If the centre of gravity is located at the forward limit, how does that affect an aeroplane's stability?

When the center of gravity (CG) is located at the forward limit, the aircraft exhibits characteristics of increased stability. This forward position of the CG leads to a greater tendency for the aircraft to return to its original flight path following a disturbance. Consequently, you would require more elevator control input to induce a change in pitch because of the inherent stability.

In this scenario, a stable aircraft tends to resist changes in its flight path, thereby necessitating stronger or more significant control actions to achieve a desired change in attitude. This means that the pilot would need to apply excessive elevator control movements to overcome the stability inherent in the forward CG position.

Understanding this behavior is crucial for pilots, as it informs them of the handling characteristics they might expect during flight.