What was found
CRACKED SUPPORT ANGLE IN AFT FLAP WHEEL ATTACHED TO INBOARD SIDE OF RH DEFLECTION CONTROL ARM. / REMOVED AND REPLACED SUPPORT ANGLE AT AFT FLAP R/H I/B OF DEFLECTION RIB PER SRM 51-40-02
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED SUPPORT ANGLE IN AFT FLAP WHEEL ATTACHED TO INBOARD SIDE OF RH DEFLECTION CONTROL ARM. / REMOVED AND REPLACED SUPPORT ANGLE AT AFT FLAP R/H I/B OF DEFLECTION RIB PER SRM 51-40-02