As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING MAINTENANCE, A CRACK WAS FOUND IN THE T/E OF THE LT WING AT WS 148 APPROXMATE 6" AFT OF THE REAR SPAR. THE CRACK IS JUST OVER 2.5" LONG IN SKIN, PN 50-110028-16. ALSO STIFFENER PN 50-11028-12 IS CRACKED ON THE INSIDE OF THE WING IN THIS SAME AREA.