As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 2A INSP THE LT AFT FUSELAGE SKIN WAS FOUND TO HAVE 2 EA CRACKS TOTALING 3.01MM (.118") IN LENGTH AT A RIVET ON FRAME 79 BELOW STRINGER 06L. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR IAW DER APPROVED TECH DISPOSITION ETD2013-145-029290, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 08/15/13.