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  • JSSG 2009 : A

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    AIR VEHICLE SUBSYSTEMS (JOINT SERVICE SPECIFICATION GUIDE)

    Available format(s):  Hardcopy, PDF

    Superseded date:  15-05-2021

    Language(s): 

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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

    PART 1
    1 SCOPE
    2 APPLICABLE DOCUMENTS
    3 REQUIREMENTS
    4 VERIFICATIONS
    5 PACKAGING
    6 NOTES
    PART 2
    1 SCOPE
    2 APPLICABLE DOCUMENTS
    3 REQUIREMENTS
    4 VERIFICATIONS
    APPENDICES
    APPENDIX A: LANDING SUBSYSTEM
    APPENDIX B: HYDRAULIC POWER SUBSYSTEM
    APPENDIX C: AUXILIARY POWER SUBSYSTEM
    APPENDIX D: ENVIRONMENTAL CONTROL SUBSYSTEM
    APPENDIX E: FUEL SUBSYSTEM
    APPENDIX F: AERIAL REFUELING SUBSYSTEM
    APPENDIX G: FIRE AND EXPLOSION HAZARD PROTECTION
                SUBSYSTEM
    APPENDIX H: ELECTRICAL POWER SUBSYSTEM
    APPENDIX I: MECHANICAL SUBSYSTEMS
    APPENDIX J: CARGO, AERIAL DELIVERY, AND SPECIAL
                OPERATIONS SUBSYSTEM
    APPENDIX K: VERTICAL TAKEOFF AND LANDING (VTOL) -
                SHORT TAKEOFF AND LANDING (STOL) POWER
                DRIVE SUBSYSTEMS
    APPENDIX L: PROPELLER SUBSYSTEM
    APPENDIX M: PNEUMATIC SUBSYSTEM

    Abstract - (Show below) - (Hide below)

    Describes the item definition, performance, operating characteristics, reliability, maintainability, physical characteristics, general design, installation, and interface requirements for Air Vehicle Subsystems.

    General Product Information - (Show below) - (Hide below)

    Committee FSC 15GP
    Development Note Supersedes AFGS 87145 (A). (12/2007) Supersedes AFGS 87154 (A). (01/2014) Supersedes MIL F 87168. (02/2014)
    Document Type Standard
    Product Note NEW CHILD NOT 1 2018 IS NOW ADDED
    Publisher US Military Specs/Standards/Handbooks
    Status Superseded
    Superseded By
    Supersedes

    Standards Referenced By This Book - (Show below) - (Hide below)

