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Which outcome occurs when an aircraft's automatic stabilizer abruptly disengages during landing approach due to unexpected wind shear?

A)Pilot induced oscillation escalates rapidly
B)Engine flameout risk is significantly lowered
C)Fuel consumption decreases noticeably afterwards
D)Flaps automatically retract preventing stalls

💡 Explanation

Pilot induced oscillation quickly worsens because the abrupt stabilizer loss prevents *damping*. Pilots tend to overcompensate rapidly, therefore oscillations get amplified rather than naturally mitigated because there is a lack of dampening authority.

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