ISO 10296:1992
Current
Aircraft — Hybrid remote power controllers — General requirements
Hardcopy , PDF
English, French
07-23-1992
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.
| Committee |
ISO/TC 20/SC 1
|
| DevelopmentNote |
Also numbered as BS G248(1993). (06/2005)
|
| DocumentType |
Standard
|
| Pages |
11
|
| PublisherName |
International Organization for Standardization
|
| Status |
Current
|
| 18/30334464 DC : 0 | BS ISO 20949 - AIRCRAFT - SMART CONTACTOR - GENERAL REQUIREMENTS |
| ISO 2678:1985 | Environmental tests for aircraft equipment — Insulation resistance and high voltage tests for electrical equipment |
| ISO 7137:1995 | Aircraft — Environmental conditions and test procedures for airborne equipment |
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