    MIL HDBK 516 : C AIRWORTHINESS CERTIFICATION CRITERIA
    MIL DTL 9490 : E FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
    SAE ARP 1796 : 2015 ENGINE BLEED AIR SYSTEMS FOR AIRCRAFT
    MIL HDBK 510-1 : A AEROSPACE FUELS CERTIFICATION
    AFGS 87219 : B ELECTRICAL POWER SYSTEMS, AIRCRAFT
    SAE AIR 4566 : 2015 CRASHWORTHY LANDING GEAR DESIGN
    SAE AS 4073 : 2013(R2018) AIR CYCLE AIR CONDITIONING SYSTEMS FOR MILITARY AIR VEHICLES
    SAE AIR 4246 : 2012 CONTAMINANTS FOR AIRCRAFT TURBINE ENGINE FUEL SYSTEM COMPONENT TESTING
    MIL PRF 83323 : D TESTER, UNIVERSAL RECEPTACLE, AERIAL REFUELING
    MIL HDBK 510 : A AEROSPACE FUELS CERTIFICATION
    STANAG 7191 : 2013 AIR-TO-AIR (AERIAL) REFUELLING EQUIPMENT: BOOM-RECEPTACLE SYSTEM AND INTERFACE REQUIREMENTS
    SAE ARP 6078 : 2012 AIRCRAFT FUEL TANK INERTING SYSTEMS
    SAE AIR 5774 : 2012 COMPOSITE FUEL TANKS, FUEL SYSTEM DESIGN CONSIDERATIONS
    SAE AIR 4170 : 2016 RETICULATED POLYURETHANE FOAM EXPLOSION SUPPRESSION MATERIAL FOR FUEL SYSTEMS AND DRY BAYS
    SAE MAP 749 : 2015 AIRCRAFT TURBINE ENGINE FUEL SYSTEM COMPONENT ENDURANCE TEST PROCEDURE (ROOM TEMPERATURE CONTAMINATED FUEL)
    SAE AIR 1277 : 2005 COOLING OF MILITARY AVIONIC EQUIPMENT
    SAE ARP 1595 : 2013(R2019) DESIGN AND VERIFICATION OF AIRCRAFT NOSE WHEEL STEERING SYSTEMS
    SAE AIR 1168/4 : 2016 SAE AEROSPACE APPLIED THERMODYNAMICS MANUAL ICE, RAIN, FOG, AND FROST PROTECTION
    SAE ARP 85 : 2012 AIR CONDITIONING SYSTEMS FOR SUBSONIC AIRPLANES
    SAE ARP 986 : 2015 GUIDE FOR QUALIFICATION TESTING OF AIRCRAFT AIR VALVES
    ATP 3.3.4.5 : 2013 AIR-TO-AIR (AERIAL) REFUELLING EQUIPMENT: BOOM-RECEPTACLE SYSTEM AND INTERFACE REQUIREMENTS
    SAE AIR 4023 : 2016 AIRCRAFT TURBINE FUEL CONTAMINATION HISTORY AND ENDURANCE TEST REQUIREMENTS
    SAE ARP 1270 : 2015 AIRCRAFT CABIN PRESSURIZATION CRITERIA
    SAE AIR 805 : 2017 JET BLAST WINDSHIELD RAIN REMOVAL SYSTEMS FOR COMMERCIAL TRANSPORT AIRCRAFT

