If the loaded aircraft weighs 2,207 pounds with a moment/1000 of 96.8 pound-inches, what does this indicate about the aircraft’s center of gravity?

Determining the center of gravity (CG) of an aircraft involves understanding the relationship between the aircraft's weight and its moment. The moment is calculated by multiplying the weight of the aircraft by the distance from a reference point, typically measured in inches. A moment/1000 of 96.8 pound-inches indicates that the aircraft has a total moment of 96.8 x 1000 = 96,800 pound-inches.

To assess whether the aircraft's center of gravity is within acceptable limits, it’s crucial to refer to the aircraft's specific weight and moment limits for both the normal category and utility category.

In this case, the loaded weight of 2,207 pounds and the calculated moment indicate that the CG must be evaluated against these limits. If the CG falls within the prescribed range for both categories, then the aircraft is acceptable for both normal and utility use.

Given that the answer identifies the state of being both within normal and outside utility category limits, it suggests that while the aircraft’s CG is acceptable for normal operations, it may fall outside the critical range required for utility category operations. This is important for flight safety, as operating outside the defined limits can lead to performance issues or structural stress. Thus, based on