As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON INTERNAL FUSELAGE SKIN BETWEEN FS 280.00 AND 295.00 AND STGR 25RH AND 24RH. INTERNAL FUSELAGE SKIN BETWEEN FS 280.00 AND 295.00 AND STGR 25RH AND 24RH WAS REPAIRED PER EA 23-C9-53-0904 REV. IR SECTION III - PERMANENT REPAIR