As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND CRACK IN HEAVY STRUCTURE UPPER FORWARD CORNER OF MAIN CARGO DOOR. RII REQUIRED. ALUM 2024-T3, 090, PO21582, FASTENERS USED HL18-6-10 HI LOKS, AND NAS 1103-11 BOLTS. MADE AND INSTALLED REPAIR DOUBLER IAW AERONAUTICAL SOLUTION REPORT 03-0061R.