As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 4A INSPECTION THE RT AFT FUSELAGE II SKIN WAS FOUND TO HAVE A SINGLE CRACK EMINATING FROM A RIVET AT FR 78 STR 5R. MX REMOVED THE DAMAGE, AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02501, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 05/14/13.