FIELD: engines and pumps, data processing.
SUBSTANCE: ground information-diagnostic system for safe operation of an aircraft gas turbine engine including an electronic control system containing at least two sensors of external affecting factors installed on at least one electronic control system during maintenance, with own matching devices and hardware-software interfaces, a memory unit and a unit for calculating the performance level.
EFFECT: higher accuracy and reliability of maintenance, simpler analysis of technical state of the gas turbine engine electronic control system and prediction of timely maintenance.
1 cl, 2 dwg
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