As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ON CLIMB OUT, NR 2 TORQUE LAGGED BEHIND NR 1 TORQUE GAUGE, WHICH EVENTUALLY DROPPED TO 20% & CREW SHUTDOWN THE ENG. FUEL FLOW WAS 100 LBS LESS. R & R FUEL CONTROL, ECU & PERFORMED OPERATIONS TEST, RESULTS OF OPERATIONS TEST WAS SATISFACTORY.