What are the CG limits for the Utility Category aircraft at a weight of 2130 lbs?

The correct answer indicates that for a Utility Category aircraft at a weight of 2,130 lbs, the aft center of gravity (CG) limit is 93.0 inches, and the forward CG limit is 83.0 inches. This specification is crucial for ensuring the safety and performance of the aircraft during flight.

Understanding CG limits is vital because the center of gravity directly affects the aircraft’s stability, control, and overall performance. An aircraft that is within the specified CG limits can be flown safely and effectively, while one that is outside those limits may experience flight issues, such as an inability to maintain level flight or undesirable maneuverability.

The choice that includes 93.0 as the aft limit is particularly relevant as it reflects the maximum allowable measurement for the center of gravity positioned toward the tail of the aircraft, which could be necessary for certain configurations. The forward limit of 83.0 inches ensures that the CG remains appropriately balanced forward, contributing to better handling and stability.

For utility category aircraft, these limits are often established through rigorous testing and operational analysis, ensuring that they provide a safe operational envelope for the aircraft's intended use, particularly during maneuvers that require a higher load factor or during aerobatic operations.

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