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Which consequence results when approaching an aircraft carrier landing where induced drag exceeds thrust?

A)Loss of airspeed control
B)Engine compressor stall occurs
C)Vertical stabilizer structural failure
D)Rudder effectiveness gets amplified

💡 Explanation

Loss of airspeed control occurs due to reduced thrust relative to induced drag caused by the increased angle of attack during approach because airspeed decays more rapidly impacting pilot control; therefore airspeed becomes unstable, rather than engine stall which relates to airflow disruption.

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