What was found
ACFT HAD EXCESS POWER LOSS FROM ENGINE ON CLIMBOUT. INVESTIGATION FOUND MAG BREAKER DRIVE CAM SLIPPING. CAM SCREW WAS TIGHT AND TO SPECS. SUBMITTER SUSPECTS TAPER ON ROTOR SHAFT TO BE OUT OF TOLERANCE ALLOWING CAM TO BOTTOM OUT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ACFT HAD EXCESS POWER LOSS FROM ENGINE ON CLIMBOUT. INVESTIGATION FOUND MAG BREAKER DRIVE CAM SLIPPING. CAM SCREW WAS TIGHT AND TO SPECS. SUBMITTER SUSPECTS TAPER ON ROTOR SHAFT TO BE OUT OF TOLERANCE ALLOWING CAM TO BOTTOM OUT.