As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) OPERATOR NOTICED PAINT CRACK DURING SCHEDULED MAINTENANCE. TAIL ROTOR BLADE SENT OUT FOR FURTHER INSPECTION WHICH LATER REVEALED A 45 MM SPANWISE CRACK AT 45 DEGREE ANGLE ON THRUST SIDE OF NR 1 BLADE. CRACK FOUND AT BLADE STATION 450 MM AND EXTENDED FROM TE RIVET NEAR BLADE ROOT. REVERSE SIDE OF BLADE ALSO HAD A CHORDWISE CRACK OF 15 MM.