What was found
(CAN) LEADING EDGE STRIP OF BOTH TAIL ROTOR BLADES DEBONDING. DEBONDING OCCURRED IN SAME AREA ON BOTH BLADES.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) LEADING EDGE STRIP OF BOTH TAIL ROTOR BLADES DEBONDING. DEBONDING OCCURRED IN SAME AREA ON BOTH BLADES.