What was found
CORROSION WAS FOUND IN AN INTERNAL FASTENER HOLE OF THE ACCESS DOOR CUTOUT BETWEEN STRINGERS 12 AND 15, XRS=189 - XRS=214 ON THE LT WING. THE CORROSION WAS REMOVED AND REPAIRED IAW SRM 51-22-2A, PAR 7.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION WAS FOUND IN AN INTERNAL FASTENER HOLE OF THE ACCESS DOOR CUTOUT BETWEEN STRINGERS 12 AND 15, XRS=189 - XRS=214 ON THE LT WING. THE CORROSION WAS REMOVED AND REPAIRED IAW SRM 51-22-2A, PAR 7.