What was found
AFTER STARTING THE NO.2 ENGINE SEVERAL SECONDS AFTER THE STARTER DROPPED OUT, FELT A METALLIC CLUNK IN THE PEDALS. THERE WERE NO INDICATIONS OF ANY MALFUNCTIONS IN THE INSTRUMENTS. WITH THE ENGINE AT IDLE THE IP PUSHED THE PEDALS BACK AND FORTH SLIGHTLY WITH NO INDICATIONS OF ANY MALFUNCTION. AFTER SHUTTING DOWN THE ENGINE AND THE ROTOR SYSTEM STOPPED, TESTING THE PEDALS THE LEFT PEDAL WORKS CORRECTLY, BUT THE RIGHT HAS A DISTINCT RATCHETING, WHICH CAN BE SEEN WHEN OBSERVING THE TAIL ROTOR WHILE SOMEONE PUSHES THE RIGHT PEDAL IN, THE SAME RESULT REGARDLESS OF WHICH FLIGHT STATION'S PEDALS ARE USED. AFTER TROUBLESHOOTING, MAINTENANCE DETECTED THE YAW TRIM MOTOR BINDING INTERNALLY. REMOVED AND REPLACED YAW TRIM MOTOR IAW 67-14-00, 4-1; T/F SUCCESSFULLY COMPLETED.