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BS 350:2004

Current
Current

The latest, up-to-date edition.

Conversion factors for units
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

25-05-2004

Committees responsible
Foreword
1 Scope
2 Number
3 Length
4 Area (length squared)
5 Volume and capacity (length cubed)
6 Modulus of section, first moment of area
7 Second moment of area, or geometrical moment of inertia
8 Plane angle
9 Solid angle
10 Time
11 Linear velocity (speed) (length/time)
12 Angular velocity (angle/time)
13 Frequency (number/time)
14 Acceleration (length/time squared)
15 Mass
16 Mass per unit length (or lineic mass) (formerly linear density)
   (mass/length)
17 Mass per unit area (areic mass) (mass/length squared)
18 Specific surface, or area per unit mass
19 Area per unit capacity
20 Density (volumic mass), (mass/volume)
21 Mass concentration (mass/volume)
22 Specific volume (volume/mass)
23 Mass rate of flow (mass/time)
24 Volume rate of flow (volume/time)
25 Traffic factors
26 Moment of inertia (mass x length squared)
27 Momentum (linear) (mass x velocity)
28 Angular momentum (mass x velocity x length)
29 Force (mass x acceleration)
30 Weight
31 Moment of force, or torque (force x length)
32 Force per unit length (force/length)
33 Pressure (force/area)
34 Stress (force/area)
35 Viscosity, dynamic (stress/velocity gradient)
36 Viscosity, kinematic (length squared/time)
37 Energy (work, heat, etc.)
38 Power (energy/time)
39 Temperature, including temperature difference or interval
40 Specific energy [(energy or heat)/mass]
41 Heat content, volume basis (heat/volume)
42 Specific heat capacity [heat/(mass x temperature interval)]
43 Specific entropy [heat/(mass x thermodynamic temperature)]
44 Heat capacity, volume basis [heat/(volume x temperature interval)]
45 Heat flux density [heat/(area x time)]
46 Thermal conductance (heat transfer coefficient)
47 Thermal conductivity [heat x length/(area x time x temperature
   difference)]
48 Thermal resistivity [area x time x temperature difference/(heat x
   length)]
49 Heat release date (e.g. as used in connection with furnaces)
   [heat/(volume x time)], or (power/volume)
50 Thermal diffusivity (area/time)
Annex A (informative) Commentary on imperial and metric systems
        of measurement and units
Index of symbols and abbreviations
Index of terms
Bibliography

Provides conversion factors for units of measurement for a number of quantities, which are, or have been, in general use in engineering, industry and trade.

This standard provides conversion factors for units of measurement for a number of quantities, which are, or have been, in general use in engineering, industry and trade. The subjects covered are, broadly, metrology, mechanics and heat; the standard does not deal with purely electrical units.

NOTE1 SI units are normally recommended. However, in certain circumstances use of particular units is required by legislation.

NOTE2 Electrical and light units are given in BS5775‑5 and in BS5775‑6, respectively.

NOTE3 A commentary on imperial and metric systems of measurement and units is given in Annex A.

Committee
SS/7
DevelopmentNote
Supersedes BS 350-1(1974) & 03/659657 DC (06/2004) Reviewed and confirmed by BSI, January 2010. (12/2009)
DocumentType
Standard
Pages
112
PublisherName
British Standards Institution
Status
Current
Supersedes

BS L 168:1978 Specification for bars and extruded sections of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and artificially aged) (not exceeding 200 mm diameter or minor sectional dimension) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8)
BS 2TA 1:1974 Specification for sheet and strip of commercially pure titanium (tensile strength 290-420 MPa)
BS 3628:1963 Specification for hose clips (worm drive type) for general purpose use
BS 4622:1970 Specification for grey iron pipes and fittings
BS 4577:1970 Specification for materials for resistance welding electrodes and ancillary equipment
BS 2A 57:1962 Specification for steel hexagonal-headed shear bolts (B.S.F. threads) for aircraft
BS T 67:1972 Specification for 18/10 chromium-nickel corrosion-resisting steel tube (titanium stabilized: 550 N/mm<sup>2</sup>) (weldable)
BS 2S 111:1964 Specification for aircraft material. Nickel-chromium-tungsten valve steel
BS 2C 5:1976 Specification for mating dimensions for liquid oxygen replenishment couplings
BS 2G 199:1984 Schedule for tables relating to altitudes, airspeed and Mach numbers for use in aeronautical instrument design and calibration
BS L 160:1976 Specification. Bars and extruded sections 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 721-1:1963 Specification for worm gearing Imperial units
DEFSTAN 13-99/5(2014) : 2014 REQUIREMENTS FOR DEFENCE MUNITIONS PUBLICATIONS
BS 3S 62:1964 Specification for aircraft material. 12 per cent chromium corrosion-resisting steel (45/55 tonf/sq in: limiting ruling section 6 in)
BS L 117:1975 Specification for tube of aluminium-magnesium-silicon-copper-chromium alloy (solution treated and artificially aged: not tested hydraulically) (not exceeding 10 mm thickness) (Mg 1.0, Si 0.6, Cu 0.28, Cr 0.2)
BS W13(1973) : 1973 AEROSPACE SERIES - SPECIFICATION FOR PREFORMED CORROSION-RESISTING STEEL WIRE ROPE (ISO DIAMETERS AND STRENGTHS)
BS TA 49:1973 Specification for bar and section for machining of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1000-1200 N/mm<sup>2</sup>) (limiting ruling section over 100 mm up to and including 150 mm)
BS HC 404:1977 Specification for chromium-molybdenum alloy cast iron ring pots (suitable for centrifugally cast and sand cast sealing rings, piston rings and cylinder liners)
