An airplane loaded with CG at the aft limit will commonly?

When an airplane is loaded with the center of gravity (CG) at the aft limit, it affects the handling characteristics of the aircraft significantly. One key outcome of having the CG in a rearward position is that it causes the aircraft to feel heavy in the longitudinal axis. This is due to the shifted weight distribution which can lead to a reduced effectiveness of the control surfaces used for pitch control.

As the CG moves toward the aft limit, the aircraft may become less stable in certain phases of flight, particularly at lower speeds. It can also lead to a situation where the elevator control, used to manage pitch, requires more deflection to achieve the same response, which can create the perception of heaviness. In practical terms, pilots might find themselves working harder to maintain altitude and manage speed, particularly during climb or landing phases.

In contrast, other choices present outcomes that are not typically associated with an aft CG. For example, while an aft CG can lead to improved efficiency in some flight conditions, it is not a general rule that it "flies more efficiently" across all conditions, especially with regard to stability. Similarly, the feeling of heaviness in the longitudinal axis is distinctly linked to aft CG, whereas aspects like lateral balance control forces or descent rates are