MIL-PRF-8565 Revision K:2001
|
BATTERY STORAGE, AIRCRAFT, GENERAL SPECIFICATION FOR
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MIL-STD-704 Revision F:2004
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AIRCRAFT ELECTRIC POWER CHARACTERISTICS
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MIL-PRF-29595 Revision A:2011
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BATTERIES AND CELLS, LITHIUM, RECHARGEABLE, AIRCRAFT, GENERAL SPECIFICATION FOR
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MIL-PRF-81757 Revision D:1999
|
BATTERIES AND CELLS, STORAGE, NICKEL-CADMIUM, AIRCRAFT - GENERAL SPECIFICATION FOR
|
MIL-HDBK-502 Revision A:2013
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Product Support Analysis
|
MIL-STD-810 Revision G:2008
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ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
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MIL-E-85583 Revision A:1987
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ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR
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STANAG 3109 : 2014
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SYMBOL MARKING OF AIRCRAFT SERVICING AND SAFETY/HAZARDS POINTS
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MIL-PRF-21480 Revision B:2010
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Generator System, Electric Power, 400 Hertz, Alternating Current, Aircraft; General Specification for
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JSSG-2010 Base Document:1998
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Crew Systems
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IEEE/ISO/IEC 12207-2008
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ISO/IEC/IEEE International Standard - Systems and software engineering -- Software life cycle processes
|
MIL-E-7016 Revision F:1976
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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
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ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS
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SAE AS 90362 : 2016
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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
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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 1
|
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
|