BS 3J 12:1991
|
Specification for pressure-sensitive adhesive identification tape |
BS C 18:1976
|
Specification for V-flange couplings for aircraft piping and ducting - metric series |
BS 2M 51:1989
|
Classification for pressure and temperature for fluid systems and components |
BS 2G 143:1965
|
Specification for a.c. and d.c. rotary and linear actuators for aircraft |
BS 2G 180:1974
|
Specification for permanent splicing of aircraft electrical cables |
DEFSTAN 61-10(PT1)/1(1995) : 1995
|
GENERATOR SETS (GROUND, ENGINE DRIVEN) POWER AND DISTRIBUTION - PART 1: BOX, DISTRIBUTION 13 A 3 WAY, 240 V FOR FIELD ELECTRICAL POWER DISTRIBUTION SYSTEMS INCORPORATING CECC 75201.007 INPUT CONNECTOR |
BS 2G 134:1970
|
Specification for d.c. generators |
BS M 43:1973
|
Methods of zoning aircraft and referencing access doors and panels |
DEFSTAN 81-24/5(2004) : 2004
|
IDENTIFICATION MARKING OF TRANSPORTABLE CONTAINERS, COMPRESSED GAS |
BS M 55:1984
|
Method for rotary flexure testing of hydraulic tubing joints and fittings for aerospace use |
BS 2C 13:1988
|
Specification for sizes of aircraft gravity filling orifices and associated replenishment nozzles (metric series) |
BS 5M 23:1987
|
Specification for an identification scheme for pipelines |
DEFSTAN 59-97/3(1990) : AMD 1
|
HEAT SHRINKABLE INSULATION MATERIALS - GENERAL REQUIREMENTS, TESTS AND TEST METHODS FOR CAPABILITY APPROVAL |
DEFSTAN 05-42/2(1982) : 1982
|
PARTICULATE CONTAMINATION CLASSES FOR FLUIDS IN HYDRAULIC SYSTEMS |
MIL-STD-810 Revision G:2008
|
ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
BS G 207:1969
|
Specification for aircraft electrical circuit diagrams |
BS 3G 197:1982
|
Specification for stud-type terminal blocks for terminations on aircraft electric cables |
MIL A 5498 : D
|
ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT |
DEFSTAN 01-5/17(2011) : 2011
|
FUELS, LUBRICANTS AND ASSOCIATED PRODUCTS |
ISO 6771:2007
|
Aerospace Fluid systems and components Pressure and temperature classifications |
BS 2M 53:1997
|
Aircraft. Fluid systems. Thermal shock testing of piping and fittings |
DEFSTAN 05-43/1(1977) : 1977
|
STANDARD PROCEDURES FOR TAKING SAMPLES OF HYDRAULIC FLUIDS FOR EVALUATION OF PARTICULATE CONTAMINATION |
BS 3G 231:1997
|
Specification for conductors for general-purpose aircraft electrical cables and aerospace applications |
MIL-STD-1760 Revision E:2007
|
AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
BS 2M 52:1989
|
Method for impulse testing of hydraulic hose, tubing and fitting assemblies for aerospace fluid systems |
BS 2G 202:1988
|
Specification for design and performance requirements for airframe-fit electrical connectors for d.c. and low frequency a.c. applications |
DEFSTAN 59-35(PT0)/3(1990) : 1990
|
CONNECTORS ELECTRICAL - PART 0: GUIDE TO CONNECTORS ELECTRICAL, DIRECT CURRENT, LOW FREQUENCY AND RADIO FREQUENCY APPLICATIONS |
BS G 212:1971
|
Specification for general requirements for aircraft electrical cables |
MIL E 5400 : T
|
ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR |
BS 2G 127:1967
|
Specification for power and current transformers for use in aircraft electrical power supply systems |
STANAG 3323 : 0
|
PIPE (TUBE) CONNECTIONS TO AIRCRAFT INSTRUMENTS (IMPERIAL AND METRIC) |
DEFSTAN 00-31/1(1987) : 1987
|
THE DEVELOPMENT OF SAFETY CRITICAL SOFTWARE FOR AIRBORNE SYSTEMS |
BS M 44:1974
|
Specification for identification of aircraft servicing, maintenance, ground handling and safety/hazard points |
DEFSTAN 00-971/1(1987) : 1987
|
GENERAL SPECIFICATION FOR AIRCRAFT GAS TURBINE ENGINES |
DOD STD 1788 : LATEST
|
AVIONICS INTERFACE DESIGN STANDARD (METRIC) |
BS G 209:1970
|
Specification for transformer rectifier units |
BS 2G 232:1987
|
