BS 3763(1970) : LATEST

Withdrawn

Withdrawn A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

Publisher: British Standards Institution

Published: 11-23-2012

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Document Type	Standard
Status	Withdrawn
Publisher	British Standards Institution
Pages
ISBN
Superseded By	BS 3763(1976) : LATEST

Standards Referenced By This Book - (Show below) - (Hide below)

BS 3G100-2.3.0(1972) : 1972	SPECIFICATION FOR GENERAL REQUIREMENTS FOR EQUIPMENT FOR USE IN AIRCRAFT - ALL EQUIPMENT - ENVIRONMENTAL CONDITIONS - STANDARD TEST REQUIREMENTS
BS L161(1976) : 1976	SPECIFICATION - HAND AND DIE FORGINGS OF ALUMINIUM-ZINC-MAGNESIUM-COPPER-CHROMIUM ALLOY (SOLUTION TREATED AND ARTIFICIALLY AGED TO AN OVERAGED CONDITION) (ZN 5.6, MG 2.5, CU 1.6, CR 0.22)
BS 4604-2(1970) : 1970	SPECIFICATION FOR THE USE OF HIGH STRENGTH FRICTION GRIP BOLTS IN STRUCTURAL STEELWORK - METRIC SERIES - HIGHER GRADE (PARALLEL SHANK)
BS TA47(1973) : 1973	SPECIFICATION FOR FORGING STOCK OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON ALLOY (TENSILE STRENGTH 1050-1220 N/MM[2]) (LIMITING RULING SECTION 100 MM)
BS L168(1978) : 1978	SPECIFICATION FOR BARS AND EXTRUDED SECTIONS OF ALUMINIUM-COPPER-MAGNESIUM-SILICON-MANGANESE ALLOY (SOLUTION TREATED AND ARTIFICIALLY AGED) (NOT EXCEEDING 200 MM DIAMETER OR MINOR SECTIONAL DIMENSION) (CU 4.4, MG 0.5, SI 0.7, MN 0.8)
BS L165(1978) : 1978	SPECIFICATION FOR SHEET AND STRIP OF ALUMINIUM-COATED ALUMINIUM-COPPER-MAGNESIUM-SILICON-MANGANESE ALLOY (SOLUTION TREATED AND ARTIFICIALLY AGED) (CU 4.4, MG 0.5, SI 0.8, MN 0.8)
BS 3G100-2.2(1972) : 1972	SPECIFICATION FOR GENERAL REQUIREMENTS FOR EQUIPMENT FOR USE IN AIRCRAFT - ALL EQUIPMENT - MAGNETIC INFLUENCE
BS 2L99(1972) : 1972	SPECIFICATION FOR INGOTS AND CASTINGS OF ALUMINIUM-SILICON-MAGNESIUM ALLOY (SOLUTION TREATED AND PRECIPITATION TREATED) (SI 7, MG 0.3)
BS 3G100-2.3.8(1972) : 1972	SPECIFICATION FOR GENERAL REQUIREMENTS FOR EQUIPMENT FOR USE IN AIRCRAFT - ALL EQUIPMENT - ENVIRONMENTAL CONDITIONS - SALT MIST
BS T67(1972) : 1972	SPECIFICATION FOR 18/10 CHROMIUM-NICKEL CORROSION-RESISTING STEEL TUBE (TITANIUM STABILIZED: 550 N/MM[2]) (WELDABLE)
BS TA43(1972) : 1972	SPECIFICATION FOR FORGING STOCK OF TITANIUM-ALUMINIUM-ZIRCONIUM-MOLYBDENUM-SILICON ALLOY (TENSILE STRENGTH 990-1140 N/MM[2]) (LIMITING RULING SECTION 65 MM)
