As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C/W TAIL ROTOR BLADE VISUAL INSPECTION IN AD 96-01-08, A 5.3 INCH LONG CORD-WISE CRACK WAS DISCOVERED ON THE CONVEX SURFACE OF THE BLADE .25 INCH BELOW THE END OF THE DOUBLER. CRACK SIZE AND LOCATION IS THE SAME AS SHOWN IN THE ILLUSTRATION CONTAINED IN THE AD.