As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT EEC FAILED DURING TAKE-OFF, ENGINE INDICATIONS WERE IN TRANSIENT LIMTS. [07-09-07] DOWNLOADED RIGHT EEC AND FOUND CODE F1-10 DISPLAYED FOR BLEED VALVE TORQUE MOTOR. CHECKED WIRING BETWEEN TORQUE MOTOR AND EED NO DEFECTS NOTED. REMOVED AND REPLACED TORQUE MOTOR WITH OVERHAULED UNIT USING NEW PARTS. GROUND RAN ENGINE RAN ENGINE. OPS AND LEAK CHECK WAS GOOD. WORK PERFORMED PER PWA 545 MM.