Part 5	British standard specification for cartridge fuses for aircraft. Part 5. Cartridge fuse-links (type d)	1966	British Standards Institution
Box 240	G 177	Nyvin type electrical cables for aircraft	1961	British Standards Institution
Box 240	G 178	Crimped joints (non-insulated) for general purpose electrical cables for aircraft	1961	British Standards Institution
Box 240	G 179 : Part 1	British standard specification for hand-operated circuit-breakers for aircraft. Part. 1 single-pole circuit-breakers	1962	British Standards Institution
Box 240	G 179 : Part 2	British standard specification for hand-operated circuit-breakers for aircraft. Part. 2. Three-pole circuit-breakers	1966	British Standards Institution
Box 240	G 180	British standard specification for in-line connection of aircraft electrical cables	1962	British Standards Institution
Box 240	G 181	British standard specification for electric lamps for aircraft	1963	British Standards Institution
Box 240	G 182	British standard specification for subsonic machmeters for aircraft	1963	British Standards Institution
Box 240	G 183	British standard specification for interconnections in analogue data transmission system in aircraft	1963	British Standards Institution
Box 240	G 184 TO G188	British standard specification for aluminium terminal ends and in-line connectors for hexagonal crimping to aircraft aluminium electrical cables	1964	British Standards Institution
Box 240	G 189	British standard specification for tensil type electrical cables for aircraft	1964	British Standards Institution
Box 240	G 190	British standard specification for cabin altimeters for aircraft	1964	British Standards Institution
Box 240	G 191	British standard specification for lighting for aircraft indicators using integral filament lamps	1965	British Standards Institution
Box 240	G 192	British standard specification for efglas type electric cables with copper conductors for aircraft	1965	British Standards Institution
Box 240	G 193	British standard specification for aircraft lamp holders	1966	British Standards Institution
Box 240	G 194	British standard specification for lever-operated manual switches for aircraft	1965	British Standards Institution
Box 240	G 195	British standard specification for minyvin* type electric cables for aircraft	1966	British Standards Institution
Box 240	G 196	British standard specification for static invertors for aircraft	1966	British Standards Institution
Box 240	G 197	British standard specification for terminal blocks for terminations on aircraft electric cables	1967	British Standards Institution
Box 240	G 198 : Part 1.	British standard specification for binding and identification sleeves for aircraft electric cables and equipment wires. Part. 1. Elastomeric sleeves	1967	British Standards Institution
Box 240	G 198 : Part 2.	British standard: aerospace series specification for binding and identification sleeves for electric cables and equipment wires. Part. 2. Slip-on and spring-on sleeves	1969	British Standards Institution
Box 240	G 199	British standard: aerospace series tables relating pressure to altitudes, airspeeds and mach numbers for use in aeronautical instrument design and calibration	1967	British Standards Institution
Box 240	G 200	British standard: aerospace series specification for miniature lever-operated manual switches	1967	British Standards Institution
Box 240	G 201	British standard: aerospace series specification for counter and pointer pressure altimeters	1967	British Standards Institution
Box 240	G 202	British standard: aerospace series specification for design and performance requirements for aircraft electrical plugs and sockets for d.c. And low frequency a.c. Applications	1968	British Standards Institution
Box 240	G 203	British standard: aerospace series specification for unified screws with captive facing and locking washers	1967	British Standards Institution
Box 240	G 204	British standard: aerospace series specification for copper terminal ends for crimping to electric cables with copper conductors	1967	British Standards Institution
Box 240	G 205 : Part 1	British standard: aerospace series specification for secondary batteries (acid and alkaline). Part. 1. General requirements	1969	British Standards Institution
Box 240	G 206	British standard: aerospace series specification for fepsil type electric cables with copper conductors	1969	British Standards Institution
Box 240	G 207	British standard: aerospace series specification for aircraft electrical circuit diagrams	1969	British Standards Institution
Box 240	G 208	British standard: aerospace series specification for general requirements for electrical relays up to 10 a rating	1970	British Standards Institution
Box 240	G 209	British standard: aerospace series specification for transformer rectifier units	1970	British Standards Institution
Box 240	G 210	British standard: aerospace series specification for ptfe insulated equipment wires (with silver plated copper conductors)	1970	British Standards Institution
Box 240	G 211	British standard: aerospace series specification for reflection - reducing coating of instrument windows and lighting wedges	1971	British Standards Institution
Box 240	G 212	British standard: aerospace series specification for general requirements for aircraft electrical cables	1971	British Standards Institution
Box 240	G 213	British standard: aerospace series specification for mechanically operated switches. Part 1. General requirements	1972	British Standards Institution
Box 240	G 214	British standard: aerospace series specification for dimensions of sealed beam landing lamps	1972	British Standards Institution
Box 240	G 215	British standard: aerospace series specification for thermocouple extension cables for aircraft (nickel-chromium and nickel-aluminium)	1972	British Standards Institution
Box 240	G 216	British standard: aerospace series specification for hand operated, thermally compensated, miniature, single and triple pole circuit breakers	1975	British Standards Institution
Box 240	G 217	British standard: aerospace series specification for general requirements for cockpit lighting controllers	1975	British Standards Institution
Box 240	G 218 : Part 1	British standard: aerospace series specification for proximity switches for aircraft. Part 1. General requirements	1975	British Standards Institution
Box 240	G 218 : Part 2	British standard specification: aerospace series proximity switches for aircraft. Part 2. Requirements for magnetic proximity switches incorporating reed contact units	1976	British Standards Institution
Box 240	G 218 : Part 3	British standard: aerospace series specification for proximity switches for aircraft. Part 3. Requirements for inductive proximity switches	1976	British Standards Institution
Box 240	G 219	British standard: aerospace series specification for general requirements for ground support electrical supplies	1975	British Standards Institution
Box 240	G 220	British standard specification: aerospace series crimped terminations to stranded flexible thermocouple cables of the nickel-chromium and nickel-aluminium types	1976	British Standards Institution
Box 240	G 221	British standard aerospace series: specification for minyvin type electric cables (metric units)	1976	British Standards Institution
Box 240	G 222	British standard aerospace series: specification for efglas type electric cables (metric units)	1976	British Standards Institution
Box 240	G 223	British standard: aerospace series: specification for screen terminating devices for aircraft electric cables	1977	British Standards Institution
Box 241	G 224	British standard aerospace series: specification for lever-operated manual switches for aircraft	1978	British Standards Institution
Box 241	G 225	British standard aerospace series: specification for performance of environment-resistant terminal junction modules with removable crimp-type contacts	1979	British Standards Institution
Box 241	G 226	British standard aerospace series: specification for counter and pointer, servo type, pressure altimeter systems	1979	British Standards Institution
Box 241	G 227	British standard aerospace series: specification for tersil type electric cables (metric units)	1979	British Standards Institution
Box 241	G 229 : ISO 7137 - 1981	British standard aerospace series: schedule for environmental conditions and test procedures for airborne equipment [iso title: aircraft - environmental conditions and test procedures for airborne equipment]	1982	British Standards Institution
Box 241	2 G.100 : Part 1	British standard specification for general requirements for electrical equipment and indicating instruments for aircraft. Part 1. Identification, declarations and construction	1961	British Standards Institution
Box 241	2 G.100 : Part 2	British standard specification for general requirements for electrical equipment and indicating instruments for aircraft. Part 2. Environmental and operating conditions	1962	British Standards Institution
Box 241	2G. 100 : Part 2 : Section 2	British standard: aerospace series specification for general requirements for aircraft electrical equipment and indicating instruments. Part 2. Environmental and operational conditions. Section 2. Radio interference	1967	British Standards Institution
Box 241	2G. 100 : Part 3	General requirements for aircraft electrical equipment. Part 3. Characteristics of electrical power systems and equipment	1960	British Standards Institution
Box 241	2G. 100 : Part 3	British standard: aerospace series specification for general requirements for aircraft electrical equipment and indicating instruments. Part 3. Characteristics of aircraft electrical systems	1968	British Standards Institution
Box 241	2G. 101	British standard: aerospace series specification for general requirements for aircraft indicators	1975	British Standards Institution
Box 241	2G. 111	British standard specification for rate of climb indicators for aircraft	1955	British Standards Institution
Box 241	2G. 112	British standard specification for air-driven directional gyroscopes for aircraft	1956	British Standards Institution
Box 241	2G. 113	British standard specification for manifold pressure gauges for aircraft	1956	British Standards Institution
Box 241	2G. 114	British standard specification for direct current ratiometer indicators for aircraft	1953	British Standards Institution
Box 241	2G. 115	British standard specification for sensitive altimeters for aircraft	1956	British Standards Institution
Box 241	2G 117	British standard: aerospace series specification for pressure-driven airspeed indicators	1975	British Standards Institution
Box 241	2G. 121	British standard specification for hand-operated circuit-breakers for extra-low voltage d.c. Systems in aircraft	1953	British Standards Institution
Box 241	2G. 124 : Part 1	British standard specification for a.c. Generators for aircraft. Part 1: constant frequency	1966	British Standards Institution
Box 241	2G. 124 : Part 2	British standard specification for a.c. Generators for aircraft. Part 2: variable frequency	1966	British Standards Institution
Box 241	2G. 127	British standard: aerospace series specification for power and current transformers for use in aircraft electrical power supply systems	1967	British Standards Institution
Box 241	2G. 132	British standard: aerospace series: specification for general requirements for electromagnetically operated contactors for aircraft	1981	British Standards Institution
Box 241	2G. 134	British standard: aerospace series specification for d.c. Generators	1970	British Standards Institution
Box 241	2G. 135	British standard: aerospace series specification for electrically-heated pitot and pitot static pressure heads	1967	British Standards Institution
Box 241	2G. 143	British standard specification for a.c. And d.c. Rotary and linear actuators for aircraft	1965	British Standards Institution
Box 241	2G. 146	British standard specification for d.c. Motors for aircraft	1966	British Standards Institution
Box 241	2G. 147 : Part 1	British standard specification for a.c. Motors for aircraft. Part 1. Three-phase constant frequency squirrel-cage induction motors	1966	British Standards Institution
Box 241	2G. 147 : Part 2	British standard specification for a.c. Motors for aircraft. Part 2. Three-phase variable frequency squirrel-cage induction motors	1966	British Standards Institution
Box 241	2G. 148	British standard specification for general purpose platinum wire thermometer bulbs and connectors for aircraft	1963	British Standards Institution
Box 241	2G. 173	British standard specification for performance and interchangeability requirements for plugs and sockets for ground electrical supply to aircraft	1964	British Standards Institution
Box 241	2G. 178	British standard specification for crimped joints for general purpose aircraft electrical cables	1965	British Standards Institution
Box 241	2G. 180	British standard: aerospace series specification for permanent splicing of aircraft electrical cables	1874	British Standards Institution
Box 241	2G. 181	British standard: aerospace series specification for aircraft filament lamps	1968	British Standards Institution
Box 241	2G. 182	British standard: aerospace series specification for pressure-driven machmeters for aircraft	1975	British Standards Institution
Box 241	2G. 196	British standard: aerospace series specification for static invertors	1971	British Standards Institution
Box 241	2G. 197	British standard aerospace series: specification for stud-type terminal blocks for terminations on aircraft electric cables	1978	British Standards Institution
Box 241	2G. 198 : Part 1	British standard aerospace series: sleeves for aircraft electric cables and equipment wires. Part 1. Specification for elastomeric sleeves for binding and identification	1982	British Standards Institution
Box 241	2G. 205	British standard specification: aerospace series lead-acid and nickel-cadmium secondary batteries	1976	British Standards Institution
Box 241	2G. 213	British standard: aerospace series specification for mechanically operated switches	1974	British Standards Institution
Box 241	2G. 221	British standard aerospace series: specification for minyvin type electric cables (metric units)	1080	British Standards Institution
Box 241	3G. 100 : Part 0	British standard: aerospace series specification for general requirements for equipment in aircraft. Part 0. Introduction	1972	British Standards Institution
Box 241	3G. 100 : Part 0	British standard aerospace series: specification for general requirements for equipment for use in aircraft. Part 0. Introduction	1980	British Standards Institution
Box 241	3G. 100 : Part 1.	British standard: aerospace series specification for general requirements for equipment in aircraft. Part 1. Identification, declarations and construction	1971	British Standards Institution
Box 241	3G. 100 : Part 1.	British standard: aerospace series specification for general requirements for equipment for use in aircraft. Part 1. Identification and declarations	1973	British Standards Institution
Box 241	3G. 100 : Part 2 : Section 1	British standard: aerospace series specification for general requirements for equipment for use in aircraft. Part 2. All equipment. Section 1. Construction	1973	British Standards Institution
Box 241	3G. 100 : Part 2 : Section 2	British standard: aerospace series specification for general requirements for equipment in aircraft. Part 2. All equipment. Section 2. Magnetic influence	1972	British Standards Institution
Box 241	3G. 100 : Part 2 : Section 3 : Subsection 3.0	British standard: aerospace series specification for general requirements for equipment in aircraft. Part 2. All equipment. Section 3. Environmental conditions .. Subsection 3.0. Standard test requirements	1972	British Standards Institution
Box 241	3G. 100 : Part 2 : Section 3 : Subsection 3.2	British standard: aerospace series specification for general requirements for equipment in aircraft. Part 2. All equipment. Section 3. Environmental conditions. Subsection 3.2. Temperature - pressure requirements	1970	British Standards Institution
Box 241	3G. 100 : Part 2 : Section 3 : Subsection 3.3	British standard: aerospace series specification for general requirements for equipment in aircraft. Part 2. All equipment. Section 3. Environmental conditions. Subsection 3.3. Mould growth	1972	British Standards Institution
Box 241	3G. 100 : Part 2 : Section 3 : Subsection 3.4	British standard: aerospace series specification for general requirements for equipment in aircraft. Part 2. All equipment. Section 3. Environmental conditions. Subsection 3.4. Differential pressure requirements	1972	British Standards Institution
Box 241	3G. 100 : Part 2 : Section 3 : Subsection 3.5	British standard: aerospace series specification for general requirements for equipment in aircraft. Part 2. All equipment. Section 3. Environmental conditions. Subsection 3.5. Explosion-proofness	1972	British Standards Institution
Box 241	3G. 100 : Part 2 : Section 3 : Subsection 3.6	British standard: aerospace series specification for general requirements for equipment in aircraft. Part 2. All equipment. Section 3.6 acceleration requirements	1972	British Standards Institution
Box 241	3G. 100 : Part 2 : Section 3 : Subsection 3.7	British standard: aerospace series specification for general requirements for equipment in aircraft. Part 2. All equipment. Section 3. Environmental conditions. Subsection 3.7. Tropical exposure	1972	British Standards Institution
Box 241	3G. 100 : Part 2 : Section 3 : Subsection 3.8	British standard: aerospace series specification for general requirements for equipment in aircraft. Part 2. All equipment. Section 3. Environmental conditions. Subsection 3.8. Salt mist	1972	British Standards Institution
Box 241	3G. 100 : Part 2 : Section 3 : Subsection 3.9	British standard: aerospace series specification for general requirements for equipment in aircraft. Part 2. All equipment. Section 3. Environmental conditions. Subsection 3.9. Ice formation	1972	British Standards Institution
Box 241	3G. 100 : Part 3 : Section 3 : Subsection 3.10	British standard: aerospace series specification for general requirements for equipment for use in aircraft. Part 2. All equipment. Section 3. Environmental conditions. Subsection 3.10 impact icing	1974	British Standards Institution
Box 241	3G. 100 : Part 2 : Section 3 : Subsection 3.11	British standard: aerospace series specification for general requirements for equipment for use in aircraft. Part 2. All equipment. Section 3. Environment conditions. Subsection 3.11. Water-proofness	1973	British Standards Institution
Box 241	3G. 100 : Part 2 : Section 3 : Subsection 3.12	British standard: aerospace series specification for general requirements for equipment for use in aircraft. Part 2. All equipment. Section 3. Environmental conditions. Subsection 3.12. Fluid contamination	1973	British Standards Institution
