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  • MIL-E-7080 Revision B:1962

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    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF

    Available format(s):  PDF

    Superseded date:  31-05-1994

    Language(s): 

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    Describes selection and installation of electric equipment in piloted aircraft.

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

    Committee FSC 16GP
    Document Type Standard
    Publisher US Military Specs/Standards/Handbooks
    Status Superseded
    Superseded By

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

    MIL-T-5842 Revision B:1985 TRANSPARENT AREAS ON AIRCRAFT SURFACES [WINDSHIELDS AND CANOPIES] RAIN REMOVING AND WASHING SYSTEMS FOR, DEFROSTING, DEICING, DEFOGGING, GENERAL SPECIFICATION FOR
    MIL-L-6503 Revision H:1975 LIGHTING EQUIPMENT, AIRCRAFT, GENERAL SPECIFICATION FOR INSTALLATION OF
    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)/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
    MIL-W-5088 Revision L:1991 Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881)
    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 F 9490 : D FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-A-19736 Revision A:1960 AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR
    DEFSTAN 00-970(PT7)SEC2/SUPP4/5(2015) : INTERIM DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 4: DESIGN AND CONSTRUCTION (SUBPART D)
    MIL-B-81365 Base Document:1966 BLEED AIR SYSTEMS, GENERAL SPECIFICATIONS FOR
    DEFSTAN 00-970(PT7)SEC2/SUPP4/6(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 4: DESIGN AND CONSTRUCTION (SUBPART D)
    SAE AS 8700 : 1999 INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, 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-E-22285 Base Document:1959 EXTINGUISHING SYSTEM, FIRE, AIRCRAFT, HIGH-RATE DISCHARGE TYPE, INSTALLATION AND TEST OF
    MIL-D-23222 Revision A:1971 DEMONSTRATION REQUIREMENTS FOR HELICOPTERS
    MIL-I-8673 Base Document:1955 INSTALLATION AND TEST OF AIRCRAFT FLEXIBLE WEAPONS SYSTEMS
    MIL I 18373 : B INSTRUMENT AND NAVIGATION EQUIPMENT, AIRCRAFT, INSTALLATION OF
    MIL R 18370 : A RELEASE SYSTEMS FOR THE EJECTION OF LIFE RAFTS FROM NAVAL PATROL AND TRANSPORT SERIES AIRCRAFT, DESIGN REQUIREMENTS FOR
    MIL-I-8700 Revision A:1970 INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL I 7304 : B INDICATOR, PRESSURE TORQUE SENSITIVE TYPE A 9
    DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
    MIL-A-23622 Base Document:1963 ACTUATOR, AIRCRAFT, ELECTRO-MECHANICAL, LINEAR, DIRECT CURRENT
    MIL-E-25499 Revision C:1970 ELECTRICAL SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION OF, GENERAL REQUIREMENTS FOR
    MIL-I-8671 Revision D:1994 INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS
    MIL-F-23447 Base Document:1962 FIRE WARNING SYSTEMS, AIRCRAFT, RADIATION SENSING TYPE, TEST AND INSTALLATION OF
    MIL-S-38399 Revision A:1975 STARTER, PNEUMATIC, AIRCRAFT ENGINE GENERAL SPECIFICATION FOR
    MIL-C-81774 Revision A:1973 CONTROL PANEL, AIRCRAFT, GENERAL REQUIREMENTS FOR
    MIL-F-8615 Revision D:1976 FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG]
    MIL-S-7470 Revision A:1975 SHAFT, POWER TRANSMISSION, AIRCRAFT ACCESSORY, GENERAL SPECIFICATION FOR
    MIL-L-85762 Revision A:1988 LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION
    MIL-W-18326 Revision A:1956 WELDING OF MAGNESIUM ALLOYS, GAS AND ARC, MANUAL AND MACHINE PROCESSES FOR
    MIL-D-8708 Revision C:1991 DEMONSTRATION REQUIREMENTS FOR AIRPLANES
    MIL-I-8672 Revision B:1969 INSTALLATION AND TEST OF AIRCRAFT PYROTECHNIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR [ASG]
    MIL-L-5667 Revision B:1964 LIGHTING EQUIPMENT, AIRCRAFT INSTRUMENT PANEL, GENERAL SPECIFICATION FOR INSTALLATION OF [ASG]
    MIL-C-18244 Revision A:1962 CONTROL AND STABILIZATION SYSTEMS, AUTOMATIC, PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR

