As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING MX INSPECTION, FUSELAGE SKIN WAS FOUND TO BE CRACKED ACROSS A RIVET HOLE APPROX 16MM IN LENGTH BETWEEN FRAME 77-78 JUST ABOVE STR 6R. MX INSTALLED A REPAIR DOUBLER ON THE AFFECTED AREA, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.