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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    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

    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    Superseded date:  23-07-2013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    Status Superseded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)

    MIL-I-83294 Base Document:1971 INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, GENERAL SPECIFICATION FOR
    MIL-F-87154 Base Document:1980 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
    DEFSTAN 00-970(PT0)/9(2012) : 2012 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)/7(2011) : 2011 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)/12(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/11(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/8(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/10(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
    SAE ARP 1401 : 2012 AIRCRAFT FUEL SYSTEM AND COMPONENT ICING TEST
    DEFSTAN 00-970(PT7)SEC7/3(2010) : 2010 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
    SAE AIR 1749 : 2013 AIRCRAFT ENGINE FUEL FEED AND TRANSFER COMPONENT PRESSURE DEFINITIONS
    MIL-N-25161 Revision C:1969 NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2

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

    MIL-A-25896 Revision E:1983 ADAPTER, PRESSURE FUEL SERVICING, NOMINAL 2.5 INCH DIAMETER
    MIL-STD-704 Revision F:2004 AIRCRAFT ELECTRIC POWER CHARACTERISTICS
    MIL B 83054 : B BAFFLE AND INERTING MATERIAL, AIRCRAFT FUEL TANK
    MIL-G-26988 Revision C:1971 GAGE, LIQUID QUANTITY, CAPACITOR TYPE TRANSISTORIZED, GENERAL SPECIFICATION FOR
    MIL-STD-701 Revision P:1992 LISTS OF STANDARD SEMICONDUCTOR DEVICES
    MS24355 Revision C:2016 COUPLING, RECEPTION - TYPE MA-2, FLIGHT-PRESSURE-REFUELING, ASSEMBLY OF
    MS24335 Revision C:1994 Flange, Bulkhead Mounting, Hydraulic, Self-Sealing Coupling
    MIL-C-38373 Revision B:1975 CAP, FLUID TANK FILLER
    BB-N-411 Revision C:1973 NITROGEN, TECHNICAL
    MIL STD 470 : B MAINTAINABILITY PROGRAM REQUIREMENTS (FOR SYSTEMS AND EQUIPMENTS)
    MIL-STD-889 Revision C:2016 DISSIMILAR METALS
    MS29520 Revision H:1992 ENVELOPE DIMENSIONS NOZZLE, PRESSURE FUEL SERVICING LOCKING AIRCRAFT, TYPE D-1 AND D-2
    MS29525 Revision F:1991 CAP PRESSURE FUEL SERVICING, NOMINAL 2 1/2 INCH DIAMETER, FLUSH TYPE
    MS33583 Revision C:1993 TUBING END, DOUBLE FLARE, STANDARD DIMENSIONS FOR
    MIL-STD-143 Revision B:1969 STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF
    MIL-STD-461 Revision G:2015 REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
    MS33645 Revision C:1977 RECEPTACLE, GROUNDING, INSTALLATION OF
    MIL-C-81511 Revision F:1992 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
    MS33584 Revision C:1990 TUBING END, STANDARD DIMENSIONS FOR FLARED
    MIL-STD-100 Revision G:1997 ENGINEERING DRAWINGS
    MIL-I-83294 Base Document:1971 INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, GENERAL SPECIFICATION FOR
    MS33611 Revision A:1983 TUBE BEND RADII
    MIL T 83323 : A (2) TESTER, UNIVERSAL RECEPTACLE, AERIAL REFUELING
    MS29526 Revision E:1991 CAP PRESSURE FUEL SERVICING, NOMINAL 2 1/2 INCH DIAMETER NON FLUSH TYPE
    QQ-P-416 Revision F:1991 PLATING, CADMIUM (ELECTRODEPOSITED)
    MS33514 Revision G:1990 FITTING END, STANDARD DIMENSIONS FOR FLARELESS TUBE CONNECTION AND GASKET SEAL (ASG)
    MIL-STD-1247 Revision D:2009 MARKINGS, FUNCTIONS AND HAZARDS DESIGNATIONS OF HOSE, PIPE, AND TUBE LINES FOR AIRCRAFT MISSILE, AND SPACE SYSTEMS
    MIL-R-27521 Revision A:1971 RECEPTACLE, FLYING BOOM, AERIAL REFUELING GENERAL SPECIFICATION FOR
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