A turbine-powered aircraft's thermal anti-icing system for the wing leading edges is indicating a fault. The system uses engine bleed air. Which of the following is the most likely cause for the system to fail to operate correctly?
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A
The pneumatic de-icing boots are operating simultaneously.
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B
The chemical rain repellent system reservoir is empty.
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C
The anti-ice valve has failed to open.
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D
The windshield wiper motor has shorted out.