As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EXTERIOR FUSELAGE MCD AFT HINGE AFT END HAS LARGE CRACK TO ATTACH SCREW HOLE, FROM LOBE. REPLACED HINGE SEGMENT IAW SRM 51-30-5, 51-30-2 & IAW DWG 52FX1433 REV E & INSTALLED NEW HINGE PIN IAW SRM 51-30-2 & DRAWING 52FX1433 REV E. OPS CHECK GOOD IAW MM 52-34-000-5