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