As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) TAKEOFF WAS ABORTED DUE TO ELECTRONIC ENGINE CONTROL FAULT OCCURRENCE WHEN POWER LEVER WAS ADVANCED TO TAKEOFF NOTCH. CUSTOMER MONITORED THE SITUATION AND AS THERE WAS NO CHANGE IN ENGINE PERFORMANCE ASSOCIATED WITH THESE F/A, THE ACFT RETURNED TO SERVICE AFTER CLEARING THE ELECTRONIC ENGINE CONTROL FAULT.