Commercial Pilot Airplane (CAX) Performance Practice Exam

The situation involves determining whether the combined weight of the pilot and copilot, when added to the empty weight of the aircraft, keeps the center of gravity (CG) within acceptable limits. In this case, the empty weight of the aircraft is 1,271 pounds, and the combined weight of the pilot and copilot is 355 pounds.

To assess whether the CG is maintained within limits, you would typically check the CG location against the aircraft's specifications, which provide CG limits for various loaded configurations. If the total weight of the aircraft (empty weight plus pilot and copilot weight) is within these limits, then the aircraft will remain within the CG envelope.

The correct assertion in this scenario indicates that the aircraft remains within the CG envelope with the given weights. This implies that the combined weight of the pilot and copilot does not shift the CG outside of the acceptable range.

An understanding of the aircraft's weight and balance data is essential. If provided with accurate weight and CG positions (which typically include the location of the loading points), one could derive if the total weight distribution remains within the prescribed limits, thus confirming the answer. Therefore, indicating that it will indeed remain within the CG envelope accurately reflects this understanding.