What was found
DURING POST-FLIGHT INSPECTION, THE T/R FIPS SLIP RINGWIRES WERE FOUND TO BE CHAFED AND BROKEN, CAUSING ARCING DAMAGE ON THE TAIL ROTOR HUB DAMPER BRACKETS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING POST-FLIGHT INSPECTION, THE T/R FIPS SLIP RINGWIRES WERE FOUND TO BE CHAFED AND BROKEN, CAUSING ARCING DAMAGE ON THE TAIL ROTOR HUB DAMPER BRACKETS.