As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
R/H FWD FUSELAGE SKIN AT #3 PACK DOOR CUT OUT UPPER AFT CORNER HAS 3 CRACKS PROPAGING OUT OF 2 EA. FASTENER HOLES. (MARKED) PERFORMED REPAIR ON #3 ACM DOOR JAMB UPPER AFT CORNER REF. MD-11 SRM 53-20-15-2R REPAIR 3 FIG.201 SHEET 3. "MAJOR REPAIR"