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

    MIL R 6749 : 0 RHEOSTATS: AIRCRAFT POWER
    MS33540 Revision J:1986 SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR
    MIL F 15160 : G FUSE, INSTRUMENT, POWER, AND TELEPHONE, GENERAL SPECIFICATION FOR
    MIL-L-6503 Revision H:1975 LIGHTING EQUIPMENT, AIRCRAFT, GENERAL SPECIFICATION FOR INSTALLATION OF
    MIL S 6744 : LATEST
    MIL I 7032 : G INVERTER, AIRCRAFT, GENERAL SPECIFICATION FOR [ASG]
    MIL-C-7762 Revision A:1967 COMPASS, INSTALLATION OF
    MIL-S-61 Revision B:1959 SHUNTS, INSTRUMENT, EXTERNAL, 50 MILLIVOLT (LIGHTWEIGHT TYPE)
    MIL-A-6752 Revision A:1953 AMMETER, VOLTMETERS, AND LOADMETERS; DIRECT CURRENT
    MIL-L-6723 Revision C:1987 LIGHT, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-E-6051 Revision D:1967 ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM
    MIL G 6162 : B GENERATOR AND STARTER GENERATOR, ELECTRIC DIRECT CURRENT, NOMINAL 30 VOLTS AIRCRAFT GENERAL SPECIFICATION
    MIL-L-18276 Revision C:1964 LIGHTING, AIRCRAFT INTERIOR, INSTALLATION OF
    MIL S 8834 : F SWITCH, TOGGLE, POSITIVE BREAK, GENERAL SPECIFICATION FOR
    MS3106 Revision D:1992 CONNECTOR, PLUG, ELECTRIC, STRAIGHT, SOLDER CONTACTS, AN TYPE
    MS25043 Revision K:1987 COVER, ELECTRICAL CONNECTOR, RECEPTACLE, AN TYPE
    MIL C 7115 : F CONVERTER, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-STD-143 Revision B:1969 STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF
    MIL F 5372 : D FUSE, CURRENT LIMITER TYPE, AIRCRAFT
    MIL-M-8609 Revision B:1965 MOTOR, DC 28 VOLT SYSTEM AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-STD-203 Revision G:1991 AIRCREW STATION CONTROLS AND DISPLAYS FOR FIXED WING AIRCRAFT
    MIL F 15733 : G FILTERS & CAPACITORS, RADIO FREQUENCY INTERFERENCE
    MIL S 3950 : F SWITCH, TOGGLE ENVIRONMENTALLY SEALED, GENERAL SPECIFICATION FOR
    MIL G 7703 : D GUARD, SWITCH, GENERAL SPECIFICATION FOR
    MIL R 6106 : J RELAYS, ELECTROMAGNETIC [INCLUDING ESTABLISHED RELIABILITY [ER] TYPES
    MIL-STD-250 Revision D:1974 AIRCREW STATION CONTROLS AND DISPLAYS FOR ROTARY WING AIRCRAFT
    MIL-M-7969 Revision C:1965 Motors, Alternating Current, 400-Cycle, 115/200-Volt System, Aircraft, General Specification for
    MS 33539 : B INSTALLATION CLEARANCE TYPE XII DRIVE, (GENERATOR WIDE SPEED RANGE)
    L P 406 : LATEST PLASTICS, ORGANIC, GENERAL SPECIFICATION, TEST METHODS
    MIL-L-5667 Revision B:1964 LIGHTING EQUIPMENT, AIRCRAFT INSTRUMENT PANEL, GENERAL SPECIFICATION FOR INSTALLATION OF [ASG]
    MS 33630 : B SWITCH, TOGGLE, INSTALLATION OF
    MIL S 6743 : LATEST SWITCHES, PUSHBUTTON AND LIMIT
    MIL-B-5087 Revision B:1964 BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS
    MIL-W-5088 Revision L:1991 Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881)
    AND10305 Revision 5:1949 INSTALLATION CLEARANCE - TYPE 12 AND TYPE 17 DRIVE (GENERATOR - POWER TAKE-OFF)
    MIL-F-7179 Revision G:1993 FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM
    MIL-C-5809 Revision G:1987 CIRCUIT BREAKERS, TRIP-FREE, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL S 6807 : D SWITCHES, ROTARY, SELECTOR POWER - GENERAL SPECIFICATION FOR
    AN3156 Revision 5:1953 CLAMP - BATTERY HOLD-DOWN
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