What was found
(CAN) DURING 100 HR INSPECTION OF THE HELICOPTER, IT WAS NOTED THAT ENGINE RPM INDICATION ON THE DUAL TACH WAS HIGH AT 103.0 PERCENT TO 103.5 PERCENT. DUAL TACH AND GOVENOR CONTROLLER WERE REPLACED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) DURING 100 HR INSPECTION OF THE HELICOPTER, IT WAS NOTED THAT ENGINE RPM INDICATION ON THE DUAL TACH WAS HIGH AT 103.0 PERCENT TO 103.5 PERCENT. DUAL TACH AND GOVENOR CONTROLLER WERE REPLACED.