What was found
RIGHT T/E, INBD MAIN FLAP DEBONDED. REMOVED AND REPLACED THE FLAP WEDGE IAW SRM 51-40-02, AND CMM 57-53-05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT T/E, INBD MAIN FLAP DEBONDED. REMOVED AND REPLACED THE FLAP WEDGE IAW SRM 51-40-02, AND CMM 57-53-05.