What was found
DURING INSPECTION, CORROSION WAS FOUND IN RIGHT SILL AT ANCHOR HOLES FRAME 22 TO FRAME 23. THE RIGHT SILL AT FRAME 22 TO FRAME 23 WAS REPAIRED 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 IN RIGHT SILL AT ANCHOR HOLES FRAME 22 TO FRAME 23. THE RIGHT SILL AT FRAME 22 TO FRAME 23 WAS REPAIRED IN ACCORDANCE WITH SRM 51-40-02.