BS G 216:1975
|
Specification for hand operated, thermally compensated, miniature, single and triple pole circuit breakers |
DEFSTAN 47-25/1(1982) : 1982
|
PIPELINES AND PIPE COUPLINGS FOR AIRCRAFT FLUID SYSTEMS (METRIC) |
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 |
STANAG 3456 : 0
|
AIRCRAFT ELECTRICAL POWER SYSTEM CHARACTERISTICS |
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 2G 143:1965
|
Specification for a.c. and d.c. rotary and linear actuators for aircraft |
STANAG 3368 : 2014
|
INTERNAL AIRCRAFT ENGINE STARTING SYSTEM |
BS 2G 180:1974
|
Specification for permanent splicing of aircraft electrical cables |
DEFSTAN 00-13/3(1994) : 1994
|
REQUIREMENTS FOR THE ACHIEVEMENT OF TESTABILITY IN ELECTRONIC AND ALLIED EQUIPMENT |
DEFSTAN 47-19/1(1977) : 1977 AMD 2
|
AIRCRAFT PIPE FITTINGS (INCH SERIES) - SCREW THREADS, HEXAGON SIZES, TAPPED HOLES, AND 'O' RING SEALS |
BS 2G 134:1970
|
Specification for d.c. generators |
DEFSTAN 16-26/1(1983) : 1983
|
CHARGING VALVES FOR AIRCRAFT HIGH PRESSURE NITROGEN AND HYDRAULIC FLUID SYSTEMS |
BS G 175:1959
|
Aircraft fuel nozzle grounding plugs and sockets |
DEFSTAN 47-23/1(1980) : 1980
|
BEAD PROFILE FOR AIRCRAFT PIPING AND DUCTING (FLEXIBLE CONNECTIONS) |
BS G 195:1966
|
Specification for Minyvin type electric cables for aircraft |
STANAG 3659 : 2002
|
ELECTRICAL BONDING REQUIREMENTS FOR METALLIC AIRCRAFT SYSTEMS |
FAA AC 20-53 : 2006
|
PROTECTION OF AIRCRAFT FUEL SYSTEMS AGAINST FUEL VAPOR IGNITION CAUSED BY LIGHTNING |
MIL-E-22285 Base Document:1959
|
EXTINGUISHING SYSTEM, FIRE, AIRCRAFT, HIGH-RATE DISCHARGE TYPE, INSTALLATION AND TEST OF |
MIL B 83054 : B
|
BAFFLE AND INERTING MATERIAL, AIRCRAFT FUEL TANK |
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 |
MIL-P-46111 Revision C:1978
|
PLASTIC FOAM, POLYURETHANE (FOR USE IN AIRCRAFT) |
BS 2C 13:1988
|
Specification for sizes of aircraft gravity filling orifices and associated replenishment nozzles (metric series) |
BS 3M 60:1998
|
Separable tube fittings for fluid systems, 24° cone. General specification |
BS 5M 23:1987
|
Specification for an identification scheme for pipelines |
MIL-C-7762 Revision A:1967
|
COMPASS, INSTALLATION OF |
STANAG 3294 : 0
|
AIRCRAFT FUEL CAPS AND FUEL CAP ACCESS COVERS |
MIL O 27210 : F
|
OXYGEN, AVIATOR'S BREATHING, LIQUID AND GAS |
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 2G 221:1980
|
Specification for Minyvin type electric cables (metric units) |
BS G 207:1969
|
Specification for aircraft electrical circuit diagrams |
DEFSTAN 59-76/1(1981) : 1981
|
TRANSFORMERS AND INDUCTORS - GENERAL REQUIREMENTS FOR THE PROCUREMENT OF TRANSFORMERS AND INDUCTORS - CAPABILITY APPROVAL |
SAE AS 401 : 1993
|
POWERPLANT FIRE DETECTION INSTRUMENTS - THERMAL AND FLAME CONTACT TYPES (RECIPROCATING ENGINE POWERED AIRCRAFT) |
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 |
BS G 227:1979
|
Specification for Tersil type electric cables (metric units) |
DEFSTAN 00-29/1(1982) : 1982
|
FUNGAL CONTAMINATION AFFECTING THE DESIGN OF MILITARY MATERIAL |
ISO 6771:2007
|
Aerospace Fluid systems and components Pressure and temperature classifications |
MIL-R-7705 Revision B:1975
|
RADOME, GENERAL SPECIFICATION FOR |
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 |
