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Anybody to comment on the switching logic of the Antiicing System. I learned that the Ice Sensor is switching Pitot Heat to ~200°C inflight with the Antiicing Switch in 'Auto'? Switch to 'ON' would keep it at that value?
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On the airbus, the probe heat computers manage the level of heating. Inflight, the pitots are heated to the high value. The position of the push button has no effect.