This content is not included in your SAE MOBILUS subscription, or you are not logged in.
WIRE, ELECTRICAL, POLYTETRAFLUOROETHYLENE/POLYIMIDE INSULATED, NORMAL WEIGHT, NICKEL COATED, HIGH STRENGTH 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 AS22759/87 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.
* Redlines comparisons are available for those standards listed in the Revision History that contain a radio button. A redline comparison of the current version against a revision is accomplished by selecting the radio button next to the standard and then selecting 'compare'. At this time, Redline versions only exist for some AMS standards. SAE will continue to add redline versioning with ongoing updates to SAE MOBILUS.