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NTSB investigation record

LAX08CA159

Completed

Robinson R22· N268SH

Date
May 31, 2008
Location
Salt Lake City, UT
Conditions
VMC
Record
Published September 25, 2020

Primary finding

Probable cause

The student's improper use of the anti torque pedals during a practice hover autorotation, which resulted in the helicopter rolling over. Additional causes of the accident were the certificated flight instructor's inadequate supervision of the maneuver and delayed remedial action.

Investigator assessment

Analysis narrative

The student pilot made several approaches and a practice hover autorotation before repositioning the helicopter to a different area of the airport. They planned to perform more hover autorotations and the certified flight instructor (CFI) continued to guard the flight controls. The CFI initiated the hover auto without communication, which was a deviation from their normal procedures. In response to the movement the student depressed the left [improper] anti-torque pedal and the helicopter began to spin. The CFI could not regain control and the helicopter rolled. The CFI reported no pre impact mechanical malfunctions or failures with the helicopter

Source record

Factual narrative

In a written statement, the certificated flight instructor (CFI) reported that the purpose of the flight was to provide the student pilot training. The student pilot made several approaches and a practice hover autorotation before repositioning the helicopter to a different area of the airport. They planned to perform more hover autorotations and the CFI continued to guard the flight controls. The CFI deviated from the normal procedure they had practiced of communicating and counting down before rolling the throttle to the closed position. The CFI initiated the hover auto without communication. In response to the movement the student depressed the left [improper] anti-torque pedal and the helicopter began to spin. The CFI could not regain control and the helicopter rolled. The CFI further stated that the accident could have been prevented if he had briefed the student more thoroughly on the maneuver and if he had assumed authority of the controls earlier in the maneuver. The CFI reported no pre impact mechanical malfunctions or failures with the helicopter

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