As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORRODED INTERNAL DOUBLER ON PANEL 192CR. REMOVED CORROSION BY BLENDING FOUND TO BE WITHIN LIMITS REMOVED .002" PANEL NOMINAL THICKNESS .050" REF SRM 51-75-16. FOUND 1EA ELONGATED HOLE NO ALLOWABLE DAMAGE OR REPAIR FOUND IN SRM. REMOVED AND REPLACED PANEL 192CR ATTACHED ORIGINAL STIFFENERS AND NEW DOUBLER REF 51-41-02.