Which of the following factors must be taken into account when determining the wire size to use for an aircraft installation?
- Allowable power loss, permissible voltage drop, current carrying capability of the conductor, type of load (continuous or intermittent).
- Mechanical strength, allowable power loss, resistance of current return path through the aircraft structure, permissible voltage drop.
- Allowable power loss, resistance of current return path through the aircraft structure, current carrying capability of the conductor, type of load (continuous or intermittent).
vale asking:
in the book where i'm studying the correct answer is the first, I have to know the amps such are flowing
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