As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION, THE FORWARD NUT PLATE AT THE SERVICE DOOR THRESHOLD AFT OF FRAME 19 WAS FOUND TO BE CORRODED. THE CORROSION WAS REMOVED IN ACCORDANCE WITH SRM 51-10-03. A HIGH FREQUENCY EDDY CURRENT INSPECTION WAS PERFORMED WITH NO DEFECTS NOTED IN ACCORDANCE WITH NIM INTRO E. TWO DOUBLERS WERE FABRICATED IN ACCORDANCE WITH SRM 5-21-02. THE REPAIR WAS INSTALLED IN ACCORDANCE WITH SRM 51-40-02.