Box 241	3G. 100 : Part 2 : Section 3 : Subsection 3.13	British standard: aerospace series specification for general requirements for equipment for use in aircraft. Part 2. All equipment. Section 3. Environmental conditions. Subsection 3.13. Resistance to fire in designated fire zones	1973	British Standards Institution
Box 241	3G. 100 : Part 2 : Section 3 : Subsection 3.14	British standard: aerospace series specification for general requirements for equipment for use in aircraft. Part 2. All equipment. Section 3. Environmental conditions. Subsection 3.14. Acoustic vibration	1973	British Standards Institution
Box 241	3G. 100 : Part 2 : Section 3 : Subsection 3.15	British standard aerospace series: specification for general requirements for equipment for use in aircraft. Part 2. All equipment. Section 3. Environment conditions. Subsection 3.15. Change of temperature [iso title: environmental tests for aircraft equipment -. Part 2.7: change of temperature]. Subsection 3.15: 1978 - iso 2657 - 1976	1978	British Standards Institution
Box 241	3G. 100 : Part 3	British standard: aerospace series specification for general requirements for equipment in aircraft. Part 3. Characteristics of aircraft electrical systems	1972	British Standards Institution
Box 241	3G. 100 : Part 3	British standard aerospace series: specification for general requirements for equipment for use in aircraft. Part 3. Characteristics of aircraft electrical power supplies	1979	British Standards Institution
Box 241	3G. 100 : Part 4 : Section 1	British standard: aerospace series specification for general requirements for equipment for use in aircraft. Part 4. Electrical equipment. Section 1. Construction and general	1973	British Standards Institution
Box 241	3G. 100 : Part 4 : Section 1 : Subsection 1.1	British standard: aerospace series specification for general requirements for equipment for use in aircraft. Part 4. Electrical equipment. Section 1. Construction and general. Subsection 1.1. Electrical insulation tests	1973	British Standards Institution
Box 241	3G. 100 : Part 4 : Section 2	British standard: aerospace series specification for general requirements for use in aircraft. Part 4. Electrical equipment. Section 2. Electromagnetic interference at radio and audio frequencies	1973	British Standards Institution
Box 241	3G. 100 : Part 4 : Section 2	British standard aerospace series: specification for general requirements for equipment for use in aircraft. Part 4. Electrical equipment. Section 2. Electromagnetic interference at radio and audio frequencies	1980	British Standards Institution
Box 241	3G. 131	British standard for lead/acid batteries (non-aerobatic) for aircraft	1958	British Standards Institution
Box 241	3G. 148	British standard aerospace series: specification for general purpose platinum temperature sensors for aircraft	1981	British Standards Institution
Box 241	3G. 173	British standard: aerospace series specification for performance and interchangeability requirements for plugs and sockets for ground electrical supply to aircraft	1972	British Standards Institution
Box 241	3G. 178	British standard: aerospace series specification for crimped joints for aircraft electrical cables and wires	1972	British Standards Institution
Box 241	3G. 197	British standard aerospace series: specification for stud-type terminal blocks for terminations on aircraft electric cables	1982	British Standards Institution
Box 241	HC 1 : March : 1973	British standard: aerospace series specification for carbon steel castings (500 n/mm2)	1973	British Standards Institution
Box 241	HC 2 : March : 1973	British standard: aerospace series specification for carbon steel castings (500 n/mm2)	1973	British Standards Institution
Box 241	HC 3 : March : 1973	British standard: aerospace series specification for 1 % chromium - molybdenum low alloy steel castings (500 n/mm2)	1973	British Standards Institution
Box 241	HC 4 : March : 1973	British standard: aerospace series specification for 3 % chromium - molybdenum steel castings (600-700 n/mm2)	1973	British Standards Institution
Box 241	HC 5 : March : 1973	British standard: aerospace series specification for 3 % nickel case hardening steel castings (700 n/mm2)	1973	British Standards Institution
Box 241	HC 6 : March : 1973	British standard: aerospace series specification for 3 % chromium - molybdenum nitriding steel castings (850 - 1000 n/mm2)	1973	British Standards Institution
Box 241	HC 7 : May : 1974	British standard: aerospace series specification for 3 % chromium - molybdenum steel castings (850 - 1080 mpa)	1974	British Standards Institution
Box 241	HC 8 : May : 1974	British standard: aerospace series specification for 3 % chromium - molybdenum steel castings (1150 - 1300 mpa)	1974	British Standards Institution
Box 241	HC 9 : May : 1974	British standard: aerospace series specification for nickel - chromium - molybdenum steel castings (880 - 1080 mpa)	1974	British Standards Institution
Box 241	HC 10 : May : 1974	British standard: aerospace series specification for nickel - chromium - molybdenum steel castings (1150 - 1300 mpa)	1974	British Standards Institution
Box 241	HC. 100, July, 1972	British standard: aerospace series - inspection and testing procedure for iron, nickel, copper, cobalt and refractory metal base alloy castings	1972	British Standards Institution
Box 241	HC 101 : February 1973	British standard: aerospace series specification for precipitation hardening chromium - nickel -copper - molybdenum steel castings (950 n/mm2) (cr 14.0, ni 4.5, cu 2.5, mo 1.5)	1973	British Standards Institution
Box 241	HC 102 : February 1973	British standard: aerospace series specification for precipitation hardening chromium - nickel -copper - molybdenum steel castings (1250 n/mm2) (cr 14.0, ni 4.5, cu 2.5, mo 1.5)	1973	British Standards Institution
Box 241	HC 103 : May : 1974	British standard: aerospace series specification for 23% chromium - nickel - tungsten corrosion - resisting steel castings (cr 23, ni 11, w 3)	1974	British Standards Institution
Box 241	HC 104 : December : 1974	British standard: aerospace series specification for 19% chromium - 10% nickel niobium - stabilized corrosion - resisting steel castings (460 mpa)	1974	British Standards Institution
Box 241	HC 105 : November : 1974	British standard: aerospace series specification for 18% chromium - 11% nickel -2.5% molybdenum niobium - stabilized corrosion - resisting steel castings (500 mpa)	1974	British Standards Institution
Box 241	HC 106 : November : 1974	British standard: aerospace series specification for precipitation hardening chromium - nickel - copper corrosion - resisting steel castings (1250 - 1500 mpa) (cr 16, ni 4, cu 3)	1974	British Standards Institution
Box 241	HC 201 : February 1973	British standard: aerospace series specification for nickel base chromium - aluminium - tungsten= molybdenum - niobium alloy castings (cr 11. 0, al 6.0, w 3.5, mo 3.0, nb 2.0)	1973	British Standards Institution
Box 241	HC 202 : February 1973	British standard: aerospace series specification for precipitation hardening nickel base chromium - niobium - molybdenum - iron - tungsten alloy castings (cr 20.0, nb 6.6, fe 3.0, w 2.5)	1973	British Standards Institution
Box 241	HC 203 : February 1973	British standard: aerospace series specification for precipitation hardening nickel base chromium - aluminium - molybdenum - niobium alloy castings (cr 1.3.0, al 6.0, mo 4.5, nb 2.3)	1973	British Standards Institution
Box 241	HC 204 : February 1973	British standard: aerospace series specification for nickel base cobalt - chromium - aluminium - titanium - molybdenum alloy castings (co 15.0, cr 10.0, ai 5.5, ti 4.8, mo 3.0)	1973	British Standards Institution
Box 241	HC 205 : February 1974	British standard: aerospace series specification for precipitation hardening nickel base chromium - cobalt - molybdenum - titanium alloy castings (cr 20, co 20, mo 6, ti2)	1974	British Standards Institution
Box 241	HC 206 : 1975	British standard: aerospace series specification for precipitation hardening nickel base chromium - cobalt - molybdenum -titanium alloy precision castings (cr 20, co 20, mo 6, ti 2)	1975	British Standards Institution
Box 241	HC 207 : 1979	British standard aerospace series: specification for nickel base cobalt - tungsten - chromium - tantalum - hafnium titanium alloy castings (co 10, w 10, cr 9, al 5.5, ta 2.5, hf 1.5, ti 1.5)	1979	British Standards Institution
Box 241	HC 208 : 1979	British standard aerospace series: specification for nickel base cobalt - tungsten - chromium - aluminium - molybdenum - titanium - tantalum - alloy castings (co 10, w 10, cr 9, al 5.5, mo 2.5, ti 1.5, ta 1.5)	1979	British Standards Institution
Box 241	HC 209 : 1979	British standard aerospace series: specification for low carbon precipitation hardening nickel base chromium - aluminium - molybdenum - niobium alloy castings (cr 11.5, al 6, mo 4, nb 2)	1979	British Standards Institution
Box 241	HC 210 : 1979	British standard aerospace series: specification for nickel base tungsten - aluminium - chromium - molybdenum - alloy castings (w 10.5, al 6, cr 6, mo 2)	1979	British Standards Institution
Box 241	HC 211 : 1979	British standard aerospace series: specification for nickel base chromium - cobalt - molybdenum - aluminium - titanium alloy castings (cr 15.5, co 10, mo 8.3, al 4.2, ti 3.6)	1979	British Standards Institution
Box 241	HC 301 : February 1973	British standard: aerospace series specification for cobalt base chromium - nickel - tungsten alloy castings (cr 25.5, ni 10.5, w 7.5)	1973	British Standards Institution
Box 241	HC 401 : November 1974	British standard: aerospace series specification for 18% nickel maraging steel precision castings (1600 1850 mpa)	1974	British Standards Institution
Box 241	HC 402 : 1977	British standard: aerospace series: specification for cast iron ring pots (centrifugally cast) (suitable for piston rings up to 200 mm in diameter)	1977	British Standards Institution
Box 241	HC 403 : 1977	British standard: aerospace series: specification for high chromium alloy cast iron ring pots (centrifugally cast) (suitable for piston rings up to 400 mm in diameter)	1977	British Standards Institution
Box 241	HC 404 : 1977	British standard: aerospace series: specification for chromium - molybdenum alloy cast iron ring pots (suitable for centrifugally cast and sand cast sealing rings, piston rings and cylinder liners)	1977	British Standards Institution
Box 241	HC 501 : December : 1974	British standard: aerospace series specification for copper base aluminium - nickel - iron alloy castings (620 mpa) (al 9.5, ni 5, fe 5)	1974	British Standards Institution
Box 241	HC 502 : 1981	British /standard aerospace series: specification for copper base aluminium - nickel iron alloy castings (620 mpa) (al 9.5, ni 5, fe 5)	1981	British Standards Institution
Box 241	HR. 1, March, 1970	British standard: aerospace series 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)	1970	British Standards Institution
Box 241	HR. 2, August 1971	British standard: aerospace series 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)	1971	British Standards Institution
Box 241	HR. 3, April, 1972	British standard: aerospace series specification for nickel - cobalt - chromium - molybdenum - aluminium titanium heat - resisting alloy billets, bars, forgings and parts (nickel base co 20, cr 14.8, mo 5, al 4.7, ti 1.2)	1972	British Standards Institution
Box 241	HR. 4, April, 1972	British standard: aerospace series specification for nickel - chromium - cobalt - aluminium - molybdenum titanium heat -resisting alloy billets, bars, forgings and parts (nickel base cr 15, co 14.2, al 5, mo 4, ti 4)	1972	British Standards Institution
Box 241	HR. 5, October 1972	British standard: aerospace series specification for nickel - chromium - titanium heat - resisting alloy billets, bard, forgings and parts (nickel base, cr 19.5, ti 0.4)	1972	British Standards Institution
Box 241	HR. 6, October 1972	British standard: aerospace series specification for nickel - chromium - iron -molybdenum - cobalt - tungsten heat - resisting alloy billets, bars, forgings and parts (nickel base cr 21.7, fe 18.5, mo 9, co 1.5, w 0.6)	1972	British Standards Institution
Box 241	HR. 10, October, 1972	British standard: aerospace series specification for nickel - cobalt - chromium - molybdenum - titanium - aluminium heat - resisting alloy billets, bars, forgings and parts (nickel base, co 20, cr 20, mo 5.9, ti 2.1, al 0.5)	1972	British Standards Institution
Box 241	HR. 11 : March : 1973	British standard: aerospace series specification for nickel - iron - chromium - molybdenum - aluminium - titanium heat - resisting alloy billets, bars, forgings and parts (ni/co 43.5, cr 16.5, mo 3.3, al 1.2, ti 1.2, fe remainder)	1973	British Standards Institution
Box 241	HR. 40, October, 1972	British standard: aerospace series specification for cobalt - chromium - tungsten - nickel - manganese heat - resisting alloy billets, bars and forgings (cobalt base cr 20, w 15, ni 10, mn 1.5)	1972	British Standards Institution
Box 241	HR. 52 : September 1973	British standard: aerospace series specification for heat - resisting alloy billets, bars, forgings and parts (ni25.5, cr 14.7, ti 1,8, mn 1.5, mo 1.2, v 0.3, fe remainder)	1973	British Standards Institution
Box 241	HR. 53 : March 1973	British standard: aerospace series specification for nickel - iron - chromium - molybdenum - titanium heat - resisting alloy billets, bars, forgings and parts (ni/co 42.5, cr 12.5, mo 5.8, ti 3.0, fe remainder)	1973	British Standards Institution
Box 241	HR. 54, March 1970	British standard: aerospace series specification for heat - resisting martensitic steel billets, bars, forgings and parts (cr 10.5, mo 0.6, v 0.2, nb 0.3) (930/1080 mn/m: 93/108 hbar)	1970	British Standards Institution
Box 241	HR. 55 1980	British standard aerospace series: specification for nickel - iron - chromium - molybdenum - aluminium - titanium heat - resisting alloy billets, bars, forgings and parts (ni/co 43.5, cr 16.5, mo 3.3, ll 1.2, ti 1.2, fe remainder)	1980	British Standards Institution
Box 241	HR. 100 : 1968	Inspection and testing procedure for aerospace material wrought heat resisting alloys	1968	British Standards Institution
Box 241	HR. 201, March, 1970	British standards: aerospace series specification for nickel - chromium - titanium - aluminium heat - resisting alloy sheet and strip (nickel base, cr 19.5, ti 2.2, al 1.4)	1970	British Standards Institution
Box 241	HR. 202, July 1971	British standard: aerospace series 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)	1971	British Standards Institution
Box 241	HR. 203, February 1972	British standard: aerospace series specification for nickel - chromium - titanium heat - resisting alloy plate, sheet and strip (nickel base, cr 19.5, ti 0.4)	1972	British Standards Institution
Box 241	HR. 204, February 1972	British standard: aerospace series specification for nickel - chromium - iron - molybdenum - cobalt - tungsten heat - resisting alloy plate, sheet and strip (nickel base cr 22, fe 18.5, mo 9, co 1.5, w 0.6)	1972	British Standards Institution
Box 241	HR. 206 : March 1973	British standard: aerospace series specification for nickel - cobalt - chromium - molybdenum - titanium - aluminium heat - resisting alloy plate, sheet and strip (nickel base, co 20, cr 20, mo 5.9, ti 2.7, al 0.5)	1973	British Standards Institution
Box 241	HR 207 : March 1973	British standard: aerospace series specification for nickel - iron - chromium - molybdenum - aluminium - titanium heat - resisting alloy plate, sheet and strip (ni/co 43.5, cr 16.5, mo 3.3, al 1.2, ti 1.2 fe remainder)	1973	British Standards Institution
Box 241	HR. 240, October 1972	British standard: aerospace series specification for cobalt - chromium - tungsten - nickel - manganese heat - resisting alloy plate sheet and strip (cobalt base cr 20, w 15, ni 10, mn 1.5)	1972	British Standards Institution
Box 241	HR 251 : June 1974	British standard: aerospace series specification for heat - resistant alloy plate, sheet and strip (ni 25.5, cr 14.7, ti 1.8, mn 1.5, mo 1.2, v 0.3, fe remainder)	1974	British Standards Institution
Box 241	HR 401, October 1970	British standard: aerospace series 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)	1970	British Standards Institution
Box 241	HR 402 : September 1973	British standard: aerospace series specification for nickel - chromium - cobalt - aluminium heat - resisting alloy cold worked and softened seamless tubes (nickel base, cr 19.5, co 18.0, ti 2.5, al 1.5)	1973	British Standards Institution
Box 241	HR 403 : March 1973	British standard: aerospace series specification for nickel - chromium - titanium heat - resisting alloy cold - worked and softened seamless tubes (nickel base, ce 19.5 ti 0.4)	1973	British Standards Institution
Box 241	HR 404 : March 1973	British standard: aerospace series 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)	1973	British Standards Institution
Box 241	HR. 501, November 1970	British standard: aerospace series 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)	1970	British Standards Institution
Box 241	HR. 502, Noverber 1970	British standard: aerospace series 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)	1970	British Standards Institution
Box 241	HR. 503, October 1970	British standard: aerospace series specification for nickel - chromium - cobalt - titanium - aluminium heat - resisting alloy wire (0.45 mm to 2mm diameter) for thread inserts (nickel base, cr 19.5, co 18.0, ti 2.5, al 1.5)	1970	British Standards Institution
Box 241	HR. 504, November 1970	British standard: aerospace series specification for nickel - chromium - titanium heat - resisting alloy bar, wire and rivets (nickel base, cr 19.5, ti 0.4)	1970	British Standards Institution
Box 241	HR. 505 : 1981	Round wire for thread inserts	1981	British Standards Institution
Box 241	HR. 601, February 1972	British standard: aerospace series specification for nickel - chromium - titanium - aluminium heat - resisting alloy bar and wire for the manufacture of bolts, studs, set screws and nuts (nickel base, cr 19.5, ti 2.2, al 1.4)	1972	British Standards Institution
Box 241	HR. 650, April 1972	British standard: aerospace series specification for high expansion heat - resisting steel bar and wire for the manufacture of bolts, studs, set screws and nuts (ni 25.5, cr 15, ti 2, mn 1.5, mo 1.25, si 0.7, c 0.3) (limiting ruling section 20 mm)	1972	British Standards Institution
Box 241	2 HR 1 : February 1973	British standard: aerospace series 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)	1973	British Standards Institution
