As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK WITH DENT OF 24.625" X 14.125" ON FUSELAGE SKIN BETWEEN BS 392.625 AND BS 417.250 AND BETWEEN STRINGERS 24 & 26 RH. HFEC INSPECTION ACCOMPLISHED ON SKIN. CRACK WITH DENT WAS DELIMITED OF 24.5" X 14". REPAIR IS CURRENTLY BEING PERFORMED.