An airplane loaded with the Center of Gravity aft of the rear CG limit is likely to?

When an airplane is loaded with the Center of Gravity (CG) located aft of the rear CG limit, it impacts the aircraft's handling characteristics and stability. Specifically, it becomes more challenging to flare for landing. This is due to a decrease in pitch stability that occurs when the CG is too far aft.

With an aft CG, the aircraft can become more sensitive to control inputs, making it harder for the pilot to effectively manage the pitch during landing. When flaring, the pilot needs precise control to ensure the aircraft transitions smoothly from descent to level flight just before touchdown. If the CG is beyond the limit, it can result in difficulties in maintaining the desired attitude and may lead to an unstable landing approach, increasing the risk of a hard landing or a tail strike.

While the other options may contain elements relevant to the effects of CG positioning, they do not directly relate to the most pronounced operational challenges posed by an aft CG during the landing phase. Therefore, recognizing the increased difficulty in landing with an aft CG is key to understanding its implications for flight safety and control.