Name the three primary axes of an aircraft and the corresponding control surfaces.

Name the three primary axes of an aircraft and the corresponding control surfaces.

• A. Pitch axis controlled by the elevator; roll axis controlled by the ailerons; yaw axis controlled by the rudder
• B. Pitch axis by the rudder; roll by the elevator; yaw by the flaps
• C. Pitch axis by the ailerons; roll by the rudder; yaw by the elevators
• D. Pitch axis by the flaps; roll by the canards; yaw by the stabilizer

Answer: (A)

Pitch, roll, and yaw are the three primary rotational axes of an aircraft, each with a dedicated control surface. Pitch is about the lateral axis and is controlled by the elevator, which moves the nose up or down. Roll is about the longitudinal axis and is controlled by the ailerons, which tilt the wings to bank the aircraft. Yaw is about the vertical axis and is controlled by the rudder, which directs the nose left or right. This mapping—pitch with the elevator, roll with the ailerons, yaw with the rudder—is the standard arrangement for conventional aircraft.

Pitch, roll, and yaw are the three primary rotational axes of an aircraft, each with a dedicated control surface. Pitch is about the lateral axis and is controlled by the elevator, which moves the nose up or down. Roll is about the longitudinal axis and is controlled by the ailerons, which tilt the wings to bank the aircraft. Yaw is about the vertical axis and is controlled by the rudder, which directs the nose left or right. This mapping—pitch with the elevator, roll with the ailerons, yaw with the rudder—is the standard arrangement for conventional aircraft.