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Which risk increases when hydraulic pressure is lost to an airplane's flight controls at high altitude?

A)Elevated stall and spin propensity
B)Increased engine fan blade erosion
C)Elevated parasitic drag coefficient
D)Compromised avionics processor cooling

💡 Explanation

Elevated stall and spin propensity increases because the diminished control authority reduces a pilot’s ability to correct for aerodynamic instability using flight surfaces, therefore stall/spin, rather than safe flight arises, because the aerodynamic control is degraded. at high altitudes

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