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Within aircraft hydraulic flight control systems, which outcome occurs when an actuator experiences very rapid, repeated cycling?

A)Excessive heat generation occurs
B)Spool valve locks prematurely
C)Hydraulic fluid oxidization accelerates
D)Linkage backlash is automatically reduced

💡 Explanation

Excessive heat arises because rapid, repeated cycling causes significant fluid friction inside the actuator, activating viscous heating; therefore, the oil temperature increases significantly, rather than premature lockup or backlash reduction that would stem from mechanical faults alone.

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