This standard was last reviewed and confirmed in 2019.
Therefore this version remains current.
Abstract
PreviewSpecifies 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.
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Status: PublishedPublication date: 1992-08
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Edition: 1Number of pages: 11
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- ICS :
- 49.060 Aerospace electric equipment and systems
Buy this standard
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Format | Language | |
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std 1 61 | ||
std 2 61 | Paper |
- CHF61
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