As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND 10 INCH CRACK ON NR 14 UPPER WING LEADING EDGE PANEL. CRACK STARTS AT OUTBOARD AFT CORNER AREA OF PANEL. PANEL IS THIRD FIXED UPPER LEADING EDGE PANEL INBOARD OF NR 4 ENG. ACCOMPLISHED 250 DEG OVER LAY REPAIR, NEEDS CONDUCTIVE COATING, PRIMER AND TOPCOAT. COMPLETED APPLICATION OF PRIMER CONDUCTIVE COATING AND TOP COAT.