With an empty weight moment of 102.01 and other given weights, is the airplane loaded within limits?

In evaluating whether the airplane is loaded within limits based on the provided empty weight moment of 102.01, it is essential to understand how to assess the center of gravity (CG) in relation to the aircraft's loading envelope. The CG represents the balance point of the aircraft and must fall within specific limits defined by the manufacturer to ensure safe flight characteristics.

Choosing the answer indicating that the CG is within the limits signifies that calculations appropriately consider both the total weight of the aircraft and the distribution of that weight throughout the airframe. The empty weight moment provides a pivotal reference point to calculate the total moment when additional weights are included, allowing for the determination of the overall CG position.

If the CG lands within the acceptable range of the envelope, it indicates a stable and safe loading condition. This assessment involves confirming that the ratios and moments of the loaded weights maintain a CG position that complies with the aircraft's design specifications. Thus, the conclusion that the airplane is indeed within limits reflects a thorough analysis of weight distribution and balances, ensuring that they adhere to safety protocols for flight operations.