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Which outcome occurs when regenerative pump clearance increases due to wear in aircraft fuel system?

A)Reduced discharge pressure at high altitude
B)Increased fuel temperature from viscous losses
C)Elevated engine vibrations due to fuel pulsation
D)Fuel starvation from vapor lock formation

💡 Explanation

When regenerative pump clearance increases, fluid recirculates internally due to reduced flow resistance, diminishing its ability to maintain design pressure, especially in low-density atmospheric conditions (high altitude). Therefore, reduced discharge pressure results, not increased fuel temperature, engine vibrations or starvation, which have different root causes.

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