The Boeing Company
Aircraft control surface actuation systems and methods

Abstract:

Aircraft control surface actuation systems and methods are described herein. An example control surface actuation system includes an interface cable, a test interface, and a controller. The test interface is to be disposed in an electrical equipment (EE) bay of an aircraft and operatively coupled to an actuator associated with a control surface of the aircraft. The interface cable is to be connected between the test interface and the controller, and the controller is to transmit a signal via the interface cable to the test interface to control the actuator.