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Which outcome occurs when an aircraft aileron servo jams at high speed?

A)Aeroelastic flutter starts immediately
B)Increased actuator control reversal
C)Reduced risk of Dutch roll
D)Hydraulic pump damage increases drastically

💡 Explanation

Increased actuator control reversal occurs because the aerodynamic forces can overcome the available torque from the jammed servo, therefore effectively reversing the control surface's intended direction, rather than flutter which requires oscillating forces.

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