AFGS-87219 Revision B:2012
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Current
The latest, up-to-date edition.
ELECTRICAL POWER SYSTEMS, AIRCRAFT
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. VERIFICATION
5. PACKAGING
6. NOTES
APPENDIX A - ELECTRICAL POWER SYSTEMS, AEROSPACE
VEHICLES HANDBOOK FOR
Determines the performance requirements and verifications for electric power subsystems (EPS) for aerospace vehicles, including aircraft, helicopters, and missiles.
| Committee |
FSC 61GP
|
| DevelopmentNote |
Supersedes MIL E 87219. (08/2003)
|
| DocumentType |
Standard
|
| Pages |
70
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| Supersedes |
| 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)/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)/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)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| MIL-PRF-8565 Revision K:2001 | BATTERY STORAGE, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
| MIL-PRF-29595 Revision A:2011 | BATTERIES AND CELLS, LITHIUM, RECHARGEABLE, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-PRF-81757 Revision D:1999 | BATTERIES AND CELLS, STORAGE, NICKEL-CADMIUM, AIRCRAFT - GENERAL SPECIFICATION FOR |
| MIL-HDBK-502 Revision A:2013 | Product Support Analysis |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-E-85583 Revision A:1987 | ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR |
| STANAG 3109 : 2014 | SYMBOL MARKING OF AIRCRAFT SERVICING AND SAFETY/HAZARDS POINTS |
| MIL-PRF-21480 Revision B:2010 | Generator System, Electric Power, 400 Hertz, Alternating Current, Aircraft; General Specification for |
| JSSG-2010 Base Document:1998 | Crew Systems |
| IEEE/ISO/IEC 12207-2008 | ISO/IEC/IEEE International Standard - Systems and software engineering -- Software life cycle processes |
| MIL-E-7016 Revision F:1976 | ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF |
| MIL-PRF-7032 Revision H:2010 | INVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-DTL-6162 Revision C:2000 | GENERATORS AND STARTER-GENERATORS, ELECTRICAL DIRECT CURRENT, NOMINAL 30 VOLTS, AIRCRAFT GENERAL SPECIFICATION FOR |
| MIL-STD-464 Revision C:2010 | ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
| SAE AS 90362 : 2016 | CONNECTOR, RECEPTACLE, EXTERNAL ELECTRIC POWER, AIRCRAFT, 115/200 VOLT, 400 HERTZ |
| MIL-STD-1796 Revision A:2011 | AVIONICS INTEGRITY PROGRAM (AVIP) |
| MIL C 7115 : F | CONVERTER, AIRCRAFT, GENERAL SPECIFICATION FOR |
| SAE AS 1831 : 1997 | ELECTRICAL POWER, 270 V DC, AIRCRAFT, CHARACTERISTICS AND UTILIZATION OF |
| MIL-STD-882 Revision E:2012 | System Safety |
| MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
| MIL-HDBK-2165 Base Document:1995 | Testability Program for Systems and Equipments |
| MIL-HDBK-1799 Base Document:1997 | SURVIVABILITY, AERONAUTICAL SYSTEMS (FOR COMBAT MISSION EFFECTIVENESS) |
| MIL-PRF-24021 Revision K:1998 | ELECTRIC POWER MONITORS, EXTERNAL, AIRCRAFT |
| SAE AS 50881 : 2015 | WIRING AEROSPACE VEHICLE |
| JSSG-2009 Revision A:2013 | Air Vehicle Subsystems |
| STANAG 7073 : 2017 | CONNECTORS FOR AIRCRAFT ELECTRICAL SERVICING POWER |
| SAE AS 35061 : 2013(R 2018) | CONNECTOR, RECEPTACLE EXTERNAL ELECTRIC POWER, AIRCRAFT, 28 VOLT DC OPERATING POWER |
| MIL-HDBK-470 Revision A:1997 | Designing and Developing Maintainable Products and Systems, Volume I |
| MIL-STD-2161 Revision C:2014 | Paint Schemes and Exterior Markings for U.S. Navy and Marine Corps Aircraft |
| MS17793 Revision B:1974 | SCHEMATIC WIRING DIAGRAM (EXTERNAL AC POWER CONNECTOR AIRCRAFT) |
| MIL-STD-1798 Revision C:2013 | MECHANICAL EQUIPMENT AND SUBSYSTEMS INTEGRITY PROGRAM |
| MIL-STD-1553 Revision B:1978 | DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA |
| SAE AIR 4845 : 1993 | THE FMECA PROCESS IN THE CONCURRENT ENGINEERING (CE) ENVIRONMENT |
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