What was found
RIGHT FIXED LEADING EDGE SKIN HAS A 1.00 IN. CRACK THROUGH THE FASTENER AT SLAT TRACK NR 15 CUT OUT, AFT I/B CORNER. INSTALLED FILLER & DOUBLER IAW SRM 57-40-02-2R FIG 201 SHT 1. MAJOR REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT FIXED LEADING EDGE SKIN HAS A 1.00 IN. CRACK THROUGH THE FASTENER AT SLAT TRACK NR 15 CUT OUT, AFT I/B CORNER. INSTALLED FILLER & DOUBLER IAW SRM 57-40-02-2R FIG 201 SHT 1. MAJOR REPAIR.