What was found
(CAN) ON FINAL PART OF TAKEOFF ROLL THE ELECTRONIC ENGINE CONTROL LOCAL ALERT WAS DETECTED FLASHING. PARAMETERS WERE NORMAL AND TAKEOFF WAS CONTINUED. AT ROTATION, TORQUE NR 2 ENGINE INCREASED TO APPROXIMATELY 106 PERCENT WITH A STEADY ELECTRONIC ENGINE CONTROL FAULT LIGHT. AIRBORNE NR2 ENGINE POWER LEVER WAS RETARDED WITH NO RESPONSE. ELECTRONIC ENGINE CONTROL FAULT CHECKLIST WAS COMPLETE AND NORMAL ENGINEERING PARAMETERS WERE RE-ESTABLISHED. THE FLIGHT CONTINUED WITH NOT FURTHER FAULT ON THE ELECTRONIC ENGINE CONTROL SYS. ON LANDING, MAINTENANCE WAS REQUESTED TO PERFORM AN OVERTORQUE INSPECTION. NO OTHER TROUBLESHOOTING REPORTED.