As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 2A INSPECTION, THE RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 79 BELOW STRINGER 05R. MX REMOVED THE DAMAGE AROUND THE RIVET AND PERFORMED A BUSHING REPAIR IAW DER APPROVED TECHL DISPOSITION ETD2013-145-029290, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 08/15/13.