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 FR78 ONE RIVET BELOW STRINGER 4L. MAINTENNACE REMOVED THE DAMAGE AND INSTALLED A DOUBLER REPAIR IAW ETD2014-145-046706A AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.