What are the Center of Gravity (CG) limits for the Normal Category aircraft at 2550 lbs?

The correct choice indicates the Center of Gravity (CG) limits crucial for ensuring the safe operation of Normal Category aircraft at a weight of 2550 lbs. Understanding CG limits is fundamental for pilots, as they directly affect aircraft stability and control.

In this context, the AFT CG limit of 93.0 inches and the Forward CG limit of 88.6 inches signify the acceptable range where the aircraft's weight can be distributed while still maintaining its stability and handling characteristics. If the CG is located too far aft, it can lead to difficulties in controlling the aircraft, particularly during maneuvers requiring pitch adjustments. Conversely, if the CG is too far forward, it can result in increased control forces and sluggishness in the aircraft's response.

Therefore, the limits given in the correct answer are not arbitrary; they have been determined based on extensive testing and engineering standards to guarantee that the aircraft operates safely within these boundaries. When the aircraft is loaded in accordance with these CG limits, it will perform optimally, enhancing safety for all occupants.