As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) CRACK FOUND ON MAIN ROTOR BLADE LOWER SKIN THAT EXTENDS FROM THE T/E CHORD-WISE TOWARDS THE SPAR. CRACK IS APPROXIMATELY 9" IN LENGTH AND LOCATED 99.0" INBD FROM BLADE TIP. DAYLIGHT WAS VISIBLE THROUGH HALF OF THE CRACK LENGTH. THIS BLADE SN IS NOT AFFECTED BY AD CF2011-44R1, ASB 206L-09-159 OR ASB 206L-09-163A. IAW THE MM IT HAS A 4000 HOUR RETIREMENT LIFE. BLADE IS BEING REMOVED AND WILL BE INSPECTED BY MFG REP.