What was found
DURING CHECK-C MAINT THE LT INBOARD FLAP HAD HOLE WORN THRU THE LEADING EDGE WEAR STRIP OF THE FLAP, 51 INCHES FROM THE INBOARD EDGE OF THE FLAP. REMOVED DAMAGED AREA AND REPAIRED PER SRM 57-09, FIG 43.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CHECK-C MAINT THE LT INBOARD FLAP HAD HOLE WORN THRU THE LEADING EDGE WEAR STRIP OF THE FLAP, 51 INCHES FROM THE INBOARD EDGE OF THE FLAP. REMOVED DAMAGED AREA AND REPAIRED PER SRM 57-09, FIG 43.