BS 2HR 2:1973 Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)
BS 787-4:1972 Specification for mining type flameproof gate-end boxes Gate-end boxes for drilling machines (for use on 3-phase a.c. circuits up to 650 V)
BS A266-271(1977) : 1977 AMD 2811 SPECIFICATION FOR 100 DEGREES COUNTERSUNK HEAD TITANIUM ALLOY BOLTS 160000 LBF/IN[2] (1100 MPA) WITH HI-TORQUE SPEED DRIVE RECESSES
BS 2A 61:1962 Specification for aluminium alloy hexagonal headed bolts (B.A. and B.S.F. threads) for aircraft
BS 1202-3:1974 Specification for nails Aluminium nails
BS G 189:1964 Specification for Tersil type electrical cables for aircraft
BS L 110:1971 Specification for aluminium-coated sheet and strip of aluminium-copper-magnesium-manganese alloy (supplied for solution treatment by the user) (Cu 4.4, Mg 1.5, Mn 0.6)
BS AU 26:1964 Specification for towing jaw for use between trailers of 5-16 tons gross weight and towing vehicle
BS 3166:1959 Specification for thermographs (liquid-filled and vapour pressure types) for use within the temperature range -20°F to 220°F ( -30°C to 105°C)
BS 1747-2:1969 Methods for the measurement of air pollution Determination of concentration of suspended matter
BS HC9(1974) : 1974 AEROSPACE SERIES - SPECIFICATION FOR NICKEL-CHROMIUM-MOLYBDENUM STEEL CASTINGS (880-1080 MPA)
BS L 163:1978 Specification for sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy (solution treated, cold worked for flattening and aged at room temperature) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8)
BS 1104:1957 Specification for general purpose Acme screw threads
BS G 209:1970 Specification for transformer rectifier units
BS 2TA 3:1973 SPECIFICATION FOR BAR AND SECTION FOR MACHINING OF COMMERCIALLY PURE TITANIUM (TENSILE STRENGTH 390-540 N/MM[2])
BS 4344:1968 Pulley blocks for use with natural and synthetic fibre ropes
BS HR 403:1973 Specification for nickel-chromium-titanium heat-resisting alloy cold-worked and softened seamless tubes (nickel base, Cr 19.5, Ti 0.4)
BS 5141-2:1977 Specification for air heating and cooling coils Method of testing for rating of heating coils
BS 5T 2:1972 Specification for 4/1 nickel-chromium steel tube (1300 N/mm<sup>2</sup>)
BS 2875:1969 Specification for copper and copper alloys. Plate
BS 2S 129:1976 Specification for 18/9 chromium-nickel corrosion-resisting steel (titanium stabilized) billets, bars, forgings and parts (540 MPa: limiting ruling section 150 mm)
BS SP127(1959) : 1959 WASHERS FOR UNIFIED HEXAGONS FOR AIRCRAFT (PRIMARILY FOR FACING PURPOSES)
BS 2952:1958 Specification for rubber hose for i.c. engine cooling systems
BS 3L 51:1970 Specification for ingots and castings of aluminium-silicon-copper-iron-nickel-magnesium alloy (precipitation treated) (Si 2.5, Cu 1.2, Fe 1, Ni 1, Mg 0.1)
BS L 512:1973 Specification for bars and extruded sections of magnesium-6% aluminium-zinc alloy (not exceeding 150 mm diameter or minor sectional dimension) (Al 6.0, Zn 1.0)
BS TA 54:1973 Specification for forging stock of titanium-copper alloy (tensile strength 650-880 N/mm<sup>2</sup>) (limiting ruling section 75 mm)
BS 1747-1:1969 Methods for the measurement of air pollution Deposit gauges
BS S 156:1976 Specification for 4% nickel-chromium-molybdenum case-hardening steel (vacuum arc remelted) billets, bars, forgings and parts (1320-1520 MPa)
BS 3648:1963 Specification for cycle rear lamps
BS AU 50-1.0d:1998 Tyres and wheels. Tyres General
BS AU 40-4a:1966 Specification for motor vehicle lighting and signalling equipment Sealed beam headlamps
BS 3504:1962 Specification for magnesium-activated nickel for cathodes of electronic tubes and valves
BS 3L 124:1970 Specification for ingots and castings of magnesium - 10% aluminium-zinc-manganese alloy (solution treated) (Al 10, Zn 0.5, Mn 0.3)
BS HR 6:1972 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)
BS SP 118:1958 Tie rods (Unified threads) for aircraft
BS A 232:1968 Specification for 100° countersunk head steel bolts (160 000 lbf/in<sup>2</sup> (110 hbar) with Torq-set recesses)
BS 3575:1963 Specification for rivets for the attachment of friction linings
BS 4438:1969 Specification for filing cabinets and suspended filing pockets
BS 3273:1960 Specification for distant indicating thermometers for ships\' refrigerated cargo spaces
BS 2A175(1962) : 1962 SPECIFICATION FOR 100 DEGREE COUNTERSUNK HEAD ALUMINIUM ALLOY BOLTS (UNIFIED THREADS) FOR AIRCRAFT
BS 4S 106:1976 Specification. 3% chromium-molybdenum steel billets, bars, forgings and parts (930-1080 MPa: limiting ruling section 150 mm) (suitable for nitriding)
BS HC 2:1973 Specification for carbon-manganese steel castings (550 N/mm<sup>2</sup>)
BS 2G 196:1971 Specification for static invertors
BS G 102:1971 Specification for general requirements for rotating electrical machinery
BS L 109:1971 Specification for aluminium-coated sheet and strip of aluminium-copper-magnesium-manganese alloy (solution treated and aged at room temperature) (Cu 4.4, Mg 1.5, Mn 0.6)
BS 2C 4:1973 Specification for coupling dimensions for aero-engine refrigerant pressure replenishment connections
BS 4183:1967 Specification for machine screws and machine screw nuts. Metric series
BS TA 39:1971 Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1250-1420 N/mm<sup>2</sup>) (limiting ruling section 25 mm)
BS HC105(1974) : 1974 AEROSPACE SERIES - SPECIFICATION FOR 18% CHROMIUM-11% NICKEL-2.5% MOLYBDENUM NIOBIUM-STABILIZED CORROSION-RESISTING STEEL CASTINGS (500 MPA)
BS 2569-2:1965 Specification for sprayed metal coatings Protection of iron and steel against corrosion and oxidation at elevated temperatures.