DEFSTAN 59-42(PT1)/1(1990) : 1990
|
HEAT SHRINK SOLDER SHEATHS - PART 1: REQUIREMENTS AND TEST METHODS FOR CAPABILITY APPROVAL |
MIL-B-81365 Base Document:1966
|
BLEED AIR SYSTEMS, GENERAL SPECIFICATIONS FOR |
BS 5G 178-1:1993
|
Crimped joints for aircraft electrical cables and wires. Specification for design requirements (including tests) for components and tools |
DEFSTAN 05-56/1(1980) : 1980
|
GRAPHICAL SYMBOLS FOR AIRCRAFT HYDRAULIC AND PNEUMATIC SYSTEMS |
DEFSTAN 15-2/1(1987) : 1987
|
FLEXIBLE TANKS FOR USE IN AIRCRAFT FUEL AND METHANOL/WATER SYSTEMS |
MIL-C-38373 Revision B:1975
|
CAP, FLUID TANK FILLER |
DEFSTAN 16-10/3(1983) : 1983 AMD 1
|
LOW PRESSURE AIR STARTING OF AIRCRAFT ENGINES |
BS 3G 231:1997
|
Specification for conductors for general-purpose aircraft electrical cables and aerospace applications |
DEFSTAN 61-15/3(1990) : 1990 AMD 1 1991
|
PRECAUTIONS AGAINST ELECTRICAL SHOCK IN MAINTENANCE AREAS |
DEFSTAN 00-41(PT1)/1(1983) : 1983
|
MOD PRACTICES AND PROCEDURES FOR RELIABILITY AND MAINTAINABILITY PT 1 RELIABILITY DESIGN PHILOSOPHY |
DEFSTAN 91-2 : LATEST
|
PETROLEUM FUELS |
MIL-STD-1760 Revision E:2007
|
AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
BS 2C 4:1973
|
Specification for coupling dimensions for aero-engine refrigerant pressure replenishment connections |
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 |
DEFSTAN 53-94/1(1983) : 1983
|
PROTECTIVE CAPS AND PLUGS FOR AIRCRAFT PIPELINES |
BS G 212:1971
|
Specification for general requirements for aircraft electrical cables |
MIL-D-21625 Revision G:1993
|
DESIGN AND EVALUATION OF CARTRIDGES FOR CARTRIDGE ACTUATED DEVICES |
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 |
ISO 6772:2012
|
Aerospace — Fluid systems — Impulse testing of hydraulic hose, tubing and fitting assemblies |
FAA AC 20-100 : 1977
|
GENERAL GUIDELINES FOR MEASURING FIRE-EXTINGUISHING AGENT CONCENTRATIONS IN POWERPLANT COMPARTMENTS |
NFPA 326 : 2015
|
SAFEGUARDING OF TANKS AND CONTAINERS FOR ENTRY, CLEANING, OR REPAIR |
MIL C 83413 : A
|
CONNECTORS AND ASSEMBLIES, ELECTRICAL, AIRCRAFT GROUNDING, GENERAL SPECIFICATION FOR |
DEFSTAN 47-12/4(1987) : 1987
|
POLYTETRAFLUOROETHYLENE (PTFE) HOSE ASSEMBLIES (WIRE REINFORCED) FOR MEDIUM AND HIGH PRESSURE FLUID SYSTEMS IN AIRCRAFT |
DTD 5548 : AMD 1
|
GLAZING COMPOUNDS |
DTD 5627 : APR 82
|
FIBROUS POLYAMIDE MATERIAL FOR USE AS AN EXPLOSION SUPPRESSANT AND AS A BAFFLE MATERIAL IN AIRCRAFT FUEL TANKS |
MIL-W-81752 Revision A:1987
|
WINDSHIELDED SYSTEM, FIXED WING AIRCRAFT - GENERAL SPECIFICATION FOR |
DTD 5624 : MAR 81
|
FIBROUS POLYESTER MATERIAL FOR USE AS A FLAME AND FIRE SUPPRESSANT IN AIRCRAFT DRY BAYS |
DEFSTAN 00-31/1(1987) : 1987
|
THE DEVELOPMENT OF SAFETY CRITICAL SOFTWARE FOR AIRBORNE SYSTEMS |
MIL-E-18927 Revision E:1983
|
ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR |
ISO 7169:2014
|
Aerospace Separable tube fittings for fluid systems, for 24 degree cones, for pressures up to 3 000 psi or 21 000 kPa Procurement specification, inch/metric |
DEFSTAN 66-27/1(1978) : 1978 AMD 1
|
PRESSURE CONNECTIONS ON AIRCRAFT INSTRUMENTS AND ASSOCIATED EQUIPMENT |
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 M 48:1975
|
