|
BSI-2G-1472
|
1966
|
A.C. Motors for Aircraft Part 2: Three-Phase Variable Frequency Squirrel-Cage Induction Motors
|
|
BSI-2G-180
|
1974
|
Permanent Splicing of Aircraft Electrical Cables (Replaces BS G 180: 1962)
|
|
BSI-2G-182
|
1975
|
Pressure-Driven Machmeters for Aircraft (Replaces BS G 182: 1963)
|
|
BSI-2G-191
|
1988
|
Lighting for Aircraft Indicators Using Integral Filament Lamps (Replaces BS G 191: 1965)
|
|
BSI-2G-196
|
1971
|
Static Invertors (Replaces BS G 196: 1966)
|
|
BSI-2G-199
|
1984
|
Amd 1 Tables Relating to Altitudes, Airspeed and Mach Numbers for Use in Aeronautical Instrument Des
|
|
BSI-2G-201
|
1996
|
Counter and Pointer Pressure Altimeters (S)
|
|
BSI-2G-202
|
1988
|
Design and Performance Requirements for Airframe-Fit Electrical Connectors for D.C. and Low Frequenc
|
|
BSI-2G-210
|
1386
|
Amd 1 PTFE Insulated Equipment Wires and Cables, Single- and Multi-Core, with Silver Plated Copper C
|
|
BSI-2G-215-1
|
1985
|
Extension Cables for Aircraft Nickel- Chromium and Nickel- Aluminium Thermocouple Pt 1: Conductors (
|
|
BSI-2G-215-2
|
1989
|
Extension Cables for Aircraft Nickel- Chromium and Nickel- Aluminium Thermocouple Part 2: Terminatio
|
|
BSI-2G-219
|
1983
|
General Requirements for Ground Support Electrical Supplies for Aircraft (Replaces BS G 219: 1975)
|
|
BSI-2G-223
|
1989
|
Screen Terminating Devices for Aircraft Electric Cables (Replaces BS G 223: 1977)
|
|
BSI-2G-232
|
1987
|
Electrical Cables for General Airframe or Equipment Interconnect Use (135 Degrees C), Wrapped Insula
|
|
BSI-2G-238
|
1996
|
Electric Cables for General Airframe or Equipment Interconnect Use (260 Degrees Celsius), Nickel Pla
|
|
BSI-2G-239
|
1992
|
Primary Active Lithium Batteries for Use in Aircraft (Replaces BS G 239: 1987)
|
|
BSI-2HC-101
|
1989
|
Amd 2 Precipitation Hardening Chromium-Nickel-Copper- Molybdenum Steel Castings (950 MPa) (Cr 14.0,
|
|
BSI-2HC-102
|
1989
|
Amd 2 Precipitation Hardening Chromium-Nickel-Copper- Molybdenum Steel Castings (1250 MPa) (Cr 14.0,
|
|
BSI-2HC-203
|
1989
|
Nickel-Chromium- Aluminium-Molybdenum- Niobium Alloy Castings (Nickel Base Cr 13.0, Al 6.0, Mo 4.5,
|
|
BSI-2HC-204
|
1989
|
Nickel-Cobalt-Chromium- Aluminium-Titanium- Molybdenum Alloy Castings (Nickel Base Co 15.0, Cr 10.0,
|
|
BSI-2HC-207
|
1989
|
Nickel-Cobalt-Tungsten- Chromium-Aluminium- Tantalum-Hafnium- Titanium Alloy Castings, (Nickel Base
|
|
BSI-2HC-208
|
1989
|
Nickel-Cobalt-Tungsten- Chromium-Aluminium- Molybdenum Titanium- Tantalum Alloy Castings (Nickel Bas
|
|
BSI-2HC-209
|
1989
|
Low Carbon, Precipitation Hardening Nickel-Chromium- Alumimium-Molybdenum- Niobium Alloy Castings (N
|
|
BSI-2HC-210
|
1989
|
Nickel-Tungsten- Aluminium-Chromium- Molybdenum Alloy Castings (Replaces BS HC 210: 1979)
|
|
BSI-2HC-211
|
1989
|
Nickel-Chromium-Cobalt- Molybdenum-Aluminium- Titanium Alloy Castings (Nickel Base Cr 15.5, Co 10.0,
|
|
BSI-2L-126
|
1970
|