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

    A A 59155 : 0 NITROGEN, HIGH PURITY, SPECIAL PURPOSE
    NASM 1515 : 0 FASTENER SYSTEMS FOR AEROSPACE APPLICATIONS
    SAE AMS I 7171 : 2011 INSULATION BLANKET, THERMAL ACOUSTICAL
    SAE AS 1284 : 2015 STANDARD TEST PROCEDURE AND LIMIT VALUE FOR SHUTOFF SURGE PRESSURE OF PRESSURE FUEL DISPENSING SYSTEMS
    A A 59503 : C NITROGEN, TECHNICAL
    SAE AS 21237 : 2011 RING, CARGO TIEDOWN (25,000 LB), TYPE 4
    STANAG 3971 : 2013 AIR-TO-AIR REFUELLING - ATP-56
    MIL A 25896 : E ADAPTER, PRESSURE FUEL SERVICING, NOMINAL 2.5 INCH DIAMETER
    MIL B 8075 : D BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF
    SAE ARP 699 : 2015 HIGH TEMPERATURE PNEUMATIC DUCT SYSTEMS FOR AIRCRAFT
    SAE AIR 781 : 1962 GUIDE FOR DETERMINING ENGINE STARTER DRIVE TORQUE REQUIREMENTS
    SAE ARP 1665 : 1997 DEFINITION OF PRESSURE SURGE TEST AND MEASUREMENT METHODS FOR RECEIVER AIRCRAFT
    SAE AIR 1102 : 2011 TRANSPARENT AREA WASHING SYSTEMS FOR AIRCRAFT
    ABMA 9 : 2015 LOAD RATINGS AND FATIGUE LIFE FOR BALL BEARINGS
    SAE AIR 1826 : 2016 ACOUSTICAL CONSIDERATIONS FOR AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM DESIGN
    MIL PRF 6083 : G HYDRAULIC FLUID, PETROLEUM BASE, FOR PRESERVATION AND OPERATION
    MIL STD 704 : F AIRCRAFT ELECTRIC POWER CHARACTERISTICS
    SAE AS 943 : 1986 STARTER, PNEUMATIC, AIRCRAFT ENGINE, GENERAL SPECIFICATION FOR
    SAE AS 81820 : 2014 BEARINGS, PLAIN, SELF-ALIGNING, SELF-LUBRICATING, LOW SPEED OSCILLATION
    MS 3325 : 0 DRIVE PAD-ACCESSORY, 2.653 BC SQUARE, DESIGN STANDARD FOR
    MIL STD 130 : N IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
    A A 59281 : A CLEANING COMPOUND, SOLVENT MIXTURES
    MIL A 8863 : C AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES
    MIL PRF 46170 : E HYDRAULIC FLUID, RUST INHIBITED, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, NATO CODE NO. H-544
    MIL STD 883 : K TEST METHOD STANDARD - MICROCIRCUITS
    ABMA 11 : 2014 LOAD RATINGS AND FATIGUE LIFE FOR ROLLER BEARINGS
    SAE AMS P 5510 : 2013 O-RING, PREFORMED, STRAIGHT THREAD TUBE FITTING BOSS, TYPE 1 HYDRAULIC (-65 TO 160 DEGREES F)
    MIL STD 878 : B METHOD OF DIMENSIONING AND DETERMINING CLEARANCE FOR AIRCRAFT TIRES AND RIMS
    STANAG 3294 : 0 AIRCRAFT FUEL CAPS AND FUEL CAP ACCESS COVERS
    SAE AS 7949 : 2004 BEARINGS, BALL, AIRFRAME, ANTIFRICTION, GENERAL STANDARD
    SAE ARP 8615 : 2011 FUEL SYSTEM COMPONENTS: GENERAL SPECIFICATION FOR
    STANAG 3315 : 0 AIRCRAFT CABIN PRESSURIZING TEST CONNECTIONS
    MIL STD 810 : G ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    MIL PRF 7808 : L LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE
    MIL T 81259 : B TIE DOWN, AIRFRAME DESIGN, REQUIREMENTS FOR
