As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING 100 HRS INSPECTION, TECH WHILE PERFORMING AD CF2008-29 FOUND LOW CLEARANCE BETWEEN THE RUDDER AND THE REAR FUSELAGE SKIN. AFTER RUDDER REMOVAL, THEY FOUND UPPER TORQUE TUBE LOWER BEARING AND LOWER TORQUE TUBE UPPER BEARING CORRODED.