• JSSG-2001 Revision B:2004

    Current The latest, up-to-date edition.

    Air Vehicle

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    Published date:  30-04-2004

    Publisher:  US Military Specs/Standards/Handbooks

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    Table of Contents - (Show below) - (Hide below)

    1. SCOPE
    2. APPLICABLE DOCUMENTS
    3. REQUIREMENTS
    4. VERIFICATION
    5. PACKAGING
    6. NOTES

    Abstract - (Show below) - (Hide below)

    Describes general requirements and verification parameters, integration, performance, and functions for the preparation of an air vehicle program-unique specification.

    Scope - (Show below) - (Hide below)

    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.

    General Product Information - (Show below) - (Hide below)

    Development Note 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)
    Document Type Standard
    Product Note NEW CHILD NOT 3 2018 IS NOW ADDED.
    Publisher US Military Specs/Standards/Handbooks
    Status Current
    Supersedes

    Standards Referenced By This Book - (Show below) - (Hide below)

    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

    Standards Referencing This Book - (Show below) - (Hide below)

    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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