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In an aircraft hydraulic system, which consequence results when rapid actuator movement induces localized boiling?

A)System pressure oscillates erratically
B)Fluid viscosity decreases linearly
C)Thermal runaway initiates gradually
D)Component seals exhibit swelling

💡 Explanation

Erratic pressure occurs because vapor bubbles from cavitation collapse violently during the implosion phase, causing pressure waves; therefore pressure deviates unpredictably rather than viscosity changing, due to the limited temperature range and implosion process.

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