As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DISCOVERED TO HAVE WATER LEAKING INTO THE CABIN AROUND THE AFT LT WING TO FUSELAGE ATTACH FRAME, X 373.150. THE FWD WING TO FUSELAGE ATTACH FRAME WAS INSPECTED FOR PRESENCE OF WATER. STAINING DUE TO WATER INGRESS WAS EVIDENT AROUND THE BOLT HEADS. CORRODED HARDWARE NOTED AT LT REAR WING TO FUSELAGE STRUTS.