BS TA41(1971) : 1971	SPECIFICATION FOR FORGING STOCK OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON-CARBON ALLOY (TENSILE STRENGTH 1205-1375 N/MM[2]) (LIMITING RULING SECTION OVER 25 MM UP TO AND INCLUDING 75 MM)
BS 2L85(1971) : 1971	SPECIFICATION FOR FORGING STOCK, BARS, EXTRUDED SECTIONS AND FORGINGS OF ALUMINIUM-COPPER-SILICON-MAGNESIUM ALLOY (SOLUTION TREATED AND PRECIPITATION TREATED) (CU 1.5, SI 1, MG 0.8)
BS TA53(1973) : 1973	SPECIFICATION FOR BAR AND SECTION FOR MACHINING OF TITANIUM-COPPER ALLOY (TENSILE STRENGTH 650-880 N/MM[2]) (LIMITING RULING SECTION 75 MM)
BS 2HR503(1973) : 1973	SPECIFICATION FOR NICKEL-CHROMIUM-COBALT-TITANIUM-ALUMINIUM HEAT-RESISTING ALLOY WIRE FOR THREAD INSERTS (0.45 MM TO 2 MM DIAMETER) (NICKEL BASE, CR 19.5, CO 18.0, TI 2.5, AL 1.5)
BS T64(1972) : 1972	SPECIFICATION FOR CARBON-MANGANESE STEEL TUBE (550 N/MM[2]) (TUBE LESS THAN 12.5 MM OUTSIDE DIAMETER) (WELDABLE)
BS L117(1975) : 1975	SPECIFICATION FOR TUBE OF ALUMINIUM-MAGNESIUM-SILICON-COPPER-CHROMIUM ALLOY (SOLUTION TREATED AND ARTIFICIALLY AGED: NOT TESTED HYDRAULICALLY) (NOT EXCEEDING 10 MM THICKNESS) (MG 1.0, SI 0.6, CU 0.28, CR 0.2)
BS 2HR504(1973) : 1973	SPECIFICATION FOR NICKEL-CHROMIUM-TITANIUM HEAT-RESISTING ALLOY BAR, WIRE AND RIVETS (NICKEL BASE, CR 19.5, TI 0.4)
BS L111(1971) : 1971	SPECIFICATION FOR BARS AND EXTRUDED SECTIONS OF ALUMINIUM-MAGNESIUM-SILICON-MANGANESE ALLOY (SOLUTION TREATED AND PRECIPITATION TREATED) (SUITABLE FOR WELDING) (MG 0.8, SI 1, MN 0.7)
BS L119(1975) : 1975	SPECIFICATION FOR INGOTS AND CASTINGS OF ALUMINIUM-COPPER-NICKEL-MANGANESE-TITANIUM-ZIRCONIUM-COBALT-ANTIMONY ALLOY (SOLUTION TREATED AND ARTIFICIALLY AGED) (CU 5.0, NI 1.5, MN 0.25, TI 0.2, ZR 0.2, CO 0.2, SB 0.2)
BS TA52(1973) : 1973	SPECIFICATION FOR SHEET AND STRIP OF TITANIUM-COPPER ALLOY (TENSILE STRENGTH 690-920 N/MM[2])
BS 2TA28(1974) : 1974	SPECIFICATION FOR FORGING STOCK AND WIRE OF TITANIUM-ALUMINIUM-VANADIUM ALLOY (TENSILE STRENGTH 1100-1300 MPA) (LIMITING RULING SECTION 20 MM) (PRIMARILY INTENDED FOR THE MANUFACTURE OF FASTENERS COMPLYING WITH THE REQUIREMENTS OF THE 'A' SERIES OF BRITISH STANDARDS)
BS 2HR401(1973) : 1973	SPECIFICATION FOR NICKEL-CHROMIUM-TITANIUM-ALUMINIUM HEAT-RESISTING ALLOY COLD WORKED AND SOFTENED SEAMLESS TUBES (NICKEL BASE, CR 19.5, TI 2.2, AL 1.4)
