As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 4A INSPECTION THE REAR FUSELAGE 1 SKIN WAS FOUND TO BE CRACKED AT FRAME 75 BETWEEN STRINGERS 1R AND 2R. MX PERFORMED A DOUBLER REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-02353, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.