During a climb, which flight control surface would you primarily use?

During a climb, the primary flight control surface used is the elevator. The elevator is located on the tail of the aircraft and is responsible for controlling the pitch movement. By pulling back on the control yoke or stick, the pilot raises the elevator, which increases the angle of attack of the wings. This action generates additional lift, allowing the aircraft to climb efficiently.

The other control surfaces play different roles. Ailerons are used to control roll and are crucial during turns rather than straight climbs. The rudder controls yaw and compensates for adverse yaw during turns, making it less relevant during a climb. Flaps are used primarily to increase lift at lower speeds during takeoff and landing phases and are not typically deployed during a climb in normal operation. Thus, the elevator is the key control surface used for managing the aircraft’s ascent.