As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING SCHEDULED INSPECTION, CRACKS WERE FOUND ON THE INBOARD LEADING EDGE SKIN THAT DOVE TAILS ONTO THE TOP OF THE MAIN SPAR INSIDE THE CABIN. CRACKS WERE AT FS 91.50 AND WS 23.16. THE CRACK ON THE RIGHT WING IS RUNNING FROM THE AFT EDGE FORWARD ABOUT 3 INCH, THE LEFT CRACK IS LOCATED IN THE CENTER OF THE OF THE TAB AND IS ABOUT 1.25".