As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) AIRCRAFT WAS CLEARED FOR T/O. POWER WAS ADVANCED TO 93.5% N1 ON BOTH ENGINES. APPROXIMATELY 1 SECOND LATER LT ENGINE FAILED. T/O WAS REJECTED. AME TROUBLESOT THE SNAG AND DISCOVERED THAT THE LT ENGINE FUEL PUMP PRESSURE WAS NOT WITHIN ACCEPTABLE LIMITS. FUEL PUMP AND FUEL CONTROL UNIT REPLACED.