What was found
(CAN) IN CRUISE AT 5,000 FEET, THE RPM OF THE TURBINE AND ROTOR WAS INCREASING. THE MAIN ROTOR BLADE PITCH WAS INCREASED AND THE TORQUEMETER SHOWED AN EXCEEDANCE OF 105 PERCENT. REDUCTION OF THE POWER LEVER MAINTAINED THE ROTOR AND ENGINE SPEEDS. AN AUTOROTATION WAS CARRIED OUT. POST-FLIGHT THE TURBINE, FUEL CONTROL UNIT, AND THE GOVERNOR WERE SENT TO A REPAIR SHOP FOR EVALUATION. A FURTHER REPORT WILL FOLLOW.