Box 241	2 HR 2 : February 1973	British standard: aerospace series 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)	1973	British Standards Institution
Box 241	2 HR. 100 : 1971	British standard: inspection and testing procedure for aerospace material wrought heat resisting alloys	1971	British Standards Institution
Box 241	2 HR 201 : June 1974	British standard: aerospace series specification for nickel - chromium - titanium - aluminium heat - resisting alloy plate, sheet and strip (nickel base, cr 19.5, ti 2.2, al 1.4)	1974	British Standards Institution
Box 241	2 HR 202 : February 1973	British standard: aerospace series 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)	1973	British Standards Institution
Box 241	2 HR 401 : February 1973	British standard: aerospace series specification for nickel - chromium - titanium - aluminium heat - resisting alloy cold worked and softened seamless tube (nickel base, cr 19.5, ti 2.2, al 1.4)	1973	British Standards Institution
Box 241	2 HR 501 : February 1973	British standard: aerospace series 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)	1973	British Standards Institution
Box 241	2 HR 502 : February 1973	British standard: aerospace series 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)	1973	British Standards Institution
Box 241	2 HR 503 : February 1973	British standard: aerospace series 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)	1973	British Standards Institution
Box 241	2 HR 504 : February 1973	British standard: aerospace series specification for nickel - chromium - titanium heat - resisting alloy bar, wire and rivets (nickel base, cr 19.5, ti 0.4)	1973	British Standards Institution
Box 241	2 HR 601 : 1975	British standard: aerospace series specification for nickel - chromium - titanium - aluminium heat - resisting alloy bar, wire for the manufacture of fasteners (maximum diameter or minor sectional dimension 25 mm) (nickel base, cr 19.5, ti 2.2, al 1.4)	1975	British Standards Institution
Box 241	3 HR 100 : 1978	British standard: aerospace series: procedure for inspection and testing of wrought heat - resisting alloys	1978	British Standards Institution
Box 241	J. 10, November, 1958	British standard for pressure - sensitive adhesive waterproof p.v.c. Tape for aeronautical purposes	1958	British Standards Institution
Box 241	J. 11, November 1958	British standard for pressure - sensitive adhesive paper masking tape for aeronautical purposes	1958	British Standards Institution
Box 241	J. 12, December, 1966	British standard specification for pressure - sensitive adhesive identification tape for aeronautical purposed	1966	British Standards Institution
Box 241	2J.10, March 1967	British standard specification for pressure - sensitive adhesive waterproof pvc tape for aeronautical purposes	1967	British Standards Institution
Box 241	2J. 11, September 1968	British standard: aerospace series specification for pressure - sensitive adhesive paper masking tape	1968	British Standards Institution
Box 241	2J. 12 : 1975	British standard: aerospace series specification for pressure - sensitive adhesive identification tape	1975	British Standards Institution
Box 241	3J 10 : 1975	British standard: aerospace series specification for pressure - sensitive adhesive waterproof pvc tape	1975	British Standards Institution
Box 241	3J 11 : 1975	British standard: aerospace series specification for pressure - sensitive adhesive paper masking tape	1975	British Standards Institution
Box 241	2 K. 11. September 1930	British standard specification for aircraft material - iron castings for cylinders (water - cooled and air - cooled), pistons and valve guides	1930	British Standards Institution
Box 241	4 K. 6. October 1928	British standard specification for aircraft material - cast iron piston ring pots (sand cast and chill cast)	1928	British Standards Institution
Box 242	L. 74, November, 1959	British standard for aircraft material aluminium-magnesium alloy ingots and castings	1959	British Standards Institution
Box 242	L. 75, November, 1959	British standard for aircraft material aluminium-silicon-magnesium alloy ingots and castings	1959	British Standards Institution
Box 242	L. 76, January, 1959	British standard for aircraft material aluminium-copper-magnesium-silicon-manganese alloy billets and bars for forging and forgings (solution treated and aged at room temperature)	1959	British Standards Institution
Box 242	L. 77, January, 1959	British standard for aircraft material aluminium-copper-magnesium-silicon-manganese alloy billets and bars for forging and forgings (solution treated and precipitation treated)	1959	British Standards Institution
Box 242	L. 78, November, 1959	British standard for aircraft material aluminium-silicon-copper alloy ingots and castings (solution treated and precipitation treated)	1959	British Standards Institution
Box 242	L. 79, November, 1959	British standard for aircraft material aluminium-silicon-copper alloy ingots and castings	1959	British Standards Institution
Box 242	L. 80, January, 1961	British standard for aircraft material aluminium-2 and 1/4 per cent magnesium alloy sheets and strips (soft)	1961	British Standards Institution
Box 242	L. 81, January, 1961	British standard for aircraft material aluminium-2 and 1/4 per cent magnesium alloy sheets and strips (half hard)	1961	British Standards Institution
Box 242	L. 82, January, 1961	British standard for aircraft material aluminium-3 and 1/2 per cent magnesium alloy sheets and strips (soft)	1961	British Standards Institution
Box 242	L. 83, January, 1961	British standard for aircraft material aluminium-copper-nickel-magnesium-iron-silicon alloy forging stock, bars, extruded sections and forgings (solution treated and precipitation treated)	1961	British Standards Institution
Box 242	L. 84, January, 1961	British standard for aircraft material aluminium-copper- silicon-magnesium alloy bars and extruded sections (solution treated and aged at room temperature)	1961	British Standards Institution
Box 242	L. 85, January, 1961	British standard for aircraft material aluminium-copper- silicon-magnesium alloy forging stock, bars, extruded sections and forgings (solution treated and precipitation treated)	1961	British Standards Institution
Box 242	L. 86, September, 1961	British standard for aircraft material aluminium-copper-magnesium alloy wires for solid, cold forged rivets (not exceeding 3 and 8 inch diameter)	1961	British Standards Institution
Box 242	L. 87, March, 1964	British standard for aircraft material aluminium-copper-magnesium-silicon-manganese alloy hexagonal bars for nuts, couplings and hollow machined parts)	1964	British Standards Institution
Box 242	L. 88, January, 1966	British standard for aircraft material aluminium-alloy-coated aluminium-zinc-magnesium-sopper-chromium alloy sheets and strips (solution treated and precipitation treated)	1966	British Standards Institution
Box 242	L. 89, August, 1966	British standard for aircraft material aluminium-coated aluminium-sopper-magnesium-silicon-manganese alloy sheets and strips to close tolerances (solution treated and aged at room temperature)	1966	British Standards Institution
Box 242	L. 90, August, 1966	British standard specification for aircraft material aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy sheets and strips to close tolerances (solution treated and precipitation treated)	1966	British Standards Institution
Box 242	L. 91, June, 1967	British standard aerospace series: specification for aluminium-copper alloy ingots and castings	1967	British Standards Institution
Box 242	L. 92, June, 1967	British standard aerospace series: specification for aluminium-copper alloy ingots and castings	1967	British Standards Institution
Box 242	L. 93, June, 1968	British standard aerospace series: specification for aluminium-copper- magnesium-silicon-manganese alloy plate (solution treated, controlled stretched and precipitation treated)	1968	British Standards Institution
Box 242	L. 94, February, 1968	British standard aerospace series: specification for aluminium-copper- magnesium-silicon-manganese alloy plate (solution treated and precipitation treated: not controlled stretched)	1968	British Standards Institution
Box 242	L. 95, February, 1968	British standard: aerospace series specification for aluminium-zinc-magnesium-copper- chromium alloy plate (solution treated, controlled stretched and precipitation treated)	1968	British Standards Institution
Box 242	L. 96, February, 1968	British standard: aerospace series: specification for aluminium-zinc-magnesium-copper- chromium alloy plate (solution treated and precipitation treated: not controlled stretched)	1968	British Standards Institution
Box 242	L. 97, February, 1968	British standard: aerospace series specification for aluminium-copper-magnesium-manganese alloy plate (solution treated, controlled stretched and aged at room temperature)	1968	British Standards Institution
Box 242	L. 98, February, 1968	British standard: aerospace series specification for aluminium-copper-magnesium-manganese alloy plate (solution treated and aged at room temperature: not controlled stretched)	1968	British Standards Institution
Box 242	L. 99, January, 1969	British standard: aerospace series specification for aluminium-silicon-magnesium alloy ingots and castings (solution treated and precipitation treated)	1969	British Standards Institution
Box 242	L. 102, August, 1971	British standard: aerospace series specification for bars and extruded sections of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature)	1971	British Standards Institution
Box 242	L. 103, August, 1971	British standard: aerospace series specification for forging stock and forgings of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature)	1971	British Standards Institution
Box 242	L. 104, August, 1971	British standard: aerospace series specification for sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and precipitation treated)	1971	British Standards Institution
Box 242	L. 105, August, 1971	British standard: aerospace series specification for tube of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature)	1971	British Standards Institution
Box 242	L. 106, September, 1971	British standard: aerospace series specification for sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy (supplied for solution treatment by the user)	1971	British Standards Institution
Box 242	L. 107, September, 1971	British standard: aerospace series specification for sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy (supplied for solution treatment by the user)	1971	British Standards Institution
Box 242	L. 108, September, 1971	British standard: aerospace series specification for close toleranced sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy (supplied for solution treatment by the user)	1971	British Standards Institution
Box 242	L. 109, September, 1971	British standard: aerospace series specification for aluminium-coated sheet and strip of aluminium-copper-magnesium-manganese alloy (solution treated and aged at room temperature)	1971	British Standards Institution
Box 242	L. 110, September, 1971	British standard: aerospace series specification for aluminium-coated sheet and strip of aluminium-copper-magnesium-manganese alloy (supplied for solution treatment by the user)	1971	British Standards Institution
Box 242	L. 111 September, 1971	British standard: aerospace series specification for bars and extruded sections of aluminium-magnesium-silicon-manganese alloy (solution treated and precipitation treated) (suitable for welding)	1971	British Standards Institution
Box 242	L. 112 September, 1971	British standard: aerospace series specification for forging stock and forgings of aluminium-magnesium-silicon-manganese alloy (solution treated and precipitation treated) (suitable for welding)	1971	British Standards Institution
Box 242	L. 113 September, 1971	British standard: aerospace series specification for sheet and strip of aluminium-magnesium-silicon-manganese alloy (solution treated and precipitation treated) (suitable for welding)	1971	British Standards Institution
Box 242	L. 114 September, 1971	British standard: aerospace series specification for tube of aluminium-magnesium-silicon-manganese alloy (solution treated and precipitation treated) (not exceeding 10mm wall thickness) (suitable for welding)	1971	British Standards Institution
Box 242	L. 115 September, 1971	British standard: aerospace series specification for plate of aluminium-magnesium-silicon-manganese alloy (solution treated, controlled stretched and precipitation treated) (not exceeding 25m thickness) (suitable for welding)	1971	British Standards Institution
Box 242	L. 116, March, 1973	British standard: aerospace series specification for tube of 99% aluminium	1973	British Standards Institution
Box 242	L. 117:1975	British standard: aerospace series specification for tube of aluminium-magnesium-silicon-copper-chromium alloy	1975	British Standards Institution
Box 242	L. 118:1975	British standard: aerospace series specification for tube of aluminium-magnesium-silicon-copper-chromium alloy	1975	British Standards Institution
Box 242	L. 119:1975	British standard: aerospace series specification for ingots and castings of aluminium-copper-nickel manganese-titanium-zirconium-cobalt-antimony alloy	1975	British Standards Institution
Box 242	L. 150:1975	British standard: aerospace series specification for sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy	1975	British Standards Institution
Box 242	L. 151:1975	British standard: aerospace series specification for aluminium-coated sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy	1975	British Standards Institution
Box 242	L. 152:1975	British standard: aerospace series specification for aluminium-coated sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy	1975	British Standards Institution
Box 242	L. 153:1975	British standard: aerospace series specification for aluminium-coated sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy	1975	British Standards Institution
Box 242	L. 154:1977	British standard: aerospace series specification for ingots and castings of aluminium-copper-silicon alloy	1977	British Standards Institution
Box 242	L. 155:1977	British standard: aerospace series specification for ingots and castings of aluminium-copper-silicon alloy	1977	British Standards Institution
Box 242	L. 156:1978	British standard: aerospace series specification for sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy	1978	British Standards Institution
Box 242	L. 157:1978	British standard: aerospace series specification for sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy	1978	British Standards Institution
Box 242	L. 158:1978	British standard: aerospace series specification for close toleranced sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy	1978	British Standards Institution
Box 242	L. 159:1978	British standard: aerospace series specification for close toleranced sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy	1978	British Standards Institution
Box 242	L. 160:1976	British standard: aerospace series bars and extruded sections of aluminium-zinc-magnesium-copper-chromium alloy	1976	British Standards Institution
Box 242	L. 161:1976	British standard: aerospace series hand and die forgings of aluminium-zinc-magnesium-copper-chromium alloy	1976	British Standards Institution
Box 242	L. 162:1976	British standard: aerospace series cold compresses hand forgings of aluminium-zinc-magnesium-copper-chromium alloy	1976	British Standards Institution
Box 242	L. 163:1978	British standard: aerospace series specification for sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy	1978	British Standards Institution
Box 242	L. 164:1978	British standard: aerospace series specification for sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy	1978	British Standards Institution
Box 242	L. 165:1978	British standard: aerospace series specification for sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy	1978	British Standards Institution
Box 242	L. 166:1978	British standard aerospace series: specification for close toleranced sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy	1978	British Standards Institution
Box 242	L. 167:1978	British standard aerospace series: specification for close toleranced sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy	1978	British Standards Institution
Box 242	L. 168:1978	British standard aerospace series: specification for bars and extruded sections of aluminium-copper-magnesium-silicon-manganese alloy	1978	British Standards Institution
Box 242	L. 500, January 1967	British standard for aircraft material inspection and testing procedure for wrought magnesium-base alloys	1967	British Standards Institution
Box 242	L. 501, January 1967	British standard for aircraft material magnesium-aluminium-zinc alloy extruded bars and sections	1967	British Standards Institution
Box 242	L. 502, January 1967	British standard for aircraft material magnesium-aluminium-zinc alloy forging stock and forgings	1967	British Standards Institution
Box 242	L. 503, January 1967	British standard for aircraft material magnesium-aluminium-zinc alloy extruded tubes	1967	British Standards Institution
Box 242	L. 504, January 1967	British standard for aircraft material magnesium-3% zinc-zirconium alloy sheets and strips	1967	British Standards Institution
Box 242	L. 505, January 1967	British standard for aircraft material magnesium-3% zinc-zirconium alloy extruded bars and sections	1967	British Standards Institution
Box 242	L. 506, January 1967	British standard for aircraft material magnesium-3% zinc-zirconium alloy forging stock and forgings	1967	British Standards Institution
Box 242	L. 507, January 1967	British standard for aircraft material magnesium-1 and 1/4% zinc-zirconium alloy sheets and strips	1967	British Standards Institution
Box 242	L. 508, January 1967	British standard for aircraft material magnesium-1 and 1/4% zinc-zirconium alloy extruded bars and sections	1967	British Standards Institution
Box 242	L. 509, January 1967	British standard for aircraft material magnesium-1 and 1/4% zinc-zirconium alloy extruded tubes.	1967	British Standards Institution
Box 242	L. 510, January 1967	British standard for aircraft material magnesium-aluminium-zinc-manganese alloy sheets and strips	1967	British Standards Institution
Box 242	L. 511, January 1967	British standard for aircraft material magnesium-aluminium-zinc-manganese alloy sheets and strips	1967	British Standards Institution
Box 242	L. 512:March:1973	British standard: aerospace series specification for bars and extruded sections of magnesium-6% aluminium-zinc alloy	1973	British Standards Institution
Box 242	L. 513:March:1973	British standard: aerospace series specification for forging stock and forgings of magnesium-6% aluminium-zinc alloy	1973	British Standards Institution
