As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 4A INSPECTION THE LT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET AT FR79 1 RIVET ABOVE STRINGER 6L. MAINTENACE REMOVED THE DAMAGE AND INSTALLED A BUSHING REPAIR IAW ETD2014-145-046706, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.