BS L514(1973) : 1973	SPECIFICATION FOR FORGING STOCK AND FORGINGS OF MAGNESIUM-3% ZINC-ZIRCONIUM ALLOY (ZN 3.0, ZR 0.6)
BS 4022(1970) : 1970	SPECIFICATION FOR PREFABRICATED GYPSUM WALLBOARD PANELS
BS L118(1975) : 1975	SPECIFICATION FOR TUBE OF ALUMINIUM-MAGNESIUM-SILICON-COPPER-CHROMIUM ALLOY (SOLUTION TREATED AND ARTIFICIALLY AGED: TESTED HYDRAULICALLY) (NOT EXCEEDING 10 MM THICKNESS) (MG 1.0, SI 0.6, CU 0.28, CR 0.2)
BS N4(1974) : 1974	SPECIFICATION FOR FULL FACE MASK ASSEMBLIES FOR USE IN CONTAMINATED ATMOSPHERES
BS TA48(1973) : 1973	SPECIFICATION FOR FORGINGS OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON ALLOY (TENSILE STRENGTH 1050-1200 N/MM[2]) (LIMITING RULING SECTION 100 MM)
BS 3L58(1971) : 1971	SPECIFICATION FOR WIRE FOR SOLID, COLD-FORGED RIVETS OF ALUMINIUM-5% MAGNESIUM ALLOY (NOT EXCEEDING 10 MM DIAMETER)
BS 2T57(1972) : 1972	SPECIFICATION FOR 4/1 NICKEL-CHROMIUM STEEL TUBE (1150 N/MM[2])
BS L167(1978) : 1978	SPECIFICATION FOR CLOSE TOLERANCED SHEET AND STRIP OF ALUMINIUM-COATED ALUMINIUM-COPPER-MAGNESIUM-SILICON-MANGANESE ALLOY (SOLUTION TREATED AND ARTIFICIALLY AGED) (CU 4.4, MG 0.5, SI 0.8, MN 0.8)
BS CP143-12(1970) : 1970	CODE OF PRACTICE FOR SHEET ROOF AND WALL COVERINGS - CODE OF PRACTICE FOR SHEET ROOF AND WALL COVERINGS - COPPER - METRIC UNITS
BS 2TA4(1973) : 1973	SPECIFICATION FOR FORGING STOCK OF COMMERCIALLY PURE TITANIUM (TENSILE STRENGTH 390-540 N/MM[2])
BS 2L87(1971) : 1971	SPECIFICATION FOR HEXAGONAL BARS FOR NUTS, COUPLINGS AND HOLLOW MACHINED PARTS OF ALUMINIUM-COPPER-MAGNESIUM-SILICON-MANGANESE ALLOY (SOLUTION TREATED AND PRECIPITATION TREATED) (FREE FROM PERIPHERAL AND ASYMMETRIC COARSE GRAIN) (NOT LESS THAN 14 MM NOR MORE THAN 36 MM ACROSS FLATS) (CU 4.4, MG 0.5, SI 0.7, MN 0.8)
BS TA57(1974) : 1974	SPECIFICATION FOR PLATE OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON ALLOY (TENSILE STRENGTH 1030-1220 MPA) (MAXIMUM THICKNESS 65 MM)
BS 3L86(1971) : 1971	SPECIFICATION FOR WIRE FOR SOLID, COLD-FORGED RIVETS OF ALUMINIUM-COPPER-MAGNESIUM ALLOY (NOT EXCEEDING 10 MM DIAMETER) (CU 2.5, MG 0.3)
BS 9076 N001-004(1974) : 1974 AMD 3815	DETAIL SPECIFICATION FOR FIXED METALLIZED POLYETHYLENE TEREPHTHALATE (PETP) FILM OR METALLIZED POLYCARBONATE FILM DIELECTRIC CAPACITORS - RECTANGULAR NON-METALLIC CASE AXIAL OR RADIAL TERMINATIONS, CENTRALLY SPACED - FULL ASSESSMENT LEVEL
