As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 0.125 INCH CRACK AT FASTENER IN FUSELAGE SKIN JUST AFT OF STA 390, S21R. AN INTERIM REPAIR WAS INSTALLED IAW ECRA 5331-01229 AND A DIP WAS INITIATED TO ACCOMPLISH A PERMANENT REPAIR WITHIN 6,000 FLIGHT CYCLES OR 24 MONTHS WHICH EVER OCCURS FIRST FROM ACCOMPLISHMENT OF THE INTERIM REPAIR.