What was found
TAIL ROTOR BLADE DISBOND DETECTED DURING DAILY INSPECTION. FOUND APPROXIMATELY 1 INCH BY 1 INCH SKIN DELAMINATION AT TIP WEIGHT AREA. POSSIBLY CAUSED BY RUST FORMING ON TIP WEIGHT HARDWARE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TAIL ROTOR BLADE DISBOND DETECTED DURING DAILY INSPECTION. FOUND APPROXIMATELY 1 INCH BY 1 INCH SKIN DELAMINATION AT TIP WEIGHT AREA. POSSIBLY CAUSED BY RUST FORMING ON TIP WEIGHT HARDWARE.