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  • MIL E 25499 : C

    Withdrawn A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
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    ELECTRICAL SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION OF, GENERAL REQUIREMENTS FOR

    Available format(s):  Hardcopy, PDF

    Withdrawn date:  09-28-1995

    Language(s): 

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    Details general requirements for design and installation of ac and dc electrical systems in military aircraft.

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

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    Status Withdrawn

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

    MIL L 6503 : H LIGHTING EQUIPMENT, AIRCRAFT, GENERAL SPECIFICATION FOR INSTALLATION OF
    MIL STD 7080 : 0 SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT
    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)/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
    MIL D 83029 : A DRIVE ASSEMBLY, CONSTANT SPEED, GENERAL SPECIFICATION FOR
    MIL S 8512 : D SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF
    SAE ARP 4729 : 2017 DOCUMENT FOR 270 VOLTAGE DIRECT CURRENT (270 V DC) SYSTEM
    MIL F 8615 : D FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG]
    MIL R 25532 : A ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR
    MIL A 9482 : 0 ANTI-ICING EQUIPMENT FOR AIRCRAFT HEATED SURFACE TYPE, GENERAL SPECIFICATION FOR

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

    MS 24435 : A POWER RECEPTACLE, AIRCRAFT, ELECTRONIC TEST EQUIPMENT, WIRING OF
    MIL F 25381 : A FLIGHT TESTING, ELECTRICAL SYSTEM, PILOTED AIRCRAFT AND GUIDED MISSILE, GENERAL REQUIREMENTS FOR
    MIL STD 704 : F AIRCRAFT ELECTRIC POWER CHARACTERISTICS
    MIL I 7032 : G INVERTER, AIRCRAFT, GENERAL SPECIFICATION FOR [ASG]
    MIL STD 810 : G ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    MIL M 25500 : B MOCKUP TESTING, ELECTRICAL SYSTEM, PILOTED AIRCRAFT AND GUIDED MISSILE, GENERAL REQUIREMENTS FOR
    MIL E 7016 : F ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF
    MIL E 24021 : J NOTICE 1 ELECTRIC POWER MONITORS, EXTERNAL, AIRCRAFT
    MIL STD 461 : G REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
    MS 24442 : B WIRING DIAGRAM - EXTERNAL POWER RECEPTACLE, 28 VOLT-DC, COMMON BUS SYSTEM
    MIL STD 100 : G ENGINEERING DRAWINGS
    MIL STD 462 : D MEASUREMENT OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS
    MIL I 27273 : A INVERTER, POWER, STATIC, GENERAL SPECIFICATION FOR
    MS 17793 : B SCHEMATIC WIRING DIAGRAM (EXTERNAL AC POWER CONNECTOR AIRCRAFT)
    MIL W 5088 : L WIRING, AEROSPACE VEHICLE
    MIL E 7080 : B ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF
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