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During an aircraft landing with deactivated spoilers, which consequence results from the delayed deployment of reverse thrust?

A)Increased ground roll distance
B)Decreased airframe stress
C)Enhanced elevator authority
D)Reduced engine wear rate

💡 Explanation

Increased ground roll occurs because delayed reverse thrust reduces the deceleration, diminishing the retarding force. The *ground friction coefficient* remains the primary slowing mechanism; therefore, roll distance increases rather than decreasing stress from braking or impacting engine component wear.

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