As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING VISUAL INSPECTION NOTICED THAT RIGHT WING INBOARD TKS PANEL WAS DEFORMED ALONG LEADING EDGE FROM WS.37.00 TO WS 51.00. UPON INSPECTION OF BACKSIDE OF LEADING EDGE FOUND THAT LEADING EDGE WAS PUSHED IN APPROX .50 INCHES DEEP AND .50 INCHES WIDE BETWEEN NOTED WING STATIONS. TKS SYSTEM WAS TESTED AND SEEMED TO OPERATE NORMALLY.