Which controls are considered the primary flight controls of an aircraft?

The primary flight controls of an aircraft are essential for the basic maneuvering and stability during flight. These controls consist of ailerons, elevators, and rudder, each fulfilling a unique function crucial for controlling the aircraft's attitude and direction.

Ailerons are located on the wings and control the roll of the aircraft. When the pilot moves the control yoke or stick, the ailerons deflect in opposite directions, allowing the aircraft to tilt to one side or the other, which is vital for banking turns.

Elevators are located on the horizontal stabilizer at the tail section. They control the pitch of the aircraft, allowing it to climb or descend. By pulling back on the yoke, the elevators move upward, causing the aircraft to pitch up and gain altitude, while pushing forward has the opposite effect.

The rudder is situated on the vertical stabilizer and is responsible for controlling yaw, which is the left and right movement of the aircraft's nose. The pilot uses the rudder to coordinate turns and maintain straight flight, particularly when banking.

Understandably, the other options consist of components that assist in flight but do not serve as primary controls. For instance, flaps, slats, and spoilers primarily affect lift and drag during