As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A 100 HOUR INSPECTION, NOTED THE TOP CORNER OF THE TRAILING EDGE OF THE RUDDER WAS DAMAGED (APPARENTLY FROM BEING PUSHED BACKWARDS) CAUSING SKINS TO SEPARATE FROM THE CENTER FILL MATERIAL (OR CORE). THE DAMAGE IS 1.25 INCHES DOWN FROM THE TOP ALONG THE TRAILING EDGE AND .75 INCH FORWARD OF TRAILING EDGE ALONG TOP OF RUDDER. NO DAMAGE EVIDENT AT HINGE OR MOUNTING AREA.