As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
R/H FIXED LEADING EDGE SKIN HAS A .250 IN. CRACK AT SLAT TRACK #10 CUT OUT AFT I/B CORNER. INSTALLED FILLER AND DOUBLER ON R/H FIXED LEADING EDGE SKIN AT WING SLAT #10 PER SRM 57-40-02-2R FIG 201 SHT 1. REPAIR OF WING FIXED LEADING EDGE, LOWER SURFACE AT SLAT TRACK CUTOUT. "MAJOR REPAIR".