Which consequence results when an aircraft's aileron control cable jams near the wingtip, preventing aileron deflection?

A)Reduced roll control authority remains

B)Unintended yaw during roll initiation✓

C)Complete lift loss on affected wing

D)Elevated stall speed on both wings

💡 Explanation

Unintended yaw occurs due to asymmetric drag. When the cable jams, the intended differential lift for roll cannot be generated; *adverse yaw* manifests because the descending wing produces more drag than the ascending wing, therefore causing the aircraft to yaw rather than purely roll.

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Which consequence results when an aircraft's aileron control cable jams near the wingtip, preventing aileron deflection?

💡 Explanation

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