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  • MIL F 38363 : B (3)

    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    FUEL SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR

    Available format(s): 

    Superseded date:  23-07-2013

    Language(s): 

    Published date:  12-01-2013

    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    Criteria for design, performance, installation, and testing and maintenance of the fuel system and subsystems of aircraft powered by air breathing engines.

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

    Document Type Standard
    Publisher US Military Specs/Standards/Handbooks
    Status Superseded

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

    SAE ARP 1401 : 2012 AIRCRAFT FUEL SYSTEM AND COMPONENT ICING TEST
    MIL I 83294 : 0 INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, GENERAL SPECIFICATION FOR
    DEFSTAN 00-970(PT7)SEC7/3(2010) : 2010 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
    MIL N 25161 : C NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2
    MIL F 87154 : 0 FUEL SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES WRIGHT PATTERSON AFB OH 45433-6503
    DEFSTAN 00-970(PT7)SEC7/1(2006) : 2006 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
    MIL T 25920 : C TESTS, GROUND AND FLIGHT, AIRCRAFT GAS TURBINE PROPULSION SYSTEM INSTALLATION
    DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
    SAE AIR 1749 : 2013 AIRCRAFT ENGINE FUEL FEED AND TRANSFER COMPONENT PRESSURE DEFINITIONS

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

    MIL A 25896 : E ADAPTER, PRESSURE FUEL SERVICING, NOMINAL 2.5 INCH DIAMETER
    MIL STD 704 : F AIRCRAFT ELECTRIC POWER CHARACTERISTICS
    MIL B 83054 : B BAFFLE AND INERTING MATERIAL, AIRCRAFT FUEL TANK
    MIL G 26988 : C GAGE, LIQUID QUANTITY, CAPACITOR TYPE TRANSISTORIZED, GENERAL SPECIFICATION FOR
    MIL STD 701 : P LISTS OF STANDARD SEMICONDUCTOR DEVICES
    MS 24355 : C COUPLING, RECEPTION - TYPE MA-2, FLIGHT-PRESSURE-REFUELING, ASSEMBLY OF
    MS 24335 : C FLANGE, BULKHEAD MOUNTING, HYDRAULIC, SELF-SEALING COUPLING
    MIL C 38373 : B CAP, FLUID TANK FILLER
    BB N 411 : C NITROGEN, TECHNICAL
    MIL STD 470 : B MAINTAINABILITY PROGRAM REQUIREMENTS (FOR SYSTEMS AND EQUIPMENTS)
    MIL STD 889 : C DISSIMILAR METALS
    MS 29520 : H ENVELOPE DIMENSIONS NOZZLE, PRESSURE FUEL SERVICING LOCKING AIRCRAFT, TYPE D-1 AND D-2
    MS 29525 : F CAP PRESSURE FUEL SERVICING, NOMINAL 2 1/2 INCH DIAMETER, FLUSH TYPE
    MS 33583 : C TUBING END, DOUBLE FLARE, STANDARD DIMENSIONS FOR
    MIL STD 143 : B STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF
    MIL STD 461 : G REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
    MS 33645 : C RECEPTACLE, GROUNDING, INSTALLATION OF
    MIL C 81511 : F CONNECTOR, ELECTRICAL, CIRCULAR, HIGH DENSITY, QUICK DISCONNECT ENVIRONMENT RESISTING, AND ACCESSORIES GENERAL SPECIFICATION FOR
    MIL V 38003 : NOTICE 1 VALVE, FUEL LEVEL CONTROL, FUEL TANK, AIRCRAFT GENERAL SPECIFICATION FOR
    MS 33584 : C TUBING END, STANDARD DIMENSIONS FOR FLARED
    MIL STD 100 : G ENGINEERING DRAWINGS
    MIL I 83294 : 0 INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, GENERAL SPECIFICATION FOR
    MS 33611 : A TUBE BEND RADII
    MIL T 83323 : A (2) TESTER, UNIVERSAL RECEPTACLE, AERIAL REFUELING
    MS 29526 : E CAP PRESSURE FUEL SERVICING, NOMINAL 2 1/2 INCH DIAMETER NON FLUSH TYPE
    QQ P 416 : F PLATING, CADMIUM (ELECTRODEPOSITED)
    MS 33514 : G FITTING END, STANDARD DIMENSIONS FOR FLARELESS TUBE CONNECTION AND GASKET SEAL (ASG)
    MIL STD 1247 : D MARKINGS, FUNCTIONS AND HAZARDS DESIGNATIONS OF HOSE, PIPE, AND TUBE LINES FOR AIRCRAFT MISSILE, AND SPACE SYSTEMS
    MIL R 27521 : A RECEPTACLE, FLYING BOOM, AERIAL REFUELING GENERAL SPECIFICATION FOR
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