JSSG-2009 Revision A:2013

Superseded

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AIR VEHICLE SUBSYSTEMS (JOINT SERVICE SPECIFICATION GUIDE)

Available format(s): PDF

Superseded date: 05-15-2021

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.

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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
ISBN
Pages
Product Note	NEW CHILD NOT 1 2018 IS NOW ADDED
Published
Publisher	US Military Specs/Standards/Handbooks
Status	Superseded
Superseded By	JSSG-2009-1 Base Document:2018 JSSG-2009-2 Base Document:2018 JSSG-2009-8 Base Document:2018
Supersedes	AFGS 87145 : A NOTICE 1 AFGS-87154 Revision A:1992

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
NASM1515:2011	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 Revision C:2011	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 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
SAE AS 943 : 1986	STARTER, PNEUMATIC, AIRCRAFT ENGINE, GENERAL SPECIFICATION FOR
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
MIL-PRF-46170 Revision E:2013	HYDRAULIC FLUID, RUST INHIBITED, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, NATO CODE NO. H-544
MIL-STD-883 Revision K:2016	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 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
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
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 Revision C:1970	BRAKE SYSTEMS, WHEEL, AIRCRAFT, DESIGN OF
JSSG-2000 Revision B:2004	AIR SYSTEM
JSSG-2007 Base Document:1998	JOINT SERVICE SPECIFICATION GUIDE - ENGINES, AIRCRAFT, TURBINE
MS3326 Base Document:1968	DRIVE PAD - ACCESSORY, 5,000 BC SQUARE, DESIGN STANDARD FOR
MIL-STD-1791 Revision C:2017	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 Revision G:2008	FILLER VALVE, AIRCRAFT OXYGEN
SAE AS 5877 : 2016	DETAILED SPECIFICATION FOR AIRCRAFT PRESSURE REFUELING NOZZLE
JSSG-2010 Base Document: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 Revision D:2012	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
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
MIL-STD-882 Revision E:2012	STANDARD PRACTICE FOR SYSTEM SAFETY
SAE AS 6039 : 2009	BEARINGS, BALL, ROD END, DOUBLE ROW, SELF-ALIGNING
MIL-STD-203 Revision G:1991	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
MS33740 Revision C:1999	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
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
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 Revision G:2012	HUMAN ENGINEERING
SAE AS 21234 : 2011	FITTING, TIEDOWN, CARGO RING (5,000 LB) AND SEAT STUD, TYPE 1
MIL-PRF-83282 Revision D:1997	HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537
MIL-PRF-87260 Revision B:2006	Foam Material, Explosion Suppression, Inherently Electrostatically Conductive, for Aircraft Fuel Tanks
SAE ARP 1796 : 2015	ENGINE BLEED AIR SYSTEMS FOR AIRCRAFT
MS9948 Base Document:1970	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 Revision C:1993	ARRESTING HOOK INSTALLATIONS, AIRCRAFT
MIL-HDBK-310 Base Document:1997	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 Revision A:1997	BEARINGS, CONTROL SYSTEM COMPONENTS, AND ASSOCIATED HARDWARE USED IN THE DESIGN AND CONSTRUCTION OF AEROSPACE MECHANICAL SYSTEMS AND SUBSYSTEMS
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
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 Base Document:1996	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
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
AASSEP-1 : 2014	AIRCRAFT JACKING
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
MIL-DTL-27422 Revision F:2014	TANK, FUEL, CRASH-RESISTANT, BALLISTIC-TOLERANT, AIRCRAFT
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 (CF3Br)
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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