As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ANNUAL INSPECTION, THE FRONT SPAR CARRY-THROUGH STRUCTURE FORWARD WEB WAS FOUND BUCKLED BELOW THE LT WING ATTACH FITTING. THE DAMAGE EXTENDED BETWEEN THE LOWER SKIN AND THE FITTING HORIZONTALLY FOR APPROX 12 INCHES. THERE WAS ADDITIONAL DEFORMATION INBOARD OF LT LOWER ATTACH FITTING. GREASE, DIRT, AND DEBRIS HAD TO BE REMOVED TO ADEQUATELY INSPECT THE AREA. AIRCRAFT HAS A PREVIOUS HISTORY OF GEAR-UP LANDING.