What was found
(CAN) DURING FLAP SYSTEM TROUBLESHOOTING A CRACK WAS IDENTIFIED ON THE THREADED BORE OF THE RT OTBD FLAP ACTUATOR AT THE STAKING PIN LOCATION.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) DURING FLAP SYSTEM TROUBLESHOOTING A CRACK WAS IDENTIFIED ON THE THREADED BORE OF THE RT OTBD FLAP ACTUATOR AT THE STAKING PIN LOCATION.