BS G184-G188(1964) : 1964 AMD 4738 SPECIFICATION FOR ALUMINIUM TERMINAL ENDS AND IN LINE CONNECTORS FOR HEXAGONAL CRIMPING TO AIRCRAFT ALUMINIUM ELECTRICAL CABLES
BS S 139:1968 Specification for 1½ per cent nickel-chromium-molybdenum steel (110/130 kgf/mm<sup>2</sup> (70/83 tonf/in<sup>2</sup>): limiting ruling section 70 mm (2¾ in))
BS HR 650:1972 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, V 0.3) (limiting ruling section 20 mm)
BS A 227:1965 Specification for steel pan head bolts (short thread: Class 3A)
BS TA 45:1973 Specification for bar and section for machining of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1100-1280 N/mm<sup>2</sup>) (limiting ruling section 25 mm)
BS 2S 146:1976 Specification for 4% nickel-chromium-molybdenum air-hardening steel (vacuum arc remelted) billets, bars, forgings and parts (1760-1960 MPa: limiting ruling section 100 mm)
BS 4337:1968 Specification for principal dimensions of hand-operated stillage trucks
BS G 203:1967 Specification for Unified screws with captive facing and locking washers
BS G 211:1971 Specification for reflection-reducing coating of instrument windows and lighting wedges
BS 3G 100-2.3.0:1972 Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Standard test requirements
BS L 161:1976 Specification. Hand and die forgings of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and artificially aged to an overaged condition) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.22)
BS TA 47:1973 Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1050-1220 N/mm<sup>2</sup>) (limiting ruling section 100 mm)
BS 3520:1962 Specification for dental wrought precious metal alloy wire
BS TA 41:1971 Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 N/mm<sup>2</sup>) (limiting ruling section over 25 mm up to and including 75 mm)
BS HR 204:1972 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)
BS HC 7:1974 Specification for 3% chromium-molybdenum steel castings (880-1080 MPa)
BS 46-1:1958 Keys and keyways and taper pins Specification. Keys and keyways
BS AU 146b:1970 Specification for standard automatic roller-type coupling for semi-trailers not exceeding 7¼ tons laden weight
BS 4082-2:1969 Specification for external dimensions for vertical in-line centrifugal pumps \'U\' Type
BS 248:1969 Specification for light rails and fishplates for use at mines
BS 2S 124:1964 Specification for aircraft material. 12 per cent chromium corrosion-resisting steel (free machining) (45/55 tonf/sq in: limiting ruling section 6 in)
BS HC 106:1974 Specification for precipitaton hardening chromium-nickel-copper corrosion-resisting steel castings (1250-1500 MPa) (Cr 16, Ni 4, Cu 3)
BS 4F 33:1961 Specification for flexible cotton rope for aeronautical purposes
BS 3T 60:1980 Specification for chromium-molybdenum steel tube (1150 MPa) (maximum thickness 8 mm)
BS G 154:1958 Screws with captive washers for aircraft
BS 2T 57:1972 Specification for 4/1 nickel-chromium steel tube (1150 N/mm<sup>2</sup>)
BS 2G 135:1967 Specification for electrically-heated pitot and pitotstatic pressure heads
BS HC 205:1974 Specification for precipitation hardening nickel base chromium-cobalt-molybdenum-titanium alloy castings (Cr 20, Co 20, Mo 6, Ti 2)
BS L 167:1978 Specification for close toleranced sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy (solution treated and artificially aged) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8)
BS 4A 4-1.2:1967 Specification for test pieces and test methods for metallic materials. Tensile tests Tensile tests - elevated temperature. Metric units
BS 5S 21:1964 Specification for aircraft material. \'20\' carbon steel (suitable for welding) (25/35 tonf/sq in: maximum size 6 inches diameter or minor sectional dimension)
BS 1202-2:1974 Specification for nails Copper nails
BS HC 402:1977 Specification for cast iron ring pots (centrifugally cast) (suitable for piston rings up to 200 mm in diameter)
BS 2TA 6:1973 Specification for sheet and strip of commercially pure titanium (tensile strength 570-730 N/mm<sup>2</sup>)
BS 2G 147-2:1966 Specification for a.c. motors for aircraft Three-phase variable frequency squirrel-cage induction motors
BS 2A 174:1962 Specification for 100° countersunk head corrosion-resisting steel bolts (Unified threads) for aircraft
BS 3A107(1962) : 1962 SPECIFICATION FOR ALUMINIUM ALLOY NUTS (UNIFIED HEXAGONS AND UNIFIED THREADS) (ORDINARY AND SLOTTED) FOR AIRCRAFT
BS 3544:1962 Methods of test for polyvinyl acetate adhesives for wood
DEFSTAN 13-99/4(2010) : 2010 REQUIREMENTS FOR DGM IPT MUNITIONS TECHNICAL PUBLICATIONS
BS AU 30b:1970 Specification for standard automatic roller-type coupling for semi-trailers of 7 tons to 14¾ tons laden weight
BS AU 29:1964 Specification for drawbar eyes and forecarriage pins for connection between trailers of 5-35 tons gross weight and towing vehicle
BS C 3:1964 Specification for aircraft material. Coupling dimensions for aircraft pressure re-oiling connection
BS 3A 108:1962 Specification for steel bolts (Unified hexagons and Unified threads) with close tolerance shanks for aircraft
BS 3241:1960 Specification for toughened polystyrene for sheet extrusion
BS HR 203:1972 Specification for nickel-chromium-titanium heat-resisting alloy plate, sheet and strip (nickel base, Cr 19.5, Ti 0.4)
BS S 138:1967 Specification for 3 per cent chromium-molybdenum-vanadium steel (vacuum remelted - air hardening) (157 kgf/mm<sup>2</sup> (100 tonf/in<sup>2</sup>): limiting ruling section 30 mm (1⅛ in))
BS AU 27:1964 Specification for towing hook for use between trailers of 5-35 tons gross weight and towing vehicle
BS 3551:1962 Specification for alloy steel shackles
BS AU 25:1964 Specification for towing hook for use between trailers of 5-14 tons gross weight and towing vehicle
BS TA 56:1974 Specification for plate of titanium-aluminium-vanadium alloy (tensile strength 895-1150 MPa) (maximum thickness 100 mm)
BS G 176-1:1960 Specification for cartridge fuses for aircraft General requirements
BS 3231:1960 Specification for thermographs (bimetallic type) for air temperatures within the range 0°F to 140°F (-20°C to 60°C)
BS M 33:1970 Specification for dimensions of elastomeric toroidal sealing rings (inch series) to Class 1 tolerances for aircraft
BS TA 38:1971 Specification for bar for machining of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1250-1420 N/mm<sup>2</sup>) (limiting ruling section 25 mm)
