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Hydraulic Pressure in R44 with Engine Failure


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Hey guys,


I have a kind of dumb question. I can't find anywhere in the POH for a Raven II R44 about what happens to hydraulic pressure if the engine quits in mid flight. Of course I practiced hundreds of autorotations and hydraulic failures but never together. Do you expect to lose hydraulic pressure if the engine quits in flight or is the pump driven by the turning main rotor?




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