BS 3G100-2.3.6(1972) : 1972	SPECIFICATION FOR GENERAL REQUIREMENTS FOR EQUIPMENT FOR USE IN AIRCRAFT - ALL EQUIPMENT - ENVIRONMENTAL CONDITIONS - ACCELERATION REQUIREMENTS
BS 4315-2(1970) : 1970	METHODS OF TEST FOR RESISTANCE TO AIR AND WATER PENETRATION - PERMEABLE WALLING CONSTRUCTIONS (WATER PENETRATION)
BS 2A229(1972) : 1972	SPECIFICATION FOR HEXAGONAL HEAD STEEL BOLTS 160000 LBF/IN[2] (1100/MPA)
BS L163(1978) : 1978	SPECIFICATION FOR SHEET AND STRIP OF ALUMINIUM-COATED ALUMINIUM-COPPER-MAGNESIUM-SILICON-MANGANESE ALLOY (SOLUTION TREATED, COLD WORKED FOR FLATTENING AND AGED AT ROOM TEMPERATURE) (CU 4.4, MG 0.5, SI 0.8, MN 0.8)
BS 2HR202(1973) : 1973	SPECIFICATION FOR NICKEL-CHROMIUM-COBALT-TITANIUM-ALUMINIUM HEAT-RESISTING ALLOY SHEET AND STRIP (NICKEL BASE, CR 19.5, CO 18.0, TI 2.5, AL 1.5)
BS T74(1972) : 1972	SPECIFICATION FOR LOW CARBON 18/10 CHROMIUM-NICKEL CORROSION-RESISTING STEEL TUBE (500 N/MM[2])
BS L159(1978) : 1978	SPECIFICATION FOR CLOSE TOLERANCED SHEET AND STRIP OF ALUMINIUM-COPPER-MAGNESIUM-SILICON-MANGANESE ALLOY (SOLUTION TREATED AND ARTIFICIALLY AGED) (CU 4.4, MG 0.5, SI 0.8, MN 0.8)
BS TA42(1971) : 1971	SPECIFICATION FOR FORGINGS OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON-CARBON ALLOY (TENSILE STRENGTH 1205-1375 N/MM[2]) (LIMITING RULING SECTION OVER 25 MM UP TO AND INCLUDING 75 MM)
BS 41(1973) : 1973	SPECIFICATION FOR CAST IRON SPIGOT AND SOCKET FLUE OR SMOKE PIPES AND FITTINGS
BS 2TA3(1973) : 1973	SPECIFICATION FOR BAR AND SECTION FOR MACHINING OF COMMERCIALLY PURE TITANIUM (TENSILE STRENGTH 390-540 N/MM[2])
BS 5T2(1972) : 1972	SPECIFICATION FOR 4/1 NICKEL-CHROMIUM STEEL TUBE (1300 N/MM)
BS 3170(1972) : 1972	SPECIFICATION FOR FLEXIBLE COUPLINGS FOR POWER TRANSMISSION
BS 2TA5(1973) : 1973	SPECIFICATION FOR FORGINGS OF COMMERCIALLY PURE TITANIUM (TENSILE STRENGTH 390-540 N/MM[2])
BS L164(1978) : 1978	SPECIFICATION FOR SHEET AND STRIP OF ALUMINIUM-COATED ALUMINIUM-COPPER-MAGNESIUM-SILICON-MANGANESE ALLOY (SOLUTION TREATED AND AGED AT ROOM TEMPERATURE) (CU 4.4, MG 0.5, SI 0.8, MN 0.8)
BS TA45(1973) : 1973	SPECIFICATION FOR BAR AND SECTION FOR MACHINING OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON ALLOY (TENSILE STRENGTH 1100-1280 N/MM[2]) (LIMITING RULING SECTION 25 MM)
