As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING, AFT OF NR 3 LEADING EDGE SLAT ON TOP OF WING, A PREVIOUS OVERLAY REPAIR IS PEELING UP. AREA 2 BY 9 INCHES. DAMAGE BETWEEN LEADING EDGE SLAT AND FWD WING SPAR. PREVIOUS HOT BOND REPAIR ON NR 3 L/E SLAT IS SEPARATING. REMOVED DAMAGED MATERIAL FROM SLAT. NEW CORE MATERIAL CUT AND READY TO POT IN. FITTED HONEYCOMB FILLER MATERIAL. COMPLETED REPAIR IAW 51-70-10.