Box 242	L. 514:March:1973	British standard: aerospace series specification for forging stock and forgings of magnesium-3% zinc-zirconium alloy	1973	British Standards Institution
Box 242	L. 515:March:1973	British standard: aerospace series specification for sheet and strip of magnesium-1 and 1/4% zinc-zirconium alloy	1973	British Standards Institution
Box 242	2L .48, November, 1959	British standard for aircraft material 99.7per cent primary (virgin) aluminium notched bars and ingots for re-melting	1959	British Standards Institution
Box 242	2L .49, November, 1959	British standard for aircraft material 99 per cent secondary aluminium notched bars and ingots for re-melting	1959	British Standards Institution
Box 242	2L .50, November, 1959	British standard for aircraft material secondary aluminium notched bars and ingots for re-melting	1959	British Standards Institution
Box 242	2L .51, November, 1959	British standard for aircraft material aluminium alloy ingots and castings	1959	British Standards Institution
Box 242	2L .52, November, 1959	British standard for aircraft material aluminium alloy ingots and castings	1959	British Standards Institution
Box 242	2L .53, November, 1959	British standard for aircraft material aluminium alloy ingots and castings	1959	British Standards Institution
Box 242	2L .54, January, 1961	British standard for aircraft material 99 percent aluminium tubes	1961	British Standards Institution
Box 242	2L .55, January 1961	British standard for aircraft material aluminium -2 and 1/4 percent magnesium alloy tubes	1961	British Standards Institution
Box 242	2L .56, January 1961	British standard for aircraft material aluminium -2 and 1/4 percent magnesium alloy tubes	1961	British Standards Institution
Box 242	2L .58, September,1961	British standard for aircraft material aluminium -5 percent magnesium alloy wires for solid, cold forged rivets	1961	British Standards Institution
Box 242	2L .59, January, 1961	British standard for aircraft material aluminium -manganese alloy sheets and strips	1961	British Standards Institution
Box 242	2L .60, January, 1961	British standard for aircraft material aluminium -manganese alloy sheets and strips	1961	British Standards Institution
Box 242	2L .61, January, 1961	British standard for aircraft material aluminium -manganese alloy sheets and strips	1961	British Standards Institution
Box 242	2L .62, January, 1961	British standard for aircraft material aluminium -copper-magnesium-silicon-manganese alloy tubes	1961	British Standards Institution
Box 242	2L .63, January, 1961	British standard for aircraft material aluminium -copper-magnesium-silicon-manganese alloy tubes	1961	British Standards Institution
Box 242	2L .64, October, 1959	British standard for aircraft material aluminium -copper-magnesium-silicon-manganese alloy bars and extruded sections	1959	British Standards Institution
Box 242	2L .65, October, 1959	British standard for aircraft material aluminium -copper-magnesium-silicon-manganese alloy bars and extruded sections	1959	British Standards Institution
Box 242	2L .67, January, 1961	British standard for aircraft material 99 per cent aluminium tubes	1961	British Standards Institution
Box 242	2L .70, January, 1961	British standard for aircraft material aluminium -copper-magnesium-silicon-manganese alloy sheets and strips	1961	British Standards Institution
Box 242	2L .71, January, 1961	British standard for aircraft material aluminium -copper-magnesium-silicon-manganese alloy sheets and strips	1961	British Standards Institution
Box 242	2L .72, January, 1961	British standard for aircraft material aluminium-coated aluminium -copper-magnesium-silicon-manganese alloy sheets and strips	1961	British Standards Institution
Box 242	2L .73, January, 1961	British standard for aircraft material aluminium-coated aluminium -copper-magnesium-silicon-manganese alloy sheets and strips	1961	British Standards Institution
Box 242	2L .77, January, 1961	British standard: aerospace series specification for forging stock and forgings of aluminium-copper-magnesium-silicon-manganese alloy	1961	British Standards Institution
Box 242	2L .78, June,1967	British standard: aerospace series specification for aluminium-silicon-copper alloy ingots and castings	1967	British Standards Institution
Box 242	2L 80: March 1973	British standard: aerospace series specification for sheet and strip of aluminium-2 and 1/4 % magnesium alloy	1973	British Standards Institution
Box 242	2L 81: March 1973	British standard: aerospace series specification for sheet and strip of aluminium-2 and 1/4 % magnesium alloy	1973	British Standards Institution
Box 242	2L. 83, August, 1971	British standard: aerospace series specification for forging stock, bars, extruded sections and forgings of aluminium-copper-nickel-magnesium-iron-silicon alloy	1971	British Standards Institution
Box 242	2L. 84, August, 1971	British standard: aerospace series specification for bars and extruded sections of aluminium-copper-silicon-magnesium alloy	1971	British Standards Institution
Box 242	2L. 85, August, 1971	British standard: aerospace series specification for forging stock, bars, extruded sections and forgings of aluminium-copper-silicon-magnesium alloy	1971	British Standards Institution
Box 242	2L. 86, August, 1971	British standard specification for aircraft material aluminium-copper-magnesium alloy wires for solid, cold forged rivets	1971	British Standards Institution
Box 242	2L. 87, August, 1971	British standard: aerospace series specification for hexagonal bars for nuts, couplings and hollow machined parts of aluminium-copper-magnesium-silicon-manganese alloy	1971	British Standards Institution
Box 242	2L. 88, August, 1971	British standard: aerospace series specification for aluminium-alloy-coated sheet and strip of aluminium-zinc-magnesium-copper-chromium alloy	1971	British Standards Institution
Box 242	2L. 89, August, 1971	British standard: aerospace series specification for close toleranced sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy	1971	British Standards Institution
Box 242	2L. 90, August, 1971	British standard: aerospace series specification for close toleranced sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy	1971	British Standards Institution
Box 242	2L. 91, March, 1970	British standard: aerospace series specification for ingots and castings of aluminium-copper alloy	1970	British Standards Institution
Box 242	2L. 92, March, 1970	British standard: aerospace series specification for ingots and castings of aluminium-copper alloy	1970	British Standards Institution
Box 242	2L. 93, August, 1971	British standard: aerospace series specification for plate of aluminium-copper-magnesium-silicon-manganese alloy	1971	British Standards Institution
Box 242	2L. 94, August, 1971	British standard: aerospace series specification for plate of aluminium-copper-magnesium-silicon-manganese alloy	1971	British Standards Institution
Box 242	2L. 95, August, 1971	British standard: aerospace series specification for plate of aluminium-zinc-magnesium-copper-chromium alloy	1971	British Standards Institution
Box 242	2L. 96, August, 1971	British standard: aerospace series specification for plate of aluminium-zinc-magnesium-copper-chromium alloy	1971	British Standards Institution
Box 242	2L. 97, August, 1971	British standard: aerospace series specification for plate of aluminium-copper-magnesium-manganese alloy	1971	British Standards Institution
Box 242	2L. 98, August, 1971	British standard: aerospace series specification for plate of aluminium-copper-magnesium-manganese alloy	1971	British Standards Institution
Box 242	2L. 99, March, 1972	British standard: aerospace series specification for ingots and castings of aluminium-silicon- magnesium alloy	1972	British Standards Institution
Box 242	BS 2L. 100: 1961	Inspection and testing procedure for aircraft material aluminium and aluminium alloys	1961	British Standards Institution
Box 242	2L. 101:1959	Inspection and testing procedure for aircraft material aluminium-base and magnesium-base ingots and castings	1959	British Standards Institution
Box 242	2L. 126, March, 1970	British standard: aerospace series specification for ingots and castings of magnesium-cerium-zinc-zirconium alloy	1970	British Standards Institution
Box 242	2L. 127, March, 1970	British standard: aerospace series specification for ingots and castings of magnesium-zinc-zirconium alloy	1970	British Standards Institution
Box 242	2L. 128, March, 1970	British standard: aerospace series specification for ingots and castings of magnesium-zinc-cerium-zirconium alloy	1970	British Standards Institution
Box 242	2L 500: March, 1973	British standard: aerospace series procedure for inspection and testing of wrought magnesium-base alloys	1973	British Standards Institution
Box 242	2L 503: March, 1973	British standard: aerospace series specification for tube of magnesium-6% aluminium-zinc alloy	1973	British Standards Institution
Box 242	2L 504: March, 1973	British standard: aerospace series specification for sheet and strip of magnesium-3% zinc-zirconium alloy	1973	British Standards Institution
Box 242	2L 505: March, 1973	British standard: aerospace series specification for bars and extruded sections of magnesium-3% zinc-zirconium alloy	1973	British Standards Institution
Box 242	2L 508: March, 1973	British standard: aerospace series specification for bars and extruded sections of magnesium-1 and 1/4 % zinc-zirconium alloy	1973	British Standards Institution
Box 242	2L 509: March, 1973	British standard: aerospace series specification for tube of magnesium-1 and 1/4 % zinc-zirconium alloy	1973	British Standards Institution
Box 242	3L. 34, March, 1961	British standard for aircraft material 99 per cent aluminium forging stock, bars, extruded sections and forgings	1961	British Standards Institution
Box 242	3L. 35, November, 1959	British standard for aircraft material "y" aluminium alloy ingots and castings	1959	British Standards Institution
Box 242	3L. 36, September, 1961	British standard for aircraft material 99 per cent aluminium wires for solid, cold forged rivets	1961	British Standards Institution
Box 242	3L. 44, March, 1961	British standard for aircraft material aluminium -2 and 1/4 per cent magnesium alloy forging stock, bars, extruded sections and forgings	1961	British Standards Institution
Box 242	3L. 51, March, 1970	British standard: aerospace series specification for ingots and castings of aluminium-silicon-copper-iron-nickel- magnesium alloy	1970	British Standards Institution
Box 242	3L. 52, March, 1970	British standard: aerospace series specification for ingots and castings of aluminium-copper-silicon-nickel-magnesium-iron alloy	1970	British Standards Institution
Box 242	3L. 53, June, 1967	British standard: aerospace series specification for aluminium-magnesium alloy ingots and castings	1967	British Standards Institution
Box 242	3L. 54, August, 1971	British standard: aerospace series specification for tube of 99% aluminium	1971	British Standards Institution
Box 242	3L. 56, August, 1971	British standard: aerospace series specification for tube of aluminium-2 and 1/4 % magnesium alloy	1971	British Standards Institution
Box 242	3L. 58, August, 1971	British standard: aerospace series specification for wire for solid, cold-forged rivets of aluminium-5% magnesium alloy	1971	British Standards Institution
Box 242	3L. 59: March 1973	British standard: aerospace series specification for sheet and strip of aluminium-manganese alloy	1973	British Standards Institution
Box 242	3L. 60: March 1973	British standard: aerospace series specification for sheet and strip of aluminium-manganese alloy	1973	British Standards Institution
Box 242	3L. 61: March 1973	British standard: aerospace series specification for sheet and strip of aluminium-manganese alloy	1973	British Standards Institution
Box 242	3L. 63, August, 1971	British standard: aerospace series specification for tube of aluminium-copper- magnesium-silicon-manganese alloy	1971	British Standards Institution
Box 242	3L. 65, August, 1971	British standard: aerospace series specification for bars and extruded sections of aluminium-copper- magnesium-silicon-manganese alloy	1971	British Standards Institution
Box 242	3L. 70, August, 1971	British standard: aerospace series specification for sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy	1971	British Standards Institution
Box 242	3L. 72, August, 1971	British standard: aerospace series specification for aluminium-coated sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy	1971	British Standards Institution
Box 242	3L. 73, August, 1971	British standard: aerospace series specification for aluminium-coated sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy	1971	British Standards Institution
Box 242	3L. 78, March, 1970	British standard: aerospace series specification for ingots and castings of aluminium-silicon-copper-magnesium alloy	1970	British Standards Institution
Box 242	3L. 86, August, 1971	British standard: aerospace series specification for wire for solid, cold-forged rivets of aluminium-copper-magnesium alloy	1971	British Standards Institution
Box 242	3L. 100, August, 1971	British standard: aerospace series procedure for inspection and testing of wrought aluminium and aluminium alloys	1971	British Standards Institution
Box 242	BS 3L.101: 1970	Procedure for inspection and testing of aluminium-bases and magnesium-base ingots and castings	1970	British Standards Institution
Box 242	3L. 122, March, 1970	British standard: aerospace series specification for ingots and castings of magnesium-8% aluminium-zinc-manganese alloy	1970	British Standards Institution
Box 242	3L. 124, March, 1970	British standard: aerospace series specification for ingots and castings of magnesium10 % aluminium-zinc-manganese alloy	1970	British Standards Institution
Box 242	3L. 125, March, 1970	British standard: aerospace series specification for ingots and castings of magnesium10 % aluminium-zinc-manganese alloy	1970	British Standards Institution
Box 242	4L. 16, January, 1961	British standard for aircraft material 99 per cent aluminium sheets	1961	British Standards Institution
Box 242	4L. 17, January, 1961	British standard for aircraft material 99 per cent aluminium sheets	1961	British Standards Institution
Box 242	4l. 33 : 1959	British standard for aircraft material aluminium-silicon alloy ingots and castings	1959	British Standards Institution
Box 242	4l. 34 : 1973	British standard: aerospace series specification for forging stock, bars, extruded sections and forgings of 99% aluminium	1973	British Standards Institution
Box 242	4L. 35, March, 1970	British standard: aerospace series specification for ingots and castings of "y" aluminium alloy	1970	British Standards Institution
Box 242	4l. 36 : 1973	British standard: aerospace series specification for wire for solid, cold-forged revets of 99.5% aluminium	1973	British Standards Institution
Box 242	4L. 42, January, 1961	British standard for aircraft material aluminium-copper-magnesium-iron-nickel-silicon alloy forging stock and forgings	1961	British Standards Institution
Box 242	4L. 44, March, 1973	British standard: aerospace series specification for forging stock, bars, extruded sections and forgings of aluminium-2 and 1/4 % magnesium alloy	1973	British Standards Institution
Box 242	4L. 53, March, 1970	British standard: aerospace series specification for ingots and castings of aluminium-magnesium alloy	1970	British Standards Institution
Box 242	5L. 16: March, 1973	British standard: aerospace series specification for sheet and strip of 99% aluminium	1973	British Standards Institution
Box 242	5L. 17: March, 1973	British standard: aerospace series specification for sheet and strip of 99% aluminium	1973	British Standards Institution
Box 242	5L. 31, Novermber, 1959	British standard for aircraft material 99 per cent primary (virgin) aluminium notched bars and ingots for re-melting	1959	British Standards Institution
Box 242	5L. 37, September, 1961	British standard for aircraft material aluminium-copper-magnesium-silicon-manganese alloy wires for solid, cold forged rivets	1961	British Standards Institution
Box 242	6L. 25, January, 1961	British standard for aircraft material aluminium-copper-nickel-magnesium alloy forging stock and forgings	1961	British Standards Institution
Box 242	6L. 37, August, 1971	British standard: aerospace series specification for wire for solid, cold-forged rivets of aluminium-copper-magnesium-silicon-manganese alloy	1971	British Standards Institution
Box 242	7L. 25, August, 1971	British standard: aerospace series specification for forging stock and forgings of aluminium-copper-nickel-magnesium alloy	1971	British Standards Institution
Box 242	M.20.	British standard specification for graphited wax for aircraft purposes	1947	British Standards Institution
Box 242	M.21.	British standard specification for kaolin for aircraft purposes	1947	British Standards Institution
Box 242	M.22.	British standard specification for silica gel acid activated for aircraft purposes	1949	British Standards Institution
Box 242	M.24.	British standard specification for graphical symbols for aircraft hydraulic and pneumatic systems	1955	British Standards Institution
Box 242	M.25.	British standard specification for chemical preparations for chemical closets (portable type for aircraft)	1957	British Standards Institution
Box 242	M.26.	British standard specification for chemical preparations for chemical closets (re-circulation type) for aircraft	1957	British Standards Institution
Box 242	M.27.	British standard specification for non-fluorescent magnetic flaw detection inks for finished machined aircraft parts	1958	British Standards Institution
Box 242	M.28.	British standard specification for flat pallets for use in an aircraft	1964	British Standards Institution
Box 242	M.29.	British standard: aerospace series specification for hand operated portable fire extinguishers for aircraft	1967	British Standards Institution
Box 242	M.30.	British standard: aerospace series specification for aircraft tyre growth and clearance dimensions	1967	British Standards Institution
Box 242	M.31.	British standard: aerospace series	1970	British Standards Institution
Box 242	Supplement No.1 (1974) to M31:1970	Symbols for flight dynamics	1970	British Standards Institution
Box 242	M.32.	British standard: aerospace series specification for dimensions of aircraft accessory drives and mounting pads	1969	British Standards Institution
Box 242	M.33	British standard: aerospace series specification for dimensions of electrometric toroidal sealing rings (inch series) to class 1 tolerances for aircraft		British Standards Institution
Box 242	M.34.	British standard: aerospace series method of preparation and use of radiographic techniques	1970	British Standards Institution
