SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT

Amended by

MIL-STD-7080 Notice 1 - Validation:2019

Available format(s)

PDF

Language(s)

English

Publisher

US Military Specs/Standards/Handbooks

Committee	FSC 16GP
DocumentType	Standard
Pages	26
ProductNote	NEW CHILD NOT 1 2019 IS NOW ADDED.
PublisherName	US Military Specs/Standards/Handbooks
Status	Current
Supersedes	MIL-E-7080 Revision B:1962

SAE AIR 4004 : 2015	GUIDE FOR INSTALLATION OF ELECTRICAL WIRE AND CABLE ON AIRCRAFT LANDING GEAR
SAE ARP 94910 : 2012	AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR
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)/17(2016) : 2016	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)/15(2015) : 2015	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)/13(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(PT0)/16(2015) : 2015	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
SAE AS 18276 : 2014	LIGHTING, AIRCRAFT INTERIOR, INSTALLATION OF
SAE ARP 4404 : 2013 : R2019	AIRCRAFT ELECTRICAL INSTALLATIONS
SAE ARP 4404 : 2013	AIRCRAFT ELECTRICAL INSTALLATIONS
MIL-HDBK-516 Revision C:2014	AIRWORTHINESS CERTIFICATION CRITERIA
MIL-DTL-9490 Revision E:2008	FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
SAE AS 50881 : 2015	WIRING AEROSPACE VEHICLE
JSSG-2009 Revision A:2013	Air Vehicle Subsystems
SAE AS 94900 : 2007	AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR

