As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AT PHASE INSPECTION , FOUND ONE 2.5 INCH CRACK, 8 INCHES FROM AFT LOWER INBOARD EDGE AND ONE 1.5 INCH CRACK IN LOWER FORWARD AREA OF THE LEFT OUTER WING LEADING EDGE SKIN,1 INCH CRACK IN 000-110133-21 STIFFENER RIB, AND 000-110133-9 CLIP LOOSE AT THREADED MOUNTING FLANGE FASTENERS.