As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK FROM RIVET HOLE BOTTOM LEFT CORNER TO OUTER EDGE OF FITTING. CRACK LENGTH APPROXIMATELY .5000 INCH. THIS IS ONE OF FOUR EARS THAT ATTACH TO THE PYLON LONGERONS. THIS PART OF THE ASSEMBLY THAT THE TAIL ROTOR GEARBOX ATTACHES TO. CAUSE UNKNOWN AT THIS TIME.