What was found
DURING INSPECTION, CORROSION WAS FOUND AT STRINGER 21L AT FRAME 9 THROUGH FRAME 10 AT THE RIVETS AND THE END OF FRAME 13. 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 AT STRINGER 21L AT FRAME 9 THROUGH FRAME 10 AT THE RIVETS AND THE END OF FRAME 13. THE STRINGER WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.