What was found
DURING INSPECTION, CORROSION WAS FOUND IN THE CIRCUMFERENTIAL SKIN SPLICE BETWEEN FRAMES 14 AND 16 AND STRINGERS 21L TO 20R. THE SKIN SPLICE WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, CORROSION WAS FOUND IN THE CIRCUMFERENTIAL SKIN SPLICE BETWEEN FRAMES 14 AND 16 AND STRINGERS 21L TO 20R. THE SKIN SPLICE WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-02.