As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TWO AREAS OF DISBOND ON MAIN ROTOR BLADE. (TOP SURFACE STARTS AT BLADE STA 232 AND EXTENDS SPANWISE APPROXIMATELY 4 INCHES ALONG LEADING EDGE STRIP, EXTENDING AFT APPROXIMATELY 4 INCHES CHORDWISE). LOWER SURFACE STARTING AT BLADE STA 237, APPROXIMATELY EXTENDING SPANWISE 4 INCHES, LOCATED AFT OF LEADING EDGE 3 INCHES APPROX .75 IN CHORDWISE.