As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, CRACK ON SEAT TRACK VERT FLANGE AT BS 1000 LBL 11.33. VERIFIED END OF CRACK WITH EDDY CURRENT. STOP DRILL END OF CRACK USING NR 10 DRILL BIT. INSTALLED REPAIR PARTS IAW DWG AIA/E/2731. CORROSION TASK CARD NUMBER C53-210-05. NON-ROUTINE TASK CARD NUMBER 12540.