JSSG-2001 Revision B:2004
Current
Current
The latest, up-to-date edition.
Air Vehicle
Available format(s)
PDF
Published date
30-04-2004
Publisher
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. VERIFICATION
5. PACKAGING
6. NOTES
Describes general requirements and verification parameters, integration, performance, and functions for the preparation of an air vehicle program-unique specification.
This Joint Service Specification Guide (JSSG) establishes general requirements and verification parameters, integration, performance, and functions for the preparation of an air vehicle program-unique specification. The program specification developed from this JSSG will be used for contractual commitments between the Government and the prime contractor for the procurement of an air vehicle.
| DevelopmentNote |
B NOTICE 1 - Notice of Validation. (02/2009) Supersedes MIL HDBK 1799. (07/2013) B NOTICE 2 - Notice of Validation. (12/2013) Supersedes MIL HDBK 336/1. (01/2014)
|
| DocumentType |
Standard
|
| Pages |
766
|
| ProductNote |
NEW CHILD NOT 3 2018 IS NOW ADDED.
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| Supersedes |
| ATP 3.3.4.6 : 2016 | AIR-TO-AIR (AERIAL) REFUELING EQUIPMENT: PROBE-DROGUE INTERFACE CHARACTERISTICS |
| STANAG 3447 : 2016 | AIR-TO-AIR (AERIAL) REFUELLING EQUIPMENT: PROBE-DROGUE INTERFACE CHARACTERISTICS |
| SAE ARP 94910 : 2012 | AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR |
| 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)/13(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)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-HDBK-510 Revision A:2014 | AEROSPACE FUELS CERTIFICATION |
| MIL-HDBK-510-1 Revision A:2010 | AEROSPACE FUELS CERTIFICATION |
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| JSSG-2009 Revision A:2013 | Air Vehicle Subsystems |
| SAE AS 94900 : 2007 | AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR |
| SAE AIR 1168/4 : 2016 | SAE AEROSPACE APPLIED THERMODYNAMICS MANUAL ICE, RAIN, FOG, AND FROST PROTECTION |
| SAE AS 1284 : 2015 | STANDARD TEST PROCEDURE AND LIMIT VALUE FOR SHUTOFF SURGE PRESSURE OF PRESSURE FUEL DISPENSING SYSTEMS |
| STANAG 3971 : 2013 | AIR-TO-AIR REFUELLING - ATP-56 |
| STANAG 3370 : 2004 | AIRCREW STATION ALERTING SYSTEMS |
| SAE ARP 1665 : 1997 | DEFINITION OF PRESSURE SURGE TEST AND MEASUREMENT METHODS FOR RECEIVER AIRCRAFT |
| STANAG 3217 : 2006 | OPERATION OF CONTROLS AND SWITCHES AT AIRCREW STATIONS |
| STANAG 3802 : 2008 | SCREWDRIVER RECESSES (HIGH PERFORMANCE) |
| MIL-F-8785 Revision C:1980 | FLYING QUALITIES OF PILOTED AIRPLANES |
| ISO 46:1973 | Aircraft — Fuel nozzle grounding plugs and sockets |