    BB E 2879 : A EXTINGUISHER, FIRE, CARBON DIOXIDE (CO[2]), PORTABLE, WITH MOUNTING BRACKET, FOR AVIATION USE
    SAE AIR1639A : 1999 SAFETY CRITERIA FOR PNEUMATIC STARTING SYSTEMS
    STANAG 3109 : 2014 SYMBOL MARKING OF AIRCRAFT SERVICING AND SAFETY/HAZARDS POINTS
    AS 3990-1993 Mechanical equipment - Steelwork (Reconfirmed 2016)
    MIL STD 2218 : 0 THERMAL DESIGN, ANALYSIS & TEST PROCEDURES FOR AIRBORNE ELECTRONIC EQUIPMENT
    STANAG 3278 : 2014 AIRCRAFT TOWING ATTACHMENTS AND DEVICES
    SAE AIR 1467 : 1999 GAS ENERGY LIMITED STARTING SYSTEMS
    SAE AIR 1204 : 2009 CONTROL OF WATER CARRYOVER FROM THE ENVIRONMENTAL CONTROL SYSTEM AND CONDENSATION ON THE STRUCTURE
    ASME B46.1 : 2009 SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY)
    STANAG 3372 : 2014 LOW PRESSURE AIR AND ASSOCIATED ELECTRICAL CONNECTIONS FOR AIRCRAFT ENGINE STARTING
    SAE ARP 85 : 2012 AIR CONDITIONING SYSTEMS FOR SUBSONIC AIRPLANES
    MIL B 8584 : C BRAKE SYSTEMS, WHEEL, AIRCRAFT, DESIGN OF
    JSSG 2000 : B AIR SYSTEM
    JSSG 2007 : 0 JOINT SERVICE SPECIFICATION GUIDE - ENGINES, AIRCRAFT, TURBINE
    MS 3326 : 0 DRIVE PAD - ACCESSORY, 5,000 BC SQUARE, DESIGN STANDARD FOR
    MIL STD 1791 : C DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT
    SAE AS 1055 : 2013 FIRE TESTING OF FLEXIBLE HOSE, TUBE ASSEMBLIES, COILS, FITTINGS AND SIMILAR SYSTEM COMPONENTS
    MIL DTL 7891 : G FILLER VALVE, AIRCRAFT OXYGEN
    SAE AS 5877 : 2016 DETAILED SPECIFICATION FOR AIRCRAFT PRESSURE REFUELING NOZZLE
    JSSG 2010 : 1998 CREW SYSTEMS
    SAE AS 18802 : 2013 FUEL AND OIL LINES, AIRCRAFT, INSTALLATION OF
    SAE AS 6882 : 1999 WATER REPELLENT, WINDOW AND WINDSHIELD, GLASS AND PLASTIC
    MIL DTL 5513 : D SWIVEL JOINT, HYDRAULIC
    SAE AS 8905 : 2012 FITTINGS AND CARGO RINGS, TIE-DOWN, AIRCRAFT FLOOR
    SAE AIR 1174 : 2001 INDEX OF STARTING SYSTEM SPECIFICATIONS AND STANDARDS
    SAE AS 5440 : 2011 HYDRAULIC SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION REQUIREMENTS FOR
    SAE AMS P 83461 : 1998 PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT, IMPROVED PERFORMANCE AT 275 DEG F (135 DEG C)
    MS 3329 : A DRIVE PAD - ACCESSORY, 10,000 BC ROUND, DESIGN STANDARD FOR
    MIL E 7016 : F ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF
    SAE AIR 1662 : 2013 MINIMIZATION OF ELECTROSTATIC HAZARDS IN AIRCRAFT FUEL SYSTEMS
    MS 3328 : A DRIVE PAD - ACCESSORY, 8,000 BC ROUND, DESIGN STANDARD FOR
    SAE AMS 2430 : 2015 SHOT PEENING
    MIL STD 411 : F AIRCREW STATION ALERTING SYSTEMS
    SAE AIR 1087 : 1999 AIRCRAFT ACCESSORY DRAG TORQUE DURING ENGINE STARTS
    DOD PRF 85734 : A LUBRICATING OIL, HELICOPTER TRANSMISSION SYSTEM, SYNTHETIC BASE
    MIL HDBK 1568 : 0 MATERIAL AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS
    MIL HDBK 454 : B GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT
