As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-19 CHECK THE NR 5 LEADING EDGE SLAT AT THE INBOARD AND OUTBOARD ENDS OF WEDGE WAS FOUND TO BE DELAMINATED. MAINTENANCE REMOVED DAMAGED AREA OF SKIN ON THE NR 5 LEADING EDGE SLAT AT THE INBOARD AND OUTBOARD END OF WEDGE. APPLIED ADHESIVE, REPLACEMENT SKIN, AND DOUBLERS IAW SRM.