BS 3401:1961 Specification for beryllium copper crinkle washers
BS 3664:1963 Specification for film badges for personnel radiation monitoring
BS 5141-1:1975 Specification for air heating and cooling coils Method of testing for rating of cooling coils
BS 3G 100-2.3.2:1970 Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Temperature-pressure requirements
BS 2S 93:1964 Specification for aircraft material. \'40\' carbon steel (normalized) (35/45 tonf/sq in: limiting ruling section 6 in)
BS L 158:1978 Specification for close toleranced sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8)
BS 3226:1960 Specification for thimbles for natural fibre ropes
BS L 115:1971 Specification for plate of aluminium-magnesium-silicon-manganese alloy (solution treated, controlled stretched and precipitation treated) (not exceeding 25 mm thickness) (suitable for welding) (Mg 0.8, Si 1, Mn 0.7)
BS 2A 60:1962 Specification for cadmium-plated steel hexagonal-headed shear bolts (B.S.F. threads) for aircraft
BS 2A 230:1974 Specification for 100° countersunk head steel bolts [1100 MPa with Hi-torque speed drive recesses]
BS 4345:1968 Specification for slotted angles
BS T 72-T 73:1977 Specifications for 18/10 chromium-nickel corrosion-resisting steel tube for hydraulic purposes (niobium/titanium stabilized: 550 MPa)
BS L 154:1977 Specification for ingots and castings of aluminium-copper-silicon alloy (solution treated and aged at room temperature) (Cu 4, Si 1)
BS AU 28:1964 Specification for towing jaw for use between trailers of 5-35 tons gross weight and towing vehicle
BS G 212:1971 Specification for general requirements for aircraft electrical cables
BS 3509:1962 Specification for spirit level vials
BS 3177:1959 Method for determining the permeability to water vapour of flexible sheet materials used for packaging
BS 3G 100-2.3.8:1972 Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Salt mist
BS 3A 171:1962 Specification for aluminium alloy pan head bolts (Unified threads) for aircraft
BS HC 301:1973 Specification for cobalt base chromium-nickel-tungsten alloy castings (Cr 25.5, Ni 10.5. W 7.5)
BS 874-1:1986 Methods for determining thermal insulating properties Introduction, definitions and principles of measurement
BS G 175:1959 Aircraft fuel nozzle grounding plugs and sockets
BS TA 51:1973 Specification for forgings of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1000-1200 N/mm<sup>2</sup>) (limiting ruling section over 100 mm up to and including 150 mm)
BS HC 206:1975 Specification for precipitation hardening nickel base chromium-cobalt-molybdenum-titanium alloy precision castings (Cr 20, Co 20, Mo 6, Ti 2)
BS G 195:1966 Specification for Minyvin type electric cables for aircraft
BS 3929:1965 Specification for domestic solid fuel ignition pokers and portable undergrate ignition burners for use with commercial butane
BS 327:1964 Specification for power-driven derrick cranes
BS 2S 147:1976 Specification for 0.5% nickel-chromium-molybdenum steel bars for the manufacture of forged bolts and forged nuts
BS 1432:1987 Specification for copper for electrical purposes: high conductivity copper rectangular conductors with drawn or rolled edges
BS 3146-1:1974 Specification for investment castings in metal Carbon and low alloy steels
BS 1806:1989 Specification for dimensions of toroidal sealing rings (\'O\'-rings) and their housings (inch series)
BS 3146-2:1975 Specification for investment castings in metal Corrosion and heat resisting steels, nickel and cobalt base alloys
BS 3692:1967 Specification for ISO metric precision hexagon bolts, screws and nuts. Metric units
BS 3698:1964 Specification for calcium plumbate priming paints
BS 2F 52:1959 Flax reinforcement webbing for aeronautical purposes
BS S 141:1968 Specification for 12 per cent chromium corrosion-resisting steel (60/80 kgf/mm<sup>2</sup> (38/51 tonf/in<sup>2</sup>): limiting ruling section 150 mm (6in))
BS 2HR 503:1973 Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy wire for thread inserts (0.45 mm to 2 mm diameter) (nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)
BS 2A 26:1962 Specification for corrosion-resisting steel hexagonal-headed bolts (B.A and B.S.F. threads) for aircraft
BS 3594-1:1963 Specification for pipe wrenches Stillson type wrenches
BS T 64:1972 Specification for carbon-manganese steel tube (550 N/mm<sup>2</sup>) (tube less than 12.5 mm outside diameter) (weldable)
BS S 151:1975 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)
BS 4A 116:2012 Steel pan head bolts (Unified threads), cadmium plated, for aircraft
BS G 177:1961 Specification for Nyvin type electrical cables for aircraft
BS 2S 114:1964 Specification for aircraft material. Manganese-molybdenum steel (55/65 tonf/sq in: limiting ruling section 2½ inches)
BS TA 52:1973 Specification for sheet and strip of titanium-copper alloy (tensile strength 690-920 N/mm<sup>2</sup>)
BS 2A 58:1962 Specification for steel hexagonal nuts (B.S.F. threads) for shear bolts for aircraft
BS 3594-2:1965 Specification for pipe wrenches Footprint type wrenches
BS T 77:1980 Specification for chromium-molybdenum steel tube (900 MPa) (weldable)
BS 3649:1963 Recommendations for original printing plates
BS HC 403:1977 Specification for high chromium alloy cast iron ring pots (centrifugally cast) (suitable for piston rings up to 400 mm in diameter)
BS 2TA 28:1974 Specification for forging stock and wire of titanium-aluminium-vanadium alloy (tensile strength 1100-1300 MPa) (limiting ruling section 20 mm) (primarily intended for the manufacture of fasteners complying with the requirements of the \'A\' series of British Standards)
BS 4A 4-1.3:1967 Specification for test pieces and test methods for metallic materials. Tensile tests Uninterrupted creep and rupture tests. Metric units
BS 2HR 401:1973 Specification for nickel-chromium-titanium-aluminium heat-resisting alloy cold worked and softened seamless tubes (nickel base, Cr 19.5, Ti 2.2, Al 1.4)
BS 2A 210:1962 Specification for brass nuts (Unified hexagons and Unified threads) for aircraft
BS HR 4:1972 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)
BS G 192:1965 Specification for Efglas type electric cables with copper conductors for aircraft
BS A 226:1965 Specification for steel hexagon head bolts (short thread: Class 3A)
BS SP 76:1958 Snap head steel rivets for aircraft