| MIL-STD-130 Revision N:2007 | IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
| STANAG 7096 : 0 | LOCATION, ACTUATION AND SHAPE OF AIRFRAME CONTROLS |
| MIL-DTL-5624 Revision W:2016 | TURBINE FUEL, AVIATION, GRADES JP-4 AND JP-5 |
| MIL-A-8863 Revision C:1993 | AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES |
| MIL-HDBK-1763 Base Document:1998 | AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES |
| STANAG 7041 : LATEST | INTEGRATED HELMET MOUNTED DISPLAYS FOR ROTARY WING AIRCRAFT |
| ATP 56 : B | AIR TO AIR REFUELLING |
| STANAG 3806 : 0 | AIRCRAFT HIGH PRESSURE GASEOUS NITROGEN SYSTEMS REPLENISHMENT CONNECTORS |
| STANAG 3869 : 0 | AIRCREW STATION CONTROL PANELS |
| STANAG 3294 : 0 | AIRCRAFT FUEL CAPS AND FUEL CAP ACCESS COVERS |
| STANAG 3315 : 1998 | AIRCRAFT CABIN PRESSURIZING TEST CONNECTIONS |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| STANAG 3701 : 0 | AIRCRAFT INTERIOR COLOUR SCHEMES |
| STANAG 7090 : 2007 | GUIDE SPECIFICATIONS FOR NATO GROUND FUELS |
| MIL-T-81259 Revision B:1991 | TIE DOWN, AIRFRAME DESIGN, REQUIREMENTS FOR |
| STANAG 7044 : 0 | FUNCTIONAL ASPECTS OF MISSION PLANNING STATION INTERFACE DESIGN |
| MIL-STD-1787 Revision B:1996 | AIRCRAFT DISPLAY SYMBOLOGY |
| STANAG 3278 : 2014 | AIRCRAFT TOWING ATTACHMENTS AND DEVICES |
| STANAG 3372 : 2014 | LOW PRESSURE AIR AND ASSOCIATED ELECTRICAL CONNECTIONS FOR AIRCRAFT ENGINE STARTING |
| STANAG 3504 : 0 | CATHODE RAY TUBE HEAD-DOWN DISPLAYS (MONOCHROME) |
| MIL-N-5877 Revision E:1992 | NOZZLE, PRESSURE FUEL SERVICING LOCKING TYPE D 1 AND D 2 NOMINAL 1 1/2 INCH DIAMETER |
| JSSG-2007 Base Document:1998 | JOINT SERVICE SPECIFICATION GUIDE - ENGINES, AIRCRAFT, TURBINE |
| STANAG 3681 : 0 | CRITERIA FOR PRESSURE REFUELLING OF AIRCRAFT |
| STANAG 3639 : 2004 | AIRCREW STATION DIMENSIONAL DESIGN FACTORS |
| ISO 102:1990 | Aircraft — Gravity filling orifices |
| MIL-STD-1760 Revision E:2007 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
| STANAG 3870 : 0 | EMERGENCY ESCAPE/EVACUATION LIGHTING |
| STANAG 3595 : 2009 | AIRCRAFT FITTING FOR PRESSURE REPLENISHMENT OF GAS TURBINE ENGINES WITH OIL |
| MIL PRF 5624 : S | TURBINE FUEL, AVIATION, GRADES JP-4, JP-5 AND JP-5/JP-8 ST |
| MIL-STD-411 Revision F:1997 | AIRCREW STATION ALERTING SYSTEMS |
| MIL P 15024 : E | PLATES, TAGS AND BANDS FOR IDENTIFICATION OF EQUIPMENT |
| MIL C 83733/17 : 0 | CONNECTOR, RACK AND PANEL, SPRING LOADED MOUNTING ASSEMBLY |
| STANAG 3237 : 1997 | APERTURE OF TERMINAL RING OR LINK OF AIRCRAFT LIFTING SLINGS |
| MIL-PRF-25017 Revision H:2011 | INHIBITOR, CORROSION/LUBRICITY IMPROVER, FUEL SOLUBLE (NATO S-1747) |
| STANAG 3847 : 0 | HELICOPTER IN-FLIGHT REFUELLING (HIFR) EQUIPMENT |
