An aircraft loaded with a weight of 4,700 pounds has a CG of 97.0 inches. What could be the new CG after adjustments?

To determine the new center of gravity (CG) of an aircraft after adjustments, it's important to understand that the CG can change depending on the distribution of weight within the aircraft. In this scenario, the original CG is at 97.0 inches with a total weight of 4,700 pounds.

When making adjustments to weight and balance, moving weight forward will generally bring the CG forward, while moving weight to the rear will push the CG further back. Each of the choices represents a potential new CG position after these adjustments. The correct answer indicates a shift downward to 95.3 inches, which implies that the adjustments made (whether redistributing weight or removing weight from specific locations) were sufficient to lower the CG from its original position.

Given that the aircraft originally had a CG at 97.0 inches, the new CG must reflect a plausible adjustment based on typical operational scenarios. The choice of 95.3 inches signifies a legitimate move in CG, as it represents a shift downward that would maintain operational safety, considering factors like stability and performance metrics.

In the context of practical aviation operations, adjustments to CG are crucial for maintaining aircraft control and performance. Thus, understanding the weight distribution and its impact on CG is essential for pilots,