What are the Normal Category G limits for the aircraft?

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!

The Normal Category G limits for aircraft are established to ensure safety and structural integrity during operation. The correct answer establishes a positive limit of 3.8 Gs and a negative limit of -1.5 Gs, aligning with the general standards set for aircraft in the Normal Category.

These limits indicate the maximum load factors the aircraft can safely withstand during normal operations. The positive limit reflects the ability of the aircraft to handle forces when pulling up or during maneuvers requiring an upward load (e.g., during climbing turns), while the negative limit relates to the downward forces the aircraft can endure, such as during abrupt descent or turbulence.

Understanding these G limits is crucial for pilots as exceeding them can result in structural failure or loss of control. The values given in this answer are typical for general aviation aircraft intended for transportation and recreational flights and provide a safety margin.

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