As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE TRIM (PITCH) INDICATOR WHILE IN CRUISE IS AT THE MOST FWD PART OF THE TRIM INDICATOR. REMOVED AND REPLACED THE ELEVATOR TRIM TABA CONTROL WHEEL P/N 5565756-3. ALSO REPLACED POINTER ARM ASSY. P/N 5565756. ALSO REPLACED POINTER ARM ASSY P/N 6661053-15, POINTER P/N 666042-12 AND ADDED (2) SHIMS P/N 6661042-16. I.AW SB REF: FIG 1 DETAIL C AND THE MM CHAP 27-32-01. ALL RIGGING CHECKS AND OPERATIONAL CHECKS SATISFACTORY AT THIS TIME.