As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON ACCESS TO LT HORIZONTAL STAB ACCESS PANEL 333AB; NOTED THAT THE SHARK-FIN PLATE DAMAGED & CRACKED UPON ACCESS TO LT HORIZONTAL STAB ACCESS PANEL 333AB NOTED THAT THE SHARK-FIN PLATE DAMAGED. REMOVED DAMAGED SHARK FIN IAW SRM 51-40-02-0G-0. RECEIVED NEW SHARK FIN AND INSTALLED IAW SRM 51-40-02-0G-0.