Which consequence results when excessive servo flutter develops in an aircraft's electromechanical flight controls at high speed?

A)Reduced stall angle of attack

B)Reversal of control surface effectiveness✓

C)Increased engine fuel consumption

D)Elevated cabin pressure oscillations

💡 Explanation

Control reversal occurs because servo flutter excites structural modes beyond the servo's bandwidth, leading to an inverse aerodynamic response rather than intended deflection; therefore, pilots lose correct axis control, rather than other aerodynamic or engine effects.

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Which consequence results when excessive servo flutter develops in an aircraft's electromechanical flight controls at high speed?

💡 Explanation

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