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Which outcome occurs when a flight control system fails during landing gear deployment?

A)Asymmetric elevator trim condition
B)Unintended spoiler panel deployment
C)Rudder locked near full deflection
D)Reverse thrusters engage prematurely

💡 Explanation

In a fly-by-wire system, failure during gear deployment can trigger erroneous flight control signals because software manages hydraulics. The asymmetric elevator trim arises therefore, rather than unintended spoilers, with flaps controlling spoilers separately.

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