BS TA 48:1973 Specification for forgings of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1050-1200 N/mm<sup>2</sup>) (limiting ruling section 100 mm)
BS 3L 58:1971 Specification for wire for solid, cold-forged rivets of aluminium-5% magnesium alloy (not exceeding 10 mm diameter)
BS HR 251:1974 Specification for heat-resisting 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)
BS 3G 100-2.3.6:1972 Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Acceleration requirements
BS 2A 229:1972 Specification for hexagonal head steel bolts 160000 lbf/in<sup>2</sup> (1100/MPa)
BS 2799:1974 Specification for power-driven tower cranes for building and engineering construction
BS G 174:1959 Invertors for secondary electrical supplies for aircraft
BS 2L 77:1971 Specification for forging stock and forgings of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and precipitation treated) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8)
BS G 200:1967 Specification for miniature lever-operated manual switches
BS S 126:1964 Specification for aircraft material. 23/14 chromium-nickel heat-resisting steel (niobium stabilized) (35 tonf/sq in: limiting ruling section 6 in)
BS N 4:1974 SPECIFICATION FOR FULL FACE MASK ASSEMBLIES FOR USE IN CONTAMINATED ATMOSPHERES
BS L 114:1971 Specification for tube of aluminium-magnesium-silicon-manganese alloy (solution treated and precipitation treated) (not exceeding 10 mm wall thickness) (suitable for welding) (Mg 0.8, Si 1, Mn 0.7)
BS TA 42:1971 Specification for forgings of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 N/mm<sup>2</sup>) (limiting ruling section over 25 mm up to and including 75 mm)
BS AU 91:1965 Specification for dimensions of electrical cable connectors for starter battery taper terminal posts (cars and light commercial vehicles using positive earth system)
BS HC 401:1974 Specification for 18% nickel maraging steel precision castings (1600-1850 MPa)
BS 3770:1964 Specification for zinc naphthenate and zinc naphthenate concentrates
BS 950-2:1967 Specification for artificial daylight for the assessment of colour Viewing conditions for the graphic arts industry
BS 3813-1:1964 Specification for incinerators for waste from trade and residential premises Capacities between 50 lb/h and 1000 lb/h
BS L 113:1971 Specification for sheet and strip of aluminium-magnesium-silicon-manganese alloy (solution treated and precipitation treated) (suitable for welding) (Mg 0.8, Si 1, Mn 0.7)
BS M 34:1970 Method of preparation and use of radiographic techniques
BS 2S 92:1964 Specification for aircraft material. Carbon-manganese steel (suitable for welding) (40/55 tonf/sq in: limiting ruling section 4 in)
BS 2SP81&2SP82(1973) : 1973 SPECIFICATION FOR SNAP HEAD HIGH NICKEL-COPPER ALLOY RIVETS
BS 2HR 502:1973 Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy cold drawn and solution heat treated wire for springs (nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)
BS 3A 116:1962 Specification for steel pan head bolts (Unified threads) for aircraft
BS T 75:1972 Specification for low carbon 17/12 chromium-nickel-molybdenum corrosion-resisting steel tube (500 N/mm<sup>2</sup>)
BS 196:1961 Specification for protected-type non-reversible plugs, socket-outlets cable-couplers and appliance-couplers with earthing contacts for single phase a.c. circuits up to 250 volts
BS TA 50:1973 Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1000-1200 N/mm<sup>2</sup>) (limiting ruling section over 100 mm up to and including 150 mm)
BS 2G 127:1967 Specification for power and current transformers for use in aircraft electrical power supply systems
BS L 162:1976 Specification. Cold compressed hand forgings of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and artificially aged to an overaged condition) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.22)
BS 2A 29:1962 Specification for aluminium alloy hexagonal nuts (B.A and B.S.F. threads) (ordinary and slotted) for aircraft
BS 2L 98:1971 Specification for plate of aluminium-copper-magnesium-manganese alloy (solution treated and aged at room temperature: not controlled stretched) (Cu 4.4, Mg 1.5, Mn 0.6)
BS S 158:1977 Specification for 1% chromium-molybdenum steel bars for the manufacture of forged bolts and forged nuts
BS 2HR 501:1973 Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy cold drawn wire for springs (nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)
BS 2S 113:1964 Specification for aircraft material. \'40\' carbon steel bright bars for machining (45-55 tonf/sq in: limiting ruling section 1 inch) (primarily intended for the manufacture of nuts)
BS SP 90:1961 Specification for corrosion-resisting steel split cotter pins for aircraft
BS 3547:1962 Specification for electrically-heated food conveyors and carriers
BS 3769:1964 Specification for copper naphthenate and copper naphthenate concentrates
BS C 16:1973 Specification for dimensions for gaseous oxygen replenishment couplings for aircraft
10/30212959 DC : 0 BS A 400 - SPECIFICATION FOR CORROSION-RESISTING STEEL NUTS, PLAIN AND SLOTTED (UNIFIED HEXAGONS AND UNIFIED THREADS) FOR SHEAR BOLTS FOR AIRCRAFT
BS 2S 98:1964 Specification for aircraft material. 2½ per cent nickel-chromium-molybdenum steel (high carbon) (75/85 tonf/sq in: limited ruling section 6 in)
BS CP118(1969) : 1969 AMD 1129 THE STRUCTURAL USE OF ALUMINIUM
BS 2TA 4:1973 Specification for forging stock of commercially pure titanium (tensile strength 390-540 N/mm<sup>2</sup>)
BS 4082-1:1969 Specification for external dimensions for vertical in-line centrifugal pumps \'I\' Type
BS 4001-2:1967 Care and maintenance of underwater breathing apparatus Standard diving equipment
BS HC 3:1973 Specification for 1% chromium-molybdenum low alloy steel castings (700 N/mm<sup>2</sup>)
BS 419:1966 Specification for varnished fabrics and tapes for electrical purposes
BS 2TA 2:1973 Specification for sheet and strip of commercially pure titanium (tensile strength 390-540 N/mm<sup>2</sup>)
BS 4954-2:1978 Methods for testing and rating induction units for air distribution systems Acoustic testing and rating
BS 2S 131:1977 Specification for high thermal expansion steel billets, bars, forgings and parts (620 MPa: limiting ruling section 150 mm)
BS HR 404:1973 Specification for nickel-cobalt-chromium-molybdenum-titanium-aluminium heat-resisting alloy cold worked solution treated seamless tubes (nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.1, Al 0.5)
