What was found
TAIL ROTOR TRIM TAB DEBONDED APPROXIMATELY 90 MM ON BOTH SIDES, STARTING ON THE INBOARD END. TAIL ROTOR INSTALLED. FOUND ON PREFLIGHT, POSSIBLE IMPROPER BONDING DURING MANUFACTURE. PART RETURNED TO MFG FOR EVALUATION.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TAIL ROTOR TRIM TAB DEBONDED APPROXIMATELY 90 MM ON BOTH SIDES, STARTING ON THE INBOARD END. TAIL ROTOR INSTALLED. FOUND ON PREFLIGHT, POSSIBLE IMPROPER BONDING DURING MANUFACTURE. PART RETURNED TO MFG FOR EVALUATION.