Engine Performance Check Sample Clauses
Engine Performance Check. Compliance with full rated performances as defined in the Aircraft flight manual will be demonstrated (i) by an on-wing static inspection, (ii) by testing any system of the powerplants (engines, nacelles and accessories) and (iii) by performing an engine power assurance run in accordance with Part 1, Chapter 2 of the ISATM. The Seller shall promptly correct, in accordance with the AMM, any discrepancies found in the course of the performance of such powerplant tests so as to comply with the Delivery Conditions.
Engine Performance Check. 13.1 At the end of the last flight of each day, Contractor must record the following helicopter parameters: * Pressure altitude at landing (PRESS. ALT.) * Outside air temperature (OAT) * Gas producer at operating rpm (GAS PROD) * Torque at operating rpm (TORQUE) * Turbine temperature at operating rpm (TURB. TEMP. ACT.) * Idle turbine temperature (IDLE TEMP.) * The time it takes (seconds) during shutdown for the gas producer rpm to coast down from idle rpm to Ng tachometer stoppage (COST DOWN TIME)
13.2 Contractor must record the Engine Health Indicator Test form (FC-123).
13.3 Contractor must compare each flight’s information to establish a trend in engine performance. An engine trend chart must be established and maintained by the pilots and be available to DOJ. At least once during each 10 hours of flight time, or every 10 days, whichever occurs first, Contractor must check the engine performance as recommended by the manufacturer, and record the results in the aircraft’s log books. If engine performance is suspect, Contractor must notify DOJ. Any time a helicopter’s capability to perform is suspect, Contractor must contact DOJ.
Engine Performance Check. China Eastern A340-300 Buyback Agreement Reference CT1105153 33 ***