BS 3457(1973) : 1973
BS TA56(1974) : 1974	SPECIFICATION FOR PLATE OF TITANIUM-ALUMINIUM-VANADIUM ALLOY (TENSILE STRENGTH 895-1150 MPA) (MAXIMUM THICKNESS 100 MM)
BS TA38(1971) : 1971	SPECIFICATION FOR BAR FOR MACHINING OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON-CARBON ALLOY (TENSILE STRENGTH 1250-1420 N/MM[2]) (LIMITING RULING SECTION 25 MM)
BS TA54(1973) : 1973	SPECIFICATION FOR FORGING STOCK OF TITANIUM-COPPER ALLOY (TENSILE STRENGTH 650-880 N/MM[2]) (LIMITING RULING SECTION 75 MM)
BS L166(1978) : 1978	SPECIFICATION FOR CLOSE TOLERANCED SHEET AND STRIP OF ALUMINIUM-COATED ALUMINIUM-COPPER-MAGNESIUM-SILICON-MANGANESE ALLOY (SOLUTION TREATED AND AGED AT ROOM TEMPERATURE) (CU 4.4, MG 0.5, SI 0.8, MN 0.8)
BS 3470(1975) : 1975	SPECIFICATION FOR FIELD GATES AND POSTS
BS 2HR502(1973) : 1973	SPECIFICATION FOR NICKEL-CHROMIUM-COBALT-TITANIUM-ALUMINIUM HEAT-RESISTING ALLOY COLD DRAWN AND SOLUTION HEAT TREATED WIRE FOR SPRINGS (NICKEL BASE, CR 19.5, CO 18.0, TI 2.5, AL 1.5)
BS TA50(1973) : 1973	SPECIFICATION FOR FORGING STOCK OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON ALLOY (TENSILE STRENGTH 1000-1200 N/MM[2]) (LIMITING RULING SECTION OVER 100 MM UP TO AND INCLUDING 150 MM)
BS T75(1972) : 1972	SPECIFICATION FOR LOW CARBON 17/12 CHROMIUM-NICKEL-MOLYBDENUM CORROSION-RESISTING STEEL TUBE (500 N/MM[2])
BS L162(1976) : 1976	SPECIFICATION - COLD COMPRESSED HAND FORGINGS OF ALUMINIUM-ZINC-MAGNESIUM-COPPER-CHROMIUM ALLOY (SOLUTION TREATED AND ARTIFICIALLY AGED TO AN OVERAGED CONDITION) (ZN 5.6, MG 2.5, CU 1.6, CR 0.22)
BS 2L98(1971) : 1971	SPECIFICATION FOR PLATE OF ALUMINIUM-COPPER-MAGNESIUM-MANGANESE ALLOY (SOLUTION TREATED AND AGED AT ROOM TEMPERATURE: NOT CONTROLLED STRETCHED) (CU 4.4, MG 1.5, MN 0.6)
BS L158(1978) : 1978	SPECIFICATION FOR CLOSE TOLERANCED SHEET AND STRIP OF ALUMINIUM-COPPER-MAGNESIUM-SILICON-MANGANESE ALLOY (SOLUTION TREATED AND AGED AT ROOM TEMPERATURE) (CU 4.4, MG 0.5, SI 0.8, MN 0.8)
BS L115(1971) : 1971	SPECIFICATION FOR PLATE OF ALUMINIUM-MAGNESIUM-SILICON-MANGANESE ALLOY (SOLUTION TREATED, CONTROLLED STRETCHED AND PRECIPITATION TREATED) (NOT EXCEEDING 25 MM THICKNESS) (SUITABLE FOR WELDING) (MG 0.8, SI 1, MN 0.7)
BS 2HR201(1974) : 1974	SPECIFICATION FOR NICKEL-CHROMIUM-TITANIUM-ALUMINIUM HEAT-RESISTING ALLOY PLATE, SHEET AND STRIP (NICKEL BASE, CR 19.5, TI 2.2, AL 1.4)
