Circuit Breaker, Aircraft, Trip-Free Push Pull, Type I, Dual Safety, -55 Thru +121 Degree C
- Aerospace Standard
Data Sets - Support Documents
|TABLE VI||Fusing characteristic test (sample size vs overload)|
SAE Subcommittee AE-8B1, Protective Devices, shall be associated with those activities directed by the Aerospace Electronics and Electrical System Division of SAE, and SAE Committee AE-8, Aerospace Electric/Electronic Distribution Systems, for the development and application of protective devices and associated hardware standards and specifications.