MIL-F-21346 Revision B:1976	FUSEHOLDERS, BLOCK, AND SHROUD TYPE, AND ASSOCIATED FUSE CLIPS; GENERAL SPECIFICATION FOR
MS33540 Revision J:1986	SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR
MIL-C-5026 Revision F:1984	CUTOUT RELAY, ENGINE GENERATOR
MIL F 15160 : G	FUSE, INSTRUMENT, POWER, AND TELEPHONE, GENERAL SPECIFICATION FOR
MIL-F-25381 Revision A:1972	FLIGHT TESTING, ELECTRICAL SYSTEM, PILOTED AIRCRAFT AND GUIDED MISSILE, GENERAL REQUIREMENTS FOR
MIL-STD-704 Revision F:2004	AIRCRAFT ELECTRIC POWER CHARACTERISTICS
MIL-STD-970 Base Document:1987	STANDARDS AND SPECIFICATIONS, ORDER OF PREFERENCE FOR THE SELECTION OF
MIL-F-85731 Base Document:1986	FASTENER, POSITIVE LOCKING, ELECTRONIC EQUIPMENT GENERAL SPECIFICATION FOR
MS3506 Revision C:1992	CONNECTOR, RECEPTACLE EXTERNAL ELECTRIC POWER, AIRCRAFT, 28 VOLT DC OPERATING POWER
MIL E 87219 : 0	ELECTRICAL POWER SYSTEMS, AIRCRAFT (REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT PATTERSON AFB OH 45433-6503
MIL-D-23222 Revision A:1971	DEMONSTRATION REQUIREMENTS FOR HELICOPTERS
MIL-P-81653 Revision B:1980	POWER CONTROLLER, SOLID STATE, GENERAL SPECIFICATION FOR
MIL I 7032 : G	INVERTER, AIRCRAFT, GENERAL SPECIFICATION FOR [ASG]
MS3505 Revision A:1992	COVER FOR USE WITH MS90362 EXTERNAL POWER RECEPTACLE
MIL-E-85583 Revision A:1987	ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR
MIL G 21480 : A	GENERATOR SYSTEM, 400 HERTZ ALTERNATING CURRENT, AIRCRAFT GENERAL SPECIFICATION FOR
MS3456 Revision D:1976	CONNECTORS, PLUG, ELECTRICAL, REAR RELEASE, CRIMP CONTACT, AN TYPE
MIL S 8805 : D	SWITCHES, AND SWITCH ASSEMBLIES, SENSITIVE AND PUSH, SNAP ACTION, GENERAL SPECIFICATION FOR
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 C 83383 : C	CIRCUIT BREAKER, REMOTE CONTROL THERMAL, TRIP FREE, GENERAL SPECIFICATION FOR
MS17845 Revision F:1992	SHIELD FOR USE WITH MS90362 EXTERNAL POWER RECEPTACLES
MIL-E-6051 Revision D:1967	ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM
MIL-M-25500 Revision B:1969	MOCKUP TESTING, ELECTRICAL SYSTEM, PILOTED AIRCRAFT AND GUIDED MISSILE, GENERAL REQUIREMENTS FOR
MIL-C-81790 Revision A:1990	CONNECTORS, RECEPTACLE, EXTERNAL ELECTRIC POWER, AIRCRAFT, GENERAL SPECIFICATION FOR
MIL-E-25499 Revision C:1970	ELECTRICAL SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION OF, GENERAL REQUIREMENTS FOR
MIL P 15024 : E	PLATES, TAGS AND BANDS FOR IDENTIFICATION OF EQUIPMENT
MIL G 6162 : B	GENERATOR AND STARTER GENERATOR, ELECTRIC DIRECT CURRENT, NOMINAL 30 VOLTS AIRCRAFT GENERAL SPECIFICATION
MIL-STD-889 Revision C:2016	DISSIMILAR METALS
MIL E 24021 : J NOTICE 1	ELECTRIC POWER MONITORS, EXTERNAL, AIRCRAFT
MIL C 83413 : A	CONNECTORS AND ASSEMBLIES, ELECTRICAL, AIRCRAFT GROUNDING, GENERAL SPECIFICATION FOR
MIL-C-85485 Revision A:1983	CABLE, ELECTRIC, FILTER LINE, RADIO FREQUENCY ABSORPTIVE
MIL S 8834 : F	SWITCH, TOGGLE, POSITIVE BREAK, GENERAL SPECIFICATION FOR
MIL C 27536 : B	COUPLING, CLAMP, GROOVED, V-BAND
MIL-STD-965 Revision B:1993	PARTS CONTROL PROGRAM
MIL S 22885 : E	SWITCH, PUSH BUTTON, ILLUMINATED, GENERAL SPECIFICATION FOR
MIL-V-85603 Base Document:1989	VOLTMETER, DC, AIRCRAFT, DIGITAL DISPLAY GENERAL SPECIFICATION FOR
MIL C 7115 : F	CONVERTER, AIRCRAFT, GENERAL SPECIFICATION FOR
MIL-F-8378 Revision B:1975	FREQUENCY METERS, AIRCRAFT 380 TO 420 HERTZ AND 350 TO 450 HERTZ
MS90362 Revision C:1976	CONNECTOR, RECEPTACLE EXTERNAL ELECTRIC POWER, AIRCRAFT, 115/200 VOLT, 400 HERTZ
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-461 Revision G:2015	REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
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-8879 Revision C:1991	SCREW THREADS, CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER, GENERAL SPECIFICATION FOR
MIL S 3950 : F	SWITCH, TOGGLE ENVIRONMENTALLY SEALED, GENERAL SPECIFICATION FOR
MIL B 8565 : J	BATTERY AND CELL, STORAGE, AIRCRAFT, GENERAL SPECIFICATION FOR
MIL G 7703 : D	GUARD, SWITCH, GENERAL SPECIFICATION FOR
MIL R 6106 : J	RELAYS, ELECTROMAGNETIC [INCLUDING ESTABLISHED RELIABILITY [ER] TYPES
MIL-S-4040 Revision G:2012	Solenoid, Electrical General Specification for (No S/S Document)
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
MIL-M-8650 Revision C:1976	Mockups, Aircraft, General Specification for
MIL-B-85584 Revision B:1995	BATTERY RELAY CONTROL UNIT, AIRCRAFT
MIL B 81757 : C	BATTERIES & CELLS STORAGE, NICKEL CADMIUM, AIRCRAFT GENERAL SPECIFICATION FOR
MIL-S-6150 Revision D:1987	STARTER, ENGINE, ELECTRICAL, DIRECT CRANKING, AIRCRAFT 28 VOLT DC
MIL C 5015 : G	CONNECTOR, ELECTRICAL, CIRCULAR THREADED AN TYPE, GENERAL SPECIFICATION FOR
MS25042 Revision K:1987	COVER, ELECTRICAL CONNECTOR, PLUG, AN TYPE
MIL-D-8708 Revision C:1991	DEMONSTRATION REQUIREMENTS FOR AIRPLANES
MIL-STD-462 Revision D:1993	MEASUREMENT OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS
MIL F 19207 : D (1) SUPP 1	FUSEHOLDER, EXTRACTOR POST TYPE, BLOWN FUSE INDICATING AND NONINDICATING GENERAL SPECIFICATION FOR
MIL-I-85071 Revision A:1992	INVERTERS, AIRCRAFT, DC TO AC, GENERAL SPECIFICATION FOR
MIL-S-81551 Base Document:1968	SWITCH, TOGGLE, HERMETICALLY SEALED, GENERAL SPECIFICATION FOR
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)
MIL-R-23761-1 Revision A:1977	REGULATOR CONTROL PANEL, AIRCRAFT DIRECT CURRENT GENERATOR, 28 VOLT
MIL F 5373 : D	FUSEHOLDER, BLOCK TYPE, AIRCRAFT
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-7742 Revision D:1991	SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR
MIL-STD-1553 Revision B:1978	DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA
MIL N 25027 : G	NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F
MIL-STD-961 Revision E:2003	DEFENSE AND PROGRAM-UNIQUE SPECIFICATIONS FORMAT AND CONTENT