|
MIL PRF 8565 : K
|
BATTERY STORAGE, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL STD 704 : F
|
AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
|
MIL PRF 29595 : A
|
BATTERIES AND CELLS, LITHIUM, RECHARGEABLE, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL PRF 81757 : D
|
BATTERIES AND CELLS, STORAGE, NICKEL-CADMIUM, AIRCRAFT - GENERAL SPECIFICATION FOR |
|
MIL HDBK 502 : A
|
PRODUCT SUPPORT ANALYSIS |
|
MIL STD 810 : G
|
ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
|
MIL E 85583 : A
|
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 : B
|
GENERATOR SYSTEM, ELECTRIC POWER, 400 HERTZ, ALTERNATING CURRENT, AIRCRAFT - GENERAL SPECIFICATION FOR |
|
JSSG 2010 : 1998
|
CREW SYSTEMS |
|
IEEE 12207 : 2008
|
SYSTEMS AND SOFTWARE ENGINEERING - SOFTWARE LIFE CYCLE PROCESSES |
|
MIL E 7016 : F
|
ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF |
|
MIL PRF 7032 : H
|
INVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL DTL 6162 : C
|
GENERATORS AND STARTER-GENERATORS, ELECTRICAL DIRECT CURRENT, NOMINAL 30 VOLTS, AIRCRAFT GENERAL SPECIFICATION FOR |
|
MIL STD 464 : C
|
ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
|
SAE AS 90362 : 2016
|
CONNECTOR, RECEPTACLE, EXTERNAL ELECTRIC POWER, AIRCRAFT, 115/200 VOLT, 400 HERTZ |
|
MIL STD 1796 : A
|
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 : E
|
STANDARD PRACTICE FOR SYSTEM SAFETY |
|
MIL STD 461 : G
|
REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
|
MIL HDBK 2165 : 0
|
TESTABILITY PROGRAM FOR SYSTEMS AND EQUIPMENTS |
|
MIL HDBK 1799 : 0
|
SURVIVABILITY, AERONAUTICAL SYSTEMS (FOR COMBAT MISSION EFFECTIVENESS) |
|
MIL PRF 24021 : K
|
ELECTRIC POWER MONITORS, EXTERNAL, AIRCRAFT |
|
SAE AS 50881 : 2015
|
WIRING AEROSPACE VEHICLE |
|
JSSG 2009 : A
|
AIR VEHICLE SUBSYSTEMS (JOINT SERVICE SPECIFICATION GUIDE) |
|
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 : A
|
DESIGNING AND DEVELOPING MAINTAINABLE PRODUCTS AND SYSTEMS - VOLUME 1 |
|
MIL STD 2161 : C
|
PAINT SCHEMES AND EXTERIOR MARKINGS FOR U.S. NAVY AND MARINE CORPS AIRCRAFT |
|
MS 17793 : B
|
SCHEMATIC WIRING DIAGRAM (EXTERNAL AC POWER CONNECTOR AIRCRAFT) |
|
MIL STD 1798 : C
|
MECHANICAL EQUIPMENT AND SUBSYSTEMS INTEGRITY PROGRAM |
|
MIL STD 1553 : B
|
DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA |
|
SAE AIR 4845 : 1993
|
THE FMECA PROCESS IN THE CONCURRENT ENGINEERING (CE) ENVIRONMENT |