What was found
INSPECTION FOUND LT WING LEADING EDGE OF NR 1 FORE FLAP CHAFED DUE TO CONTACT WITH SPOILER ACTUATOR HYDRAULIC LINE. THE LEADING EDGE OF NR 1 FORE FLAP WAS REPLACED IAW ECRA 5753-01100.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND LT WING LEADING EDGE OF NR 1 FORE FLAP CHAFED DUE TO CONTACT WITH SPOILER ACTUATOR HYDRAULIC LINE. THE LEADING EDGE OF NR 1 FORE FLAP WAS REPLACED IAW ECRA 5753-01100.