As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING HELI LOGGING OPERATION THE PILOT NOTICED INCREASED RIGHT PEDAL REQUIRED TO MAINTAIN POSITION. WHEN IT BECAME OBVIOUS THAT WIND CONDITIONS WERE NOT RESPONSIBLE THE HELICOPTER LANDED WHERE IT WAS FOUND THAT THE BLADE HAD A 10" CRACK CHORDWISE ACROSS THE TOP OF THE BLADE APPROXIMATELY 1.5" INTO ABRASION STRIP AND WITHIN 1.5" OF TRAILING EDGE AT STN.162.