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Which undesired effect occurs when a helicopter's cyclic control aggressively commands forward flight?

A)Dynamic roll-over
B)Compressibility stall
C)Ground resonance emerges
D)Engine over-torquing occurs

💡 Explanation

Dynamic roll-over is a risk because the differential lift causes sideways thrust while landing gear friction prevents lateral movement, therefore the helicopter rolls, rather than translating as intended; compressibility stall affects high speed flight.

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