As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED ON LT FRAME RADIUS AT FS 1160, 5 ABOVE UPPER CUSP AREA. FAB AND INSTALLED TWO REPAIRS IAW COTNEY DWG NR D93-R49 AND 51-1-8 AND 51-1-20D WHERE SEVERAL HOLES WERE DRILLED IN FRAME AT FS 1160 LT, 5 ABOVE UPPER CUSP. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04945 TASK NR Y1403.