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  • MIL-I-18802 Revision A:1962

    Withdrawn A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.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

    Available format(s):  PDF

    Withdrawn date:  18-03-1998

    Language(s): 

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    Describes installation of oil and fuel lines in aircraft.

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

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    Status Withdrawn

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

    MIL-O-19838 Base Document:1956 OIL SYSTEMS, AIRCRAFT, INSTALLATION AND TEST OF
    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)/7(2011) : 2011 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)/12(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)/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
    MIL-A-19736 Revision A:1960 AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR
    MIL-D-8685 Revision B:1967 DATA AND TESTS, ENGINEERING, CONTRACT REQUIREMENTS FOR GUIDED MISSILE TARGET SYSTEMS
    MIL-T-18232 Revision B:1968 TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR

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

    MIL-T-8606 Revision C:1973 TUBING, STEEL, CORROSION RESISTANT (18-8 STABILIZED AND EXTRA LOW CARBON)
    MS33786 Revision B:2013 FITTING, INSTALLATION, FLARED TUBE AND HOSE, SWIVEL
    MIL T 5578 : C TANK, FUEL, AIRCRAFT, SELF-SEALING
    MIL-F-18280 Revision F:1995 FITTING, FLARELESS TUBE, FLUID CONNECTION
    MIL H 25579 : E HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR
    MIL H 8794 : D HOSE, RUBBER, HYDRAULIC, FUEL AND OIL RESISTANT
    MS33515 Revision J:1973 FITTING END, STANDARD DIMENSIONS FOR BULKHEAD FLARELESS TUBE CONNECTIONS
    AND10104 : REV 5 TUBING, STEEL, CORROSION RESISTANT, ROUND, STANDARD DIMENSIONS FOR
    MS21919 Revision E:1981 CLAMP, LOOP TYPE, CUSHIONED, SUPPORT
    MS33656 Revision J:1987 FITTING END, STANDARD DIMENSIONS FOR FLARED TUBE CONNECTION AND GASKET SEAL
    MIL T 6396 : E TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING
    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
    MS33584 Revision C:1990 TUBING END, STANDARD DIMENSIONS FOR FLARED
    MS33611 Revision A:1983 TUBE BEND RADII
    MIL H 8795 : D HOSE ASSEMBLY, RUBBER HYDRAULIC, FUEL AND OIL RESISTANT
    MIL T 5579 : 0 TANK, SELF-SEALING OIL, AIRCRAFT
    MS33514 Revision G:1990 FITTING END, STANDARD DIMENSIONS FOR FLARELESS TUBE CONNECTION AND GASKET SEAL (ASG)
    MIL-B-5087 Revision B:1964 BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS
    MS28741 Revision K:2010 HOSE ASSEMBLY, DETACHABLE END FITTING, MEDIUM PRESSURE
    MIL C 22263 : B COUPLING FUEL LINE, FLEXIBLE, 125 PSI, GENERAL SPECIFICATION FOR
    MS33790 Base Document:1958 BEND DATA, MINIMUM, HYDRAULIC, PNEUMATIC, FUEL AND OIL HOSE
    MIL-S-7742 Revision D:1991 SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR
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