As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 5A INSPECTION, THE LT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FR75 ABOVE STR02L. MX REMOVED THE DAMAGED PORTION OF SKIN AND PERFORMED A TRIPLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02501, THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 06/29/13.