As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SHORTLY AFTER TAKE OFF, LEFT PEDAL WAS APPLIED WITH A BINDING IN THE PEDAL CONTROLS. AN UNUSUAL SOUND WAS COMING WHEN PEDAL INPUT WAS APPLIED. MAINTENANCE PULLED MULTIPLE FAILURE CODES RELATED TO THE YAW ANTICIPATOR STORED IN THE VEMD. INSPECTED ENTIRE TAIL ROTOR CONTROL SYSTEM INCLUDING THE FENESTRON WITH NO BINDING OR ABNORMAL NOISES NOTED