IEEE/AIEE 805-1960

Procedure is applicable to aircraft motors which operate from constant-frequency, nominally 400-cycle-per-second, constantvoltage, (nominally 115 volt line to neutral, 3-phase four-wire or 115 volt single-phase) alternating-current aircraft power systems. This aircraft power system is defined by paragraph 3.2.1.3, Type I of Military Specification No. MIL-E-7894. The test methods described herein will be suitable for test of machines of different frequency and voltage ranges. However, test equipment must be chosen suitable for the desired ranges

The purpose of this Procedure is to define uniform acceptable methods for making tests to determine the performance of alternating-current, 400-cycle-per-second, aircraft type, induction electric motors

- Inactive-Withdrawn.