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  • DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007

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    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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    Superseded date:  29-01-2010

    Language(s):  English

    Published date:  01-01-2007

    Publisher:  UK Ministry of Defence Standards

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    Table of Contents - (Show below) - (Hide below)

    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

    Abstract - (Show below) - (Hide below)

    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.

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    Development Note Supersedes DEFSTAN 00-970(PT7)SEC7/1(2006). (03/2007)
    Document Type Standard
    Publisher UK Ministry of Defence Standards
    Status Superseded
    Superseded By
    Supersedes

    Standards Referencing This Book - (Show below) - (Hide below)

    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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