MIL-STD-7080 Base Document:1994
Current
Current
The latest, up-to-date edition.
Selection and Installation of Aircraft Electric Equipment
Amended by
Available format(s)
PDF
Language(s)
English
Published date
31-05-1994
Publisher
£13.91
Excluding VAT
| DocumentType |
Standard
|
| Pages |
27
|
| ProductNote |
NEW CHILD NOT 1 2019 IS NOW ADDED.
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| Supersedes |
| 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 |
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| 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 ARP4404C | 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 |
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| 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 |
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