BS L515(1973) : 1973	SPECIFICATION FOR SHEET AND STRIP OF MAGNESIUM-11/4% ZINC-ZIRCONIUM ALLOY (SUITABLE FOR WELDING BY INERT-GAS SHIELDED ARC TECHNIQUES) (ZN 1.25, ZR 0.6)
BS 2HR501(1973) : 1973	SPECIFICATION FOR NICKEL-CHROMIUM-COBALT-TITANIUM-ALUMINIUM HEAT-RESISTING ALLOY COLD DRAWN WIRE FOR SPRINGS (NICKEL BASE, CR 19.5, CO 18.0, TI 2 - 5, AL 1.5)
BS L154(1977) : 1977	SPECIFICATION FOR INGOTS AND CASTINGS OF ALUMINIUM-COPPER-SILICON ALLOY (SOLUTION TREATED AND AGED AT ROOM TEMPERATURE) (CU 4, SI 1)
BS CP2012-1(1974) : 1974	CODE OF PRACTICE FOR FOUNDATIONS FOR MACHINERY - FOUNDATIONS FOR RECIPROCATING MACHINES
BS 2HR1(1973) : 1973	SPECIFICATION FOR NICKEL-CHROMIUM-TITANIUM-ALUMINIUM HEAT-RESISTING ALLOY BILLETS, BARS, FORGINGS AND PARTS (NICKEL BASE, CR 19.5, TI 2.2, AL 1.4)
BS L112(1971) : 1971	SPECIFICATION FOR FORGING STOCK AND FORGINGS OF ALUMINIUM-MAGNESIUM-SILICON-MANGANESE ALLOY (SOLUTION TREATED AND PRECIPITATION TREATED) (SUITABLE FOR WELDING) (MG 0.8, SI 1, MN 0.7)
BS T69(1972) : 1972	SPECIFICATION FOR COLD DRAWN 18/10 CHROMIUM-NICKEL CORROSION-RESISTING STEEL TUBE (TITANIUM STABILIZED: 800 N/MM[2]) (WELDABLE)
BS 3G100-2.3.3(1972) : 1972	SPECIFICATION FOR GENERAL REQUIREMENTS FOR EQUIPMENT FOR USE IN AIRCRAFT - ALL EQUIPMENT - ENVIRONMENTAL CONDITIONS - MOULD GROWTH
BS CP1018(1971) : 1971	ELECTRIC FLOOR WARMING SYSTEMS FOR USE WITH OFF-PEAK AND SIMILAR SUPPLIES OF ELECTRICITY
BS TA40(1971) : 1971	SPECIFICATION FOR BAR FOR MACHINING OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON-CARBON ALLOY (TENSILE STRENGTH 1205-1375 N/MM[2]) (LIMITING RULING SECTION OVER 25 MM UP TO AND INCLUDING 75 MM)
BS L155(1977) : 1977	SPECIFICATION FOR INGOTS AND CASTINGS OF ALUMINIUM-COPPER-SILICON ALLOY (SOLUTION TREATED AND ARTIFICIALLY AGED) (CU 4, SI 1)
BS TA55(1973) : 1973	SPECIFICATION FOR FORGINGS OF TITANIUM-COPPER ALLOY (TENSILE STRENGTH 650-880 N/MM[2]) (LIMITING RULING SECTION 75 MM)
BS 9074 N002(1974) : 1974	DETAIL SPECIFICATION FOR FIXED POLYSTYRENE FOIL DIELECTRIC CAPACITORS - TUBULAR INSULATED CASE, AXIAL TERMINATIONS - FULL ASSESSMENT LEVEL
BS 2L83(1971) : 1971	SPECIFICATION FOR FORGING STOCK, BARS, EXTRUDED SECTIONS AND FORGINGS OF ALUMINIUM-COPPER-NICKEL-MAGNESIUM-IRON-SILICON ALLOY (SOLUTION TREATED AND PRECIPITATION TREATED) (CU 2, NI 1, MG 1, SI 0.9, FE 0.9)
