As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CLT - Q6 - MAJOR REPAIR - CRACK ON FUSELAGE SKIN AT LOWER FORWARD RADIUS OF LOWER HINGE CUTOUT AT AFT ENTRY DOOR AT BS 960 BETWEEN S15L TO S16L. REPAIRED FUSELAGE SKIN AT LOWER FORWARD RADIUS OF LOWER HINGE CUTOUT AT AFT ENTRY DOOR AT BS 960 BETWEEN S15L TO S16L IAW TYPICAL REPAIR 53-60-10.