BS 10:1962 Specification for flanges and bolting for pipes, valves, and fittings
BS 778:1966 Specification for steel pipes and joints for hydraulic purposes
DEFSTAN 13-99/1(2009) : 2009 REQUIREMENTS FOR DGM IPT MUNITIONS TECHNICAL PUBLICATIONS
BS 3518-2:1962 Methods of fatigue testing Rotating bending fatigue tests
DEFSTAN 13-99/3(2010) : 2010 REQUIREMENTS FOR DGM IPT MUNITIONS TECHNICAL PUBLICATIONS
BS 2SP87&2SP88(1973) : 1973 AEROSPACE SERIES - 100 DEGREES COUNTERSUNK HEAD HIGH NICKEL-COPPER ALLOY RIVETS
BS HC8(1974) : 1974 AEROSPACE SERIES - SPECIFICATION FOR 3% CHROMIUM-MOLYBDENUM STEEL CASTINGS (1150-1300 MPA)
BS A101(1969) : 1969 GENERAL REQUIREMENTS FOR TITANIUM BOLTS
BS HR 51:1973 Specification for heat-resisting alloy billets, bars, forgings and parts (Ni 25.5, Cr 14.7, Ti 2, Mn 1.5, Mo 1.2, Si 0.7, V 0.3, Fe remainder)
BS 10:2009 Specification for flanges and bolting for pipes, valves and fittings
BS 2S 130:1976 Specification for 18/9 chromium-nickel corrosion-resisting steel (niobium stabilized) billets, bars, forgings and parts (540 MPa: limiting ruling section 150 mm)
BS 2L 83:1971 Specification for forging stock, bars, extruded sections and forgings of aluminium-copper-nickel-magnesium-iron-silicon alloy (solution treated and precipitation treated) (Cu 2, Ni 1, Mg 1, Si 0.9, Fe 0.9)
BS 2L 97:1971 Specification for plate of aluminium-copper-magnesium-manganese alloy (solution treated, controlled stretched and aged at room temperature) (Cu 4.4, Mg 1.5, Mn 0.6)
BS SP94(1964) : 1964 BRONZE OIL-RETAINING BUSHES AND THRUST WASHERS - FOR AIRCRAFT
BS 2L 127:1970 Specification for ingots and castings of magnesium-zinc-zirconium alloy (precipitation treated) (Zn 4.5, Zr 0.7)
BS 2L 126:1970 Specification for ingots and castings of magnesium-cerium-zinc-zirconium alloy (precipitation treated) (rare earth metals 3.0, Zn 2.3, Zr 0.6)
BS A 400:2010 Specification for nuts, plain and slotted (unified hexagons and unified threads) for shear bolts for aircraft in corrosion-resisting steel
BS 3037-1:1958 Specification for tyres for crane rail wheels Double-flanged parallel-tread tyres
BS G 207:1969 Specification for aircraft electrical circuit diagrams
BS L 165:1978 Specification for sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy (solution treated and artificially aged) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8)
BS 3G 100-2.2:1972 Specification for general requirements for equipment for use in aircraft. All equipment Magnetic influence
BS 2L 99:1972 Specification for ingots and castings of aluminium-silicon-magnesium alloy (solution treated and precipitation treated) (Si 7, Mg 0.3)
BS TA 43:1972 Specification for forging stock of titanium-aluminium-zirconium-molybdenum-silicon alloy (tensile strength 990-1140 N/mm<sup>2</sup>) (limiting ruling section 65 mm)
BS HR 53:1973 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)
BS 2S 117:1964 Specification for aircraft material. 1 per cent chromium steel (55/65 tonf/sq in: limiting ruling section 1⅛ inch)
BS 2S 112:1964 Specification for aircraft material. Semi-free cutting carbon steel, bright bars for machining (40-50 tonf/sq in: maximum size ½ inch diameter or minor sectional dimension) (primarily intended for the manufacture of nuts)
BS 11:1959 Flat bottom railway rails
BS 2L 85:1971 Specification for forging stock, bars, extruded sections and forgings of aluminium-copper-silicon-magnesium alloy (solution treated and precipitation treated) (Cu 1.5, Si 1, Mg 0.8)
BS TA 53:1973 Specification for bar and section for machining of titanium-copper alloy (tensile strength 650-880 N/mm<sup>2</sup>) (limiting ruling section 75 mm)
BS 2HR 504:1973 Specification for nickel-chromium-titanium heat-resisting alloy bar, wire and rivets (nickel base, Cr 19.5, Ti 0.4)
BS 4430-2:1969 Recommendations for the safety of powered industrial trucks Operation and maintenance
BS M 32:1969 Specification for dimensions of aircraft accessory drives and mounting pads
BS L 111:1971 Specification for bars and extruded sections of aluminium-magnesium-silicon-manganese alloy (solution treated and precipitation treated) (suitable for welding) (Mg 0.8, Si 1, Mn 0.7)
BS L 119:1975 Specification for ingots and castings of aluminium-copper-nickel-manganese-titanium-zirconium-cobalt-antimony alloy (solution treated and artificially aged) (Cu 5.0, Ni 1.5, Mn 0.25, Ti 0.2, Zr 0.2, Co 0.2, Sb 0.2)
BS SP139 & SP140(1969) : 1969 AEROSPACE SERIES - SPECIFICATION FOR CORROSION-RESISTING STEEL CRINKLE WASHERS
BS L 118:1975 Specification for tube of aluminium-magnesium-silicon-copper-chromium alloy (solution treated and artificially aged: tested hydraulically) (not exceeding 10 mm thickness) (Mg 1.0, Si 0.6, Cu 0.28, Cr 0.2)
BS TA 57:1974 Specification for plate of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1030-1220 MPa) (maximum thickness 65 mm)
BS C 9:1970 Specification for coupling dimensions for high pressure air charging valves for aircraft
BS 3L 86:1971 Specification for wire for solid, cold-forged rivets of aluminium-copper-magnesium alloy (not exceeding 10 mm diameter) (Cu 2.5, Mg 0.3)
BS HR 240:1972 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)
BS 2L 87:1971 Specification for hexagonal bars for nuts, couplings and hollow machined parts of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and precipitation treated) (free from peripheral and asymmetric coarse grain) (not less than 14 mm nor more than 36 mm across flats) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8)
BS HC 1:1973 Specification for carbon steel castings (500 N/mm<sup>2</sup>)
BS 2930:1970 Specification for surgical spring trusses
BS T 74:1972 Specification for low carbon 18/10 chromium-nickel corrosion-resisting steel tube (500 N/mm<sup>2</sup>)
BS 2T 66:1980 Specification for 18/10 chromium-nickel corrosion-resisting steel tube (niobium stabilized: 550 MPa) (weldable)
BS L 159:1978 Specification for close toleranced sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and artificially aged) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8)
BS 3T 53:1980 Specification for chromium-molybdenum steel tube (700 MPa) (outside diameter not less than 12.5 mm) (weldable)
BS HC 5:1973 Specification for 3% nickel case hardening steel castings (700 N/mm<sup>2</sup>)
