As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING TAKEOFF ROLL, AFTER SETTING TAKEOFF POWER REACHED UP TO 60% ONLY THE TAKE0FF WAS REJECTED BELOW 80 KNOTS. DURING TROUBLESHOOTING, THE STRAINER AND FUEL FLOW DIVIDER VALVE WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE AFTER GROUND RUNS CHECKS.