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Which risk increases when differential control linkage fails in an aircraft?

A)Aggravated aileron reversal at lower speeds
B)Uncoordinated turns during manual flight
C)Elevator flutter at cruise altitude
D)Rudder lock due turbulence impact.

💡 Explanation

Uncoordinated turns are more prevalent because the differential control linkage, which normally assists coordinated aileron and rudder movements, malfunctions; this disables coordinated control, therefore making manual turns difficult rather than problems like aileron reversal, elevator flutter, or even rudder lock.

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