As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THRU V1, RUDDER BECAME EXTREMELY STIFF AND REMAINED STIFF UNTIL AFTER AIRCRAFT CAME TO A TAXI. YAW DAMPER WAS CYCLED ON THEN OFF TWICE AND APPEARED TO FUNCTION NORMALLY. REMOVED FAULTY LT AND RT RUDDER BIAS STRUTS. INSTALLED LT AND RT UNIT IAW HAWKER 1000 MM 27-20-10. OPERATIONAL CHECK SATISFACTORY.