• Shopping Cart
    There are no items in your cart

MIL-STD-7080 Base Document:1994

Current

Current

The latest, up-to-date edition.

Selection and Installation of Aircraft Electric Equipment

Available format(s)

PDF

Language(s)

English

Published date

05-31-1994

US$20.00
Excluding Tax where applicable

DocumentType
Standard
Pages
27
ProductNote
NEW CHILD NOT 1 2019 IS NOW ADDED.
PublisherName
US Military Specs/Standards/Handbooks
Status
Current
Supersedes

SAE AIR 4004 : 2015 GUIDE FOR INSTALLATION OF ELECTRICAL WIRE AND CABLE ON AIRCRAFT LANDING GEAR
SAE ARP94910 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 ARP4404C 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 AS50881F Wiring Aerospace Vehicle
JSSG-2009 Revision A:2013 Air Vehicle Subsystems
SAE AS94900 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 (No S/S Document)
MS33540 Revision J:1986 SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR (S/S BY NASM33540)
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, Electric System, Piloted Aircraft and Guided Missile, General Requirements for (No S/S Document)
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 (NO S/S DOCUMENT)
MIL-F-85731 Base Document:1986 Fastener, Positive Locking, Electronic Equipment General Specificationfor
MS3506 Revision C:1992 Connector, Receptacle External Electric Power, Aircraft, 28 Volt DC Operating Power (S/S by SAE-AS35061)
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 (S/S by SAE-AS35051)
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 (S/S by SAE-AS34561)
MIL S 8805 : D SWITCHES, AND SWITCH ASSEMBLIES, SENSITIVE AND PUSH, SNAP ACTION, GENERAL SPECIFICATION FOR
MIL-S-61 Revision B:1959 SHUNT, INSTRUMENT, EXTERNAL, 50 MILLIVOLT (LIGHTWEIGHT TYPE) (S/S BY A-A-55524)
MIL-A-6752 Revision A:1953 Ammeters, 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 (S/S by SAE-AS17845)
MIL-E-6051 Revision D:1967 Electromagnetic Compatibility Requirements, Systems (S/S by MIL-STD-464)
MIL-M-25500 Revision B:1969 Mockup Testing, Electrical System, Piloted Aircraft and Guided Missile, General Requirements for (No S/S Document)
MIL-C-81790 Revision A:1990 Connectors, Receptacle, External Electric Power, Aircraft, General Specification for (S/S by SAE-AS81790)
MIL-E-25499 Revision C:1970 Electrical System, Aircraft, Design and Installation of, General Requirements for (No S/S Document)
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 Galvanic Compatibility of Electrically Conductive Materials
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 (S/S BY MIL-HDBK-965)
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 (No S/S Document)
MS90362 Revision C:1976 Connector, Receptacle, External Electric Power, Aircraft, 115/200 Volt, 400 Hertz (S/S by SAE-AS90362)
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: Location, Arrangement and Actuation of, for Fixed Wing Aircraft
MIL F 15733 : G FILTERS & CAPACITORS, RADIO FREQUENCY INTERFERENCE
MIL-S-8879 Revision C:1991 Screw Threads, Controlled Radius Root withIncreased Minor Diameter, General Specification for (S/S by SAE-AS8879)
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 (NO S/S DOCUMENT)
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 VOLTS DC (NO S/S DOCUMENT)
MIL C 5015 : G CONNECTOR, ELECTRICAL, CIRCULAR THREADED AN TYPE, GENERAL SPECIFICATION FOR
MS25042 Revision K:1987 Cover, Electrical Connector; Plug, AN Type (S/S by SAE-AS25042)
MIL-D-8708 Revision C:1991 Demonstration: Aircraft Weapon Systems, General Specification for
MIL-STD-462 Revision D:1993 MEASUREMENT OF ELECTROMAGNTIC INTERFERENCE CHARACTERISTICS (S/S BY MIL-STD-461)
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 (S/S by MIL-PRF-7032)
MIL-S-81551 Base Document:1968 SWITCH, TOGGLE, HERMETICALLY SEALED, GENERAL SPECIFICATION FOR (NO S/S DOCUMENT)
MIL-B-5087 Revision B:1964 Bonding, Electrical, and Lightning Protection, for Aerospace Systems (S/S by MIL-STD-464)
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 Systems (S/S by MIL-STD-7179)
MIL-C-5809 Revision G:1987 Circuit Breakers, Trip-Free, Aircraft, General Specification for (S/S by SAE-AS58091)
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 Bus
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

Access your standards online with a subscription

  • Simple online access to standards, technical information and regulations.

  • Critical updates of standards and customisable alerts and notifications.

  • Multi-user online standards collection: secure, flexible and cost effective.

US$20.00
Excluding Tax where applicable