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  • JSSG-2009 Revision A:2013

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    AIR VEHICLE SUBSYSTEMS (JOINT SERVICE SPECIFICATION GUIDE)

    Available format(s):  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    Superseded date:  15-05-2021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    Status Superseded
    Superseded By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)

    STANAG 7191 : 2013 AIR-TO-AIR (AERIAL) REFUELLING EQUIPMENT: BOOM-RECEPTACLE SYSTEM AND INTERFACE REQUIREMENTS
    SAE ARP 6078 : 2012 AIRCRAFT FUEL TANK INERTING SYSTEMS
    DEFSTAN 00-970(PT0)/17(2016) : 2016 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/14(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/15(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/13(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/16(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    AFGS-87219 Revision B:2012 ELECTRICAL POWER SYSTEMS, AIRCRAFT
    SAE AIR 4566 : 2015 CRASHWORTHY LANDING GEAR DESIGN
    MIL-HDBK-510 Revision A:2014 AEROSPACE FUELS CERTIFICATION
    SAE ARP 1796 : 2015 ENGINE BLEED AIR SYSTEMS FOR AIRCRAFT
    MIL-HDBK-510-1 Revision A:2010 AEROSPACE FUELS CERTIFICATION
    SAE AS 4073 : 2013(R2018) AIR CYCLE AIR CONDITIONING SYSTEMS FOR MILITARY AIR VEHICLES
    SAE AIR 1277 : 2005 COOLING OF MILITARY AVIONIC EQUIPMENT
    MIL-HDBK-516 Revision C:2014 AIRWORTHINESS CERTIFICATION CRITERIA
    MIL-DTL-9490 Revision E:2008 FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
    SAE AIR 4246 : 2012 CONTAMINANTS FOR AIRCRAFT TURBINE ENGINE FUEL SYSTEM COMPONENT TESTING
    MIL-PRF-83323 Revision D:2016 TESTER, UNIVERSAL RECEPTACLE, AERIAL REFUELING
    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 ARP 85 : 2012 AIR CONDITIONING SYSTEMS FOR SUBSONIC AIRPLANES
    SAE ARP 986 : 2015 GUIDE FOR QUALIFICATION TESTING OF AIRCRAFT AIR VALVES
    SAE AIR 805 : 2017 JET BLAST WINDSHIELD RAIN REMOVAL SYSTEMS FOR COMMERCIAL TRANSPORT AIRCRAFT
    SAE AIR 5774 : 2012 COMPOSITE FUEL TANKS, FUEL SYSTEM DESIGN CONSIDERATIONS
    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
    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

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

    A-A-59155 Base Document:2003 NITROGEN, HIGH PURITY, SPECIAL PURPOSE
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    SAE AS 21237 : 2011 RING, CARGO TIEDOWN (25,000 LB), TYPE 4
    STANAG 3971 : 2013 AIR-TO-AIR REFUELLING - ATP-56
    MIL-A-25896 Revision E:1983 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 Revision G:2013 HYDRAULIC FLUID, PETROLEUM BASE, FOR PRESERVATION AND OPERATION
    MIL-STD-704 Revision F:2004 AIRCRAFT ELECTRIC POWER CHARACTERISTICS
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    SAE AS 81820 : 2014 BEARINGS, PLAIN, SELF-ALIGNING, SELF-LUBRICATING, LOW SPEED OSCILLATION
    MS3325 Base Document:1968 DRIVE PAD-ACCESSORY, 2.653 BC SQUARE, DESIGN STANDARD FOR
    MIL-STD-130 Revision N:2007 IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
    A-A-59281 Revision A:2007 CLEANING COMPOUND, SOLVENT MIXTURES
    MIL-A-8863 Revision C:1993 AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES
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    SAE AS 1055 : 2013 FIRE TESTING OF FLEXIBLE HOSE, TUBE ASSEMBLIES, COILS, FITTINGS AND SIMILAR SYSTEM COMPONENTS
    MIL-DTL-7891 Revision G:2008 FILLER VALVE, AIRCRAFT OXYGEN
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    JSSG-2010 Base Document:1998 Crew Systems
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    SAE AS 8905 : 2012 FITTINGS AND CARGO RINGS, TIE-DOWN, AIRCRAFT FLOOR
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    ASME B46.1 : 2009 SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY)
    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°F (135°C)
    MS3329 Revision A:1969 DRIVE PAD - ACCESSORY, 10,000 BC ROUND, DESIGN STANDARD FOR
    MIL-E-7016 Revision F:1976 ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF
    SAE AIR 1662 : 2013 MINIMIZATION OF ELECTROSTATIC HAZARDS IN AIRCRAFT FUEL SYSTEMS
    MS3328 Revision A:1969 DRIVE PAD - ACCESSORY, 8,000 BC ROUND, DESIGN STANDARD FOR
    SAE AMS 2430 : 2015 SHOT PEENING
    MIL-STD-411 Revision F:1997 AIRCREW STATION ALERTING SYSTEMS
    SAE AIR 1087 : 1999 AIRCRAFT ACCESSORY DRAG TORQUE DURING ENGINE STARTS
    DOD-PRF-85734 Revision A:2004 LUBRICATING OIL, HELICOPTER TRANSMISSION SYSTEM, SYNTHETIC BASE
    MIL-HDBK-1568 Base Document:1996 MATERIAL AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS
    MIL-HDBK-454 Revision B:2007 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
    NASM1312:2012 FASTENER TEST METHODS METHOD 11 TENSION FATIGUE
    SAE ARP 1270 : 2015 AIRCRAFT CABIN PRESSURIZATION CRITERIA
    MIL-STD-7080 Base Document:1994 SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT
    SAE AS 50141 : 2012 TUBE, PNEUMATIC TIRE, AIRCRAFT
    MS9950 Base Document:1970 COVER ACCESSORY DRIVE 5,000 BC ROUND QAD
    MIL-PRF-87257 Revision C:2017 HYDRAULIC FLUID, FIRE RESISTANT, LOW TEMPERATURE, SYNTHETIC HYDROCARBON BASE, AIRCRAFT AND MISSILE
    SAE AIR 1811 : 2015 LIQUID COOLING SYSTEMS
    MS3336 Base Document:1970 ACCESSORY DRIVES AIRCRAFT ENGINE, REFERENCE CHART FOR
    MIL-STD-464 Revision C:2010 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 Base Document:2011 RECEPTACLES, ELECTRIC, AIRCRAFT STORAGE BATTERY
    MIL-PRF-83323 Revision D:2016 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 Revision G:2014 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 Revision D:1991 LAUNCHING SYSTEM, NOSE GEAR TYPE, AIRCRAFT
    MS9949 Base Document:1970 COVER - ACCESSORY DRIVE 8,000 BC ROUND QAD
    MIL-STD-1568 Revision D:2015 MATERIALS AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS
    MIL-L-8552 Revision C:1965 LANDING GEAR, AIRCRAFT SHOCK ABSORBER [AIR OIL TYPE]
    JSSG-2001 Revision B:2004 Air Vehicle
    MIL-HDBK-5400 Base Document:1995 ELECTRONIC EQUIPMENT, AIRBORNE GENERAL GUIDELINES FOR
    MIL-DTL-38999 Revision M:2015 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 Revision A:1988 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 Revision C:1969 NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2
    MIL-S-8812 Revision D:1975 STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR
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