Standards Development
This document specifies:
— the tests for finished wiring, including connectors and, if necessary, terminals, terminal ends, junction boxes, circuit breakers, etc.;
— the requirements for verification of aircraft electrical wiring;
— continuity of circuits;
— dielectric strength;
— insulation resistance;
— partial discharge for operating voltages above 230/400 V a.c. (see also TR 4907[1]).
These tests do not concern equipment installed in the aircraft (see operation of systems) and do not apply to the wiring used in instrumentation.
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