As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TAIL ROTOR CONTROLS BINDING AND STIFF IN HOVER. NO OBVIOUS DEFECTS. REMOVED BLADES AND MOUNTING FORKS. VISUALLY INSPECTED SURFACES OF TEFLON AND STEEL BUSHINGS AND FOUND NO DEFECTS. PERFORMED SLIDING FRICTION TEST AND FOUND NO DEFECTS. REASSEMBLED, TORQUED AND SAFETIED AS REQUIRED. INSTALLED 2 SERVICEABLE BLADES AND STATIC BALANCED. INSPECTED IAW BO-105. RE, 301, MM CH 33, 34, & 107. TT 8818.8 TSI 31.2