As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION WAS FOUND ON THE LEFT SECTION 46 WING-TO-BODY FAIRING SCREW HOLES COMMON TO THE FUSELAGE SKIN. AFTER CORROSION WAS REMOVED, 5 SCREW HOLES LOCATED BETWEEN STATIONS 1092 TO 1137 AND STRINGERS 37 AND 38 LEFT. HIGH FREQUENCY EDDY CURRENT WAS ACCOMPLISHED TO ENSURE ALL CORROSION HAD BEEN REMOVED. BOEING APPROVED TO REPAIR THE HOLES BY INSTALLING INTERNALLY COUNTERSUNK FREEZE PLUGS PER THE SRM. EA B767-53-009310.