As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAIN ROTOR BLADE S/N AC86-00479 HAS AREAS OF DISBOND ON LOWER SIDE SKIN JUST AFT OF TITANIUM LEADING EDGE. FIRST AREA IS 47.50 INCHES OUTBOARD OF ROOT END AND IS APPROXIMATELY 13 INCHES BY 1 INCH. SECOND AREA IS 201 INCHES OUTBOARD OF ROOT END AND APPROXIMATELY 8 INCHES BY 1 INCH.