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| MIL-S-85419 (AS)
indicate imminent failure which might compromise safety of
flight.
4.5.1 Calibration.
4.5.1.1 Starter Mode. The starter/APU shall be subjected to
three start cycles against the flywheel at each of the conditions
specified in Table III and the performance shall meet or exceed
the requirements of Figures 13 and 14.
TABLE III - CALIBRATION TEST CONDITIONS, STARTER MODE
*May be conducted at local prevailing ambient provided that data
are corrected to sea level.
4.5.1.2 APU Mode. The starter/APU shall be started and operated
as an APU while performance is determined at the conditions
specified in Table IV.
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