What are the primary flight controls of a Cessna 152?

What are the primary flight controls of a Cessna 152?

• A. Ailerons, elevator, and rudder
• B. Flaps, spoilers, and elevator
• C. Ailerons, flaps, and rudder
• D. Elevator, rudder, and trim

Answer: (A)

The primary flight controls of a Cessna 152 consist of the ailerons, elevator, and rudder, which are crucial for controlling the aircraft's movement around its three axes: roll, pitch, and yaw. Ailerons are located on the trailing edge of each wing and are responsible for roll control. When the pilot moves the control yoke left or right, one aileron moves up while the other moves down, creating a difference in lift that rolls the aircraft in the desired direction. The elevator, located on the tail of the aircraft, controls pitch. By pulling back on the control yoke, the elevator moves upward, increasing aerodynamic lift at the tail and causing the nose of the aircraft to rise. Conversely, pushing forward decreases the lift, lowering the nose. The rudder, also situated at the tail, is used to control yaw. It allows the pilot to steer the aircraft left or right, countering the adverse yaw effect caused by the ailerons during turns and maintaining coordinated flight. The other options include controls that play important roles in flight but are not classified as primary. For instance, flaps increase lift and drag during takeoff and landing but do not contribute directly to the aircraft's control in terms

The primary flight controls of a Cessna 152 consist of the ailerons, elevator, and rudder, which are crucial for controlling the aircraft's movement around its three axes: roll, pitch, and yaw.

Ailerons are located on the trailing edge of each wing and are responsible for roll control. When the pilot moves the control yoke left or right, one aileron moves up while the other moves down, creating a difference in lift that rolls the aircraft in the desired direction.

The elevator, located on the tail of the aircraft, controls pitch. By pulling back on the control yoke, the elevator moves upward, increasing aerodynamic lift at the tail and causing the nose of the aircraft to rise. Conversely, pushing forward decreases the lift, lowering the nose.

The rudder, also situated at the tail, is used to control yaw. It allows the pilot to steer the aircraft left or right, countering the adverse yaw effect caused by the ailerons during turns and maintaining coordinated flight.

The other options include controls that play important roles in flight but are not classified as primary. For instance, flaps increase lift and drag during takeoff and landing but do not contribute directly to the aircraft's control in terms