DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
Available format(s)
Hardcopy , PDF
Superseded date
29-01-2010
Superseded by
Language(s)
English
Published date
01-01-2007
Publisher
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LEAFLET 700 PROPULSION SYSTEM INSTALLATIONS
LEAFLET 701 REFUELLING AND DEFUELLING SYSTEMS
LEAFLET 702 FUEL SYSTEMS
LEAFLET 703 PNEUMATIC SYSTEMS
LEAFLET 704 HYDRAULIC SYSTEMS
LEAFLET 705 TRANSMISSION SYSTEMS
LEAFLET 706 ELECTRICAL INSTALLATIONS
LEAFLET 707 RADIO AND RADAR INSTALLATIONS
LEAFLET 708 BONDING AND SCREENING
LEAFLET 709 GUN INSTALLATIONS
LEAFLET 710 ARMAMENT INSTALLATIONS
LEAFLET 711 ICE PROTECTION
LEAFLET 712 FIRE PRECAUTIONS
LEAFLET 713 MAGNETIC COMPASS INSTALLATIONS
LEAFLET 714 TRANSPORT ROTORCRAFT - ROLE EQUIPMENT INSTALLATIONS
LEAFLET 715 OPTICAL TRANSPARENT COMPONENTS - DESIGN,
INSTALLATION, TESTING AND REQUIREMENTS FOR CLEAR
VISION
LEAFLET 716 STATIC AND PITOT PRESSURE SYSTEMS
LEAFLET 717 PROTECTION FROM THE EFFECTS OF NUCLEAR
EXPLOSIONS, LASER WEAPONS, CHEMICAL AND
BIOLOGICAL WARFARE AGENTS
LEAFLET 718 INSTALLATION OF EXPLOSIVE DEVICES
LEAFLET 719 PRESSURISED GAS STORAGE VESSELS
LEAFLET 720 AIR LAUNCHED WEAPON INSTALLATIONS
LEAFLET 721 EMERGENCY LIFERAFT INSTALLATIONS
LEAFLET 722 FOLDING COMPONENTS
LEAFLET 723 RESCUE HOIST AND SONAR HOIST INSTALLATIONS
LEAFLET 724 INSTRUMENT/DISPLAY INSTALLATIONS
LEAFLET 725 AVIONIC EQUIPMENT INSTALLATIONS
LEAFLET 726 Not Issued
LEAFLET 727 HEALTH AND USAGE MONITORING SYSTEMS
LEAFLET 728 SOFTWARE
LEAFLET 729 SAFETY CRITICAL SOFTWARE
LEAFLET 730 Not Issued
LEAFLET 731 CONDITIONING SYSTEMS
LEAFLET 732 ROTOR SYSTEMS
APPENDIX No 1 - Not Issued
APPENDIX No 2 - U.S. MILITARY SPECIFICATIONS, STANDARDS AND
HANDBOOKS
Applies the design and construction of all turbine engine propulsion system installations including all the equipment and sub-systems necessary for the satisfactory operation of the engine.
| DevelopmentNote |
Supersedes DEFSTAN 00-970(PT7)SEC7/1(2006). (03/2007)
|
| DocumentType |
Standard
|
| Pages |
663
|
| PublisherName |
UK Ministry of Defence Standards
|
| Status |
Superseded
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| SupersededBy | |
| Supersedes |
| 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 |
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