What was found
DURING INSPECTION, CORROSION WAS FOUND AT STRINGER 21R AT FRAME 10 THROUGH FRAME 11. THE STRINGER 21R AT FRAME 10 THROUGH FRAME 11 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 AT STRINGER 21R AT FRAME 10 THROUGH FRAME 11. THE STRINGER 21R AT FRAME 10 THROUGH FRAME 11 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.