As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EXTERIOR FUSELAGE AFT MOST FUSELAGE MOUNTED MAIN CARGO DOOR HINGE SEGMENT HAS CORNER CRACKED SECOND LUG FWD OF AFT END VERIFIED WITH HFEC. REMOVED CRACKED HINGE IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW HINGE IAW DWG 52FX1433 REV E AND SRM 51-30-2.