What was found
DURING INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE SKIN BETWEEN FRAMES 61 AND 62 AND STRINGERS 21L AND 21R. THE SKIN WAS REPAIRED IAW SRM 53-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE SKIN BETWEEN FRAMES 61 AND 62 AND STRINGERS 21L AND 21R. THE SKIN WAS REPAIRED IAW SRM 53-31-01.