What is a common risk associated with light stick forces when the CG is outside the limits?

When the center of gravity (CG) is outside the specified limits, the aircraft can exhibit undesirable flight characteristics, one of which is inadvertent over-rotation. This occurs because the balance of forces and moments acting on the aircraft can be significantly altered, making it more difficult for pilots to control the aircraft during various phases of flight.

In particular, when the CG is too far forward or aft, it affects the pitch stability and control authority of the flight control surfaces. If the CG is too far forward, for example, the aircraft may require more control force to achieve the desired pitch attitude, potentially leading to a scenario where the pilot inadvertently pitches the aircraft beyond normal rotational limits during maneuvers. This over-rotation can lead to situations like stalling or even loss of control if not managed properly.

Achieving and maintaining proper CG limits is critically important because it directly influences the aircraft's handling characteristics and safety margins. Understanding the risks involved when the CG is not within specified range helps pilots take necessary precautions to prevent situations like inadvertent over-rotation.