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.
-
Status: PublishedPublication date: 1992-08
-
Edition: 1Number of pages: 11
-
- ICS :
- 49.060 Aerospace electric equipment and systems
Buy this standard
en
| Format | Language | |
|---|---|---|
| std 1 61 | ||
| std 2 61 | Paper |
- CHF61
Life cycle
Got a question?
Check out our FAQs
Customer care
+41 22 749 08 88
Opening hours:
Monday to Friday - 09:00-12:00, 14:00-17:00 (UTC+1)