MIL-E-7080 Revision B:1962
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Electric Equipment, Aircraft, Selection and Installation of (S/S by MIL-STD-7080)
Available format(s)
PDF
Published date
06-06-1962
Publisher
Superseded date
05-31-1994
Superseded by
US$20.00
Excluding Tax where applicable
Describes selection and installation of electric equipment in piloted aircraft.
| DocumentType |
Standard
|
| Pages |
22
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
| MIL-T-5842 Revision B:1985 | Transparent Areas On Aircraft Surfaces (Windshields And Canopies), Rain Removing And Washing Systems For, De-Frosting, De-Icing, 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 Refueling 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 Specification 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 AS8700 | 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 (No S/S Document) |
| 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 (S/S by SAE-AS8700) |
| 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 System, Aircraft, Design and Installation of, General Requirements for (No S/S Document) |
| 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 (No S/S Document) |
| MIL-C-81774 Revision A:1973 | Control Panel, Aircraft, General Requirements For |
| MIL-F-8615 Revision D:1976 | Fuel System Components, General Specification for (S/S by SAE-ARP8615) |
| 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 (S/S BY MIL-STD-2219) |
| MIL-D-8708 Revision C:1991 | Demonstration: Aircraft Weapon Systems, General Specification for |
| MIL-I-8672 Revision B:1969 | Installation and Test of Aircraft Pyrotechnic Equipment in Aircraft, General Specification for (No S/S Document) |
| MIL-L-5667 Revision B:1964 | Lighting Equipment, Aircraft Instrument Panel, General Specification for Installation of (No S/S Document) |
| MIL-C-18244 Revision A:1962 | Control and Stabilization Systems: Automatic, Piloted Aircraft, General Specification for |
| MIL R 6749 : 0 | RHEOSTATS: AIRCRAFT POWER |
| MS33540 Revision J:1986 | SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR (S/S BY NASM33540) |
| 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 (No S/S Document) |
| 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-L-6723 Revision C:1987 | Lights, Aircraft, General Specification for |
| MIL-E-6051 Revision D:1967 | Electromagnetic Compatibility Requirements, Systems (S/S by MIL-STD-464) |
| 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 (S/S by SAE-AS18276) |
| MIL S 8834 : F | SWITCH, TOGGLE, POSITIVE BREAK, GENERAL SPECIFICATION FOR |
| MS3106 Revision D:1992 | Connector, Plug, Electric, Straight, Solder Contacts, AN Type (S/S by SAE-AS31061) |
| MS25043 Revision K:1987 | Cover, Electrical, Connector, Receptacle, AN Type (S/S by SAE-AS25043) |
| MIL C 7115 : F | CONVERTER, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-STD-143 Revision B:1969 | STANDARDS & SPECIFICATIONS, ORDER OF PRECEDENCE FOR THE SELECTION OF (S/S BY MIL-STD-970) |
| 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: Location, Arrangement and Actuation of, 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 (NO S/S DOCUMENT) |
| 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 (No S/S Document) |
| MS 33630 : B | SWITCH, TOGGLE, INSTALLATION OF |
| MIL S 6743 : LATEST | SWITCHES, PUSHBUTTON AND LIMIT |
| 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) |
| AND10305 Revision 5:1949 | INSTALLATION CLEARANCE-TYPE XII AND TYPE XVII DRIVE (GENERATOR-POWER TAKE-OFF) (NO S/S DOCUMENT) |
| 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 6807 : D | SWITCHES, ROTARY, SELECTOR POWER - GENERAL SPECIFICATION FOR |
| AN3156 Revision 5:1953 | Clamp - Battery Hold-Down |
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