As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
GSO - INSPECTION FOUND THE LEFT WING UPPER SURFACE TRAILING EDGE PANEL AT OUTBOARD END OF OUTBOARD FLAP WITH A 1 INCH CRACK IN DOUBLER ATTACHED TO INBOARD SIDE. THE CRACKED DOUBLER WAS REMOVED. A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-1 AND 51-30-2. (M)