    SAE AIR 1667 : 2013 ROTOR BLADE ELECTROTHERMAL ICE PROTECTION DESIGN CONSIDERATIONS
    SAE AS 6038 : 2011 BEARINGS, BALL, BELLCRANK, ANTIFRICTION, AIRFRAME
    ASME B1.15 : 1995 UNIFIED INCH SCREW THREADS (UNJ THREAD FORM)
    NASM 1312 : 0 FASTENER TEST METHODS METHOD 11 TENSION FATIGUE
    SAE ARP 1270 : 2015 AIRCRAFT CABIN PRESSURIZATION CRITERIA
    MIL STD 7080 : 0 SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT
    SAE AS 50141 : 2012 TUBE, PNEUMATIC TIRE, AIRCRAFT
    MS 9950 : 0 COVER ACCESSORY DRIVE 5,000 BC ROUND QAD
    MIL PRF 87257 : C HYDRAULIC FLUID, FIRE RESISTANT, LOW TEMPERATURE, SYNTHETIC HYDROCARBON BASE, AIRCRAFT AND MISSILE
    SAE AIR 1811 : 2015 LIQUID COOLING SYSTEMS
    MS 3336 : 0 ACCESSORY DRIVES AIRCRAFT ENGINE, REFERENCE CHART FOR
    MIL STD 464 : C ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS
    SAE AS 90362 : 2016 CONNECTOR, RECEPTACLE, EXTERNAL ELECTRIC POWER, AIRCRAFT, 115/200 VOLT, 400 HERTZ
    MIL PRF 18148/3 : 0 RECEPTACLES, ELECTRIC, AIRCRAFT STORAGE BATTERY
    MIL PRF 83323 : D TESTER, UNIVERSAL RECEPTACLE, AERIAL REFUELING
    SAE AS 21236 : 2011 RING, CARGO TIEDOWN (10,000 LB), TYPE 3
    SAE AIR 1243 D: 2013(S2018) ANTI BLOW-BY DESIGN PRACTICE FOR CAP SEALS
    SAE AIR 1160 : 1999 AIRCRAFT ENGINE AND ACCESSORY DRIVES AND FLANGE STANDARDS
    STANAG 3098 : 2014 AIRCRAFT JACKING
    SAE ARP 994 : 2016 DESIGN OF TUBING INSTALLATIONS FOR AEROSPACE HYDRAULIC SYSTEMS
    MIL PRF 23699 : G LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE, NATO CODE NUMBERS: O-152, O-154, O-156, AND O-167
    SAE AIR 1277 : 2005 COOLING OF MILITARY AVIONIC EQUIPMENT
    MIL L 22589 : D LAUNCHING SYSTEM, NOSE GEAR TYPE, AIRCRAFT
    MS 9949 : 0 COVER - ACCESSORY DRIVE 8,000 BC ROUND QAD
    MIL STD 1568 : D MATERIALS AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS
    MIL L 8552 : C LANDING GEAR, AIRCRAFT SHOCK ABSORBER [AIR OIL TYPE]
    JSSG 2001 : B AIR VEHICLE
    MIL HDBK 5400 : 0 ELECTRONIC EQUIPMENT, AIRBORNE GENERAL GUIDELINES FOR
    MIL DTL 38999 : M CONNECTORS, ELECTRICAL, CIRCULAR, MINIATURE, HIGH DENSITY, QUICK DISCONNECT (BAYONET, THREADED OR BREECH COUPLING), ENVIRONMENT RESISTANT WITH CRIMP REMOVABLE CONTACTS OR HERMETICALLY SEALED WITH FIXED, SOLDERABLE CONTACTS, GENERAL SPECIFICATION FOR
    MIL STD 1290 : A LIGHT FIXED & ROTARY-WING AIRCRAFT CRASH RESISTANCE
    SAE AS 8879 : 2004 SCREW THREADS - UNJ PROFILE, INCH CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER
    MIL N 25161 : C NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2
    MIL S 8812 : D STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR
    MIL STD 882 : E STANDARD PRACTICE FOR SYSTEM SAFETY
    SAE AS 6039 : 2009 BEARINGS, BALL, ROD END, DOUBLE ROW, SELF-ALIGNING