Box 242	M.35	British standard: aerospace series method for magnetic particle flaw detection of materials and components	1970	British Standards Institution
Box 242	M.36.	British standard: aerospace series method for ultrasonic testing of special forgings by an immersion technique using flat-bottomed holes as a reference standard	1970	British Standards Institution
Box 242	M.37.	British standard: aerospace series method for the etch inspection of metallic materials and components	1970	British Standards Institution
Box 242	M.38	British standard: aerospace series guide to compilation of instructions and reports for the in-service non-destructive testing of aerospace products	1971	British Standards Institution
Box 242	M.39.	British standard: aerospace series method for penetrant inspection of aerospace materials and components	1972	British Standards Institution
Box 242	M.40.	British standard: aerospace series methods for measuring coating thickness by non-destructive testing	1972	British Standards Institution
Box 242	M.41.	British standard: aerospace series methods of numbering propulsion units and components and describing their direction of rotation	1972	British Standards Institution
Box 242	M.42.	British standard: aerospace series methods for non-destructive testing of fusion and resistance welds in thin gauge materials	1972	British Standards Institution
Box 242	M.43.	British standard: aerospace series methods of zoning aircraft and referencing access door and panels	1973	British Standards Institution
Box 242	M.44.	British standard: aerospace series specification for identification of aircraft servicing, maintenance ground handling and safety /hazard points	1974	British Standards Institution
Box 242	M.45.	British standard: aerospace series specification for aircraft tyres	1974	British Standards Institution
Box 242	M.46.	British standard: aerospace series specification for tubing put side diameters nd thicknesses	1974	British Standards Institution
Box 242	M.47.	British standard: aerospace series specification for retreated tyres for aircraft	1975	British Standards Institution
Box 242	M.48.	British standard: aerospace series specification for dimensions of elastomeric toroidal sealing rings for aerospace use-inch series		British Standards Institution
Box 242	M.49.	British standard: aerospace series specification for marking of hydraulic components	1977	British Standards Institution
Box 242	M.50.	British standard: aerospace series specification for clearance dimensions for tripod jacks for aircraft	1980	British Standards Institution
Box 242	M.51.	British standard: aerospace series: classification for pressure and temperature for fluid systems and components	1982	British Standards Institution
Box 242	2 M.23,	British standard identification scheme for aircraft pipelines	1957	British Standards Institution
Box 242	2M 41:1977 ISO 482-1977	British standard: aerospace series methods of numbering propulsion units and components and describing their direction of rotation	1977	British Standards Institution
Box 242	3 M.23 : 1968	Specification for an identification scheme for pipelines	1968	British Standards Institution
Box 242	4 M.23 : 1977	Specification for an identification scheme for pipelines	1977	British Standards Institution
Box 242	N.1 : 1969	Specification for oxygen masks for use in demand systems	1969	British Standards Institution
Box 242	N.2 : 1972	Specification for chemical oxygen generators for aircraft	1972	British Standards Institution
Box 242	N.3 : 1973	Specification for gaseous breathing oxygen supplies	1973	British Standards Institution
Box 242	N.4 : 1974	Specification for full mask assemblies for use in contaminated atmospheres	1974	British Standards Institution
Box 242	N.100 : 1967	Specification for general requirements for aircraft oxygen equipment	1967	British Standards Institution
Box 242	2N.100 : 1973	Specification for general requirements for aircraft oxygen systems and equipment	1973	British Standards Institution
Box 242	PAS1 : Part 2 : 1975	Specification for heavy duty engine oils. Part 2 mil-l2104b	1975	British Standards Institution
Box 242	PAS1 : Part 3 : 1975	Specification for heavy duty engine oils. Part 3 caterpillar series 3	1975	British Standards Institution
Box 242	PAS2 : 1975	Specification for straight mineral lubricating oils	1975	British Standards Institution
Box 242	PAS5 : 1975	Specification for mineral turbine oils	1975	British Standards Institution
Box 242	PAS6 : Part 1 : 1975	Specification for extreme pressure gear oils. Part 1 cs 3000a	1975	British Standards Institution
Box 242	PAS6 : Part 3 : 1975	Specification for extreme pressure gear oils. Part 3. Mil-l-2105b	1975	British Standards Institution
Box 242	PAS17 : 1974	Specification for sheeting, sheets and pillow slips	1974	British Standards Institution
Box 242	PAS19 : 1975	Specification for towels and napkins	1975	British Standards Institution
Box 242	PL.1 : 1951	Specification for synthetic resin (phenolic) mouldings for aircraft	1951	British Standards Institution
Box 242	PL.2 : 1969	Specification for phenolic resin-bonded cotton fabric round tube (maximum internal diameter 75mm or 3in)	1969	British Standards Institution
Box 242	PL.3 : 1969	Specification for phenolic resin-bonded cotton fabric round rod (maximum internal diameter 75mm or 3in)	1969	British Standards Institution
Box 242	2PL.1 : 1966	Specification for phenolic mouldings for aeronautical purposes	1966	British Standards Institution
Box 242	R.1 : 1954	Specification for sizes and forms of civil aircraft radio equipment	1954	British Standards Institution
Box 242	R.2 : 1956	Specification for basic characteristic of radio service selection and intercommunication systems for civil aircraft	1956	British Standards Institution
Box 243	S. 93. January, 1949	British standard specification for aircraft material. 35 ton steel (normalised) (limiting ruling section 6 in.)	1949	British Standards Institution
Box 243	S. 108. January, 1949	British standard specification for aircraft material. Chromium-nickel heat-resisting steel (23/14)	1949	British Standards Institution
Box 243	S. 109. January, 1949	British standard specification for aircraft material. Chromium-nickel heat-resisting steel (23/18)	1949	British Standards Institution
Box 243	S. 110. January, 1949	British standard specification for aircraft material. Chromium-nickel steel (corrosion-resisting)	1949	British Standards Institution
Box 243	S. 114. August, 1950	British standard specification for aircraft material. 55 ton manganese-molybdenum steel (for the manufacture of machine bolts not exceeding half in. B.s.f., 'medium tensile' nuts over half in. B.s.f. And similar standard aircraft parts only)	1950	British Standards Institution
Box 243	S. 115. April, 1952	British standard specification for aircraft material. 1 per cent chromium steel	1952	British Standards Institution
Box 243	S. 118. February, 1954	British standard specification for aircraft material. 55 ton, low nickel-chromium-molybdenum steel ((limiting ruling section 4 in.)	1954	British Standards Institution
Box 243	S. 122. April, 1957	British standard specification for aircraft material. Low nickel-chromium steel (bars only for the manufacture of hot forged bolts of half in. To one and a half in. Shank diameter)	1957	British Standards Institution
Box 243	S. 123. February, 1958	British standard specification for aircraft material. 55 ton, 3 per cent chromium-molybdenum steel (limiting ruling section 6 in.)	1958	British Standards Institution
Box 243	S. 124. October, 1960	British standard specification for aircraft material. Corrosion-resisting chromium steel (free machining) (45-55 ton/sq. In: limiting ruling section 6 in.)	1960	British Standards Institution
Box 243	S. 125. January, 1964	British standard specification for aircraft material. 23/14 chromium-nickel heat-resisting steel (titanium stabilized) (35 ton/sq. In: limiting ruling section 6 in.)	1964	British Standards Institution
Box 243	S. 126. January, 1964	British standard specification for aircraft material. 23/14 chromium-nickel heat-resisting steel (niobium stabilized) (35 ton/sq. In: limiting ruling section 6 in.)	1964	British Standards Institution
Box 243	S. 127. January, 1964	British standard specification for aircraft material. 24/17 chromium-nickel heat-resisting steel (titanium stabilized) (35 ton/sq. In: limiting ruling section 6 in.)	1964	British Standards Institution
Box 243	S. 128. January, 1964	British standard specification for aircraft material. 24/17 chromium-nickel heat-resisting steel (niobium stabilized) (35 ton/sq. In: limiting ruling section 6 in.)	1964	British Standards Institution
Box 243	S. 129. January, 1964	British standard specification for aircraft material. 18/9 chromium-nickel corrosion-resisting steel (titanium stabilized) (35 ton/sq. In: limiting ruling section 6 in.)	1964	British Standards Institution
Box 243	S. 130. January, 1964	British standard specification for aircraft material. 18/9 chromium-nickel corrosion-resisting steel (niobium stabilized) (35 ton/sq. In: limiting ruling section 6 in.)	1964	British Standards Institution
Box 243	S. 131. October, 1965	British standard specification for aircraft material. High thermal expansion steel (40 ton/sq. In: limiting ruling section 6 in.)	1965	British Standards Institution
Box 243	S. 132. October, 1965	British standard specification for aircraft material. 3 per cent chromium-molybdenum-vanadium steel (suitable for nitriding) (85/95 ton/sq. In: limiting ruling section two and a half inches.)	1965	British Standards Institution
Box 243	S. 133. October, 1965	British standard specification for aircraft material. Three quarter per cent nickel-chromium case-hardening steel	1965	British Standards Institution
Box 243	S. 134. October, 1965	British standard specification for aircraft material. 3 per cent chromium-molybdenum-vanadium steel (air hardening) (100 ton/sq. In: limiting ruling section one and an eighth inches.)	1965	British Standards Institution
Box 243	S. 135. October, 1965	British standard specification for aircraft material. 1 per cent carbon-chromium steel (limiting ruling section 1 inch)	1965	British Standards Institution
Box 243	S. 136. January, 1967	British standard specification for aircraft material. 1 per cent carbon-chromium steel (vacuum remelted: limiting ruling section 1 inch)	1967	British Standards Institution
Box 243	S. 137. May, 1967	British standard aerospace series specification for high chromium-nickel corrosion-resisting steel bright bars (free machining)	1967	British Standards Institution
Box 243	S. 138. August, 1967	British standard aerospace series specification for 3 per cent chromium-molybdenum-vanadium steel (vacuum melted-air hardening) (157 kgf/sq. In): limiting ruling section 30mm (one and an eighth inches.)	1967	British Standards Institution
Box 243	S. 139. April, 1968	British standard aerospace series specification for one and a half per cent nickel-chromium-molybdenum steel (110/130 kgf/sq. Mm (70/83 ton/sq. In.): limiting ruling section 70 mm (two and three quarter in.)	1968	British Standards Institution
Box 243	S. 140. April, 1968	British standard aerospace series specification for two and a half per cent nickel-chromium-molybdenum steel (110/130 kgf/sq. Mm (70/83 ton/sq. In.): limiting ruling section 150 mm (6 in.)	1968	British Standards Institution
Box 243	S. 141. April, 1968	British standard aerospace series specification for twelve per cent chromium corrosion-resisting steel (60/80 kgf/sq. Mm (38/51 ton/sq. In.): limiting ruling section 150 mm (6 in.)	1968	British Standards Institution
Box 243	S. 142. April, 1968	British standard aerospace series specification for 1 per cent chromium-molybdenum steel (90/110 kgf/sq. Mm (50/70 ton/sq. In.): limiting ruling section 40 mm (one and a quarter in.) (suitable for welding)	1968	British Standards Institution
Box 243	S. 143. February, 1969	British standard aerospace series specification for chromium-nickel-copper-molybdenum corrosion-resisting steel (precipitation hardening) 93/108 hbar	1969	British Standards Institution
Box 243	S. 144. February, 1969	British standard aerospace series specification for chromium-nickel-copper-molybdenum corrosion-resisting steel (precipitation hardening) 113/133 hbar	1969	British Standards Institution
Box 243	S. 145. February, 1969	British standard aerospace series specification for chromium-nickel-copper-molybdenum corrosion-resisting steel (precipitation hardening) 127/147 hbar	1969	British Standards Institution
Box 243	S. 146. February, 1969	British standard aerospace series specification for 4 % nickel-chromium-molybdenum steel (air hardening-vacuum remelted) 176/196 hbar: limiting ruling section 100 mm (4 in)	1969	British Standards Institution
Box 243	S. 147. July, 1969	British standard aerospace series specification for nickel-chromium-molybdenum steel (bar for the manufacture of forged bolts only)	1969	British Standards Institution
Box 243	S. 148. July, 1969	British standard aerospace series specification for low nickel-chromium steel (bar for the manufacture of forged bolts only)	1969	British Standards Institution
Box 243	S. 149. February, 1972	British standard aerospace series specification for 1.75 % nickel-chromium-molybdenum steel (bar for the manufacture of forged bolts and forged nuts only)	1972	British Standards Institution
Box 243	S 150 : 1975	British standard aerospace series 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)	1975	British Standards Institution
Box 243	S 151 : 1975	British standard aerospace series specification for chromium-nickel-molybdenum-vanadium heat-resisting steel billets, bars, forgings and parts (930 - 1130 mpa: limiting ruling section 150 mm) (cr 12, ni 2.5, mo 1.7, v 0.3)	1975	British Standards Institution
Box 243	S 152 : 1975	British standard aerospace series 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)	1975	British Standards Institution
Box 243	S 153 : 1976	British standard aerospace series specification for two and a half % nickel-chromium-molybdenum steel billets, bars, forgings and parts (1230 - 1430 mpa: limiting ruling section 40 mm)	1976	British Standards Institution
Box 243	S 154 : 1976	British standard aerospace series specification for two and a half % nickel-chromium-molybdenum steel billets, bars, forgings and parts (880 - 1080 mpa: limiting ruling section 150 mm)	1976	British Standards Institution
Box 243	S 155 : 1976	British standard aerospace series specification for nickel-silicon-chromium-molybdenum-vanadium steel (vacuum arc remelted) billets, bars, forgings and parts (1900 - 2100 mpa: limiting ruling section 75 mm)	1976	British Standards Institution
Box 243	S 156 : 1976	British standard aerospace series specification for 4 % nickel-chromium-molybdenum case hardened steel (vacuum arc remelted) billets, bars, forgings and parts (1320 - 1520 mpa)	1976	British Standards Institution
Box 243	S 157 : 1976	British standard aerospace series specification for 3 % nickel-chromium-molybdenum case-hardening steel billets, bars, forgings and parts (1180 - 1380 mpa)	1976	British Standards Institution
Box 243	S 158 : 1977	British standard aerospace series specification for 1 % chromium-molybdenum steel bars for the manufacture of forged bolts and forged nuts	1977	British Standards Institution
Box 243	S 159 : 1981	British standard aerospace series specification for 12 % chromium-nickel-molybdenum-vanadium heat-resisting steel bars for the manufacture of fasteners (1100 - 1300 mpa: limiting ruling section 50 mm)	1981	British Standards Institution
Box 243	S. 201. August, 1967	British standard aerospace series specification for patented cold drawn carbon steel wire and springs (high duty unground wire)	1967	British Standards Institution
Box 243	S. 202. August, 1967	British standard aerospace series specification for patented cold drawn carbon steel wire and springs (high duty ground wire)	1967	British Standards Institution
Box 243	S. 203. August, 1967	British standard aerospace series specification for carbon steel wire and springs (high duty unground wire - hardened and tempered)	1967	British Standards Institution
Box 243	S. 204. August, 1967	British standard aerospace series specification for chromium-vanadium steel wire and springs (high duty ground wire - hardened and tempered)	1967	British Standards Institution
Box 243	S. 205. February, 1969	British standard aerospace series specification for austenitic chromium-nickel steel wire and springs	1969	British Standards Institution
Box 243	S. 500, April, 1956	British standard specification for aircraft material inspection and testing procedure for steel sheets and strips for aircraft	1956	British Standards Institution
Box 243	S. 510, March, 1956	British standard specification for aircraft material 28 ton carbon steel sheets and strips (suitable for welding)	1956	British Standards Institution
Box 243	S. 511, March, 1956	British standard specification for aircraft material deep drawing carbon steel sheets and strips (suitable for welding)	1956	British Standards Institution
Box 243	S. 512, March, 1956	British standard specification for aircraft material tinned steel sheets and strips	1956	British Standards Institution
Box 243	S. 513, March, 1956	British standard specification for aircraft material spring steel strips	1956	British Standards Institution
Box 243	S. 514, March, 1956	British standard specification for aircraft material 50 ton carbon-manganese steel sheets and strips (40 ton 0.1 per cent proof stress) (suitable for welding)	1956	British Standards Institution
Box 243	S. 515, March, 1956	British standard specification for aircraft material 30 ton carbon-manganese steel sheets and strips(softened) (suitable for welding)	1956	British Standards Institution
Box 243	S. 516, March, 1956	British standard specification for aircraft material 60 ton carbon-manganese steel sheets and strips (50 ton 0.1 per cent proof stress)	1956	British Standards Institution
Box 243	S. 517, March, 1956	British standard specification for aircraft material 75 ton carbon-manganese steel sheets and strips (65 ton 0.1 per cent proof stress)	1956	British Standards Institution
Box 243	S. 518, March, 1956	British standard specification for aircraft material 50 ton chromium-molybdenum steel sheets and strips (40 ton 0.1 per cent proof stress) (suitable for welding)	1956	British Standards Institution
Box 243	S. 519, March, 1956	British standard specification for aircraft material 75 ton chromium-molybdenum steel sheets and strips (65 ton 0.1 per cent proof stress) (suitable for welding)	1956	British Standards Institution
Box 243	S. 520, March, 1956	British standard specification for aircraft material cold-rolled chromium-nickel steel sheets and strips (corrosion-resisting) (40 ton 0.1 per cent proof stress)	1956	British Standards Institution
