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Which risk significantly increases when exceeding a helicopter's retreating blade stall airspeed limit during forward flight?

A)Loss of control authority
B)Rotor blade thermal runaway
C)Increased engine combustion instability
D)Compressor stall induced hyperventilation

💡 Explanation

Loss of control authority increases greatly due to asymmetric lift. Retreating blade stall occurs because the advancing blade travels at a higher relative airspeed than the retreating one, therefore lift is asymmetrically reduced rather than being uniformly distributed.

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