As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 2A INSPECTION THE LT SIDE FUSELAGE SKIN WAS FOUND TO BE CRACKED IN 2 PLACES AT A RIVET ON FRAME 77 BELOW STRINGER 8L. MX REMOVED THE DAMAGE AND PERFORMED A FREEZE PLUG REPAIR IAW APPROVED ETD2013-145-027513, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.