As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING CYCLE CARD INSPECTION THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED IN 2 PLACES AT A SINGLE RIVET ON FRAME 77 BELOW STRINGER 8L. MX PERFORMED A BUSHING REPAIR IAW DER APPROVED ETD2013-145-019577, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.