What was found
MAIN ROTOR BLADE FIBERGLASS BEHIND THE SPLICE AREA IS TORN AND SEPARATED BEYOND LIMITS. HELICOIL AT THE ROOT END IS STRIPPED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAIN ROTOR BLADE FIBERGLASS BEHIND THE SPLICE AREA IS TORN AND SEPARATED BEYOND LIMITS. HELICOIL AT THE ROOT END IS STRIPPED.