This course focuses on electromechanical systems used in turbine- powered aircraft, including actuators, motors, relays, and control mechanisms. It examines the integration of electrical and mechanical components in systems such as flight controls, landing gear, braking, and environmental control systems. Students develop an understanding of system operation, control logic, and fault diagnosis. Emphasis is placed on interpreting technical documentation, performing system analysis, and applying safe and compliant maintenance practices, ensuring alignment with EASA Part- 66 Module 11 standards.