FUSE, CURRENT LIMITER TYPE, AIRCRAFT

Available format(s)

Hardcopy , PDF

Superseded date

05-04-2023

Language(s)

English

Published date

12-01-2015

Publisher

SAE International

1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. MARKING
6. NOTES

Specifies the requirements for current limiter type fuses for use in aircraft primary electrical power systems conforming to MIL-STD-704.

SAE AS28938A:2015(R2023)	FUSE, LIMITER TYPE, ENCLOSED LINK, INTERMEDIATE RATING, AIRCRAFT
MIL STD 11991 : A	GENERAL STANDARD FOR PARTS, MATERIALS, AND PROCESSES

MIL-STD-704 Revision F:2004	AIRCRAFT ELECTRIC POWER CHARACTERISTICS
SAE AS 28938 : 2015	FUSE, LIMITER TYPE, ENCLOSED LINK, INTERMEDIATE RATING, AIRCRAFT
MIL-STD-889 Revision C:2016	DISSIMILAR METALS
ANSI/NCSL Z540 1 : 94(R2002)	CALIBRATION - CALIBRATION LABORATORIES AND MEASURING AND TEST EQUIPMENT - GENERAL REQUIREMENTS
SAE AS 20659 : 2015	TERMINAL, LUG, CRIMP STYLE, COPPER, UNINSULATED, RING TONGUE, TYPE 1, CLASS 1, FOR 175 DEGREES C OR 260 DEGREES C TOTAL CONDUCTOR TEMPERATURE
SAE AS 7928 : 2011	TERMINALS, LUG: SPLICES, CONDUCTOR: CRIMP STYLE, COPPER, GENERAL SPECIFICATION FOR
SAE AS 50861 : 2011	WIRE, ELECTRIC, POLYVINYL CHLORIDE INSULATED, COPPER OR COPPER ALLOY
SAE AS 28937 : 2015	FUSE, LIMITER TYPE, ENCLOSED LINK, 5-60 AMP, AIRCRAFT
MIL-STD-202 Revision H:2015	ELECTRONIC AND ELECTRICAL COMPONENT PARTS
MIL-STD-1285 Revision D:2004	MARKING OF ELECTRICAL AND ELECTRONIC PARTS
SAE AS 53731 : 2014	FUSE HOLDER, BLOCK TYPE, AIRCRAFT
ISO 10012-1:1992	Quality assurance requirements for measuring equipment Part 1: Metrological confirmation system for measuring equipment

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