As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INBOARD FLAP WEDGE ON INBOARD FLAP HAS 3 DENTS. TWO DENTS REMOVED BY DRILLING AND THIRD DENT REMOVED BY CUTTING 1 INCH HOLE. DYE CHECKED AREA FOR CRACKS, NONE FOUND. PLUGGED THE DRILLED HOLES WITH RIVETS PER SRM 57-01-00, FIGURE 2 SHEET 2. REPAIRED 1 IN HOLE WITH FLUSH REPAIR PER SRM 57-01-00 FIGURE 5 SHEET 2 AND FIGURE 8 SHEET 1. USED TI-6AL-4V FOR DOUBLER PER AARD 51-60-00-05.