As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BEARING DEBONDING CAUSING BINDING. OB BUSHING ON INNER SLEEVE HAD SLIPPED. GRIP BUSHINGS WORN. ACTION TAKEN: C/W PRE INSPECTION AND FOUND INNER SLEEVE BUSHING NOT SEATED. DISASSEMBLED AS FAR AS NECESSARY FOR REPAIR, CLEANED AND VISUALLY INSPECTED PARTS. REASSEMBLED TAIL ROTOR WITH NEW SEALS 2 EA SERVICEABLE BLADES AND STATIC BALANCED. REPAIRED IAW REM 301AND BO105 MM CHAPTER 34 AND 107.