Which instability occurs when thrust reversers are deployed late during landing?

A)Adverse yaw moment increases sharply✓

B)Nose wheel shimmy intensifies rapidly

C)Aerodynamic braking effectiveness decreases

D)Compressor stall risk amplifies greatly

💡 Explanation

A late thrust reverser deployment generates asymmetric thrust, creating differential drag; this causes an adverse yaw moment because the centers of thrust aren't aligned. A nose-wheel impact would result at different forces rather than a yaw effect; therefore, adverse yaw is the primary concern.

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Which instability occurs when thrust reversers are deployed late during landing?

💡 Explanation

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