In the Utility Category, what is the AFT CG limit at 93.0?

Prepare for the UND Certified Flight Instructor (CFI) Test. Study with flashcards and multiple choice questions, each with hints and explanations. Get ready for your exam!

In the Utility Category for an aircraft, the AFT CG (center of gravity) limit at a certain weight, such as 93.0 inches, refers to the maximum allowable AFT CG location for safe flight operations. The specific AFT CG limit varies based on aircraft configuration and weight, and it is critical for maintaining the aircraft's stability and control in flight.

The option indicating 2050 lbs aligns with the established weight and balance criteria for the Utility Category aircraft at that specific AFT CG limit. An AFT CG that is too far rearward can lead to reduced stability and impaired control, particularly during critical phases of flight like takeoff, landing, and in-flight maneuvers. Therefore, identifying the correct weight associated with the AFT CG limit ensures the pilot adheres to safe operational practices.

In contrast, the other weight options provided do not meet the criteria for the safe operation of the aircraft in its specified configuration, leading to an unsuitable balance for flight. Maintaining proper weight related to the AFT CG is essential for the overall safety and performance of the aircraft.

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