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NTSB investigation record

WPR09CA173

Completed

Robinson helicopter R22Beta· N74815

Date
March 30, 2009
Location
Chandler, AZ
Conditions
VMC
Record
Published September 25, 2020

Primary finding

Probable cause

The certified flight instructor's inadequate supervision of the student pilot during a hover demonstration and his subsequent loss of helicopter control that resulted in a dynamic rollover.

Investigator assessment

Analysis narrative

The purpose of the flight was for the certified flight instructor (CFI) to demonstrate the helicopter to a prospective student who had no prior helicopter flying experience. They had just performed an hour of uneventful flight and decided to practice hover maneuvers over a turf area adjacent to the airport helipad. The CFI briefed the student on the sensitivity of the helicopter controls during a hover and then passed over the controls to the student. The student unsuccessfully attempted to perform a hover and the CFI then regained control. He elected to let the student try to hover again, and as he relinquished control, the helicopter rolled to the left. The CFI attempted to correct the deviation; however, during recovery the low rotor rpm warning horn sounded. He increased the throttle, but the skid made contact with the ground and the helicopter rolled onto its side. The helicopter sustained substantial damage to the rotor system and gearbox during the accident sequence.

Source record

Factual narrative

The purpose of the flight was for the certified flight instructor (CFI) to demonstrate the helicopter to a prospective student who had no prior helicopter flying experience. They had just performed an hour of uneventful flight, and decided to practice hover maneuvers over a turf area adjacent to the airport helipad. The CFI briefed the student on the sensitivity of the helicopter controls during a hover, and then passed over control. The student unsuccessfully attempted to perform a hover, and the CFI then regained control. He elected to let the student try to hover again, and as he relinquished control, the helicopter rolled to the left. The CFI attempted to correct the deviation; however, during recovery the low rotor rpm warning horn sounded. He increased the throttle, but the skid made contact with the ground and the helicopter rolled onto its side. The helicopter sustained substantial damage to the rotor system and gearbox during the accident sequence.

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