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Circuit Breakers, Trip-Free, Aircraft General Specification For
- Aerospace Standard
- AS58091
- Issued
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
The primary function of this specification is to cover the general requirements of one-, two-, and three-pole trip-free circuit breakers for use in aircraft electric systems conforming to MIL-STD-704. As a secondary function, this specification may possibly cover the general requirements of one-, two- and three-pole circuit breakers for use in primary vehicles, other than aircraft, when mounted directly to the structure.
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Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
TABLE I | Qualification inspection (single phase circuit breakers) | |
TABLE IA | Qualification inspection (3-phase circuit breakers) | |
TABLE II | Sampling plan A tests | |
TABLE III | Group B inspection | |
TABLE IV | Sampling plan C tests | |
TABLE V | Impact force | |
TABLE VI | Strength of threaded parts | |
TABLE VII | Interruption (formerly rupture) test procedures | |
TABLE VIII | Single-phase circuit breakers | |
TABLE IX | Three-phase circuit breakers |
Issuing Committee
AE-8B1 Protective Devices Committee
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.
Reference
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