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Which risk increases when a tailstrike occurs during aircraft takeoff rotation caused by excessive pitch?

A)Elevator servo-jamming probability surges
B)Rudder effectiveness is dangerously lowered
C)Unrecoverable stall susceptibility dramatically rises
D)Center-of-gravity exceeds aft limit

💡 Explanation

An increased risk of unrecoverable stall happens because the tailstrike effectively increases the angle of attack beyond the critical angle; therefore, a stall is more likely, rather than servo jamming which is unrelated to aircraft attitude during a tailstrike event.

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