What was found
(CAN) WHILE CARRYING OUT POST-ENGINE CHANGE GROUND RUNS. THE NR 1 ENGINE SUFFERED AN OVER TORQUE OF 149 PERCENT WHEN MOVING THE POWER LEVER FROM DISCING TO FLIGHT IDLE. THE CAUSE OF THE OVER TORQUE WAS DETERMINED TO BE FROM A BINDING PCU. THE PCU WAS REPLACED, THE PROPELLER ASSY WAS REPLACED DUE TO THE OVER TORQUE, AND THE ENGINE WAS INSPECTED IAW DASH 8 AMM ATA 71-00-00, AND PW-123 ENGINE MM ATA 5-10-00. THE AIRCRAFT WAS RETURNED TO SERVICE.