Specification for electric cables for general airframe or equipment interconnect use (135°C), wrapped insulation |
MIL-PRF-5503 Revision G:2013
|
ACTUATORS: AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
BS M 48:1975
|
Specification for dimensions of elastomeric toroidal sealing rings for aerospace use - inch series |
BS M 60:1986
|
Specification for separable tube fittings for fluid systems |
BS 3G 230:2000
|
Specification for general requirements for aircraft electrical cables (second series) |
BS 2G 146:1966
|
Specification for d.c. motors for aircraft |
BS G 203:1967
|
Specification for Unified screws with captive facing and locking washers |
BS 2G 223:1989
|
Specification for screen terminating devices for aircraft electric cables |
MIL-STD-461 Revision G:2015
|
REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
BS 2G 199:1984
|
Schedule for tables relating to altitudes, airspeed and Mach numbers for use in aeronautical instrument design and calibration |
DEFSTAN 00-42(PT4)/3(2014) : 2014
|
RELIABILITY AND MAINTAINABILITY ACTIVITY - PART 4: TESTABILITY |
MIL-D-81641 Base Document:1972
|
DISPLAY, HEAD UP, GENERAL SPECIFICATION FOR |
BS G 224:1978
|
Specification for lever-operated manual switches for aircraft |
DEFSTAN 00-41(PT1)/2(1989) : 1989
|
MOD PRACTICES AND PROCEDURES FOR RELIABILITY AND MAINTAINABILITY - PART 1: RELIABILITY DESIGN PHILOSOPHY |
MIL-H-8775 Revision D:1976
|
HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR |
BS 3G 210:1996
|
Specification for PTFE insulated equipment wires and cables, single- and multi-core, with silver plated copper conductors (190°C) or nickel plated copper conductors (260°C) |
BS 2G 196:1971
|
Specification for static invertors |
MIL D 87213 : 0
|
DISPLAYS/OPTICALLY GENERATED REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
BS 2G 219:1983
|
Specification for general requirements for ground support electrical supplies for aircraft |
BS C 9:1970
|
Specification for coupling dimensions for high pressure air charging valves for aircraft |
BS 6G 205-1:1995
|
Secondary batteries for aircraft Specification for lead-acid batteries |
MIL F 8815 : D
|
FILTER AND FILTER ELEMENTS, FLUID PRESSURE, HYDRAULIC LINE, 15 MICRON ABSOLUTE AND 5 MICRON ABSOLUTE, TYPE 11 SYSTEMS; GENERAL SPECIFICATION FOR |
MIL-H-5440 Revision H:1993
|
HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
BS G 217:1975
|
Specification for general requirements for cockpit lighting controllers |
BS 2917-1:1993
|
Graphic symbols and circuit diagrams for fluid power systems and components. Specification for graphic symbols |
ARINC 404A : 1974
|
AIR TRANSPORT EQUIPMENT CASES AND RACKING |
BS 3G 233:1990
|
Specification for electric cables for general airframe or equipment interconnect use (135°C), extruded insulation |
BS G 102:1971
|
Specification for general requirements for rotating electrical machinery |
MIL-W-5088 Revision L:1991
|
Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
BS 4G 229:1996
|
Schedule for environmental conditions and test procedures for airborne equipment |
MIL-I-8700 Revision A:1970
|
INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
BS G 222:1976
|
Specification for Efglas type electric cables (metric units) |
DEFSTAN 00-970/VOL1/1(1983) : AMD 14
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - AEROPLANES |
BS ISO 16889 : 2008
|
HYDRAULIC FLUID POWER - FILTERS - MULTI-PASS METHOD FOR EVALUATING FILTRATION PERFORMANCE OF A FILTER ELEMENT |
DEFSTAN 00-970/VOL2/1(1984) : 1984
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - ROTORCRAFT |
STANAG 3212 : 2017
|
DIAMETERS FOR GRAVITY FILLING ORIFICES |
DEFSTAN 00-52/4(2014) : 2014
|
THE GENERAL REQUIREMENTS FOR PRODUCT ACCEPTANCE AND MAINTENANCE TEST SPECIFICATIONS AND TEST SCHEDULES |