Specification for dimensions of elastomeric toroidal sealing rings for aerospace use - inch series |
MIL P 8184 : E
|
PLASTIC SHEET, ACRYLIC, MODIFIED |
DEFSTAN 16-21/2(1986) : 1986 AMD 1 1986
|
MARKING OF AIRCRAFT HYDRAULIC COMPONENTS |
MIL-P-6992 Base Document:1950
|
PUMP ASSEMBLY, FUEL, ELECTRICALLY DRIVEN, AIRCRAFT HEATER |
BS 5G 205-1:1990
|
Secondary batteries for aircraft Specification for lead-acid batteries |
DEFSTAN 17-2/3(1989) : 1989
|
REPLENISHMENT EQUIPMENT FOR AERO ENGINE THRUST AUGMENTATION (REFRIGERANT INJECTION) SYSTEMS |
MIL-H-5484 Revision C:1964
|
HEATER, AIRCRAFT, COMBUSTION TYPE |
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 |
MIL-M-8609 Revision B:1965
|
MOTOR, DC 28 VOLT SYSTEM AIRCRAFT, GENERAL SPECIFICATION FOR |
BS G 203:1967
|
Specification for Unified screws with captive facing and locking washers |
MIL-STD-461 Revision G:2015
|
REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
BS 6275-1:1982
|
Hydraulic fluid power filter elements Method of evaluating filtration performance (multi-pass method) |
MIL-STD-12 Revision D:1981
|
ABBREVIATIONS FOR USE ON DRAWINGS, SPECIFICATIONS FOR STANDARDS AND IN TECHNICAL DOCUMENTS |
DEFSTAN 59-36/5(1995) : 1995
|
SELECTION OF ELECTRONIC AND ELECTRICAL COMPONENTS FOR USE IN DEFENCE EQUIPMENT |
MIL-D-81641 Base Document:1972
|
DISPLAY, HEAD UP, GENERAL SPECIFICATION FOR |
STANAG 3208 : 2009
|
AIR CONDITIONING CONNECTIONS |
BS 4C 14:1991
|
Specification for aircraft pressure refuelling connectors |
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 |
STANAG 3632 : 0
|
AIRCRAFT AND GROUND SUPPORT EQUIPMENT ELECTRICAL CONNECTIONS FOR STATIC GROUNDING |
BS G 208:1970
|
Specification for general requirements for electrical relays up to 10 A rating |
ISO 7257:2016
|
Aircraft Hydraulic tubing joints and fittings Rotary flexure test |
MIL-F-23447 Base Document:1962
|
FIRE WARNING SYSTEMS, AIRCRAFT, RADIATION SENSING TYPE, TEST AND INSTALLATION OF |
STANAG 4270 : 0
|
AVIATION FUEL DESIGN PARAMETER FOR FUTURE NATO LAND BASED TURBINE POWERED MILITARY AIRCRAFT |
MIL F 38363 : B (3)
|
FUEL SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR |
DEFSTAN 16-6/2(1991) : 1991
|
CHARGING VALVE FOR AIRCRAFT LIQUID SPRING UNDERCARRIAGE UNITS |
MIL-STD-1472 Revision G:2012
|
HUMAN ENGINEERING |
BS 2G 219:1983
|
Specification for general requirements for ground support electrical supplies for aircraft |
DTD 5625 : JUN 80
|
STANDARD ANNEALED FLOAT GLASS FOR AIRCRAFT GLAZING |
DEFSTAN 00-52/1(1985) : 1985
|
THE GENERAL REQUIREMENTS FOR TEST SPECIFICATIONS AND TEST SCHEDULES |
BS C 9:1970
|
Specification for coupling dimensions for high pressure air charging valves for aircraft |
DEFSTAN 61-3/5(1992) : INTERIM
|
GENERIC SPECIFICATION FOR BATTERIES, NON RECHARGEABLE, PRIMARY |
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 |
BS G 206:1969
|
Specification for Fepsil type electric cables with copper conductors |
DEFSTAN 01-5/14(2005) : 2005
|
FUELS, LUBRICANTS AND ASSOCIATED PRODUCTS |
MIL-I-8673 Base Document:1955
|
INSTALLATION AND TEST OF AIRCRAFT FLEXIBLE WEAPONS SYSTEMS |
MIL-H-5440 Revision H:1993
|
HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
DEFSTAN 00-14/3(1997) : 1997
|
THE USE OF ATLAS IN THE DEFENCE INDUSTRY |
MIL-STD-462 Revision D:1993
