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  • MIL-C-38373 Revision B:1975

    Withdrawn A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

    CAP, FLUID TANK FILLER

    Available format(s):  PDF

    Withdrawn date:  12-12-2007

    Language(s): 

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    Gives various types of gravity fill, filler caps for fluid tanks.

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

    Committee FSC 1560
    Development Note B NOTICE 1 - Notice of Cancellation without Replacement. B NOTICE 2 - Notice of Reinstatement. B NOTICE 3 - Notice of Inactivation for New Design. B NOTICE 4 - Notice of Cancellation without Replacement. (01/2008)
    Document Type Standard
    Publisher US Military Specs/Standards/Handbooks
    Status Withdrawn

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

    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
    MIL BULL 343 : A DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF
    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)/11(2013) : 2013 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)/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
    DEFSTAN 00-970(PT7)SEC7/3(2010) : 2010 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
    MIL F 38363 : B (3) FUEL SYSTEM, AIRCRAFT, 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
    MIL-T-5955 Revision C:1970 TRANSMISSION SYSTEM, VTOL-STOL GENERAL REQUIREMENTS FOR

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

    MIL L 7808 : K (1) LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE
    MIL-STD-129 Revision R:2014 Military Marking for Shipment and Storage
    MIL-STD-130 Revision N:2007 IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
    MIL L 23699 : E LUBRICATING OIL, AIRCRAFT TURBINE ENGINES, SYNTHETIC BASE
    RR-C-271 Revision G:2016 CHAINS AND ATTACHMENTS, CARBON AND ALLOY STEEL
    MIL-L-27502 Base Document:1972 LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, ESTER BASE
    MIL T 5624 : R TURBINE FUEL, AVIATION, GRADES JP 4 AND JP 5
    MIL-STD-889 Revision C:2016 DISSIMILAR METALS
    MIL-STD-831 Base Document:1963 TEST REPORTS, PREPARATION OF
    MS27379 Revision A:1969 ADAPTER, FLUID TANK FILLER
    MS33588 Revision E:1984 NUTS, SELF LOCKING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY USAGE REQUIREMENTS FOR
    TT-S-735 Revision A:1988 STANDARD TEST FLUIDS, HYDROCARBON
    MS20995 Revision E:1974 WIRE, SAFETY OR LOCK
    MIL L 6081 : C LUBRICATING OIL, JET ENGINE
    MIL-G-5572 Revision F:1969 GASOLINE, AVIATION, GRADES 80/87, 100/130, 115/145
    MIL-STD-143 Revision B:1969 STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF
    MIL T 25524 : D TURBINE FUEL, AVIATION, THERMALLY STABLE
    MIL-S-8879 Revision C:1991 SCREW THREADS, CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER, GENERAL SPECIFICATION FOR
    MIL-STD-1523 Revision A:1984 AGE CONTROLS OF AGE-SENSITIVE ELASTOMERIC MATERIAL
    MIL-L-22851 Revision D:1990 LUBRICATING OIL, AIRCRAFT PISTON ENGINE, (ASHLESS DISPERSANT)
    MIL-STD-794 Revision E:1982 PART AND EQUIPMENT, PROCEDURES FOR PACKAGING AND PACKING OF
    MIL-L-6082 Revision E:1990 LUBRICATING OIL, AIRCRAFT PISTON ENGINE (NONDISPERSANT MINERAL OIL)
    MS33666 Revision C:1975 PACKING, PREFORMED AERONAUTICAL, ELASTOMERIC, RANGE OF SIZES (ASG)
    FED-STD-595 Revision C:2008 COLORS USED IN GOVERNMENT PROCUREMENT
    O-E-760 Revision D:1987 ETHYL ALCOHOL (ETHANOL), DENATURED ALCOHOL, PROPRIETARY SOLVENTS & SPECIAL INDUSTRIAL SOLVENTS
    MIL N 25027 : G NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F
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