As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING AN AIRWORTHINESS, PREFLIGHT INSPECTION, ONE CRACK ESTIMATIED TO BE .03125"-.0625" WAS FOUND ON THE CENTER TIP BLOCK SEAL OF THE TAIL ROTOR BLADE WHEN COMPLYING WITH INSTRUCTIONS LAID OUT IN THE MM A ADDITIONAL CRACK WAS FOUND ON THE TRAILING TIP BLOCK SEAL. THE SECOND CRACK HAD NOT SHOWN INDICATIONS THROUGH THE PAINT.