What was found
MAIN CARGO DOOR FRAME AFT ACT AREA HAS CRACK. REPAIRED IAW AERONAUTICAL SOLUTIONS REPORT 03-011 IR DTD 12/30/03. MATERIAL USED 2024-T3 .090 PO 21582, FASTENERS USED 1103-11 BOLTS, AND HL62-6-9. THIS REPAIR IS A MAJOR REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAIN CARGO DOOR FRAME AFT ACT AREA HAS CRACK. REPAIRED IAW AERONAUTICAL SOLUTIONS REPORT 03-011 IR DTD 12/30/03. MATERIAL USED 2024-T3 .090 PO 21582, FASTENERS USED 1103-11 BOLTS, AND HL62-6-9. THIS REPAIR IS A MAJOR REPAIR.