This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Circuit Breaker, Aircraft, Trip-Free Push Pull, Type I, Dual Safety, -55 Thru +121 Degree C
- Aerospace Standard
- AS58091/1
- Issued
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| TABLE I | ||
| TABLE II | ||
| TABLE III | ||
| TABLE IV | ||
| TABLE V | ||
| TABLE VI | Fusing characteristic test (sample size vs overload) |
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
| Number | Title |
|---|---|
| MIL-W-22759/32 | This document is not part of the subscrption. |
| MIL-W-81381/21 | This document is not part of the subscrption. |
| MIL-W-83381/22 | This document is not part of the subscrption. |
* 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.