As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
GSO - INSPECTION FOUND A 1 INCH CRACK EXTENDING BEYOND STOP HOLE IN RT WING UPPER SURFACE FIXED LEADING EDGE. THE ADJACENT SKIN AT O/B TRACK FOR NR 5 SLAT WAS WARPED. THE DAMAGED AREA WAS ROUTED OUT IAW SRM 57-30-4. REPAIR DOUBLER AND FILTER WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2. (W)