MIL-E-85583 Revision A:1987
Current
Current
The latest, up-to-date edition.
ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR
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Outlines three phase, four wire, 115/200 volt, 400 Hz ac variable input speed electric power generating channels, known as the General Package used on aircraft.
| Committee |
FSC 6115
|
| DevelopmentNote |
Supersedes MIL E 23001 (B) & MIL E 23001/3 (D). (06/2009)
|
| DocumentType |
Standard
|
| Pages |
47
|
| ProductNote |
NEW CHILD NOT 1 2019 IS NOW ADDED.
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| Supersedes |
| MIL-STD-7080 Base Document:1994 | Selection and Installation of Aircraft Electric Equipment |
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| 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)/14(2014) : 2014 | 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)/13(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)/12(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 |
| DEFSTAN 00-970(PT0)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
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| MIL-HDBK-516 Revision C:2014 | Airworthiness Certification Criteria |
| MIL-D-8708 Revision C:1991 | Demonstration: Aircraft Weapon Systems, General Specification for |
| MIL L 7808 : K (1) | LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE |
| MIL-STD-481 Revision B:1988 | CONFIGURATION CONTROL - ENGINEERING CHANGES (SHORT FORM), DEVIATIONS AND WAIVERS (S/S BY MIL-STD-973) |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| MIL-STD-704 Revision F:2004 | Aircraft Electric Power Characteristics |
| MIL-STD-130 Revision N:2007 | Identification Marking of U.S. Military Property |
| MIL L 23699 : E | LUBRICATING OIL, AIRCRAFT TURBINE ENGINES, SYNTHETIC BASE |
| MIL-STD-275 Revision E:1984 | PRINTED WIRING FOR ELECTRONIC EQUIPMENT (REFER TO IPC-D275 OR IPC-2221) |
| MS14169 Revision C:1980 | Circular Spline and Adapter Details Engine Driven Accessories |
| MIL-STD-1686 Revision C:1995 | Electrostatic Discharge Control Program for Protection of Electrical and Electronic Parts, Assemblies and Equipment (Excluding Electrically Initiated Explosive Devices) (S/S by ANSI/ESD S20.20) |
| MS3376 Revision B:1971 | NUT, SELF LOCKING, REDUCED HEIGHT, STEEL, 450 DEG. F, 12 POINT, CAPTIVE WASHER |
| MIL-STD-1562 Revision W:1991 | LISTS OF STANDARD MICROCIRCUITS (NO S/S DOCUMENT) |
| MIL R 39015 : C (3) | RESISTOR, VARIABLE, WIRE WOUND (LEAD SCREW ACTUATED), ESTABLISHED RELIABILITY GENERAL SPECIFICATION FOR |
| MIL-STD-1515 Revision A:1978 | Fastener Systems for Aerospace Applications (S/S by NASM1515) |
| MS90415 Revision C:1988 | NUT, SELF-LOCKING, STEEL, 160KSI, 450 DEG. F 12 POINT, CAPTIVE WASHER (S/S BY NASM90415) |
| MIL STD 2068 : 0 | RELIABILITY DEVELOPMENT TESTS |
| MIL-S-8879 Revision C:1991 | Screw Threads, Controlled Radius Root withIncreased Minor Diameter, General Specification for (S/S by SAE-AS8879) |
| MIL-STD-794 Revision E:1982 | PART AND EQUIPMENT, PROCEDURES FOR PACKAGING AND PACKING OF |
| MIL-T-7928 Revision G:1976 | Terminals, Lug: Splices, Conductor: Crimp Style, Copper, General Specification for (S/S BY SAE-AS7928) |
| MIL-P-116 Revision J:1988 | PRESERVATION, METHODS OF (S/S BY MIL-STD-2073-1) |
| MIL-Q-9858 Revision A:1963 | Quality Program Requirements (No S/S Document) |
| MIL H 5606 : G | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT; MISSILE AND ORDNANCE |
| MIL-STD-1629 Revision A:1980 | PROCEDURES FOR PERFORMING A FAILURE MODE, EFFECTS AND CRITICALITY ANALYSIS (NO S/S DOCUMENT) |
| QQ-P-416 Revision F:1991 | Plating, Cadmium (Electrodeposited) (S/Sby SAE-AMS-QQ-P-416) |
| MIL P 55110 : LATEST | PRINTED WIRING BOARD, RIGID GENERAL SPECIFICATION FOR |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
| MIL C 6021 : H NOTICE 1 | CASTINGS, CLASSIFICATION AND INSPECTION OF |
| FED-STD-595 Revision C:2008 | Colors Used in Government Procurement (S/S By SAE-AMS-STD-595) |
| MIL-STD-785 Revision B:1980 | RELIABILITY PROGRAM FOR SYSTEMS AND EQUIPMENT DEVELOPMENT AND PRODUCTION |
| MIL-E-81910 Revision A:1977 | Electrical Power Generating and Control Equipment, Aircraft, General Specifications for |
| MIL-S-7742 Revision D:1991 | Screw Threads, Standard, Optimum Selected Series: General Specification for |
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