What is the difference between the AFT CG limits in both Normal and Utility Categories?

The correct understanding in this context is that the aft center of gravity (CG) limits differ between Normal and Utility categories primarily due to the operational design and safety considerations of each category. In general, the aircraft designed under the Normal category is intended for private flying, while Utility category aircraft are capable of performing more aerobatic maneuvers and may have different performance requirements.

If they are indeed the same at a specified value, it indicates that the design parameters for both categories specify an identical aft CG limit. This reflects a design choice that ensures that even in cases where the aircraft is loaded towards the rear of the permissible limit, the handling characteristics remain consistent and safe across both categorizations. Therefore, recognizing that they share the same aft CG limit is crucial for understanding the performance capabilities and safety margins of aircraft in both categories.

The other options suggest variations in the aft CG limits, which are not applicable if both categories have the same limit. Understanding these distinctions is vital for instructors and applicants alike, as it influences flight performance and safety during operations in different scenarios and flight regimes.