| MIL-HDBK-1791 Base Document:1997 | DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT |
| STANAG 3800 : 2001 | NIGHT VISION IMAGING SYSTEM (NVIS) INTERIOR LIGHTING COMPATIBILITY DESIGN CRITERIA |
| MIL-DTL-85110 Revision B:1997 | BAR, REPEATABLE RELEASE HOLDBACK (RRHB), AIRCRAFT LAUNCHING, GENERAL REQUIREMENT FOR |
| STANAG 3647 : 0 | NOMENCLATURE IN AIRCREW STATIONS |
| STANAG 2947 : 0 | TECHNICAL CRITERIA FOR A CLOSED CIRCUIT REFUELLING SYSTEM |
| MIL-STD-464 Revision C:2010 | ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
| STANAG 7042 : 0 | IMAGE INTENSIFYING NIGHT VISION DEVICES FOR AIRCRAFT |
| ASTM D 910 : 2017-05 | SPECIFICATION FOR LEADED AVIATION GASOLINES |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| STANAG 3499 : 0 | CHARACTERISTICS OF SUPPLY EQUIPMENT FOR LIQUID OXYGEN |
| STANAG 3098 : 2014 | AIRCRAFT JACKING |
| 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 |
| MIL-STD-809 Revision B:1986 | ADAPTER, AIRCRAFT, JACKING POINT, DESIGN AND INSTALLATION OF |
| STANAG 3224 : 2005 | AIRCRAFT INTERIOR AND EXTERIOR LIGHTING NIGHT VISION GOGGLE (NVG) AND NON-NVG COMPATIBLE |
| AAP-4 : 2004 | NATO STANDARDIZATION AGREEMENTS AND ALLIED PUBLICATIONS |
| RTCA DO 208 : 91 CHG NOT 1 93 | MINIMUM OPERATIONAL PERFORMANCE STANDARDS FOR AIRBORNE SUPPLEMENTAL NAVIGATION EQUIPMENT USING GLOBAL POSITIONING SYSTEM (GPS) |
| MIL-STD-882 Revision E:2012 | System Safety |
| STANAG 3547 : 0 | CHARACTERISTICS OF REPLENISHMENT EQUIPMENT FOR LIQUID NITROGEN |
| SAE ARP 1797 : 2014 | AIRCRAFT AND AIRCRAFT ENGINE FUEL PUMP LOW LUBRICITY FLUID ENDURANCE TEST |
| MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
| MIL-STD-1773 Base Document:1988 | FIBER OPTICS MECHANIZATION OF AN AIRCRAFT INTERNAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS |
| STANAG 3994 : 2007 | APPLICATION OF HUMAN ENGINEERING TO ADVANCED AIRCREW SYSTEMS |
| STANAG 7139 : 0 | AIRCRAFT ENGINE CONTROLS, SWITCHES, DISPLAYS, INDICATORS, GAUGES AND ARRANGEMENTS |
| MIL-HDBK-1797 Base Document:1997 | FLYING QUALITIES OF PILOTED AIRCRAFT |
| STANAG 3208 : 2009 | AIR CONDITIONING CONNECTIONS |
| MIL STD 1763 : A | AIRCRAFT STORES CERTIFICATION PROCEDURES |
| MIL STD 1807 : NOTICE 1 | CRASH SURVIVABILITY OF AIRCRAFT PERSONNEL |
| MIL-DTL-83133 Revision J:2015 | TURBINE FUEL, AVIATION, KEROSENE TYPE, JP-8 (NATO F-34), NATO F-35, AND JP-8+100 (NATO F-37) |
| MIL-A-8861 Revision B:1986 | AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS |
| STANAG 3766 : 2017 | GREASE NIPPLES |
| STANAG 3632 : 0 | AIRCRAFT AND GROUND SUPPORT EQUIPMENT ELECTRICAL CONNECTIONS FOR STATIC GROUNDING |
| STANAG 3447 : 2016 | AIR-TO-AIR (AERIAL) REFUELLING EQUIPMENT: PROBE-DROGUE INTERFACE CHARACTERISTICS |
