As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
VERTICAL STAB. RUDDER ARM WEIGHT EDGES ARE ERODED / REMOVED AND INSTALLED NEW VERTICAL STAB. RUDDER ARM WEIGHT IAW B737 51-21-73-370-801; CMM 55-40-09; AMM 20-50-11-910-801; SRM 51-40-02-0G-0; AMM 27-21-11-400-801 SEAL GAP CHECK GOOD ATAG: WN0643