Patent ID: 8594903

Claim:
A method of monitoring the performance of an aircraft-mounted auxiliary power unit having adjustable inlet guide vanes, the method comprising: determining whether a reference exhaust gas temperature of the auxiliary power unit has been achieved by monitoring a difference between an inlet guide vane angle scheduled and an inlet guide vane angle requested; selecting a count factor based on the magnitude of the monitored difference between the inlet guide vane angle scheduled and the inlet guide vane angle requested; incrementing or decrementing a counter by the selected count factor; comparing the counter against a predetermined threshold condition, the threshold condition being different from an at-limit condition, the reaching of the predetermined threshold condition by the counter being indicative of deteriorating performance of the auxiliary power unit and providing an operational margin within which continued operation of the auxiliary power unit is still permitted prior to a next related maintenance operation; and conditioned upon the predetermined threshold condition being reached, advising an operator of the aircraft to select a future operating plan for the aircraft suitable for continued operation of the auxiliary power unit within the operational margin.