What was found
DURING INSPECTION, CORROSION WAS FOUND ON THE EDGE OF STRINGER 21R AT FRAME 11 THROUGH 12. THE STRINGER 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 EDGE OF STRINGER 21R AT FRAME 11 THROUGH 12. THE STRINGER WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.