Includes the requirements for these components for use in aircraft electrical systems having voltage and frequency characteristics conforming to ISO/R 222, at any ambient temperature from -65 to +85 degrees centigrade, and all altitudes from 0 to 24 000 m. Gives terminology, requirements for dimensions, current, voltage and breaking-capacity ratings, time/current characteristics and tests.
Status: PublishedPublication date: 1976-03
Edition: 1Number of pages: 20
Technical Committee: ISO/TC 20/SC 1 Aerospace electrical requirements
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|std 1 124|
|std 2 124||Paper|