Box 243	S. 521, March, 1956	British standard specification for aircraft material chromium-nickel steel sheets and strips (corrosion-resisting) (40 ton 0.1 per cent proof stress)	1956	British Standards Institution
Box 243	S. 522, March, 1956	British standard specification for aircraft material 23/14 chromium-nickel steel sheets and strips (heat-resisting)	1956	British Standards Institution
Box 243	S. 523, March, 1956	British standard specification for aircraft material 23/18 chromium-nickel steel sheets and strips (heat-resisting)	1956	British Standards Institution
Box 243	S. 524, May, 1969	British standard aerospace series specification for cold-rolled 18/10 chromium-nickel corrosion-resisting steel sheet and strip (titanium stabilized: 80 hbar)	1969	British Standards Institution
Box 243	S. 525, May, 1969	British standard aerospace series specification for cold-rolled 18/10 chromium-nickel corrosion-resisting steel sheet and strip (niobium stabilized: 80 hbar)	1969	British Standards Institution
Box 243	S. 526, May, 1969	British standard aerospace series specification for softened 18/10 chromium-nickel corrosion-resisting steel sheet and strip (titanium stabilized: 54 hbar)	1969	British Standards Institution
Box 243	S. 527, May, 1969	British standard aerospace series specification for softened 18/10 chromium-nickel corrosion-resisting steel sheet and strip (niobium stabilized: 54 hbar)	1969	British Standards Institution
Box 243	S. 528, January, 1970	British standard aerospace series specification for 23/14 chromium-nickel heat-resisting steel sheet and strip (titanium stabilized: 54 hbar) (elevated temperature properties not verified)	1970	British Standards Institution
Box 243	S. 529, January, 1970	British standard aerospace series specification for 23/14 chromium-nickel heat-resisting steel sheets and strips (niobium stabilized: 54 hbar) (elevated temperature properties not verified)	1970	British Standards Institution
Box 243	S. 530, January, 1970	British standard aerospace series specification for 24/17 chromium-nickel heat-resisting steel sheet and strip (titanium stabilized: 54 hbar) (elevated temperature properties not verified)	1970	British Standards Institution
Box 243	S. 531, January, 1970	British standard aerospace series specification for 24/17 chromium-nickel heat-resisting steel sheet and strip (niobium stabilized: 54 hbar) (elevated temperature properties not verified)	1970	British Standards Institution
Box 243	S. 532, September, 1969	British standard aerospace series specification for chromium-nickel-copper-molybdenum corrosion resisting steel sheet and strip (precipitation hardened: 98/118 hbar)	1969	British Standards Institution
Box 243	S. 533, September, 1969	British standard aerospace series specification for chromium-nickel-copper-molybdenum corrosion resisting steel sheet and strip (precipitation hardened: 118/137 hbar)	1969	British Standards Institution
Box 243	S. 534, May, 1969	British standard aerospace series specification for chromium-molybdenum steel sheet and strip (88/108 hbar) (suitable for welding)	1969	British Standards Institution
Box 243	S. 535, May, 1969	British standard aerospace series specification for chromium-molybdenum steel sheet and strip (115/130 hbar) (suitable for welding)	1969	British Standards Institution
Box 243	S. 536, January, 1970	British standard aerospace series specification for low carbon 18/10 chromium-nickel corrosion resisting steel sheet and strip (50 hbar)	1970	British Standards Institution
Box 243	S. 537, January, 1970	British standard aerospace series specification for low carbon 17/12 chromium-nickel-molybdenum corrosion resisting steel sheet and strip (50 hbar)	1970	British Standards Institution
Box 243	S. 538 : 1975	British standard aerospace series specification for chromium-nickel-molybdenum-vanadium heat-resisting steel sheet and strip (9300 - 1130 mpa: maximum thickness 6mm) (cr 12, ni 2.5, mo 1.7, v 0.3)	1975	British Standards Institution
Box 243	2 S. 91, January, 1964	British standard specification for aircraft material. Mild steel (suitable for bearing shells)	1964	British Standards Institution
Box 243	2 S. 92, January, 1964	British standard specification for aircraft material. Carbon-manganese steel (suitable for welding) (40/55 ton/sq. In: limiting ruling section 4 in.)	1964	British Standards Institution
Box 243	2 S. 93, July, 1964	British standard specification for aircraft material. '40' carbon steel (normalized) (35/45 ton/sq. In: limiting ruling section 6 in.)	1964	British Standards Institution
Box 243	2 S. 94, January, 1955	British standard specification for aircraft material. 55 ton low alloy steel (limiting ruling section two and a half in.)	1955	British Standards Institution
Box 243	2 S. 95, January, 1964	British standard specification for aircraft material. One and a half per cent nickel-chromium-molybdenum steel (55/65 ton/sq. In: limiting ruling section 4 in.)	1964	British Standards Institution
Box 243	2 S. 96, January, 1964	British standard specification for aircraft material. Two and a half per cent nickel-chromium-molybdenum steel (55/65 ton/sq. In: limiting ruling section 6 in.)	1964	British Standards Institution
Box 243	2 S. 97, January, 1964	British standard specification for aircraft material. Two and a half per cent nickel-chromium-molybdenum steel (65/75 ton/sq. In: limiting ruling section 6 in.)	1964	British Standards Institution
Box 243	2 S. 98, January, 1964	British standard specification for aircraft material. Two and a half per cent nickel-chromium-molybdenum steel (high carbon) (75/85 ton/sq. In: limiting ruling section 6 in.)	1964	British Standards Institution
Box 243	2 S. 100, January, 1949	British standard specification for aircraft material. Inspection and testing procedure for aircraft steels	1949	British Standards Institution
Box 243	2S.102,	Specification for aircraft material carbon -molybdenum steel (wire only for the manufacture of forged bolts)	1964	British Standards Institution
Box 243	2S.103,	Specification for aircraft material low nickel-chromium steel (wire only for the manufacture of forged bolts)	1964	British Standards Institution
Box 243	2S.105,	Specification for aircraft material carbon steel (wire only for the manufacture of forged bolts not exceeding shank diameter)	1964	British Standards Institution
Box 243	2S.106,	Specification for aircraft material 3 per cent chromium-molybdenum steel (suitable for nitriding) (60/70 ton/sq in: limiting ruling section 6 in)	1964	British Standards Institution
Box 243	2S,107,	Specification for aircraft material 3 per cent nickel-chromium -molybdenum case hardening steel	1964	British Standards Institution
Box 243	2S.111,	Specification for aircraft material nickel-chromium- tungsten valve steel	1964	British Standards Institution
Box 243	2S.112,	Specification for aircraft material semi-free cutting carbon steel, bright bars for machining (40/50 ton/sq in: maximum size 1/2 inch diameter or minor sectional dimension (primarily intended for the manufacture of nuts))	1964	British Standards Institution
Box 243	2S.113,	Specification for aircraft material '40'carbon steel bright bars for machining (45-55 ton/sq in: limiting ruling section 1 inch (primarily intended for the manufacture of nuts))	1964	British Standards Institution
Box 243	2S.114,	Specification for aircraft material manganese-molybdenum steel (55/65 ton/sq in: limiting ruling section 2 1/2 inches)	1964	British Standards Institution
Box 243	2S.116,	Specification for aircraft material'40' carbon steel (55-65 ton/sq in: limiting ruling section 3/4 inch) (primarily intended for the manufacture of machined bolts)	1964	British Standards Institution
Box 243	2S.117,	Specification for aircraft material 1 per cent chromium steel (55/65 ton/sq in: limiting ruling section 1 1/8 inch))	1964	British Standards Institution
Box 243	2S.119	British standard aircraft for aircraft material 1 1/2 per cent nickel -chromium -molybdenum steel (65/75 ton/sq in: limiting ruling section 2 1/2 in)	1964	British Standards Institution
Box 243	2S.120	Specification for aircraft material 2 1/2 per cent nickel- chromium- molybdenum steel (oil hardening) (100tonf/sq in: limiting ruling section 2 1/2 in)	1964	British Standards Institution
Box 243	2S.124,	Specification for aircraft material 12 per cent chromium corrosion -resisting steel (free machining) (45/55 ton/sq in: limiting ruling section 6 in)	1964	British Standards Institution
Box 243	2S.129,	Aerospace series: specification for 18/9 chromium -nickel corrosion -resisting steel (titanium stabilized) billets, bars, forgings and parts (540 mpa: limiting ruling section 150mm)	1976	British Standards Institution
Box 243	2S.130,	Specification for 18/9 chromium -nickel corrosion -resisting steel (niobium stabilized) billets, bars, forgings and parts (540 mpa: limiting ruling section 150mm	1976	British Standards Institution
Box 243	2S.131,	Specification for high thermal expansion steel billets, bars, forgings and parts (620mpa: limiting ruling section 150mm)	1977	British Standards Institution
Box 243	2S.132,	Aerospace series specification for 3% chromium-molybdenum-vanadium steel (132/147 hbar: limiting ruling section70mm (2 3/4 in)	1969	British Standards Institution
Box 243	2S.135,	Specification for 1% carbon -chromium steel, billets, bars, forgings and parts (limiting ruling section 25 mm)	1977	British Standards Institution
Box 243	2S.136,	Specification for 1% carbon -chromium steel (vacuum arc remelted, billets, bars, forgings and parts (limiting ruling section 25 mm))	1977	British Standards Institution
Box 243	2S.137,	Specification for high-chromium-nickel corrosion-resisting steel bright bars (free machining) (880-1080 mpa: limiting ruling section 70mm)	1976	British Standards Institution
Box 243	2S.140,	Specification: aerospace series 2 1/2% nickel-chromium-molybdenum steel billets, bars, forgings and parts (1080-1280 mpa: limiting ruling section 150mm)	1976	British Standards Institution
Box 243	2S.142,	Specification for 1% chromium-molybdenum steel billets, bars, forgings and parts (900-1100 mpa: limiting ruling section 40mm)	1977	British Standards Institution
Box 243	2S.143,	Specification for chromium-nickel-copper-molybdenum corrosion -resisting steel (precipitation hardening) billets, bars, forgings and parts (930-1080 mpa)	1976	British Standards Institution
Box 243	2S.144,	Specification for chromium-nickel-copper-molybdenum corrosion -resisting steel (precipitation hardening) billets, bars, forgings and parts (1130-1330 mpa)	1976	British Standards Institution
Box 243	2S.145,	Specification for chromium-nickel-copper-molybdenum corrosion -resisting steel (precipitation hardening) billets, bars, forgings and parts (1270-1470 mpa)	1976	British Standards Institution
Box 243	2S.146,	Specification for 4% nickel-chromium-molybdenum air-hardening steel (vacuum arc remelted) billets, bars, forgings and parts (1760-1960 mpa: limiting ruling section 100mm)	1976	British Standards Institution
Box 243	2S.147,	Specification for 0.5% nickel-chromium-molybdenum steel bars for the manufacture of forged belts and forged nuts	1976	British Standards Institution
Box 243	2S.149,	Specification for 1.75% nickel-chromium-molybdenum steel bars for the manufacture of forged billets and forged nuts	1976	British Standards Institution
Box 243	2S,.500 : 1969	Inspection and testing procedure for aerospace material - steel sheet and strip (metric and inch units)	1969	British Standards Institution
Box 243	2S.510,	Aerospace series specification for carbon steel sheet and strip (430/540 mn/m2) (suitable for welding)	1970	British Standards Institution
Box 243	2S.511,	Aerospace series specification for deep drawing carbon steel sheet and strip (280/400 mn/m2) (suitable for welding)	1970	British Standards Institution
Box 243	2S.513,	Aerospace series specification for spring steel strip	1970	British Standards Institution
Box 243	2S.514,	Aerospace series specification for carbon-manganese steel sheet and strip (for use in the hardened and tempered condition:77/100hbar) (suitable for welding)	1969	British Standards Institution
Box 243	2S.515,	Aerospace series specification for carbon-manganese steel sheet and strip (softened) (for use in the softened condition:46/59 hbar) (suitable for welding)	1969	British Standards Institution
Box 243	2S.516,	Aerospace series specification for carbon-manganese steel sheet and strip (93/116 hbar)	1969	British Standards Institution
Box 243	2S.517,	Aerospace series specification for carbon -manganese steel sheet and strip (11/131 hbar)	1969	British Standards Institution
Box 243	3S.61,	Specification for aircraft material 12 per cent chromium corrosion -resisting steel (35/45 tonf/sq in: limiting ruling section 6 in)	1964	British Standards Institution
Box 243	3S.62,	Specification for aircraft material 12 per cent chromium corrosion -resisting steel (45/55 tonf/sq in: limiting ruling section 6 in)	1964	British Standards Institution
Box 243	3S.70,	Specification for aircraft material '55' carbon steel (normalized) (45/55 tonf/sq in: limiting ruling section 4 in)	1964	British Standards Institution
Box 243	3S.79,	Specification for aircraft material '55' carbon steel (hardened and tempered) (55/65 tonf/sq in: limiting ruling section 1 1/8 in)	1964	British Standards Institution
Box 243	3S.80,	Specification for aircraft material high chromium -nickel corrosion-resisiting (55/65 tonf/sq in: limiting ruling section 6 in)	1964	British Standards Institution
Box 243	3S.82,	Specification for aircraft material 4 per cent nickel-chromium -molybdenum case -hardening steel	1964	British Standards Institution
Box 243	3S.91,	Specification for mild steel billets, bars, forgings, and parts (suitable for bearing shells)	1977	British Standards Institution
Box 243	3S.95,	Aerospace specification for 1 1/2 per cent nickel-chromium -molybdenum steel (90/110 kgf.mm2 (57/70 tonf/sq in2): limiting ruling section 150 mm (6 in))	1967	British Standards Institution
Box 243	3S.99,	Specification for aircraft material 2 1/2 per cent nickel-chromium -molybdenum steel (high carbon) (80/90 tonf/sq in: limiting ruling section 6 in)	1964	British Standards Institution
Box 243	3S.100	Inspection and testing procedure for aircraft material steel	1963	British Standards Institution
Box 243	3S.100 section Nine	Aerospace series inspection and testing procedure for steel section nine wire for the manufacture of forged bolts and forged nuts only	1970	British Standards Institution
Box 243	3S.100 section Ten	Aerospace series inspection and testing procedure for steel section ten spring steel rod, wire and springs	1967	British Standards Institution
Box 243	3S.102,	Aerospace series specification for carbon-molybdenum steel (bar for the manufacture of forged bolts only)	1969	British Standards Institution
Box 243	3S.105,	Aerospace series specification for carbon steel (bar for manufacture of forged bolts only)	1969	British Standards Institution
Box 243	3S.106,	Aerospace series specification for 3% chromium -molybdenum steel (93/108 hbar (60/70tonf/sq/in2): limiting ruling section 150mm(6in))	1969	British Standards Institution
Box 243	3S.107,	Aerospace series specification for 3% nickel-chromium-molybdenum case-hardening steel	1969	British Standards Institution
Box 243	3S.132,	Specification: aerospace series 3% chromium-molybdenum-vanadium-steel billets, bars, forgings and parts (1320-1470 mpa: limiting ruling section 70 mm) (suitable for nitriding)	1976	British Standards Institution
Box 243	4S.14,	Specification for aircraft material carbon case hardening steel	1964	British Standards Institution
Box 243	4S.28,	Specification for aircraft material 4 per cent nickel-chromium-molybdenum steel (air hardening) (100 tonf/sq in: limiting ruling section 2 1/2 in))	1964	British Standards Institution
Box 243	4S.80,	Aerospace series specification for high chromium-nickel corrosion resisting steel (90/110 kg/mm2 (57/70 tonf/in2): limiting ruling section 100mm (4 in))	1967	British Standards Institution
Box 243	4S.82,	Aerospace series specification for 4% nickel-chromium-molybdenum case -hardening steel	1969	British Standards Institution
Box 243	4S.99,	Specification for 2.5% nickel-chromium- molybdenum (high carbon) steel billets, bars, forgings and parts (1230-1420 mpa: limiting ruling section 150mm)	1976	British Standards Institution
Box 243	4S.100,	Aerospace series procedure for inspection and testing of wrought steels (other than sheet, strip and tubes)	1975	British Standards Institution
Box 243	4S.106	Specification aerospace series 3% chromium- molybdenum steel billets, bars, forgings and parts (930-1080 mpa: limiting ruling secton150mm) (suitable for nitriding)	1976	British Standards Institution
Box 243	5S.15,	Specification for aircraft material 3 per cent nickel case-hardening steel	1964	British Standards Institution
Box 243	5S.21,	Specification for aircraft material '20'carbon steel (suitable for welding) (25/35 tonf/sq: maximum size 6 inches diameter or minor sectional dimension)	1964	British Standards Institution
Box 243	5S.80,	Aerospace series specification for high chromium-nickel corrosion-resisting steel, billets, bars, forgings and parts (880-1080 mpa: limiting ruling section 100mm)	1976	British Standards Institution
Box 243	5S.82,	Specification: aerospace series 4% nickel-chromium-molybdenum case-hardening steel, billets, bars, forgings and parts (1320-1520mpa)	1976	British Standards Institution
Box 243	7S.1,	Specification for aircraft material carbon steel bright bars for machining (35/45 tonf/sq in; maximum size, 4 inches diameter or minor sectional dimension)	1964	British Standards Institution
Box 243	S. P. 8 May 1939	Turnbuckles (tension rod types) for aircraft purposes	1939	British Standards Institution
Box 243	SP.9. February 1949	Split cotter pins (non-corrodible) for aircraft purposes	1949	British Standards Institution
Box 243	SP.10 & 11. February 1949	Washers for aircraft purposes (primarily for facing purposes)	1949	British Standards Institution
Box 243	SP. 13, 14, 15 & 16 February 1949	Washers for aircraft purposes (primarily for packing purposes)	1949	British Standards Institution
Box 243	SP. 18 & 19 February 1949	Washers for aircraft purposes (primarily for use with timber)	1949	British Standards Institution
Box 243	SP.20. November 1949	Panel type air filter elements for use in internal combustion engines and compressors on aircrafts	1949	British Standards Institution
Box 243	SP. 21. April 1950	Lubrication nipples	1950	British Standards Institution
Box 243	SP. 22-27. June 1950	B. A. Washers	1950	British Standards Institution
Box 243	SP. 28 29, and 30, March 1951	Solid taper pins for aeronautical purposes	1951	British Standards Institution
