How should a pilot regain control of the aircraft in a spin?

To regain control of the aircraft during a spin, the correct approach involves applying opposite rudder to the direction of the spin while simultaneously reducing the angle of attack. This technique is grounded in the aerodynamic principles governing spins.

When an aircraft enters a spin, it is usually due to an excessive angle of attack combined with yawing motion. By applying opposite rudder, you counteract the yaw that reinforces the spin's rotation. This action helps to stabilize the aircraft's attitude and prevents further tightening of the spin.

Reducing the angle of attack is crucial because spins are a function of airflow separation over the wings. Lowering the angle of attack allows the wings to regain lift and aids in stopping the spin. Once the aircraft stops spinning and returns to controlled flight, the pilot can gradually recover to normal flight parameters.

Other methods, such as increasing throttle or performing a steep climb, could inadvertently worsen the spin or delay recovery. Banking towards the spin also does not address the underlying aerodynamic issues contributing to the spin, potentially making the situation more severe. Therefore, the combination of opposing the spin with rudder and reducing angle of attack is the recognized and effective method for spin recovery.