BS L109(1971) : 1971	SPECIFICATION FOR ALUMINIUM-COATED SHEET AND STRIP OF ALUMINIUM-COPPER-MAGNESIUM-MANGANESE ALLOY - (SOLUTION TREATED AND AGED AT ROOM TEMPERATURE) (CU 4.4, MG 1.5, MN 0.6)
BS TA39(1971) : 1971	SPECIFICATION FOR FORGING STOCK OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON-CARBON ALLOY (TENSILE STRENGTH 1250-1420 N/MM[2]) (LIMITING RULING SECTION 25 MM)
BS CP143-15(1973) : 1973	CODE OF PRACTICE FOR SHEET ROOF AND WALL COVERINGS - CODE OF PRACTICE FOR SHEET ROOF AND WALL COVERINGS - ALUMINIUM - METRIC UNITS
BS TA44(1972) : 1972	SPECIFICATION FOR FORGINGS OF TITANIUM-ALUMINIUM-ZIRCONIUM-MOLYBDENUM-SILICON ALLOY (TENSILE STRENGTH 990-1140 N/MM[2]) (LIMITING RULING SECTION 65 MM)
BS 4604-1(1970) : 1970	SPECIFICATION FOR THE USE OF HIGH STRENGTH FRICTION GRIP BOLTS IN STRUCTURAL STEELWORK METRIC SERIES - PART 1: GENERAL GRADE
BS TA51(1973) : 1973	SPECIFICATION FOR FORGINGS OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON ALLOY (TENSILE STRENGTH 1000-1200 N/MM[2]) (LIMITING RULING SECTION OVER 100 MM UP TO AND INCLUDING 150 MM)
BS 2L97(1971) : 1971	SPECIFICATION FOR PLATE OF ALUMINIUM-COPPER-MAGNESIUM-MANGANESE ALLOY (SOLUTION TREATED, CONTROLLED STRETCHED AND AGED AT ROOM TEMPERATURE) (CU 4.4, MG 1.5, MN 0.6)
BS CP153-2(1970) : 1970	WINDOWS AND ROOFLIGHTS - WINDOWS AND ROOFLIGHTS - DURABILITY AND MAINTENANCE
BS 2L93(1971) : 1971	SPECIFICATION FOR PLATE OF ALUMINIUM-COPPER-MAGNESIUM-SILICON-MANGANESE ALLOY (SOLUTION TREATED, CONTROLLED STRETCHED AND PRECIPITATION TREATED) (CU 4.4, MG 0.5, SI 0.7, MN 0.8)
BS L513(1973) : 1973	SPECIFICATION FOR FORGING STOCK AND FORGINGS OF MAGNESIUM-6% ALUMINIUM-ZINC ALLOY (AL 6.0, ZN 1.0)
BS TA46(1973) : 1973	SPECIFICATION FOR BAR AND SECTION FOR MACHINING OF TITANIUM-ALUMINIUM-MOLYBDENUM-TIN-SILICON ALLOY (TENSILE STRENGTH 1050-1220 N/MM[2]) (LIMITING RULING SECTION OVER 25 MM UP TO AND INCLUDING 100 MM)
BS 835(1973) : 1973	SPECIFICATION FOR ASBESTOS-CEMENT FLUE PIPES AND FITTINGS, HEAVY QUALITY
BS 2HR2(1973) : 1973	SPECIFICATION FOR NICKEL-CHROMIUM-COBALT-TITANIUM-ALUMINIUM HEAT-RESISTING ALLOY BILLETS, BARS, FORGINGS AND PARTS - (NICKEL BASE, CR 19.5, CO 18.0, TI 2.5, AL 1.5)

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