As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CHECK, FOUND LEFT AFT FINGERNAIL COVER PANELS 414AL AND 414AR BOTH HAVE CRACKED AFT STIFFENERS. REMOVED DAMAGED STIFFENERS AND INSTALLED NEW STIFFENERS ON FINGERNAIL COVER PANELS 414AL AND 414 AR IAW SRM 51-42-05-02-01. PREPPED AND PRIMED PANELS IAW SRM 51-25-10-02-01.