If the center of gravity (CG) is loaded aft of the CG limit, what undesirable flight characteristic might a pilot experience?

The situation in which the center of gravity (CG) is loaded aft of the CG limit can significantly affect the aircraft’s performance and handling characteristics, particularly in relation to stall recovery. When the CG is too far aft, the aircraft becomes less stable. In this configuration, the elevator effectiveness is reduced, meaning that it may not respond well to control inputs, especially during critical phases of flight.

In a stall situation, a nose-up attitude occurs, and if the CG is excessively aft, the aircraft may be less responsive to elevator inputs needed to recover from the stall. This decreased effectiveness can lead to a prolonged stall or difficulty in regaining controlled flight, resulting in the potential for an unrecoverable condition. Consequently, understanding the importance of maintaining proper CG limits is essential for ensuring safe flight operations.

The other options don’t accurately capture the primary risk associated with an aft CG. Maintaining altitude may be difficult, but that isn't the primary concern in the context of CG limits. Stability during climb would be diminished rather than enhanced, and while easier maneuvering could be a characteristic of aft CG, it is not as critical an issue as stall recovery difficulties.