What was found
DURING INSPECTION, CORROSION WAS FOUND ON THE SKIN PANEL INTERNAL SIDE BETWEEN FRAME 65 AND 66 AND STRINGERS 21L AND 21R. THE DAMAGED AREA WAS REPAIRED IAW ETD 2013-145-035812.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, CORROSION WAS FOUND ON THE SKIN PANEL INTERNAL SIDE BETWEEN FRAME 65 AND 66 AND STRINGERS 21L AND 21R. THE DAMAGED AREA WAS REPAIRED IAW ETD 2013-145-035812.