As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING DAILY INSPECTION, THE TAIL ROTOR BLADE WAS FOUND TO HAVE DELAMINATED SKIN ON THE OTBD SIDE OF THE BLADE, 4 INCHES FROM END TIP OF BLADE & AFT OF LE STAINLESS STEEL STRIP. THE ALUMINUM SKIN HAD DEBONDED FROM THE SPARE APPROX 5 INCHES SPAN WISE & 3 INCHES CHORD WISE. NO SIGNS OF A TAIL ROTOR STRIKE WAS EVIDENT. THE OTHER TAIL ROTOR BLADE HAD NO SIGNS OF DAMAGE AFTER INSPECTION.