Box 243	SP. 31 and 32, March 1951	Split taper pins for aeronautical purposes	1951	British Standards Institution
Box 243	SP. 33-39, November 1951	Turnbarrels, tension rods and swaged cable-end connections for aircraft	1956	British Standards Institution
Box 243	SP. 40 May 1951	Rubber grommets for aeronautical purposes	1952	British Standards Institution
Box 243	SP. 41-46 November 1951	Tab washers for aircraft	1951	British Standards Institution
Box 243	SP. 48, September 1952	Plastic s grommets for aeronautical purposes	1952	British Standards Institution
Box 243	SP. 49 and 50, May 1953	Ball ends for swaging on cable	1953	British Standards Institution
Box 243	SP. 51 and 52, May 1953	Identification tags for swaged cabled-end assemblies for aircraft	1953	British Standards Institution
Box 243	SP. 53, June 1953	Swaged cabled-end assemblies (b.and b.s.f. Threads) for preformed and steel wire rope for aircraft	1953	British Standards Institution
Box 243	SP. 54, June 1953	Swaged cabled-end assemblies (b.and b.s.f. Threads) for preformed non-corrodible wire rope for aircraft	1953	British Standards Institution
Box 243	SP. 55 and SP. 56, June 1953	Double coil spring washers for aircraft	1953	British Standards Institution
Box 243	SP. 57 and 58, January 1955	Rivet burrs for aircraft	1955	British Standards Institution
Box 243	SP. 59 and SP. 60, March 1955	Spring catches for aeronautical purposes	1955	British Standards Institution
Box 243	SP. 61 to 64, April 1955	Wood screws for aircraft	1955	British Standards Institution
Box 243	SP. 65, August 1955	Alluminium alloy taper pins	1955	British Standards Institution
Box 243	SP. 66 and SP. 67, August 1955	Cable thimbles for aircraft	1955	British Standards Institution
Box 243	SP. 68 to SP 71 June 1956	100 countersunk precision head aluminium and aluminium alloy rivets for aircraft	1956	British Standards Institution
Box 243	SP. 72 , March 1957	Braided rubber cord assemblies for aircraft	1957	British Standards Institution
Box 243	SP 73 to 75, January 1958	Ferrules and assembly wires for braided rubber cord assemblies for aircraft	1958	British Standards Institution
Box 243	SP. 76. March 1958	Snap head steel rivets	1958	British Standards Institution
Box 243	SP 77 to 80 February 1958	Snap head high nickel-copper alloy rivets aircraft	1958	British Standards Institution
Box 243	SP. 81 and SP. 82, December 1958	Snap head high nickel-copper alloy rivets for aircraft	1958	British Standards Institution
Box 243	SP. 83 to SP. 85, February 1958	Mashroom head aluminium alloy rivets	1958	British Standards Institution
Box 243	SP. 86 March 1959	100 countersunk precision head steel rivets for aircraft	1959	British Standards Institution
Box 243	SP. 87 to SP. 88,March 1959	100 countersunk head high nickel-copper alloy rivets for aircraft	1959	British Standards Institution
Box 243	SP. 89, November 1960	Airframe bearings	1960	British Standards Institution
Box 243	SP. 90, July 1961	Corrosion-resisting steel split cotter pins for aircraft	1961	British Standards Institution
Box 243	SP. 91 and SP. 92 January 1962	Hose clips (worm drive type) for aircraft	1962	British Standards Institution
Box 243	SP. 93 October 1962	Specification for rubber grommets for aeronautical purposes	1962	British Standards Institution
Box 243	SP. 94, March, 1964	Bronze oil retaining bushes and thrust washers for aircraft	1964	British Standards Institution
Box 243	SP. 95 July, 1965	Rubber grommets (neoprene)	1965	British Standards Institution
Box 243	SP. 96, January, 1968	Internal retaining rings	1968	British Standards Institution
Box 243	SP. 107-112, May, 1954	Tab washers for unified hexagons for aircraft	1954	British Standards Institution
Box 243	SP. 113, June, 1954	Cadmium plated close tolerance shear pins for aircraft	1954	British Standards Institution
Box 243	SP. 114, March, 1955	Eye bolts (unified threads) for aircraft	1955	British Standards Institution
Box 243	SP. 115 to 117, March, 1956	Hydraulic surface-check type lubricating nipples for aircraft	1956	British Standards Institution
Box 243	SP. 118, March, 1958	Tie rods (unified threads) for aircraft	1958	British Standards Institution
Box 243	SP. 119 and SP. 120, April, 1957	High tensile steel fork joints (unified threads) for aircraft	1957	British Standards Institution
Box 243	SP. 121, January, 1958	Collars for shear pins for aircraft	1958	British Standards Institution
Box 243	SP. 122 to 125, June, 1958	Washers for unified hexagons for aircraft (primarily for packing purposes)	1958	British Standards Institution
Box 243	SP. 126 and SP. 127, March 1959	Washers for unified hexagons for aircraft (primarily for facing purposes)	1959	British Standards Institution
Box 243	SP.128 to 133, December, 1965	Wood screws for aircraft	1965	British Standards Institution
Box 243	SP. 134 to SP 138, September, 1968	Copper beryllium crinkle washers	1968	British Standards Institution
Box 243	SP. 139 and SP. 140, December, 1969	Corrosion-resisting steel crinkle washers	1969	British Standards Institution
Box 243	SP. 141, March, 1970	Design and performance requirements for toggle type panel fasteners	1970	British Standards Institution
Box 243	SP 142, October, 1970	Solid rivets (with 100 countersunk truncated radiused head made from bs l86 material)	1970	British Standards Institution
Box 243	SP 144-147, April, 1971	Corrosion resisting worm drive clamps for aircraft	1971	British Standards Institution
Box 243	SP 148-50 December, 1970	Unified aluminium alloy washers	1970	British Standards Institution
Box 243	SP 151-53 December, 1970	Unified alloy steel washers	1970	British Standards Institution
Box 243	SP 154-56 December, 1970	Unified corrosion-resistant steel washers	1970	British Standards Institution
Box 243	SP 157-163, March, 1971	Solid rivets (with universal head) made from bs l86 (sp 157 and 163), bs l58 (sp160 and 161), bs l37 (sp 162) and dtd 204 (sp 158 and 159) materials	1971	British Standards Institution
Box 243	SP 164: 1978	Design and performance requirements for turnlock, stud-type panel fasteners (metric series)	1978	British Standards Institution
Box 243	SP 165: 1980 ISO 244-1979	Sealing wire for aircraft	1979	British Standards Institution
Box 243	SP 166: 1982	Spring retaining rings for aerospace application: carbon steel circlips (metric series)	1982	British Standards Institution
Box 243	SP 168-169: October 1974	Ferrules and assembly wires for braided rubber cord assemblies (metric series)	1974	British Standards Institution
Box 243	SP 170-171: October 1974	Braided rubber cord assemblies (metric series)	1974	British Standards Institution
Box 243	2 S.P.1. September, 1927	Shackles	1927	British Standards Institution
Box 243	2 SP. 7. February, 1943	Fork joints	1943	British Standards Institution
Box 243	2 SP. 47, March, 1957	Single coil spring washers for aircraft	1957	British Standards Institution
Box 243	2SP 68 to 2SP 71 : October : 1973	100 countersunk prediction head aluminium and aluminium alloy rivets	1973	British Standards Institution
Box 243	2 SP. 73 and 74, March, 1966	Ferrules and assembly wires for braided rubber cord assemblies for aircraft	1966	British Standards Institution
Box 243	2SP 77 to 2SP 80 : October : 1973	Snap head aluminium and aluminium alloy rivets	1973	British Standards Institution
Box 243	2SP 81 and 2SP 82 : October 1973	Specifications for snap head high nickel-copper alloy rivets	1973	British Standards Institution
Box 243	2SP 83 to 85 : October : 1973	Mashroom and aluminium alloy rivets	1973	British Standards Institution
Box 243	2SP 87 to 2SP 88 : October : 1973	100 countersunk head high nickel-copper alloy rivets	1973	British Standards Institution
Box 243	2 SP.89, March, 1969	Airframe bearings (rolling bearings)	1969	British Standards Institution
Box 243	2SP 91-92, May : 1973	Carbon steel worm drive clamps for aircraft	1973	British Standards Institution
Box 243	2 SP 93: December: 1974	Elastomeric grommets (acrylonitrile-butadiene) for aerospace use	1974	British Standards Institution
Box 243	2 SP 95 December: 1974	Elastomeric grommets (polychloroprene) for aerospace use	1974	British Standards Institution
Box 243	2 SP 96: 1982	Internal retaining rings (imperial sizes)	1982	British Standards Institution
Box 243	2 SP. 101-104, September, 1956	Turnbarrels, tension rods and swaged cable-end connections (unified threads) for aircraft	1956	British Standards Institution
Box 243	2 SP. 105, March, 1955	Swaged cable-3rd assemblies (unified threads) for preformed steel wire rope (w.9) for aircraft	1955	British Standards Institution
Box 243	2 SP. 106, March, 1955	Swaged cable-end assemblies (unified threads) for preformed non-corrodible steel wire rope (w.11) for aircraft	1955	British Standards Institution
Box 243	2Sp 142 and SP 143 : November :1973	Solid rivets with 100 countersunk truncated radiused head made from bs l86 (sp142) and bs l 37 (sp 143) materials	1973	British Standards Institution
Box 243	2 SP 148-150: 1979	Unified aluminium alloy washers	1979	British Standards Institution
Box 243	2 SP 151-153:1979	Unified alloy steel washers	1979	British Standards Institution
Box 243	2 SP 154-156: 1979	Unified corrosion-resistant steel washers	1979	British Standards Institution
Box 243	2 SP 157-163: November: 1973	Solid rivets with universal head made from bs l 86(sp 157 and 163), bs l58 (sp 160 and 161), bs l37 (sp 162) and dtd 204 (sp 158 and 159) materials	1973	British Standards Institution
Box 243	3 SP. 3. February, 1943	Fork joints	1943	British Standards Institution
Box 243	5 SP. 4: 1944	Steel pins	1944	British Standards Institution
Box 244	T.53. May 1948	Specification for 45 ton chrome - molybdenum steel tubes suitable for welding for aircraft purposes	1948	British Standards Institution
Box 244	T. 54. May 1948	Specification for 35 ton steel tubes suitable for welding for aircraft purposes	1948	British Standards Institution
Box 244	T. 55. May 1948	Specification for 35 ton chromium nickel non-corrodible steel tubes (suitable for pipelines) for aircraft purposes	1948	British Standards Institution
Box 244	T. 56. May 1948	Specification for 35 ton chrome - molybdenum steel tubes (suitable for welding) for aircraft purposes	1948	British Standards Institution
Box 244	T. 57. May 1948	Specification for 75 ton nickel chromium steel tubes for aircraft purposes	1948	British Standards Institution
Box 244	T. 58. May 1948	Specification for 50 ton chromium nickel non-corrodible steel tube for aircraft purposes	1948	British Standards Institution
Box 244	T. 59. May 1948	Specification for 50 ton chrome - molybdenum steel tubes (suitable for welding) for aircraft purposes	1948	British Standards Institution
Box 244	T. 60. May 1948	Specification for 75 ton chrome - molybdenum steel tubes (suitable for welding) for aircraft purposes	1948	British Standards Institution
Box 244	T. 61. April 1954	Specification for aircraft material chromium-nickel heat-resisting steel tubes (suitable for welding)	1954	British Standards Institution
Box 244	T. 62. March 1972	Specification for mild steel tube (430 n/mm sq) (weldable)	1972	British Standards Institution
Box 244	T. 63. October 1972	Specification for softened mild steel tube for hydraulic purposes (300 n/mm sq) (suitable for welding)	1972	British Standards Institution
Box 244	T. 64. March 1972	Specification for carbon-manganese steel tube (550 n/mm sq) (tube less than 12.5mm outside diameter) (weldable)	1972	British Standards Institution
Box 244	T. 65, March 1972	Specification for chromium-molybdenum steel tube (880 n/mm sq.) (weldable)	1972	British Standards Institution
Box 244	T. 66, October 1972	Specification for 18/10 chromium-nickel corrosion-resisting steel tube (niobium stabilized: 550 n/mm sq.) (weldable)	1972	British Standards Institution
Box 244	T. 67, October 1972	Specification for 18/10 chromium-nickel corrosion-resisting steel tube (titanium stabilized: 550 n/mm sq.) (weldable)	1972	British Standards Institution
Box 244	T. 68, October 1972	Specification for cold drawn 18/10 chromium-nickel corrosion-resisting steel tube (niobium stabilized: 800 n/mm sq.) (weldable)	1972	British Standards Institution
Box 244	T. 69, October 1972	Specification for cold drawn 18/10 chromium-nickel corrosion-resisting steel tube (titanium stabilized: 800 n/mm sq.) (weldable)	1972	British Standards Institution
Box 244	T. 70, October 1972	Specification for 24/17 chromium-nickel heat-resisting steel tube (niobium stabilized: 550 n/mm sq) (elevated temperature properties not verified) (weldable)	1972	British Standards Institution
Box 244	T. 71, October 1972	Specification for 24/17 chromium-nickel heat-resisting steel tube (titanium stabilized: 550 n/mm sq) (elevated temperature properties not verified) (weldable)	1972	British Standards Institution
Box 244	t. 72- t 73 : 1977	18/10 chromium-nickel corrosion-resisting steel tube for hydraulic purposes (niobium/titanium stabilized: 550 mpa)	1977	British Standards Institution
Box 244	T. 74, October 1972	Specification for low carbon 18/10 chromium-nickel corrosion-resisting steel tube (500n/mm sq.)	1972	British Standards Institution
Box 244	T. 75, October 1972	Specification for low carbon 18/10 chromium-nickel-molybdenum corrosion-resisting steel tube (500n/mm sq.)	1972	British Standards Institution
Box 244	T. 76 : 1978	Chromium-molybdenum steel tube (770mpa) (weldable)	1978	British Standards Institution
Box 244	T. 77 : 1980	Specification for chromium-molybdenum steel tube (900 mpa) (weldable)	1980	British Standards Institution
Box 244	T. 100. June 1948	Inspection and testing procedure for steel tubes for aircraft	1948	British Standards Institution
Box 244	2T.6. May, 1948	Specification for 30 ton mild steel tubes (suitable for welding) for aircraft purposes	1948	British Standards Institution
Box 244	2T.52. November, 1940	Specification for hard drawn phosphor-bronze and phosphorus deoxidised bronze tubes for aircraft purposes	1940	British Standards Institution
Box 244	2T.53, March, 1972	Specification for chromium-molybdenum steel tube (700n/mm sq.) (tube 12.5mm outside diameter and greater) (weldable)	1972	British Standards Institution
Box 244	2T.57, October, 1972	Specification for 4/1 nickel-chromium steel tube (1150 n/mm sq.)	1972	British Standards Institution
Box 244	2T.60, March, 1972	Specification for chromium-molybdenum steel tube (1150 n/mm sq.) (maximum wall thickness 8mm)	1972	British Standards Institution
Box 244	2T66: 1980	Specification for 18/10 chromium-nickel corrosion-resisting steel tube (niobium stabilized: 550 mpa) (weldable)	1980	British Standards Institution
Box 244	2T68: 1980	Specification for cold drawn 18/10 chromium-nickel corrosion-resisting steel tube (niobium stabilized: 800 mpa) (weldable)	1980	British Standards Institution
Box 244	2T.100, April, 1972	Inspection and testing procedure for steel tubes	1972	British Standards Institution
Box 244	3T.1. June, 1942	Specification for 35-ton steel tubes for aircraft purposes	1942	British Standards Institution
Box 244	3T.35. May, 1948	Specification for 35 ton steel tubes (suitable for welding) for aircraft purposes	1948	British Standards Institution
Box 244	3T.45. May, 1948	Specification for 45 ton steel tubes (suitable for welding) for aircraft purposes	1948	British Standards Institution
Box 244	3T.50. May, 1948	Specification for 50 ton steel tubes for aircraft purposes	1948	British Standards Institution
Box 244	3T.51. may, 1945	Specification for aircraft material. High pressure seamless copper tubes	1945	British Standards Institution
Box 244	3T 53: 1980	Specification for chromium-molybdenum steel tube (700 mpa) (outside diameter not less than 12.5mm) (weldable)	1980	British Standards Institution
Box 244	3T60: 1980	Specification for chromium-molybdenum steel tube (1150 mpa) (maximum wall thickness 8mm)	1980	British Standards Institution
Box 244	3T100: 1978	British standard aerospace series: procedure for inspection and testing of steel tubes	1978	British Standards Institution
Box 244	4T.2. May, 1948	Specification for 85 ton nickel chromium steel tubes for aircraft purposes	1948	British Standards Institution
Box 244	4T.26. May, 1948	Specification for 20 ton steel tubes (suitable for welding) for aircraft purposes	1948	British Standards Institution
Box 244	4T.45, March, 1972	Specification for carbon-manganese steel tube (700 n/mm sq.) (tube 12.5mm outside diameter and greater) (weldable)	1972	British Standards Institution
Box 244	4T.47. May, 1939	Specification for brass tubes for honeycomb type radiators for aircraft purposes	1939	British Standards Institution
Box 244	4T.50, March, 1972	Specification for chromium-molybdenum steel tube (700n/mm sq.)		British Standards Institution
Box 244	5T.2, October, 1972	Specification for 4/1 nickel-chromium steel tube (1300 n/mm sq.)	1972	British Standards Institution
Box 244	5T.7. December, 1936	British standard specification for aircraft material. Seamless copper tubes for oil, petrol, gas starters and general purposes	1936	British Standards Institution
Box 244	TA. 1, April, 1968	Specification for commercially pure titanium sheet and strips (tensile strength 19-27 tonf/in squared.) (Suitable for welding)	1968	British Standards Institution
Box 244	TA. 2, April, 1968	Specification for commercially pure titanium sheet and strips (tensile strength 25-35 tonf/in squared.) (Suitable for welding)	1968	British Standards Institution
Box 244	TA. 3, April, 1968	Specification for commercially pure titanium bars for machining (tensile strength 25-35 tonf/in squared.) (Suitable for welding)	1968	British Standards Institution
Box 244	TA. 4, April, 1968	Specification for commercially pure titanium forging stock (tensile strength 25-35 tonf/in squared.) (Suitable for welding)	1968	British Standards Institution
Box 244	TA. 5, April, 1968	Specification for commercially pure titanium forgings (tensile strength 25-35 tonf/in squared.) (Suitable for welding)	1968	British Standards Institution
Box 244	TA. 6, April, 1968	Specification for commercially pure titanium sheet and strips (tensile strength 37-47 tonf/in squared.) (Suitable for welding)	1968	British Standards Institution
Box 244	TA. 7, April, 1968	Specification for commercially pure titanium bars for machining (tensile strength 35-48 tonf/in squared.) (Suitable for welding)	1968	British Standards Institution
Box 244	TA. 8, April, 1968	Specification for commercially pure titanium forging stock (tensile strength 35-48 tonf/in squared.) (Suitable for welding)	1968	British Standards Institution
Box 244	TA. 9, April, 1968	Specification for commercially pure titanium forgings (tensile strength 35-48 tonf/in squared.) (Suitable for welding)	1968	British Standards Institution
Box 244	TA. 10, April, 1968	Specification for titanium-aluminium-vanadium alloy sheets (tensile strength 62-82 tonf/in squared)	1968	British Standards Institution
