JSSG-2001 Revision B:2004
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Current
The latest, up-to-date edition.
Air Vehicle
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Published date
30-04-2004
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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.
| 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 |
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.
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| 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 |
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| MIL-HDBK-1763 Base Document:1998 | AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES |
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| 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 |
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| STANAG 3372 : 2014 | LOW PRESSURE AIR AND ASSOCIATED ELECTRICAL CONNECTIONS FOR AIRCRAFT ENGINE STARTING |
| STANAG 3504 : 0 | CATHODE RAY TUBE HEAD-DOWN DISPLAYS (MONOCHROME) |
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| JSSG-2007 Base Document:1998 | JOINT SERVICE SPECIFICATION GUIDE - ENGINES, AIRCRAFT, TURBINE |
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| 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 |
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| STANAG 3237 : 1997 | APERTURE OF TERMINAL RING OR LINK OF AIRCRAFT LIFTING SLINGS |
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| STANAG 3847 : 0 | HELICOPTER IN-FLIGHT REFUELLING (HIFR) EQUIPMENT |
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| STANAG 3647 : 0 | NOMENCLATURE IN AIRCREW STATIONS |
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| MIL-HDBK-1797 Base Document:1997 | FLYING QUALITIES OF PILOTED AIRCRAFT |
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| STANAG 3871 : 2004 | NATO GLOSSARY OF AIRCRAFT - AIRCREW INTEGRATION (AI) SPECIALIST TERMINOLOGY AND ABBREVIATIONS |
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| 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 |
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| MIL-STD-1366 Revision E:2006 | INTERFACE STANDARD FOR TRANSPORTABILITY CRITERIA |
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| MIL-A-8243 Revision D:1985 | ANTI-ICING AND DEICING-DEFROSTING FLUIDS |
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| AFGS-87242 Revision A:1991 | FLIGHT CONTROL SYSTEM - GENERAL SPECIFICATION FOR |
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| 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 |
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| STANAG 3329 : 0 | NUMERALS AND LETTERS IN AIRCREW STATIONS |
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| MIL-HDBK-1760 Revision A:2004 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
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