As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING OVERHAUL INSPECTION, THE LOWER FUSELAGE SKIN PANEL BETWEEN BS 259.50 AND BS 312 AT STRINGER 20R HAD TO BE TRIMMED TO REMOVE CORROSION DAMAGE TO THE SKIN BELOW THE FWD LAV SERVICE DOOR. REPAIRED IN ACCORDANCE WITH FAA/DER FORM 8110-3, DATED 08-14-95, AN EXTERNAL REPAIR DOUBLER WAS INSTALLED.