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WIRE, ELECTRICAL, POLYTETRAFLUOROETHYLENE/POLYMIDE INSULATED, LIGHT WEIGHT, NICKEL COATED, HIGH STRENGTH OR ULTRA HIGH STRENGTH COPPER ALLOY, 260 °C, 600 VOLT, ROHS
- Aerospace Standard
Published March 24, 2020 by SAE International in United States
Downloadable datasets availableAnnotation ability available
SPECIFICATION UPDATED TO INCLUDE AS29606 CONDUCTOR REQUIREMENTS, ROHS RESTRICTIONS AND AS22759 MODIFICATIONS.
Data Sets - Support Documents
|TABLE 1||CONSTRUCTION DETAILS FOR FINISHED WIRE|
|TABLE 2||WIRE INSULATION MATERIALS|
|TABLE 3||TAPE OVERLAP REQUIREMENTS|
|TABLE 4||FINISHED WIRE INSULATION PROPERTIES REQUIREMENTS|
|TABLE 5||TEST MANDREL AND TEST LOAD REQUIREMENTS|
|TABLE 6||FINISH WIRE PERFORMANCE CHARACTERISTICS|
AE-8D Wire and Cable Committee
SAE Subcommittee AE-8D Wire & Cable, shall be associated with those activities directed by the parent SAE Aerospace Council, the SAE Aerospace Electronics & Electrical System Division, and the SAE AE-8 Aerospace Electrical/Electronic Distribution Systems Committee, for the development and application of wires and cables and associated hardware standards and specifications.
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