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.
Related Topics:
Test equipment and instrumentation
Test procedures
Defense industry
Test facilities
Magnesium alloys
Ignition timing
Manufacturing processes
Copper alloys
Coatings, colorants, and finishes
Electric aircraft
Also known as: SAE AS 5372
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