Ingots and Castings of Magnesium-Cerium-Zinc- Zirconium Alloy (Precipitation Treated) (Replaces BS L
|
|
BSI-2L-128
|
1970
|
Ingots and Castings of Magnesium-Zinc-Cerium- Zirconium Alloy (Precipitation Treated) (Replaces BS L
|
|
BSI-2L-169
|
2002
|
Ingots (as Cast) and Castings (Solution Treated and Artificially Aged) of Aluminium-Silicon-Magnesiu
|
|
BSI-2L-500
|
1973
|
Procedure for Inspection and Testing of Wrought Magnesium-Base Alloys (Replaces BS L 500: 1967)
|
|
BSI-2L-77
|
1971
|
Forging Stock and Forgings of Aluminium- Copper-Magnesium- Silicon-Manganese Alloy (Solution Treated
|
|
BSI-2L-87
|
1971
|
Hexagonal Bars for Nuts, Couplings and Hollow Machined Parts of Al-Cu-Mg-Si-Mn Alloy (Solution and P
|
|
BSI-2L-93
|
1971
|
Plate of Aluminium- Copper-Magnesium- Silicon-Manganese Alloy (Solution Treated, Controlled Stretche
|
|
BSI-2L-95
|
1386
|
Amd 1 Plate of Aluminium-Zinc- Magnesium-Copper- Chromium Alloy (Solution Treated, Controlled Stretc
|
|
BSI-2L-97
|
1971
|
Plate of Aluminium- Copper-Magnesium- Manganese Alloy (Solution Treated, Controlled Stretched and Ag
|
|
BSI-2L-99
|
1972
|
Amd 2 Ingots and Castings of Aluminium-Silicon- Magnesium Alloy (Solution Treated and Precipitation
|
|
BSI-2M-41
|
1977
|
Methods of Numbering Propulsion Units and Components and Describing Their Direction of Rotation (Rep
|
|
BSI-2M-46
|
1986
|
Outside Diameters and Thicknesses of Tubing (Replaces BS M 46: 1974)
|
|
BSI-2M-47
|
1990
|
Retreading of Cross Ply Tyres for Aircraft (Replaces BS M 47: 1975)
|
|
BSI-2M-49
|
1997
|
Aircraft - Hydraulic Components - Marking to Indicate Fluid for Which Component is Approved Supersed
|
|
BSI-2M-50
|
1986
|
Clearance Dimensions for Tripod Jacks for Aircraft (Replaces BS M 50: 1980)
|
|
BSI-2M-51
|
1989
|
Classification for Pressure and Temperature for Fluid Systems and Components (Replaces BS M 51: 1982
|
|
BSI-2M-52
|
1989
|
Impulse Testing of Hydraulic Hose, Tubing and Fitting Assemblies for Aerospace Fluid Systems (Replac
|
|
BSI-2M-53
|
1997
|
Aircraft - Fluid Systems - Thermal Shock Testing of Piping and Fittings Supersedes BS M 53: 1983; (S
|
|
BSI-2M-54
|
1991
|
Temperature Control in the Heat Treatment of Metals (Replaces BS M 54: 1982)
|
|
BSI-2M-59
|
1993
|
Interface of Metric Couplings, 24 Degree Cone, for Aerospace Fluid Systems (ISO 7319: 1992) (Superse
|
|
BSI-2M-63
|
1993
|
Dimensions of Aerospace Fluid System Port Connection, Seal and Fitting End (ISO 7320: 1992) (Superse
|
|
BSI-2M-72
|
1996
|
Air Cargo Equipment - Minimum Airworthiness Requirements and Test Conditions for Certified Air Cargo
|
|
BSI-2PL-1
|
1966
|
Phenolic Mouldings for Aeronautical Purposes (Replaces BS PL 1: 1951)
|
|
BSI-2S-130
|
1976
|
Amd 1 18/9 Chromium-Nickel Corrosion-Resisting Steel (Niobium Stabilized) Billets, Bars, Forgings an
|
|
BSI-2S-131
|
1977
|
Amd 1 High Thermal Expansion Steel Billets, Bars, Forgings and Parts (620 MPa: Limiting Ruling Secti
|
