This standard was last reviewed and confirmed in 2023.
Therefore this version remains current.
Abstract
PreviewIncludes 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 °C, and all altitudes from 0 to 24 000 m. Gives terminology, requirements for dimensions, temperature and altitude rating, current, voltage and breaking-capacity ratings, environment, temperature rise, time/current characteristics, endurance, identification and marking, tests, type tests, production routine test, production quality tests and a method of measurement of voltage drop.
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Status: PublishedPublication date: 1975-12
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Edition: 1Number of pages: 4
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- ICS :
- 49.060 Aerospace electric equipment and systems
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| Format | Language | |
|---|---|---|
| std 1 40 | ||
| std 2 40 | Paper |
- CHF40
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