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 INTO LT FRAME RADIUS AT FS 1000, 5 ABOVE UPPER CUSP AREA. FAB REPAIR FROM 7075 .071 FORMED AND HEAT TREATED TO 7075.T6 IAW COTNEY D93-R42 TREAT AND PRIMED IAW COTNEY DWG NR D93-R42. INSTALLED REPAIR IAW COTNEY DWG NR D93-R42, DC8 SRM 51-1-21 AND 51-1-8. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04941 TASK NR Y1399.