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JSSG-2009 Revision A:2013

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

Air Vehicle Subsystems

Available format(s)

PDF

Superseded date

15-05-2021

Published date

20-11-2013

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

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

This specification establishes the item definition, performance, operating characteristics, reliability, maintainability, physical characteristics, general design, installation, and interface requirements for Air Vehicle Subsystems. This specification also establishes the analysis, inspection, demonstrations, and test procedures required by the Using Service for satisfactory completion and acceptance of subsystem component qualifications at the SFR, PDR, CDR, FF, and SVR Milestones. This specification also establishes the content and format to be used by the Using Service or contractor for preparation of the acquisition or model specification.

DevelopmentNote
Supersedes AFGS 87145 (A). (12/2007) Supersedes AFGS 87154 (A). (01/2014) Supersedes MIL F 87168. (02/2014)
DocumentType
Standard
Pages
2296
ProductNote
NEW CHILD NOT 1 2018 IS NOW ADDED
PublisherName
US Military Specs/Standards/Handbooks
Status
Superseded
SupersededBy
Supersedes

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MIL B 8075 : D BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF
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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
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MIL-PRF-6083 Revision G:2013 HYDRAULIC FLUID, PETROLEUM BASE, FOR PRESERVATION AND OPERATION
MIL-STD-704 Revision F:2004 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
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MIL-STD-130 Revision N:2007 IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
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MIL-PRF-46170 Revision E:2013 HYDRAULIC FLUID, RUST INHIBITED, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, NATO CODE NO. H-544
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MIL-STD-878 Revision B:2006 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 : 1998 AIRCRAFT CABIN PRESSURIZING TEST CONNECTIONS
MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
MIL-PRF-7808 Revision L:1997 LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE
MIL-T-81259 Revision B:1991 TIE DOWN, AIRFRAME DESIGN, REQUIREMENTS FOR
BB-E-2879 Revision A:2001 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 Base Document:1992 THERMAL DESIGN, ANALYSIS & TEST PROCEDURES FOR AIRBORNE ELECTRONIC EQUIPMENT
SAE AIR1184B : 2016 CAPACITIVE FUEL GAUGING SYSTEM ACCURACIES
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JSSG-2000 Revision B:2004 AIR SYSTEM
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SAE AS 6882 : 1999 WATER REPELLENT, WINDOW AND WINDSHIELD, GLASS AND PLASTIC
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SAE AIR 1174 : 2001 INDEX OF STARTING SYSTEM SPECIFICATIONS AND STANDARDS
ASME B46.1 : 2009 SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY)
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MIL-E-7016 Revision F:1976 ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF
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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
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MIL-HDBK-454 Revision B:2007 GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT
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SAE AS 50141 : 2012 TUBE, PNEUMATIC TIRE, AIRCRAFT
MS9950 Base Document:1970 COVER ACCESSORY DRIVE 5,000 BC ROUND QAD
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ASME B1.15 : 1995 UNIFIED INCH SCREW THREADS (UNJ THREAD FORM)
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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
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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
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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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STANAG 3208 : 2009 AIR CONDITIONING CONNECTIONS
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SAE AS 5498 : 2001 MINIMUM OPERATIONAL PERFORMANCE SPECIFICATION FOR INFLIGHT ICING DETECTION SYSTEMS
NAS331:2013 BEARING INSTALLATION AND RETENTION BY SWAGING OR STAKING
MIL-T-26561 Revision C:1984 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
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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
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MIL-HDBK-310 Base Document:1997 DEPARTMENT OF DEFENSE HANDBOOK - GLOBAL CLIMATIC DATA FOR DEVELOPING MILITARY PRODUCTS
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MIL-STD-805 Revision B:1987 TOWING FITTING AND PROVISIONS FOR FIXED WING AIRCRAFT, DESIGN, REQUIREMENTS FOR
STANAG 7073 : 2017 CONNECTORS FOR AIRCRAFT ELECTRICAL SERVICING POWER
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SAE ARP 986 : 2015 GUIDE FOR QUALIFICATION TESTING OF AIRCRAFT AIR VALVES
SAE AS 8914 : 2016 BEARING, ROLLER, SELF-ALIGNING, AIRFRAME, ANTIFRICTION
STANAG 7036 : 97 AMD 1 FUELS TO BE INTRODUCED INTO AND DELIVERED BY THE NATO PIPELINE SYSTEM (NPS)
SAE ARP 4058 : 2007 GENERAL SPECIFICATION GUIDE FOR MECHANICAL GEARED ROTARY ACTUATORS
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MIL-DTL-5498 Revision G:2013 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
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MIL-HDBK-189 Revision C:2011 RELIABILITY GROWTH MANAGEMENT
STANAG 1135 : 2017 INTERCHANGEABILITY OF FUELS, LUBRICANTS AND ASSOCIATED PRODUCTS USED BY THE ARMED FORCES OF THE NORTH ATLANTIC TREATY NATIONS
MS3327 Revision A:1969 DRIVE PAD - ACCESSORY, 5,000 BC, ROUND, DESIGN STANDARD FOR
ASTM D 5632/D5632M : 2017 : REDLINE Standard Specification for Halon 1301, Bromotrifluoromethane (CF<inf>3</inf>Br)
MS17793 Revision B:1974 SCHEMATIC WIRING DIAGRAM (EXTERNAL AC POWER CONNECTOR AIRCRAFT)
MIL-STD-1798 Revision C:2013 MECHANICAL EQUIPMENT AND SUBSYSTEMS INTEGRITY PROGRAM
ASTM D 471 : 2016-02 TEST METHOD FOR RUBBER PROPERTY - EFFECT OF LIQUIDS
JSSG-2006 Base Document:1998 JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES
SAE AS 5202 : 2005 PORT OR FITTING END, INTERNAL STRAIGHT THREAD, DESIGN STANDARD
MIL-DTL-83413-6 Revision C:2008 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 Base Document:1965 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 Revision B:1987 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 Revision E:2003 DEFENSE AND PROGRAM-UNIQUE SPECIFICATIONS FORMAT AND CONTENT
SAE ARP 1107 : 2012 TAIL BUMPERS FOR PILOTED AIRCRAFT

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