What was found
DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE I FLOOR STRUCTURE GALLEY ANGLE. THE CENTER FUSELAGE I FLOOR STRUCTURE GALLEY ANGLE WAS REPLACED AND INSTALLED WITH SOLID RIVETS 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 I FLOOR STRUCTURE GALLEY ANGLE. THE CENTER FUSELAGE I FLOOR STRUCTURE GALLEY ANGLE WAS REPLACED AND INSTALLED WITH SOLID RIVETS IN ACCORDANCE WITH SRM 51-40-02.