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within 5000 hours of operation of Centaur 40, Turbine 2nd stage blades and disk was completely damaged, I want your help to sort out the problem that led to this failure. rest of the turbine stages were damaged as a consiquence of 2nd stage failure.
because of resultant high Gas Generator Vibration scoring on tilting pads of bearing was also observed.
because of resultant high Gas Generator Vibration scoring on tilting pads of bearing was also observed.