Box 244	TA. 11, April, 1968	Specification for titanium-aluminium-vanadium alloy bars for machining (tensile strength 58-75 tonf/in squared) (limiting ruling section 6 inches)	1968	British Standards Institution
Box 244	TA. 12, April, 1968	Specification for titanium-aluminium-vanadium alloy forging stock (tensile strength 58-75 tonf/in squared) (limiting ruling section 6 inches)	1968	British Standards Institution
Box 244	TA. 13, April, 1968	Specification for titanium-aluminium-vanadium alloy forgings (tensile strength 58-75 tonf/in squared) (limiting ruling section 6 inches)	1968	British Standards Institution
Box 244	TA. 14, December, 1968	Specification for titanium-aluminium-tin alloy sheets (tensile strength 82-108 hbar)	1968	British Standards Institution
Box 244	TA. 15, December, 1968	Specification for titanium-aluminium-tin alloy bars for machining (tensile strength 79-108 hbar) (limiting ruling section 150 mm) (6 in))	1968	British Standards Institution
Box 244	TA. 16, December, 1968	Specification for titanium-aluminium-tin alloy forging stock (tensile strength 79-108 hbar) (limiting ruling section 150 mm) (6 in))	1968	British Standards Institution
Box 244	TA. 17, December, 1968	Specification for titanium-aluminium-tin alloy forgings (tensile strength 79-108 hbar) (limiting ruling section 150 mm) (6 in))	1968	British Standards Institution
Box 244	TA. 18, December, 1968	Specification for titanium-tin-zirconium-aluminium-molybdenum-silicon alloy bars for machining (tensile strength 111-134 hbar) (limiting ruling section 50 mm) (2 in))	1968	British Standards Institution
Box 244	TA. 19, December, 1968	Specification for titanium-tin-zirconium-aluminium-molybdenum-silicon alloy forging stock (tensile strength 111-134 hbar) (limiting ruling section 50 mm) (2 in))	1968	British Standards Institution
Box 244	TA. 20, December, 1968	Specification for titanium-tin-zirconium-aluminium-molybdenum-silicon alloy forgings (tensile strength 111-134 hbar) (limiting ruling section 50 mm) (2 in))	1968	British Standards Institution
Box 244	TA. 21, December, 1968	Specification for titanium-copper alloy sheets (tensile strength 54-77 hbar)	1968	British Standards Institution
Box 244	TA. 22, December, 1968	Specification for titanium-copper alloy bars for machining (tensile strength 54-77 hbar)	1968	British Standards Institution
Box 244	TA. 23, December, 1968	Specification for titanium-copper alloy forging stock (tensile strength 54-77 hbar)	1968	British Standards Institution
Box 244	TA. 24, December, 1968	Specification for titanium-copper alloy forgings (tensile strength 54-77 hbar)	1968	British Standards Institution
Box 244	TA. 25, December, 1968	Specification for titanium-tin-zirconium-aluminium-molybdenum-silicon alloy bars for machining (tensile strength 103-127 hbar) (limiting ruling section 75 mm) (3 in))	1968	British Standards Institution
Box 244	TA. 26, December, 1968	Specification for titanium-tin-zirconium-aluminium-molybdenum-silicon alloy forging stock (tensile strength 103-127 hbar) (limiting ruling section 75 mm) (3 in))	1968	British Standards Institution
Box 244	TA. 27, December, 1968	Specification for titanium-tin-zirconium-aluminium-molybdenum-silicon alloy forgings (tensile strength 103-127 hbar) (limiting ruling section 75 mm) (3 in))	1968	British Standards Institution
Box 244	TA. 28, December, 1968	Specification for titanium-aluminium-vanadium alloy forging stock (tensile strength 110-130 hbar) (limiting ruling section 19 mm) (3/4 in))	1968	British Standards Institution
Box 244	TA. 29, July, 1969	Specification for titanium-aluminium-molybdenum-tin-silicon alloy bars for machining (tensile strength 114-136 hbar) (limiting ruling section 25 mm) (1 in))	1969	British Standards Institution
Box 244	TA. 30, July, 1969	Specification for titanium-aluminium-molybdenum-tin-silicon alloy forging stock (tensile strength 114-136 hbar) (limiting ruling section 25 mm) (1 in))	1969	British Standards Institution
Box 244	TA. 31, July, 1969	Specification for titanium-aluminium-molybdenum-tin-silicon alloy forgings (tensile strength 114-136 hbar) (limiting ruling section 25 mm) (1 in))	1969	British Standards Institution
Box 244	TA. 32, July, 1969	Specification for titanium-aluminium-molybdenum-tin-silicon alloy bars for machining (tensile strength 105-127 hbar) (limiting ruling section 75 mm) (3 in))	1969	British Standards Institution
Box 244	TA. 33, July, 1969	Specification for titanium-aluminium-molybdenum-tin-silicon alloy forging stock (tensile strength 105-127 hbar) (limiting ruling section 75 mm) (3 in))	1969	British Standards Institution
Box 244	TA. 34, July, 1969	Specification for titanium-aluminium-molybdenum-tin-silicon alloy forgings (tensile strength 105-127 hbar) (limiting ruling section 75 mm) (3 in))	1969	British Standards Institution
Box 244	TA. 35, July, 1969	Specification for titanium-aluminium-molybdenum-tin-silicon alloy bars for machining (tensile strength 100-124 hbar) (limiting ruling section 150 mm) (6 in))	1969	British Standards Institution
Box 244	TA. 36, July, 1969	Specification for titanium-aluminium-molybdenum-tin-silicon alloy forging stock (tensile strength 100-124 hbar) (limiting ruling section 150 mm) (6 in))	1969	British Standards Institution
Box 244	TA. 37, July, 1969	Specification for titanium-aluminium-molybdenum-tin-silicon alloy forgings (tensile strength 100-124 hbar) (limiting ruling section 150 mm) (6 in))	1969	British Standards Institution
Box 244	TA. 38, September, 1971	Specification for bar for machining of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1250-1420 n/mm squared) (limiting ruling section 25 mm)	1971	British Standards Institution
Box 244	TA. 39, September, 1971	Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1250-1420 n/mm squared) (limiting ruling section 25 mm)	1971	British Standards Institution
Box 244	TA. 40, September, 1971	Specification for bar for machining of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 n/mm squared) (limiting ruling section over 25 mm up to and including 75 mm)	1971	British Standards Institution
Box 244	TA. 41, September, 1971	Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 n/mm squared) (limiting ruling section over 25 mm up to and including 75 mm)	1971	British Standards Institution
Box 244	TA. 42, September, 1971	Specification for forgings of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 n/mm squared) (limiting ruling section over 25 mm up to and including 75 mm)	1971	British Standards Institution
Box 244	TA. 43, June, 1972	Specification for forging stock of titanium-aluminium-zirconium-molybdenum-silicon alloy (tensile strength 990-1140 n/mm squared) (limiting ruling section 65 mm)	1972	British Standards Institution
Box 244	TA. 44, June, 1972	Specification for forgings of titanium-aluminium-zirconium-molybdenum-silicon alloy (tensile strength 990-1140 n/mm squared) (limiting ruling section 65 mm)	1972	British Standards Institution
Box 244	TA. 45, February, 1973	Specification for bar and section for machining of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1100-1280 n/mm squared) (limiting ruling section 25 mm)	1973	British Standards Institution
Box 244	TA. 46, February, 1973	Specification for bar for machining of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1050-1220 n/mm squared) (limiting ruling section over 25 mm up to and including 100 mm)	1973	British Standards Institution
Box 244	TA. 47, February, 1973	Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1050-1220 n/mm squared) (limiting ruling section 100 mm)	1973	British Standards Institution
Box 244	TA. 48, February, 1973	Specification for forgings of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1050-1220 n/mm squared) (limiting ruling section 100 mm)	1973	British Standards Institution
Box 244	TA. 49, February, 1973	Specification for bar for machining of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1000-1200 n/mm squared) (limiting ruling section over 100 mm up to and including 150 mm)	1973	British Standards Institution
Box 244	TA. 50, February, 1973	Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1000-1200 n/mm squared) (limiting ruling section over 100 mm up to and including 150 mm)	1973	British Standards Institution
Box 244	TA. 51, February, 1973	Specification for forgings of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1000-1200 n/mm squared) (limiting ruling section over 100 mm up to and including 150 mm)	1973	British Standards Institution
Box 244	TA 52 : April : 1973	Specification for sheet and strip of titanium-copper alloy (tensile strength 690-920 n/mm sq.)	1973	British Standards Institution
Box 244	TA 53 : April : 1973	Specification for bar and section for machining of titanium-copper alloy (tensile strength 650-880 n/mm sq.) (limiting ruling section 75 mm)	1973	British Standards Institution
Box 244	TA 54 : April 1973	Specification for forging stock of titanium-copper alloy (tensile strength 650-880 n/mm sq.) (limiting ruling section 75 mm)	1973	British Standards Institution
Box 244	TA 55: April 1973	Specification for forgings of titanium-copper alloy (tensile strength 650-880 n/mm sq.) (limiting ruling section 75 mm)	1973	British Standards Institution
Box 244	TA 56 : May 1974	Specification of titanium-aluminium-vanadium alloy (tensile strength 895-1150 mpa) (maximum thickness 100 mm)	1974	British Standards Institution
Box 244	TA 57 : May 1974	Specification for titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1030-1220 mpa) (maximum thickness 65 mm)	1974	British Standards Institution
Box 244	TA 58 : May 1974	Specification for plate of titanium-copper alloy (tensile strength 520-640 mpa) (maximum thickness 10 mm)	1974	British Standards Institution
Box 244	TA 59 : 1980	Specification for sheet and strip of titanium-aluminium-vanadium alloy (tensile strength 920-1180 mpa)	1980	British Standards Institution
Box 244	TA 100 : 1967	Inspection and testing procedure for aerospace material wrought titanium and titanium alloys	1967	British Standards Institution
Box 244	2TA 1 : November 1974	Specification for sheet and strip of commercially pure titanium (tensile strength 290-420 mpa)	1974	British Standards Institution
Box 244	2TA 2 : April 1973	Specification for sheet and strip of commercially pure titanium (tensile strength 390-540 n/mm square)	1973	British Standards Institution
Box 244	2TA 3 : April 1973	Specification for bar and section for machining of commercially pure titanium (tensile strength 390-540 n/mm square)	1973	British Standards Institution
Box 244	2TA 4 : April 1973	Specification for forging stock of commercially pure titanium (tensile strength 390-540 n/mm square)	1973	British Standards Institution
Box 244	2TA 5 : April 1973	Specification for forgings of commercially pure titanium (tensile strength 390-540 n/mm square)	1973	British Standards Institution
Box 244	2TA 6 : April 1973	Specification for sheet and strip of commercially pure titanium (tensile strength 570-730 n/mm square)	1973	British Standards Institution
Box 244	2TA 7 : April 1973	Specification for bar and section for machining of commercially pure titanium (tensile strength 540-740 n/mm square)	1973	British Standards Institution
Box 244	2TA 8 : April 1973	Specification for forging stock of commercially pure titanium (tensile strength 540-740 n/mm square)	1973	British Standards Institution
Box 244	2TA 9 : April 1973	Specification for forgings of commercially pure titanium (tensile strength 540-740 n/mm square)	1973	British Standards Institution
Box 244	2TA 10 : May 1974	Specification for sheet and strip of titanium-aluminium-vanadium alloy (tensile strength 960-1270 mpa)	1974	British Standards Institution
Box 244	2TA 11 : May 1974	Specification for bar and section for machining of titanium-aluminium-vanadium alloy (tensile strength 900-1160 mpa) (limiting ruling section 150 mm)	1974	British Standards Institution
Box 244	2TA 12 : May 1974	Specification for forging stock of titanium-aluminium-vanadium alloy (tensile strength 900-1160 mpa) (limiting ruling section 150 mm)	1974	British Standards Institution
Box 244	2TA 13 : May 1974	Specification for forgings of titanium-aluminium-vanadium alloy (tensile strength 900-1160 mpa) (limiting ruling section 150 mm)	1974	British Standards Institution
Box 244	2TA 21 : April 1973	Specification for sheet and strip of titanium-copper alloy (tensile strength 540-770 n/mm square)	1973	British Standards Institution
Box 244	2TA 22 : April 1973	Specification for bar and section of titanium-copper alloy (tensile strength 540-770 n/mm square)	1973	British Standards Institution
Box 244	2TA 23 : April 1973	Specification for forging stock of titanium-copper alloy (tensile strength 540-770 n/mm square)	1973	British Standards Institution
Box 244	2TA 24 : April 1973	Specification for forgings of titanium-copper alloy (tensile strength 540-770 n/mm square)	1973	British Standards Institution
Box 244	2TA 28 : May 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)	1974	British Standards Institution
Box 244	2TA 100 : February 1973	Inspection and testing of wrought titanium and titanium alloys	1973	British Standards Institution
Box 244	V. 35. November, 1947	British standard specification for aircraft material medium and low strength plywood for aircraft purposes	1947	British Standards Institution
Box 244	V. 36, September, 1952	British standard specification for Douglas fir for use in aircraft	1952	British Standards Institution
Box 244	V. 37, September, 1952	British standard specification for Sitka spruce for use in aircraft	1952	British Standards Institution
Box 244	V. 38, December, 1967	British standard: aerospace series specification for Sitka spruce as rough timber	1967	British Standards Institution
Box 244	2 V. 35, September, 1966	British standard specification for plywood for aeronautical purposes	1966	British Standards Institution
Box 244	2 V. 37, February 1968	British standard: aerospace series specification for Sitka spruce as finished timber	1968	British Standards Institution
Box 244	3 V. 4. July, 1929	British standard specification for aircraft material	1929	British Standards Institution
Box 244	5 V. 7, September, 1952	British standard specification for mahogany for use in airscrews	1952	British Standards Institution
Box 244	6 V. 3. July, 1943	British standard specification for aircraft material. High strength plywood for aircraft	1943	British Standards Institution
Box 244	W. 9. September, 1946	British standard specification for aircraft material. Preformed steel wire rope	1946	British Standards Institution
Box 244	W. 10. September, 1946	British standard specification for aircraft material. Non-corrodible steel wire rope (not preformed)	1946	British Standards Institution
Box 244	W. 11. September, 1946	British standard specification for aircraft material. Preformed non-corrodible steel wire rope	1946	British Standards Institution
Box 244	W. 12, January, 1968	British standard: aerospace series specification for preformed galvanized carbon steel wire rope (iso diameters and strengths)	1968	British Standards Institution
Box 244	W 13: September 1973	British standard: aerospace series specification for preformed corrosion-resisting steel wire rope (iso diameters and strengths)	1973	British Standards Institution
Box 244	2 W.9, August, 1965	British standard specification for aircraft material performed galvanized carbon steel wire rope	1965	British Standards Institution
Box 244	2 W.11, February, 1967	British standard specification for aircraft material preformed corrosion-resisting steel wire rope	1967	British Standards Institution
Box 244	3 W. 1. August, 1927	British standard specification for aircraft material high tensile steel wire	1927	British Standards Institution
Box 244	3 W. 6. August, 1927	British standard specification for aircraft flexible steel wire rope for kite balloon cables	1927	British Standards Institution
Box 244	6 W. 2. September, 1946	British standard specification for aircraft material steel wire rope and straining cords (not preformed)	1946	British Standards Institution
Box 244	6 W. 3. October, 1938	Streamline wires (no. 4 b.a. To 1/2 inch b.s.f. Inclusive) for aircraft purposes. Part 1. --steel rod for making streamline wires	1938	British Standards Institution
Box 244	6 W. 8. October, 1938	Tie rods (swaged) for aircraft purposes	1938	British Standards Institution
Box 244	X. 18. July 1921	British standard specification for aircraft material. Shellac varnish	1921	British Standards Institution
Box 244	X. 19. April, 1921	British standard specification for aircraft material. Acid resisting paint	1921	British Standards Institution
Box 244	X. 26, August, 1966	British standard specification for doping and finishing schemes for fabric covered aircraft	1966	British Standards Institution
Box 244	X. 27 November, 1966	British standard specification for cellulose finishing scheme for aeronautical purposes	1966	British Standards Institution
Box 244	X. 28 Novermber, 1966	British standard specification for matt synthetic finishing scheme for aeronautical purposes	1966	British Standards Institution
Box 244	X. 29 November, 1966	British standard specification for high gloss finishing scheme for aeronautical purposes	1966	British Standards Institution
Box 244	X. 30 November, 1966	British standard specification for light-weight aluminium finishing scheme (cellulose base) for aeronautical purposes	1966	British Standards Institution
Box 244	X. 31, January, 1967	British standard specification for low temperature stoving scheme for aeronautical purposes	1967	British Standards Institution
Box 244	2 X.8. December, 1920	British standard specification for aircraft material undercoating propeller varnish. (For use under finishing propeller varnish 2x.12)	1920	British Standards Institution
Box 244	2 X. 11. December, 1920	British standard specification for aircraft material. Transparent woodfiller for propellers	1920	British Standards Institution
Box 244	2 X. 12. December, 1920	British standard specification for aircraft material. Finishing propeller varnish. (For use with the undercoating propeller varnish 2x.8)	1920	British Standards Institution
Box 244	2 X.14. December, 1920	British standard specification for aircraft material. Priming varnish (for use under varnishes 2x.6 and 2x.7)	1920	British Standards Institution
Box 244	2X.17. January, 1924	British standard specification for aircraft material. Seaplane varnish	1924	British Standards Institution
Box 244	2X.18 April, 1965	British standard specification for shellac varnish for aeronautical purposes	1965	British Standards Institution
Box 244	3X. 9. August, 1925	British standard specification for aircraft material. Bituminous paint	1925	British Standards Institution
Box 244	3X. 17 April, 1965	British standard specification for varnish for aeronautical purposes	1965	British Standards Institution