BS L 164:1978 Specification for sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8)
BS HC 202:1973 Specification for precipitation hardening nickel base chromium-niobium-molybdenum-iron-tungsten alloy castings (Cr 20.0, Nb 6.6, Mo 6.0, Fe 3.0, W 2.5)
BS SP 141:1970 Specification for design and performance requirements for toggle type panel fasteners
BS S 154:1976 Specification. 2½% nickel-chromium-molybdenum steel billets, bars, forgings and parts (880-1080 MPa: limiting ruling section 150 mm)
BS HR 10:1972 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)
BS HR 5:1972 Specification for nickel-chromium-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 19.5, Ti 0.4)
BS 1965-1:1963 Specification for butt-welding pipe fittings for pressure purposes Carbon steel
BS 4536:1970 Specification for heavy duty pulley blocks for use with wire rope
BS 2G 147-1:1966 Specification for a.c. motors for aircraft Three-phase constant frequency squirrel-cage induction motors
BS 3928:1969 Method for sodium flame test for air filters (other than for air supply to I.C. engines and compressors)
BS 1486-1:1959 Lubricating nipples Lubricating nipples and adaptors for use on machinery and vehicles
BS 5189-3:1975 Dental casting investments Ethyl silicate-bonded investment materials
BS 4672-1:1971 Guide to hazards in the transport and storage of packages Climatic hazards
BS L 515:1973 Specification for sheet and strip of magnesium-1¼% zinc-zirconium alloy (suitable for welding by inert-gas shielded arc techniques) (Zn 1.25, Zr 0.6)
BS 3157:1960 Specification for latex foam rubber components for transport seating
BS HR 52:1973 Specification for heat-resisting alloy billets, bars, forgings and parts (Ni 25.5, Cr 14.7, Ti 1.8, Mn 1.5, Mo 1.2, V 0.3, Fe remainder)
BS L 103:1971 Specification for forging stock and forgings of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8)
BS 456:1961 Specification for dimensions of track circuit insulation
BS 2SP83-85(1973) : 1973 AEROSPACE SERIES - SPECIFICATION FOR MUSHROOM HEAD ALUMINIUM ALLOY RIVETS
BS 2A 24:1962 Specification for corrosion-resisting steel hexagonal nuts (B.A and B.S.F. threads) (ordinary, thin, slotted and castle) for aircraft
BS HR 40:1972 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)
BS 3S 61:1964 Specification for aircraft material. 12 per cent chromium corrosion-resisting steel (35/45 tonf/sq in: limiting ruling section 6 in)
BS 463-1:1958 Specification for sockets for wire ropes Inch units
BS 3529:1962 Specification for dimensions of flywheel housing mounting pads and brackets for i.c. engines
BS 2A 27:1962 Specification for steel hexagonal nuts (B.A. and B.S.F threads) (ordinary, thin, slotted and castle) for aircraft
BS 787-3:1971 Specification for mining type flameproof gate-end boxes Gate-end boxes with lighting transformers
BS 2A 25:1962 Specification for steel hexagonal-headed bolts (B.A. and B.S.F. threads) for aircraft
BS TA 55:1973 Specification for forgings of titanium-copper alloy (tensile strength 650-880 N/mm<sup>2</sup>) (limiting ruling section 75 mm)
BS 2G 143:1965 Specification for a.c. and d.c. rotary and linear actuators for aircraft
BS 3711:1964 Specification for railway vacuum brake cylinders, rolling ring type
BS 2A 59:1962 Specification for cadmium-plated steel hexagonal-headed bolts (B.A. and B.S.F. threads) with close tolerance shanks for aircraft
BS C 17:1973 Specification for coupling dimensions for low pressure air connections for engine starting
BS 3710:1964 Specification for brake hose couplings for locomotives and rolling stock
BS TA 44:1972 Specification for forgings of titanium-aluminium-zirconium-molybdenum-silicon alloy (tensile strength 990-1140 N/mm<sup>2</sup>) (limiting ruling section 65 mm)
BS TA 46:1973 Specification for bar and section for machining of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1050-1220 N/mm<sup>2</sup>) (limiting ruling section over 25 mm up to and including 100 mm)
BS HR 207:1973 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)
BS S155(1976) : 1976 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)
BS HR 3:1972 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)
BS HC 4:1973 Specification for 3% chromium-molybdenum steel castings (620-770 N/mm<sup>2</sup>)
BS 3518-3:1963 Methods of fatigue testing Direct stress fatigue tests
BS F 125:1973 Specification for rubber bonded compressed asbestos fibre jointing
BS 1091:1963 Specification for pressed steel gutters, rainwater pipes, fittings and accessories
BS C 15:1960 Specification for coupling dimensions for aircraft-to-tractor tow bar connections
BS 3831:1964 Specification for vitreous enamel finishes for domestic and catering appliances
BS 1747-3:1969 Methods for measurement of air pollution Determination of sulphur dioxide
BS 3110:1959 Methods for measuring the rub resistance of print
BS 950-1:1967 Specification for artificial daylight for the assessment of colour Illuminant for colour matching and colour appraisal
BS L 102:1971 Specification for bars and extruded sections of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature) (not exceeding 200 mm diameter or minor sectional dimension) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8)
BS T 76:1978 Specification for chromium-molybdenum steel tube (770 MPa) (weldable)
BS L 514:1973 Specification for forging stock and forgings of magnesium-3% zinc-zirconium alloy (Zn 3.0, Zr 0.6)
BS 787-2:1968 Specification for mining type flameproof gate-end boxes Gate-end boxes with air-break circuit-breakers (for use on 3-phase a.c. circuits up to 650 volts)
BS AU 5:1963 Specification for dimensions of a \'contact\' type coupling for vacuum and pressure braking systems on trailers and semi-trailers
BS 2G 134:1970 Specification for d.c. generators
BS C 10:1958 Coupling dimensions for aircraft ground air-conditioning connections
BS 787-1:1969 Specification for mining type flameproof gate-end boxes Gate-end boxes for direct-on-line motor starting (for use on 3-phase a.c. circuits up to 650 V)
BS 2HR 202:1973 Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy sheet and strip (nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)
BS 3054:1959 Specification for fireman\'s axe with rubber insulated handle
BS 3818:1964 Specification for self-sealing fuelling couplings for diesel locomotives and diesel railcars
