What was found
DURING INSPECTION, CORROSION WAS FOUND ON THE CIRCUMFERENTIAL SKIN SPLICE BETWEEN FRAMES 60 AND 61 AND STRINGERS 20R AND 21R. THE SKIN SPLICE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-012305.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, CORROSION WAS FOUND ON THE CIRCUMFERENTIAL SKIN SPLICE BETWEEN FRAMES 60 AND 61 AND STRINGERS 20R AND 21R. THE SKIN SPLICE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-012305.