| MIL-HDBK-1785 Base Document:1995 | SYSTEM SECURITY ENGINEERING PROGRAM MANAGEMENT REQUIREMENTS |
| STANAG 3871 : 2004 | NATO GLOSSARY OF AIRCRAFT - AIRCREW INTEGRATION (AI) SPECIALIST TERMINOLOGY AND ABBREVIATIONS |
| STANAG 3296 : 0 | AIRCRAFT GASEOUS OXYGEN REPLENISHMENT COUPLINGS |
| MIL-STD-1472 Revision G:2012 | HUMAN ENGINEERING |
| MIL T 83133 : D | TURBINE FUELS, AVIATION, KEROSENE TYPES, NATO F-34 (JP-8) AND NATO F-35 |
| MIL-PRF-83282 Revision D:1997 | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537 |
| MIL-STD-1366 Revision E:2006 | INTERFACE STANDARD FOR TRANSPORTABILITY CRITERIA |
| SAE ARP 1420 : 2002 | GAS TURBINE ENGINE INLET FLOW DISTORTION GUIDELINES |
| STANAG 2946 : 0 | FORWARD AREA REFUELLING EQUIPMENT |
| MIL F 16884 : J | FUEL, NAVAL DISTILLATE |
| STANAG 3705 : 0 | HUMAN ENGINEERING DESIGN CRITERIA FOR CONTROLS AND DISPLAYS IN AIRCREW STATIONS |
| MIL-A-8243 Revision D:1985 | ANTI-ICING AND DEICING-DEFROSTING FLUIDS |
| MIL-HDBK-310 Base Document:1997 | DEPARTMENT OF DEFENSE HANDBOOK - GLOBAL CLIMATIC DATA FOR DEVELOPING MILITARY PRODUCTS |
| MIL-STD-805 Revision B:1987 | TOWING FITTING AND PROVISIONS FOR FIXED WING AIRCRAFT, DESIGN, REQUIREMENTS FOR |
| AFGS-87242 Revision A:1991 | FLIGHT CONTROL SYSTEM - GENERAL SPECIFICATION FOR |
| STANAG 3258 : 0 | POSITION OF PILOT OPERATED NAVIGATION AND RADIO CONTROLS |
| ISO 45:1990 | Aircraft — Pressure refuelling connections |
| STANAG 3219 : 0 | LOCATION AND GROUPING OF ELECTRICAL SWITCHES IN AIRCRAFT |
| MIL STD 1533 : 0 | AIRCRAFT INTERNAL TIME DIVISION COMMAND RESPONSE MULTIPLEX DATA BUS |
| STANAG 3436 : 0 | COLOURS AND MARKINGS USED TO DENOTE OPERATING RANGES OF AIRCRAFT INSTRUMENTS |
| STANAG 7140 : 0 | AIRCRAFT FLIGHT INSTRUMENTS - LAYOUT AND DISPLAY |
| STANAG 3105 : 2014 | PRESSURE REFUELLING CONNECTIONS AND DEFUELLING FOR AIRCRAFT |
| STANAG 3329 : 0 | NUMERALS AND LETTERS IN AIRCREW STATIONS |
| RTCA DO 236 : C2013 CHG 1 2014 | MINIMUM AVIATION SYSTEM PERFORMANCE STANDARDS: REQUIRED NAVIGATION PERFORMANCE FOR AREA NAVIGATION |
| JSSG-2010-5 Base Document:1998 | Crew Systems Aircraft Lighting Handbook |
| STANAG 3950 : 0 | HELICOPTER DESIGN CRITERIA FOR CREW CRASH PROTECTION AND ANTHROPOMETRIC ACCOMMODATION |
| STANAG 3209 : 2014 | TYRE VALVE COUPLINGS |
| STANAG 3682 : 0 | ELECTROSTATIC SAFETY CONNECTION PROCEDURES FOR AVIATION FUEL HANDLING AND LIQUID FUEL LOADING/UNLOADING OPERATIONS DURING GROUND TRANSFER AND AIRCRAFT FUELLING/DEFUELLING |
| STANAG 3212 : 2017 | DIAMETERS FOR GRAVITY FILLING ORIFICES |
| MIL-HDBK-1760 Revision A:2004 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
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