As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING LE EDGE SKIN WAS FOUND CRACKED DURING A PHASE INSPECTION. THE CRACK ORIGINATED FROM THE FIRST ROUND INSPECTION PANEL NEAR WS 60.0, ON THE BOTTOM SIDE OF THE LE. ENGINEERING APPROVAL FOR REPAIR WAS OBTAINED & A REPAIR FOR THE AREA WAS PUT IN PLACE, RECORDED ON FORM 337 WITH SUPPORTING FORM 8110-3.