As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FUSELAGE SKIN WAS FOUND WITH SEVERAL SMALL AREAS OF CORROSION AT THE S-26R LAP SPLICE BETWEEN FS 700 AND 720C. THE CORRODED AREAS WERE LOCALLY CUT OUT AND LOCAL REPAIR DOUBLERS WERE INSTALLED. THE REPAIRS WERE ACCOMPLISHED PER ER/A 365577-14, REV C DATA ANALYSIS WILL BE ACCOMPLISHED WITHIN 12 MONTHS OF THE REPAIR.