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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Air Vehicle Subsystems
Available format(s)
PDF
Superseded date
15-05-2021
Superseded by
JSSG-2009-1 Base Document:2018
JSSG-2009-2 Base Document:2018
JSSG-2009-8 Base Document:2018
Published date
20-11-2013
Publisher
Important note : All end users must be registered with an Account prior to user licenses being assigned.
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.
| DevelopmentNote |
Supersedes AFGS 87145 (A). (12/2007) Supersedes AFGS 87154 (A). (01/2014) Supersedes MIL F 87168. (02/2014)
|
| DocumentType |
Standard
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| Pages |
2296
|
| ProductNote |
NEW CHILD NOT 1 2018 IS NOW ADDED
|
| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
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.
| STANAG 7191 : 2013 | AIR-TO-AIR (AERIAL) REFUELLING EQUIPMENT: BOOM-RECEPTACLE SYSTEM AND INTERFACE REQUIREMENTS |
| SAE ARP6078 | 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 AS4073A | 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 AIR4170B | 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 ARP85F | Air Conditioning Systems for Subsonic Airplanes |
| SAE ARP 986 : 2015 | GUIDE FOR QUALIFICATION TESTING OF AIRCRAFT AIR VALVES |
| SAE AIR805D | Jet Blast Windshield Rain Removal Systems for Commercial Transport Aircraft |
| SAE AIR 5774 : 2012 | COMPOSITE FUEL TANKS, FUEL SYSTEM DESIGN CONSIDERATIONS |
| SAE AIR1168/4B | 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 ARP1270B | Aircraft Cabin Pressurization Criteria |
| A-A-59155 Base Document:2003 | Nitrogen, High Purity, Special Purpose |
| NASM1515:2011 | FASTENER SYSTEMS FOR AEROSPACE APPLICATIONS |
| SAE AMSI7171A | Insulation Blanket, Thermal-Acoustical |
| SAE AS1284B | Standard Test Procedure and Limit Value for Shutoff Surge Pressure of Pressure Fuel Dispensing Systems |
| A-A-59503 Revision C:2011 | NITROGEN, TECHNICAL |
| SAE AS21237A | RING, CARGO TIEDOWN (25 000 LB), TYPE IV |
| 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 ARP699E | 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 AIR1102B | Transparent Area Washing Systems for Aircraft |
| 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 AS943A | ENTIRE STANDARD REVISEDSTARTER, PNEUMATIC, AIRCRAFT ENGINE, GENERAL SPECIFICATION FOR |
| SAE AS81820D | 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 |
| SAE AMSP5510A | O-Ring, Preformed, Straight Thread Tube Fitting Boss, Type I Hydraulic (-65 to 160 °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 AS7949B | Bearings, Ball, Airframe, Antifriction, General Standard for |
| SAE ARP8615 | 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 | 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 AIR1467B | 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 ARP85F | 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 AS1055D | Fire Testing of Flexible Hose, Tube Assemblies, Coils, Fittings, and Similar System Components |
| MIL-DTL-7891 Revision G:2008 | FILLER VALVE, AIRCRAFT OXYGEN |
| SAE AS5877B | Detailed Specification for Aircraft Pressure Refueling Nozzle |
| JSSG-2010 Base Document:1998 | Crew Systems |
| SAE AS18802 | Fuel and Oil Lines, Aircraft, Installation of |
| SAE AS6882 | Water Repellent, Window and Windshield, Glass and Plastic |
| MIL-DTL-5513 Revision D:2012 | SWIVEL JOINT, HYDRAULIC |
| SAE AS8905A | Fittings and Cargo Rings, Tie-Down, Aircraft Floor |
| SAE AIR1174B | Index of Starting System Specifications and Standards |
| ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
| SAE AS5440A | Hydraulic Systems, Military Aircraft, Design and Installation, Requirements For |
| SAE AMSP83461 | 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 AIR1662A | Minimization of Electrostatic Hazards in Aircraft Fuel Systems |
| MS3328 Revision A:1969 | DRIVE PAD - ACCESSORY, 8,000 BC ROUND, DESIGN STANDARD FOR |
| SAE AMS2430T | Shot Peening, Automatic |
| MIL-STD-411 Revision F:1997 | AIRCREW STATION ALERTING SYSTEMS |
| SAE AIR1087B | 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 AIR1667A | Rotor Blade Electrothermal Ice Protection Design Considerations |
| SAE AS6038A | Bearing, Ball, Bellcrank, Antifriction, Airframe |
| NASM1312:2012 | FASTENER TEST METHODS METHOD 11 TENSION FATIGUE |
| SAE ARP1270B | 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 AIR1811A | Liquid Cooling Systems |
| MS3336 Base Document:1970 | Accessory Drives Aircraft Engine, Reference Chart for |
| ASME B1.15 : 1995 | UNIFIED INCH SCREW THREADS (UNJ THREAD FORM) |
| 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 AS21236A | RING, CARGO TIEDOWN (10 000 LB), TYPE III |
| SAE AIR1243D | Anti Blow-By Design Practice for Cap Seals |
| SAE AIR1160C | Aircraft Engine and Accessory Drives and Flange Standards |
| STANAG 3098 : 2014 | AIRCRAFT JACKING |
| SAE ARP994B | 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 | System Safety |
| SAE AS6039D | 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 AIR4069C | Sealing of Integral Fuel Tanks |
| MS33740 Revision C:1999 | NIPPLE, PNEUMATIC STARTING, 3 INCH ID |
| STANAG 3208 : 2009 | AIR CONDITIONING CONNECTIONS |
| SAE AS21235A | FITTING, TIEDOWN, CARGO RING (10 000 LB) AND SEAT STUD, TYPE II |
| 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 AIR1539B | 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 ARP731C | General Requirements for Application of Vapor Cycle Refrigeration Systems for Aircraft |
| SAE AS50881F | Wiring Aerospace Vehicle |
| MIL-STD-1472 Revision G:2012 | HUMAN ENGINEERING |
| SAE AS21234A | FITTING, TIEDOWN, CARGO RING (5000 LB) AND SEAT STUD, TYPE I |
| 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 ARP584C | 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 ARP4386C | 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 ARP777A | Gas Actuators (Linear and Vane Rotary Type) |
| SAE AS35061A | 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 AS8914B | 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 ARP4058A | Actuators: Mechanical, Geared Rotary, General Specification For |
| AASSEP-1 : 2014 | AIRCRAFT JACKING |
| MIL-DTL-5498 Revision G:2013 | ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT |
| SAE ARP949B | 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 (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 ARP4255A | 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 AS33611 | TUBE BEND RADII |
| SAE AS4073A | 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 AIR713A | 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 ARP1107B | Tail Bumpers for Piloted Aircraft |
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