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CONNECTOR, PLUG, ELECTRICAL, SELF-LOCKING, COUPLING NUT, REAR RELEASE, CRIMP CONTACT, AN TYPE
- Aerospace Standard
Published January 04, 2018 by SAE International in United States
Downloadable datasets availableAnnotation ability available
DOCUMENT REVISED TO CLARIFY TORQUE REQUIREMENTS AND DESIGN INTENT OF ANTI-DECOUPLING MECHANISM REQUIREMENTS.
Data Sets - Support Documents
|TABLE 2||FINAL/BREAKAWAY AND FREE-ROTATING TORQUES|
SAE Subcommittee AE-8C1, Connectors, shall be associated with those activities directed by the parent SAE Aerospace Council and the SAE Aerospace Electronics and Electrical Distribution Systems Committee, for the development and application of electrical optical connector and associated hardware standards and specifications. SAE Subcommittee shall also serve the needs of the Navy, Army, and Air Force through the establishment and maintenance of User Advisory Committees.
|ANSI/Y14.5||This document is not part of the subscrption.|
|MIL-C-27500||This document is not part of the subscrption.|
|MIL-C-5015||This document is not part of the subscrption.|
|MIL-STD-1651||This document is not part of the subscrption.|
|MIL-W-25038||This document is not part of the subscrption.|
|MIL-W-25038/1||This document is not part of the subscrption.|
|MS3459C||This document is not part of the subscrption.|
|MS81969/14||This document is not part of the subscrption.|
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