As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING CLIMB AT FL200 NR 1 ENGINE TORQUE STARTED TO DECREASE. WITH NR 1 ENGINE POWER LEVER FULLY FORWARD NR 1 ENGINE TORQUE WAS 20 PERCENT LOWER THAN NR 2 ENGINE. AIRCRAFT DIVERTED. HYDRO MECHANICAL UNIT (HMU) AND FUEL PUMP REPLACED.