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Fuse, Current Limiter Type, Aircraft
- Aerospace Standard
- AS5372A
- Reaffirmed
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This specification covers the requirements for current limiter type fuses for use in aircraft primary electrical power systems conforming to MIL-STD-704. These limiters are suitable for use in AS53731 fuse holders for operation at −54 to 125 °C.
Rationale
This revision is required to correct the overload damage test requirement in 4.7.10, to delete the packaging requirements of Section 5 (MIL-P-17555 has been cancelled without replacement), to update all references, and to update the document format to the most current SAE guidelines.
AS5372A has been reaffirmed to comply with the SAE Five-Year Review policy.
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Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Unnamed Dataset 3 | ||
| Table 1 | ||
| Table 2 | Qualification inspection | |
| Table 3 | Group A inspections | |
| Table 4 | Group B inspections | |
| Table 5 | Group C inspection | |
| Table 6 | Test leads | |
| Table 7 | Terminal strength test | |
| Table 8 | Alternating current interrupt schedule | |
| Table 9 | Explosion proof test schedule | |
| Table 10 | Duty cycle |
Issuing Committee
Reference
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