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 1220, 5 ABOVE UPPER CUSP AREA. FABRICATED STRAP FOR HOLES IN FRAME AT STA 1220 IAW COTNEY DWG D93-R44. TREATED AND PRIMED IAW 51-1-8, INSTALLED STRAP IAW COTNEY DWG D93-R44. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04948 TASK NR Y1406.