What was found
INSPECTION FOUND A 5" CRACK IN ANGLE STIFFENER INSIDE #3 FLAP TRACK FAIRING. THE ANGLE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-10-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 5" CRACK IN ANGLE STIFFENER INSIDE #3 FLAP TRACK FAIRING. THE ANGLE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-10-2.