What was found
RUDDER BIAS FAULT CAS MESSAGE CAME ON AFTER ROTATION. R & R ACTUATOR NO FAULTS FOUND ON INSPECTION OF RUDDER BIAS COMPONENTS. C/W SATISFACTORY OPERATIONAL CHECKS IAW MM 27-20-00 & FT-680-0022.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RUDDER BIAS FAULT CAS MESSAGE CAME ON AFTER ROTATION. R & R ACTUATOR NO FAULTS FOUND ON INSPECTION OF RUDDER BIAS COMPONENTS. C/W SATISFACTORY OPERATIONAL CHECKS IAW MM 27-20-00 & FT-680-0022.