BS 3783:1964 Specification for X-ray lead-rubber protective aprons for personal use
BS 1486-2:1961 Lubricating nipples Heavy duty lubricating nipples
BS 3L 122:1970 Specification for ingots and castings of magnesium-8% aluminium-zinc-manganese alloy (solution treated) (Al 8, Zn 0.5, Mn 0.3)
BS 2TA 5:1973 Specification for forgings of commercially pure titanium (tensile strength 390-540 N/mm<sup>2</sup>)
BS G 217:1975 Specification for general requirements for cockpit lighting controllers
BS M 48:1975 Specification for dimensions of elastomeric toroidal sealing rings for aerospace use - inch series
BS 3755:1964 Methods of test for the assessment of odour from packaging materials used for foodstuffs
BS 3A 103:1962 Specification for steel nuts (Unified hexagons and Unified threads) (ordinary, thin, slotted and castle) for aircraft
13/30274750 DC : 0 BS 2A 204 ETC+A3 - SPECIFICATIONS FOR MACHINE SCREWS AND NUTS (UNIFIED THREADS) BELOW 1/4 INCH FOR AERONAUTICAL PURPOSES
BS L 166:1978 Specification for close toleranced sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8)
DEFSTAN 13-99/2(2009) : 2009 REQUIREMENTS FOR DGM IPT MUNITIONS TECHNICAL PUBLICATIONS
BS 4145:1967 Specification for glass mica boards for electrical purposes
BS 3063:1965 Specification for dimensions of gaskets for pipe flanges
BS 2G 146:1966 Specification for d.c. motors for aircraft
BS 2HR 201:1974 Specification for nickel-chromium-titanium-aluminium heat-resisting alloy plate, sheet and strip (nickel base, Cr 19.5, Ti 2.2, Al 1.4)
BS S 153:1976 Specification. 2½% nickel-chromium-molybdenum steel billets, bars, forgings and parts (1230-1430 MPa: limiting ruling section 40 mm)
BS 1187:1959 Specification for wood blocks for floors
BS 3L 125:1970 Specification for ingots and castings of magnesium - 10% aluminium-zinc-manganese alloy (solution treated and precipitation treated) (Al 10, Zn 0.5, Mn 0.3)
BS 3123:1959 Specification for spring calipers and spring dividers
BS 4618-3.2:1973 Recommendations for the presentation of plastics design data. Thermal properties Heat content
BS 2HR 1:1973 Specification for nickel-chromium-titanium-aluminium heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 19.5, Ti 2.2, Al 1.4)
BS 2S 116:1964 Specification for aircraft material. \'40\' carbon steel bright bars for machining (55-65 tonf/sq in: limiting ruling section ¾ inch) (primarily intended for the manufacture of machined bolts)
BS L 112:1971 Specification for forging stock and forgings of aluminium-magnesium-silicon-manganese alloy (solution treated and precipitation treated) (suitable for welding) (Mg 0.8, Si 1, Mn 0.7)
BS T 69:1972 Specification for cold drawn 18/10 chromium-nickel corrosion-resisting steel tube (titanium stabilized: 800 N/mm<sup>2</sup>) (weldable)
BS 3G 100-2.3.3:1972 Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Mould growth
BS HC 10:1974 Specification for nickel-chromium-molybdenum steel castings (1150-1300 MPa)
BS HC 6:1973 Specification for 3% chromium-molybdenum nitriding steel castings (850-1000 N/mm<sup>2</sup>)
BS S 157:1976 Specification. 3% nickel-chromium-molybdenum case-hardening steel billets, bars, forgings and parts (1180-1380 MPa)
BS TA 40:1971 Specification for bar for machining of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 N/mm<sup>2</sup>) (limiting ruling section over 25 mm up to and including 75 mm)
BS 2L 128:1970 Specification for ingots and castings of magnesium-zinc-cerium-zirconium alloy (precipitation treated) (Zn 4.5, rare earth metals 1.2, Zr 0.7)
BS L 155:1977 Specification for ingots and castings of aluminium-copper-silicon alloy (solution treated and artificially aged) (Cu 4, Si 1)
BS 2880:Addendum No. 1:1959 Methods of testing cellulose acetate flake
BS HR 206:1973 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 2.1, Al 0.5)
BS 633:1970 Specification for cotton selvedge tapes and webbing for electrical purposes
BS 1494-1:1964 Specification for fixing accessories for building purposes Fixings for sheet, roof and wall coverings
BS 3L 78:1970 Specification for ingots and castings of aluminium-silicon-copper-magnesium alloy (solution treated and precipitation treated) (Si 5, Cu 1.2, Mg 0.5)
BS 3727-3:1966 Methods for the analysis of nickel for use in electronic tubes and valves Determination of carbon
BS 3522:1962 Specification for hypodermic surgical mounted needles (Luer fitting)
BS HR 402:1973 Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy cold worked and softened seamless tubes (nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)
BS 2S 149:1976 Specification for 1.75% nickel-chromium-molybdenum steel bars for the manufacture of forged bolts and forged nuts
BS 3A 170:1962 Specification for aluminium alloy mushroom head bolts (Unified threads) for aircraft
BS 2L 93:1971 Specification for plate of aluminium-copper-magnesium-silicon-manganese alloy (solution treated, controlled stretched and precipitation treated) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8)
BS 2S 142:1977 Specification for 1% chromium-molybdenum steel billets, bars, forgings and parts (900-1100 MPa: limiting ruling section 40 mm)
BS L 105:1971 Specification for tube of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature) (not exceeding 10 mm wall thickness) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8)
BS G 190:1964 Specification for cabin altimeters for aircraft
BS L 513:1973 Specification for forging stock and forgings of magnesium-6% aluminium-zinc alloy (Al 6.0, Zn 1.0)
BS 2874:1986 Specification for copper and copper alloy rods and sections (other than forging stock)

BS 5555:1993 Specification for SI units and recommendations for the use of their multiples and of certain other units
BS 1797:1987 Schedule for tables for use in the calibration of volumetric glassware
BS 874-1:1986 Methods for determining thermal insulating properties Introduction, definitions and principles of measurement
BS 2520:1983 Specification for barometer conventions and tables, their application and use
BS 5775-10:1993 Specification for quantities, units and symbols Nuclear reactions and ionizing radiations
BS 5775-12:1993 Specification for quantities, units and symbols Characteristic numbers
BS EN ISO 18265:2013 Metallic materials. Conversion of hardness values
BS 5775-1:1993 Specification for quantities, units and symbols Space and time

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