• MIL E 7080 : B

    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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

    Superseded date:  05-31-1994

    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    Status Superseded
    Superseded By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 : B 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
    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 : A 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 : 0 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 : 0 EXTINGUISHING SYSTEM, FIRE, AIRCRAFT, HIGH-RATE DISCHARGE TYPE, INSTALLATION AND TEST OF
    MIL D 23222 : A DEMONSTRATION REQUIREMENTS FOR HELICOPTERS
    MIL I 8673 : 0 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 : A 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 : 0 ACTUATOR, AIRCRAFT, ELECTRO-MECHANICAL, LINEAR, DIRECT CURRENT
    MIL E 25499 : C 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 : 0 FIRE WARNING SYSTEMS, AIRCRAFT, RADIATION SENSING TYPE, TEST AND INSTALLATION OF
    MIL S 38399 : A STARTER, PNEUMATIC, AIRCRAFT ENGINE GENERAL SPECIFICATION FOR
    MIL-C-81774A:1973 CONTROL PANEL, AIRCRAFT, GENERAL REQUIREMENTS FOR
    MIL-F-8615 Revision D:1976 FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG]
    MIL S 7470 : A SHAFT, POWER TRANSMISSION, AIRCRAFT ACCESSORY, GENERAL SPECIFICATION FOR
    MIL L 85762 : A LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION
    MIL W 18326 : A WELDING OF MAGNESIUM ALLOYS, GAS AND ARC, MANUAL AND MACHINE PROCESSES FOR
    MIL D 8708 : C 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 : A 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
    MS 33540 : J 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 : A COMPASS, INSTALLATION OF
    MIL S 61 : B SHUNTS, INSTRUMENT, EXTERNAL, 50 MILLIVOLT (LIGHTWEIGHT TYPE)
    MIL A 6752 : A AMMETER, VOLTMETERS, AND LOADMETERS; DIRECT CURRENT
    MIL L 6723 : C 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 : C LIGHTING, AIRCRAFT INTERIOR, INSTALLATION OF
    MIL S 8834 : F SWITCH, TOGGLE, POSITIVE BREAK, GENERAL SPECIFICATION FOR
    MS 3106 : D CONNECTOR, PLUG, ELECTRIC, STRAIGHT, SOLDER CONTACTS, AN TYPE
    MS 25043 : K COVER, ELECTRICAL CONNECTOR, RECEPTACLE, AN TYPE
    MIL C 7115 : F CONVERTER, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL STD 143 : B 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 : D AIRCREW STATION CONTROLS AND DISPLAYS FOR ROTARY WING AIRCRAFT
    MIL M 7969 : C MOTOR, 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 : B BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS
    MIL W 5088 : L WIRING, AEROSPACE VEHICLE
    AND10305 : 0005 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 : G CIRCUIT BREAKERS, TRIP-FREE, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL S 6807 : D SWITCHES, ROTARY, SELECTOR POWER - GENERAL SPECIFICATION FOR
    AN 3156 : 0005 CLAMP - BATTERY HOLD-DOWN
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