The method involves including a partial final load application cycle. Temporary load values for the phases of the partially completed load application cycle are included with a given fixed value, where a zero value is given as a fixed value. The difference...

A system for detecting and correcting a thrust control malfunction in an aircraft engine. The system includes an electronic engine control (EEC) (18) unit that includes a first processing subsystem (A) and a second processing subsystem (B), and a thrust co...