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During final approach, which consequence results when differential spoiler deployment induces roll?

A)Increased control surface aerodynamic stall
B)Adverse yaw is significantly counteracted
C)Reduced induced drag at wingtips
D)Lateral stability becomes inherently unstable

💡 Explanation

The differential spoiler deployment generates unequal drag forces on the wings, inducing rolling moments. This *yaw-roll coupling* mechanism counteracts adverse yaw because the spoiler drag reduces the yawing moment caused by aileron deflection; therefore, adverse yaw is reduced rather than amplified.

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