What was found
THE LT WING FIXED LEADING EDGE SKIN HAD A 2.5 INCH CRACK FROM LOWER EDGE RUNNING FORWARD AT APPROXIMATELY XORS 810. THE CRACKED AREA WAS REMOVED. DOUBLER, FILLERS, AND FASTENERS WERE INSTALLED IAW SRM 57-00-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE LT WING FIXED LEADING EDGE SKIN HAD A 2.5 INCH CRACK FROM LOWER EDGE RUNNING FORWARD AT APPROXIMATELY XORS 810. THE CRACKED AREA WAS REMOVED. DOUBLER, FILLERS, AND FASTENERS WERE INSTALLED IAW SRM 57-00-01.