|
MEASUREMENT OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS |
MIL-T-18606 Base Document:1955
|
TEST PROCEDURES FOR AIRCRAFT ENVIRONMENT SYSTEMS |
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 |
DTD 5592 : LATEST
|
ACRYLIC SHEETS FOR AIRCRAFT GLAZING |
DEFSTAN 47-22/1(1979) : 1979
|
END FITTINGS FOR FLEXIBLE HOSE ASSEMBLIES FOR AIRCRAFT - METRIC |
BS G 174:1959
|
Invertors for secondary electrical supplies for aircraft |
MIL-P-83310 Base Document:1971
|
PLASTIC SHEET, POLYCARBONATE, TRANSPARENT |
BS G 194:1965
|
Specification for lever-operated manual switches for aircraft |
STANAG 3105 : 2014
|
PRESSURE REFUELLING CONNECTIONS AND DEFUELLING FOR AIRCRAFT |
DEFSTAN 91-48/2(1997) : 1997
|
HYDRAULIC FLUID, PETROLEUM: SUPERCLEAN NATO CODE: H-515 JOINT SERVICE DESIGNATION: OM-15 HYDRAULIC FLUID, PETROLEUM: NORMAL NATO CODE: H-520 JOINT SERVICE DESIGNATION: OM-18 |
MIL-I-8670 Revision B:1993
|
INSTALLATION OF FIXED GUNS AND ASSOCIATED EQUIPMENT IN NAVAL AIRCRAFT |
BS G 102:1971
|
Specification for general requirements for rotating electrical machinery |
MIL A 5503 : E
|
ACTUATOR, AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
MIL-W-5088 Revision L:1991
|
Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
DEFSTAN 00-50/1(1982) : 1982
|
GUIDE TO CHEMICAL ENVIRONMENTAL CONTAMINANTS AND CORROSION AFFECTING THE DESIGN OF MILITARY MATERIAL |
MIL-I-8700 Revision A:1970
|
INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
BS 2G 213:1974
|
Specification for mechanically operated switches |
DEFSTAN 00-10/1(1976) : LATEST
|
GENERAL DESIGN AND MANUFACTURING REQUIREMENTS FOR SERVICE ELECTRONIC EQUIPMENT |
MIL-T-23103 Revision A:1971
|
THERMAL PERFORMANCE EVALUATION, AIRBORNE ELECTRONIC EQUIPMENT AND SYSTEMS, GENERAL REQUIREMENTS FOR |
BS G 142:1953
|
Specification for heavy duty, electro-magnetically operated, single-pole circuit-breakers for extra-low voltage d.c. systems in aircraft |
MIL-E-7080 Revision B:1962
|
ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF |
DEFSTAN 53-70/2(1976) : 1976 AMD 2
|
DIMENSIONS OF ELASTOMERIC TOROIDAL SEALING RINGS (INCH SERIES) FOR AIRCRAFT PURPOSES |
BS G 204:1967
|
Specification for copper terminal ends for crimping to electric cables with copper conductors |
DEFSTAN 00-970/VOL1/1(1983) : AMD 14
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - AEROPLANES |
MIL-HDBK-221 Base Document:1965
|
FIRE PROTECTION DESIGN HANDBOOK FOR U.S. NAVY AIRCRAFT POWERED BY TURBINE ENGINES |
DEFSTAN 61-12(PT20)/1(1980) : 1980
|
WIRES, CORDS, AND CABLES, ELECTRICAL - METRIC UNITS - PART 20: BRAIDS, WIRE |
DEFSTAN 16-7/3(1990) : 1990
|
COMPRESSED AIR, CHARACTERISTICS, SUPPLY, PRESSURE AND HOSES FOR TECHNICAL PURPOSES |
DTD 5626 : JUN 80
|
HIGH LIGHT TRANSMISSION ANNEALED PLATE GLASS FOR AIRCRAFT GLAZING |
STANAG 3212 : 2017
|
DIAMETERS FOR GRAVITY FILLING ORIFICES |
MIL-STD-877 Base Document:1968
|
ANTENNA SUBSYSTEMS, AIRBORNE, CRITERIA FOR DESIGN AND LOCATION OF |
DEFSTAN 53-68/2(1977) : 1977 AMD 2 1984
|
V-FLANGE COUPLINGS FOR AIRCRAFT PIPING AND DUCTING (METRIC) |
DEFSTAN 17-5/2(1986) : 1986
|
POWER DRIVEN HYDRAULIC GROUND SERVICING EQUIPMENT FOR AIRCRAFT |
ISO 6773:1994
|
Aerospace Fluid systems Thermal shock testing of piping and fittings |