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SAE AS 4373 : 2012
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TEST METHODS FOR INSULATED ELECTRIC WIRE
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A-A-52082 Revision D:2009
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TAPE, LACING AND TYING, TFE-FLUOROCARBON
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RTCA DO 178 : C2011
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SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
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MIL-STD-704 Revision F:2004
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AIRCRAFT ELECTRIC POWER CHARACTERISTICS
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A-A-52084 Revision C:2015
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Tape, Lacing and Tying, Aramid
|
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MIL-STD-810 Revision G:2008
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ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
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SAE ARP 4754 : 2010
|
GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS
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A-A-52083 Revision D:2015
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Tape, Lacing and Tying, Glass
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SAE AS 22759/34 : 2016
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WIRE, ELECTRICAL, FLUOROPOLYMER-INSULATED, CROSS-LINKED MODIFIED ETFE, NORMAL WEIGHT, TIN-COATED, COPPER, 150 DEGREES C, 600 VOLT, ROHS
|
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SAE AS 5692A : 2009
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ARC FAULT CIRCUIT BREAKER (AFCB), AIRCRAFT, TRIP-FREE SINGLE PHASE AND THREE PHASE 115 VAC, 400 HZ - CONSTANT FREQUENCY
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MIL-DTL-81381 Revision C:2005
|
WIRE, ELECTRIC, POLYIMIDE-INSULATED, COPPER OR COPPER ALLOY
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|
RTCA DO 254 : 2000
|
DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
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|
SAE AS 25036 : 2015
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TERMINAL, LUG, CRIMP STYLE, COPPER, INSULATED, RING TONGUE, BELL-MOUTHED, TYPE 2, CLASS 1, (FOR 105 DEGREES C TOTAL CONDUCTOR TEMPERATURE)
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|
NASM25027:2012
|
NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F
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|
MIL-STD-1916 Base Document:1996
|
DOD PREFERRED METHODS FOR ACCEPTANCE OF PRODUCT
|
|
MIL-HDBK-454 Revision B:2007
|
GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT
|
|
MIL-STD-889 Revision C:2016
|
DISSIMILAR METALS
|
|
MIL-I-24768-1 Base Document:1992
|
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
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|
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
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|
SAE AS 8879 : 2004
|
SCREW THREADS - UNJ PROFILE, INCH CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER
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|
SAE AS 7928 : 2011
|
TERMINALS, LUG: SPLICES, CONDUCTOR: CRIMP STYLE, COPPER, GENERAL SPECIFICATION FOR
|
|
MIL-I-24768-17 Base Document:1992
|
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 Revision H:2015
|
ELECTRONIC AND ELECTRICAL COMPONENT PARTS
|
|
MIL-STD-1285 Revision D:2004
|
MARKING OF ELECTRICAL AND ELECTRONIC PARTS
|
|
MIL-STD-104 Revision C:1986
|
LIMITS FOR ELECTRICAL INSULATION COLOR
|
|
ASME Y14.100 : 2017
|
ENGINEERING DRAWING PRACTICES - ENGINEERING DRAWING AND RELATED DOCUMENTATION PRACTICES
|
|
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
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