As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) UPON INSPECTION THE TRIM TAB ACTUATOR WAS FOUND TO HAVE 2 BOLTS, P/N 130909B38, LOOSE. THE ACTUATOR SHOWED NO INDICATIONS OF DAMAGE OR MALFUNCTION, TRIM TAB FREE PLAY INSPECTION WAS WELL WITHIN TOLERANCE. BOLTS WERE TORQUED AND ANTI SABATOGE LAQUER WAS INSTALLED. THERE WAS NO EVIDENCE OF THE PART BEING REMOVED AND WAS MOST LIKELY THAT WAY SINCE THE AIRCRAFT LEFT THE FACTORY.