As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING M-CHECK FUSELAGE EXTERIOR AFT CARGO DOOR JAMB FWD LOWER CORNER HAS ELONGATED FASTENER HOLE THRU SKIN AND INTERNAL DOUBLERS AND DOOR PAN AND PAN SPLICE HOLE CLEANED UP AT .3680 IAW SRM 51-20-03. INSTALLED FREEZE PLUG IAW SRM 51-20-03-801-663A-A.