What was found
INSPECTION FOUND A 2 INCHES CRACK IN NR 3 FLAP FAIRING AFT SUPPORT ANGLE THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCHES CRACK IN NR 3 FLAP FAIRING AFT SUPPORT ANGLE THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.