As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) ON PREFLIGHT INSPECTION THE RT IB ELEVATOR TRIM TAB HINGE WAS FOUND TO BE LOOSE AND WOULD FLEX UNDER SIDE LOAD. UPON FURTHER INSPECTION IT WAS NOTICED THAT THE TRIM TAB SPAR WAS CRACKED ALONG THE LOWER EDGE BESIDE THE BOLTED ON HINGE POINT.