|
MIL C 81991 : 0
|
CONVERTER, AIRCRAFT DC TO DC, BOOST GENERAL SPECIFICATION FOR |
|
MIL I 8500 : D
|
INTERCHANGEABILITY AND REPLACEABILITY OF COMPONENT PARTS FOR AEROSPACE VEHICLES |
|
SAE ARP 926 : 1997
|
FAULT/FAILURE ANALYSIS PROCEDURE |
|
MIL STD 704 : F
|
AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
|
SAE AIR 1221 : 1971
|
ELECTROMAGNETIC COMPATIBILITY (EMC) SYSTEM DESIGN CHECKLIST |
|
MIL P 81653 : B
|
POWER CONTROLLER, SOLID STATE, GENERAL SPECIFICATION FOR |
|
MIL STD 810 : G
|
ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
|
SAE AIR 1406 : 1993
|
LIGHTNING PROTECTION AND STATIC ELECTRIFICATION |
|
MIL G 21480 : A
|
GENERATOR SYSTEM, 400 HERTZ ALTERNATING CURRENT, AIRCRAFT GENERAL SPECIFICATION FOR |
|
SAE AS 1212 : 2012
|
ELECTRIC POWER, AIRCRAFT, CHARACTERISTICS AND UTILIZATION OF |
|
SAE ARP 935 : 2013
|
CONTROL PLAN/TECHNICAL CONSTRUCTION FILE |
|
DOD STD 1686 : 0
|
ELECTROSTATIC DISCHARGE CONTROL PROGRAM FOR PROTECTION OF ELECTRICAL AND ELECTRONIC PARTS ASSEMBLIES AND EQUIPMENT (EXCLUDING ELECTRICALLY INITIATED EXPLOSIVE DEVICES)(METRIC) |
|
MIL E 6051 : D
|
ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM |
|
MIL E 7016 : F
|
ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF |
|
MIL E 25499 : C
|
ELECTRICAL SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION OF, GENERAL REQUIREMENTS FOR |
|
MIL E 5400 : T
|
ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR |
|
SAE ARP1870A:1987(S2012)
|
Aerospace Systems Electrical Bonding and Grounding for Electromagnetic Compatibility and Safety(STABILIZED Aug 2012)
|
|
SAE AIR 1277 : 2005
|
COOLING OF MILITARY AVIONIC EQUIPMENT |
|
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 143 : B
|
STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF |
|
MIL STD 461 : G
|
REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
|
MIL R 6106 : J
|
RELAYS, ELECTROMAGNETIC [INCLUDING ESTABLISHED RELIABILITY [ER] TYPES |
|
MIL Q 9858 : A
|
QUALITY PROGRAM REQUIREMENTS |
|
MIL STD 462 : D
|
MEASUREMENT OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS |
|
MIL STD 1629 : A
|
PROCEDURES FOR PERFORMING A FAILURE MODE, EFFECTS AND CRITICALITY ANALYSIS |
|
MIL I 27273 : A
|
INVERTER, POWER, STATIC, GENERAL SPECIFICATION FOR |
|
MIL B 5087 : B
|
BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS |
|
MIL T 23103 : A
|
THERMAL PERFORMANCE EVALUATION, AIRBORNE ELECTRONIC EQUIPMENT AND SYSTEMS, GENERAL REQUIREMENTS FOR |
|
MIL STD 785 : B
|
RELIABILITY PROGRAM FOR SYSTEMS AND EQUIPMENT DEVELOPMENT AND PRODUCTION |
|
MIL STD 2073 : 1978
|
DOD MATERIEL, PROCEDURES FOR DEVELOPMENT AND APPLICATION OF PACKAGING REQUIREMENTS |
|
MIL E 81910 : A
|
ELECTRICAL POWER GENERATING AND CONTROL EQUIPMENT, AIRCRAFT, GENERAL SPECIFICATIONS FOR |
|
MIL STD 1553 : B
|
DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA |
|
SAE AS 486 : 1994
|
AIRCRAFT CIRCUIT BREAKER AND FUSE ARRANGEMENT |