As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN FORWARD OF AFT CARGO DOOR DAMAGED BY DOOR OPENING STEP. AREA INSPECTED, DAMAGE LENGTH APPROX 8 INCHES LONG ACROSS STRINGER S44R BETWEEN BS 1780 - 1800, BELOW AND FWD OF CARGO DOOR SILL AREA. REPAIR CARRIED OUT IAW SRM 53-00-01 REPAIR 1 AND AVO 1847 REV A. MAJOR REPAIR.