As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING T/O ROLL THE NR 1 ENGINE TORQUE OVERSHOT TO 92 PERCENT WHILE THE POWER MANAGEMENT WAS SET AT THE T/O POSITION FOR 90 PERCENT. THE PILOT ELECTED TO ABORT T/O PROCEDURE AT LESS THAN 60 KNOTS. INVESTIGATION LED TO THE REPLACEMENT OF THE FUEL PUMP AND FUEL CONTROL BEFORE THE ACFT RETURNED TO SERVICE.