|
SAE AS 4373 : 2012
|
TEST METHODS FOR INSULATED ELECTRIC WIRE |
|
A A 52082 : D
|
TAPE, LACING AND TYING, TFE-FLUOROCARBON |
|
RTCA DO 178 : C2011
|
SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION |
|
MIL-STD-704 Revision F:2004
|
AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
|
A A 52084 : C
|
TAPE, LACING AND TYING, ARAMID |
|
MIL-STD-810 Revision G:2008
|
ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
|
SAE ARP 4754 : 2010
|
GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS |
|
A A 52083 : D
|
TAPE, LACING AND TYING, GLASS |
|
SAE AS 22759/34 : 2016
|
WIRE, ELECTRICAL, FLUOROPOLYMER-INSULATED, CROSS-LINKED MODIFIED ETFE, NORMAL WEIGHT, TIN-COATED, COPPER, 150 DEGREES C, 600 VOLT, ROHS |
|
SAE AS 5692A : 2009
|
ARC FAULT CIRCUIT BREAKER (AFCB), AIRCRAFT, TRIP-FREE SINGLE PHASE AND THREE PHASE 115 VAC, 400 HZ - CONSTANT FREQUENCY |
|
MIL-DTL-81381 Revision C:2005
|
WIRE, ELECTRIC, POLYIMIDE-INSULATED, COPPER OR COPPER ALLOY |
|
RTCA DO 254 : 2000
|
DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
|
SAE AS 25036 : 2015
|
TERMINAL, LUG, CRIMP STYLE, COPPER, INSULATED, RING TONGUE, BELL-MOUTHED, TYPE 2, CLASS 1, (FOR 105 DEGREES C TOTAL CONDUCTOR TEMPERATURE) |
|
NASM25027:2012
|
NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F |
|
MIL STD 1916 : 0
|
DOD PREFERRED METHODS FOR ACCEPTANCE OF PRODUCT |
|
MIL-HDBK-454 Revision B:2007
|
GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
|
MIL STD 889 : C
|
DISSIMILAR METALS |
|
MIL I 24768/1 : 0
|
INSULATION, PLASTIC, LAMINATED, THERMOSETTING, GLASS-CLOTH, MELAMINE-RESIN (GME) |
|
SAE ARP 4761 : 1996
|
GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
|
SAE AS 22759 : 2014
|
WIRE, ELECTRICAL, FLUOROPOLYMER-INSULATED, COPPER OR COPPER ALLOY |
|
ANSI/NCSL Z540 1 : 94(R2002)
|
CALIBRATION - CALIBRATION LABORATORIES AND MEASURING AND TEST EQUIPMENT - GENERAL REQUIREMENTS |
|
SAE AS 8879 : 2004
|
SCREW THREADS - UNJ PROFILE, INCH CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER |
|
SAE AS 7928 : 2011
|
TERMINALS, LUG: SPLICES, CONDUCTOR: CRIMP STYLE, COPPER, GENERAL SPECIFICATION FOR |
|
MIL I 24768/17 : 0
|
INSULATION, PLASTIC, LAMINATED, THERMOSETTING, GLASS-CLOTH, SILICONE-RESIN (GSG) |
|
SAE AS 50861 : 2011
|
WIRE, ELECTRIC, POLYVINYL CHLORIDE INSULATED, COPPER OR COPPER ALLOY |
|
SAE AS 81044 : 2011
|
WIRE, ELECTRICAL, CROSSLINKED POLYALKENE, CROSSLINKED ALKANE-IMIDE POLYMER, OR POLYARLYENE INSULATED, COPPER OR COPPER ALLOY |
|
SAE AS 27212 : 2011
|
TERMINAL BOARD ASSEMBLY, MOLDED-IN-STUD, ELECTRIC |
|
SAE AS 50881 : 2015
|
WIRING AEROSPACE VEHICLE |
|
MIL STD 202 : H
|
ELECTRONIC AND ELECTRICAL COMPONENT PARTS |
|
MIL STD 1285 : D
|
MARKING OF ELECTRICAL AND ELECTRONIC PARTS |
|
MIL STD 104 : C
|
LIMITS FOR ELECTRICAL INSULATION COLOR |
|
SAE AS 58091 : 2012
|
CIRCUIT BREAKERS, TRIP-FREE, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
ISO 10012-1:1992
|
Quality assurance requirements for measuring equipment Part 1: Metrological confirmation system for measuring equipment |