As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(AUS) TAIL ROTOR BLADE LEADING EDGE EROSION STRIP DELAMINATED (DEBONDED) - DEBONDING EXTENDS SPANWISE FROM AN AREA 105MM(4.13IN) FROM THE INBOARD END OF THE STRIP TO 98MM (3.85IN) FROM THE OUTBOARD END AND CHORDWISE FROM THE TRAILING EDGE TO 25MM (1IN) TOWARDS THE LEADING EDGE