What was found
LEFT WING, CRACK ON WING LEADING EDGE AT FWD I/B CORNER OF FUELING PANEL. REMOVED DAMAGED AND INSTALLED NEW DOUBLER AND FILLER AT L/H WING LEADING EDGE SKIN AT SLAT TRACK #11 IAW SRM 57-40-02-2R, REPAIR 7, FIG 201, SHEET 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING, CRACK ON WING LEADING EDGE AT FWD I/B CORNER OF FUELING PANEL. REMOVED DAMAGED AND INSTALLED NEW DOUBLER AND FILLER AT L/H WING LEADING EDGE SKIN AT SLAT TRACK #11 IAW SRM 57-40-02-2R, REPAIR 7, FIG 201, SHEET 1.