As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING AAIP INSPECTION D0521 MAIN ROTOR BLADE CUFF INSPECTION, A TRANSVERSE CRACK WAS DETECTED IN THE PAINT ON THE MAIN ROTOR BLUE BLADE. PAINT WAS REMOVED FROM THIS AREA & CRACK WAS DETERMINED TO EXIST. THIS CRACK RUNS TRANSVERSE TO THE BLADE BETWEEN THE MAIN ROTOR BLADE ROOT & VIBRATION ABSORBER FITTING ON THE BLADE.