Abstract: A method for performing maintenance on a gas turbine engine assembly includes unplugging a first connector from a first socket, the first connector electrically coupled to the engine control unit, the first socket electrically coupled to the hydromechanical unit, plugging a second connector into the first socket, the second connector electrically coupled to a driver simulator, cranking the engine core to a low speed value, and operating the driver simulator to reposition at least one of the variable stator vane assembly and the variable bypass valve from a first operational position to a second operational position that is different than the first operational position.

Abstract: An automatic engine protection system for use when electronic parts of the control system are exposed to overtemperature conditions. A thermally sensitive component, such as an engine electronic control or an electronic overspeed control, is mounted on the engine. A thermal fuse is mounted adjacent, or in thermal contact with, the speed control. The thermal fuse is placed in electrical series with a valve which controls fuel delivery to the engine. If the temperature of the fuse exceeds its melting point, indicating a possible danger to the electronic control, the fuse melts, thereby terminating fuel to the engine.

Abstract: An automatic engine protection system for use when electronic parts of the control system are exposed to overtemperature conditions. A thermally sensitive component, such as an engine electronic control or an electronic overspeed control, is mounted on the engine. A thermal fuse is mounted adjacent, or in thermal contact with, the speed control. The thermal fuse is placed in electrical series with a valve which controls fuel delivery to the engine. If the temperature of the fuse exceeds its melting point, indicating a possible danger to the electronic control, the fuse melts, thereby terminating fuel to the engine.