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WIRE, ELECTRICAL, POLYTETRAFLUOROETHYLENE/POLYMIDE INSULATED, SMOOTH SURFACE, LIGHTWEIGHT, NICKEL COATED, EXTRA HIGH STRENGTH COPPER ALLOY, 260 °C, 600 VOLTS, ROHS
- Aerospace Standard
- AS22759/194A
- Revised
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Rationale
TABLE 1 OF THE STANDARD NEEDS TO BE UPDATED TO SUPPORT CURRENT QUALIFICATION ACTIVITIES TO REFLECT THE SLIGHT WEIGHT INCREASE OF THE CONDUCTOR AS SPECIFIED IN AS29606 AND THE EFFECT THAT IT HAD ON THE FINISHED WIRE.
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| 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 |
Issuing Committee
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.
Reference
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