As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CHECK, FOUND CORROSION AROUND SCREW HOLES IN LEFT MAIN GEAR SUPPORT STRUCTURE. REMOVED CORROSION AROUND SCREW HOLES AND OVERSIZED 14 EACH HOLES TO .25 INCH IAW AERO CORP E.O. 97-580 AND RES 04452. MATERIAL LOSS LESS THAN .005 INCH. INSTALLED PANEL IAW B737 SRM 51-30-2. (X)