What are the primary flight controls of an aircraft?

The primary flight controls of an aircraft are essential for managing the aircraft's attitude and direction during flight. They consist of ailerons, elevator, and rudder.

Ailerons are responsible for controlling the roll of the aircraft, allowing it to tilt to the left or right, which is crucial for turning. The elevator, situated on the horizontal stabilizer, controls the pitch, enabling the aircraft to ascend or descend. The rudder, mounted on the vertical stabilizer, manages yaw, helping to control the aircraft's left and right movement along its vertical axis.

Together, these primary controls provide the pilot with the necessary means to maneuver the aircraft effectively and maintain stability during various stages of flight, including takeoff, cruising, and landing. Understanding the function of each control is vital for pilots, as they allow for efficient navigation and safety in the air.