What was found
DURING SHOP INSPECTION, THE LEADING EDGE WAS FOUND WORN AT THE O/B END OF FLAP. THE DAMAGE WAS REMOVED AND A DOUBLER AND FILLER INSTALLED PER MM 57-52-0, FIG 803.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SHOP INSPECTION, THE LEADING EDGE WAS FOUND WORN AT THE O/B END OF FLAP. THE DAMAGE WAS REMOVED AND A DOUBLER AND FILLER INSTALLED PER MM 57-52-0, FIG 803.