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Which outcome occurs when adverse yaw is uncorrected in flight controls?

A)Reduced control surface effectiveness occurs
B)Increased drag on the outer wing occurs
C)Higher stall speed on one-wing occurs
D)Uncoordinated turn and potential spin results

💡 Explanation

Uncorrected adverse yaw causes the aircraft to turn in the opposite direction of the aileron input via differential drag, an aerodynamic force; therefore, a skid and potential spin result, rather than coordinated flight because adverse yaw is a deviation.

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