As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
0.25 INCH CRACK FOUND ON INBOARD SIDE OF THE TRAILING EDGE OF THE TAIL ROTOR BLADE ASSEMBLY. THIS WAS FOUND DURING PREFLIGHT BY THE SCHEDULED PILOT ON DUTY, BUT THERE WERE NO FLIGHTS SCHEDULED FOR THE DAY. AFTERWARD THE MECHANIC ON DUTY VERIFIED THE CRACK WITH DYE PENETRANT. THE CRACK IS NOT IN THE LOCATION IDENTIFIED BY AD 2001-26-55 BUT IS ON THE TRAILING EDGE OF THE BLADE AND WILL REQUIRE REPAIR.