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WIRE, ELECTRICAL, POLYTETRAFLUOROETHYLENE/POLYIMIDE INSULATED, SMOOTH SURFACE, NORMAL WEIGHT, NICKEL-COATED HIGH STRNGTH OR ULTRA HIGH STRENGTH COPPER ALLOY, 260 °C, 600 VOLTS ROHS
- Aerospace Standard
Published October 24, 2019 by SAE International in United States
Downloadable datasets availableAnnotation ability available
SPECIFICATION UPDATED TO INCLUDE AS29606 CONDUCTOR REQUIREMENTS, ROHS RESTRICTIONS, HARMONIZATION WITH AS22759/187 AND AS22759 MODIFICATIONS.
Data Sets - Support Documents
|TABLE 1||CONSTRUCTION DETAILS FOR FINISHED WIRE|
|TABLE 2||WIRE INSULATION MATERIAL|
|TABLE 4||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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