Specifies the general design and performance requirements. The controllers consist of an electromagnetic device or a combined electromagnetic/solid-state device for load switching, and a solid-state control circuit for control of the load-switching devices. On aircraft, they are used to close and open the electrical circuit and to protect wiring and equipment in the event of overload or short-circuit conditions.
Status: PublishedPublication date: 1992-08
Edition: 1Number of pages: 11
Technical Committee: ISO/TC 20/SC 1 Aerospace electrical requirements
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|std 1 61|
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