    MIL STD 203 : G AIRCREW STATION CONTROLS AND DISPLAYS FOR FIXED WING AIRCRAFT
    STANAG 3747 : 2016 GUIDE SPECIFICATIONS (MINIMUM QUALITY STANDARDS) FOR AVIATION TURBINE FUELS (F-24, F-27, F-34, F-35, F-37, F-40 AND F-44)
    SAE AIR 4069 : 2016 SEALING OF INTEGRAL FUEL TANKS
    MS 33740 : C NIPPLE, PNEUMATIC STARTING, 3 INCH ID
    STANAG 3208 : 2009 AIR CONDITIONING CONNECTIONS
    SAE AS 21235 : 2011 FITTING, TIEDOWN, CARGO RING (10,000 LB) AND SEAT STUD, TYPE 2
    SAE AS 5498 : 2001 MINIMUM OPERATIONAL PERFORMANCE SPECIFICATION FOR INFLIGHT ICING DETECTION SYSTEMS
    NAS 331 : 0 BEARING INSTALLATION AND RETENTION BY SWAGING OR STAKING
    MIL T 26561 : C TESTER, TYPE MA-2 RECEPTION COUPLING BREAK-AWAY FORCE, PORTABLE
    MIL PRF 5041 : K TIRES, RIBBED TREAD, PNEUMATIC, AIRCRAFT
    SAE AIR 1539 : 2007 ENVIRONMENTAL CONTROL SYSTEM CONTAMINATION
    STANAG 3632 : 0 AIRCRAFT AND GROUND SUPPORT EQUIPMENT ELECTRICAL CONNECTIONS FOR STATIC GROUNDING
    SAE AS 8775 : 1998 HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES, GENERAL SPECIFICATION FOR
    STANAG 3447 : 2016 AIR-TO-AIR (AERIAL) REFUELLING EQUIPMENT: PROBE-DROGUE INTERFACE CHARACTERISTICS
    SAE ARP 731 : 2015 GENERAL REQUIREMENTS FOR APPLICATION OF VAPOR CYCLE REFRIGERATION SYSTEMS FOR AIRCRAFT
    SAE AS 50881 : 2015 WIRING AEROSPACE VEHICLE
    MIL STD 1472 : G HUMAN ENGINEERING
    SAE AS 21234 : 2011 FITTING, TIEDOWN, CARGO RING (5,000 LB) AND SEAT STUD, TYPE 1
    MIL PRF 83282 : D HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537
    MIL PRF 87260 : B FOAM MATERIAL, EXPLOSION SUPPRESSION, INHERENTLY ELECTROSTATICALLY CONDUCTIVE, FOR AIRCRAFT FUEL TANKS
    SAE ARP 1796 : 2015 ENGINE BLEED AIR SYSTEMS FOR AIRCRAFT
    MS 9948 : 0 COVER - ACCESSORY DRIVE 10,000 BS ROUND QAD
    SAE AIR 4766/2 : 2005 AIRBORNE CHEMICALS IN AIRCRAFT CABINS
    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
    SAE ARP 584D : 2012 COILED TUBING - CORROSION RESISTANT STEEL, HYDRAULIC APPLICATIONS, AEROSPACE
    MIL A 18717 : C ARRESTING HOOK INSTALLATIONS, AIRCRAFT
    MIL HDBK 310 : 0 DEPARTMENT OF DEFENSE HANDBOOK - GLOBAL CLIMATIC DATA FOR DEVELOPING MILITARY PRODUCTS
    SAE ARP 4386 : 2010 TERMINOLOGY AND DEFINITIONS FOR AEROSPACE FLUID POWER, ACTUATION AND CONTROL TECHNOLOGIES
    MIL HDBK 1599 : A BEARINGS, CONTROL SYSTEM COMPONENTS, AND ASSOCIATED HARDWARE USED IN THE DESIGN AND CONSTRUCTION OF AEROSPACE MECHANICAL SYSTEMS AND SUBSYSTEMS
    MIL STD 805 : B TOWING FITTING AND PROVISIONS FOR FIXED WING AIRCRAFT, DESIGN, REQUIREMENTS FOR
    STANAG 7073 : 2017 CONNECTORS FOR AIRCRAFT ELECTRICAL SERVICING POWER
    SAE ARP 777 : 2014 GAS ACTUATORS (LINEAR AND VANE ROTARY TYPE)
    SAE AS 35061 : 2013(R 2018) CONNECTOR, RECEPTACLE EXTERNAL ELECTRIC POWER, AIRCRAFT, 28 VOLT DC OPERATING POWER
