What was found
DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE II FLOOR STRUCTURE RIGHT SILL NUMBER 1. THE SILL WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE II FLOOR STRUCTURE RIGHT SILL NUMBER 1. THE SILL WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.