ERA24LA242 · Hughes 269A

The student pilot was working on adding a helicopter rating to his existing private pilot certificate and was on a solo flight to practice some landing approaches at a nearby airport. After completing the practice approaches and refueling the helicopter, the pilot flew back to his property. The pilot reported that when he entered a hover to land, the helicopter started to turn to the right “very fast.” The pilot applied full force to the left anti-torque pedal, but the helicopter continued to turn to the right. The helicopter then impacted trees and terrain. A postimpact fire consumed most of the helicopter. The weather reported at an airport about 17 nautical miles from the accident site included wind at 7 knots, with gusts to 22 knots. The pilot’s solo endorsement limited him to flights in wind conditions less than 13 knots. Following the accident, the pilot reported that he did not believe that there had been a mechanical malfunction or failure that would have prevented normal operation of the helicopter and that a wind gust had “caught” him, which resulted in the loss of control. The wreckage was examined by a Federal Aviation Administration inspector at the accident site. While the examination was limited given the extent of the fire damage, the inspector did not observe any anomalies with the helicopter’s anti-torque system that would have precluded normal operation.

Verbatim NTSB analysis and probable cause from the NTSB dataset