    AASSEP-2 : 2014 PRESSURE REFUELLING CONNECTIONS AND DEFUELLING FOR AIRCRAFT
    MIL HDBK 1587 : 0 MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEM
    SAE ARP 986 : 2015 GUIDE FOR QUALIFICATION TESTING OF AIRCRAFT AIR VALVES
    SAE AS 8914 : 2016 BEARING, ROLLER, SELF-ALIGNING, AIRFRAME, ANTIFRICTION
    SAE ARP 4058 : 2007 GENERAL SPECIFICATION GUIDE FOR MECHANICAL GEARED ROTARY ACTUATORS
    AASSEP-1 : 2014 AIRCRAFT JACKING
    MIL DTL 5498 : G ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT
    SAE ARP 949 : 1999 TURBINE ENGINE STARTING SYSTEM DESIGN REQUIREMENTS
    STANAG 3105 : 2014 PRESSURE REFUELLING CONNECTIONS AND DEFUELLING FOR AIRCRAFT
    ISO 12103-1:2016 Road vehicles Test contaminants for filter evaluation Part 1: Arizona test dust
    MIL DTL 27422 : F TANK, FUEL, CRASH-RESISTANT, BALLISTIC-TOLERANT, AIRCRAFT
    MIL HDBK 189 : C RELIABILITY GROWTH MANAGEMENT
    STANAG 1135 : 2017 INTERCHANGEABILITY OF FUELS, LUBRICANTS AND ASSOCIATED PRODUCTS USED BY THE ARMED FORCES OF THE NORTH ATLANTIC TREATY NATIONS
    MS 3327 : A DRIVE PAD - ACCESSORY, 5,000 BC, ROUND, DESIGN STANDARD FOR
    ASTM D 5632/D5632M : 2017 : REDLINE Standard Specification for Halon 1301, Bromotrifluoromethane (CF3Br)
    MS 17793 : B SCHEMATIC WIRING DIAGRAM (EXTERNAL AC POWER CONNECTOR AIRCRAFT)
    MIL STD 1798 : C MECHANICAL EQUIPMENT AND SUBSYSTEMS INTEGRITY PROGRAM
    ASTM D 471 : 2016-02 TEST METHOD FOR RUBBER PROPERTY - EFFECT OF LIQUIDS
    JSSG 2006 : 0 JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES
    SAE AS 5202 : 2005 PORT OR FITTING END, INTERNAL STRAIGHT THREAD, DESIGN STANDARD
    MIL DTL 83413/6 : C CONNECTORS AND ASSEMBLIES, ELECTRICAL, AIRCRAFT GROUNDING: RECEPTACLES, TWO PIECE, WITH INSERTS AND HOUSINGS
    SAE ARP 4255 : 2012 ELECTRICAL ACTUATION SYSTEMS FOR AEROSPACE AND OTHER APPLICATIONS
    SAE AIR 1609 : 2005 AIRCRAFT HUMIDIFICATION
    MIL HDBK 221 : 0 FIRE PROTECTION DESIGN HANDBOOK FOR U.S. NAVY AIRCRAFT POWERED BY TURBINE ENGINES
    SAE AIR 4246 : 2012 CONTAMINANTS FOR AIRCRAFT TURBINE ENGINE FUEL SYSTEM COMPONENT TESTING
    STANAG 3209 : 2014 TYRE VALVE COUPLINGS
    MIL A 8860 : B AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR
    SAE AS 33611 : 2015 TUBE BEND RADII
    SAE AS 4073 : 2013(R2018) AIR CYCLE AIR CONDITIONING SYSTEMS FOR MILITARY AIR VEHICLES
    SAE AIR 4023 : 2016 AIRCRAFT TURBINE FUEL CONTAMINATION HISTORY AND ENDURANCE TEST REQUIREMENTS
    STANAG 3212 : 2017 DIAMETERS FOR GRAVITY FILLING ORIFICES
    SAE AIR 713 : 1988 GUIDE FOR DETERMINING, PRESENTING, AND SUBSTANTIATING TURBINE ENGINE STARTING AND MOTORING CHARACTERISTICS
    MIL STD 961 : E DEFENSE AND PROGRAM-UNIQUE SPECIFICATIONS FORMAT AND CONTENT
    SAE ARP 1107 : 2012 TAIL BUMPERS FOR PILOTED AIRCRAFT
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