NTSB CAROL · Event
Event LAX97LA320
Aircraft involved
Probable cause & findings
A hard landing due to the failure of the pilot to adequately compensate for the wind direction and velocity on initiating his approach to the landing area, resulting in a loss of tail rotor authority.
Factual narrative
On September 9, 1997, at 1535 hours Pacific daylight time, a Bell 206B, N90115, experienced a hard landing and substantial damage on a parking area pad at the Minden, Nevada, airport. Upon ground impact, a main rotor blade separated and struck a parked and unoccupied Cessna 182, causing substantial damage. There were minor injuries to the pilot and one of the passengers. The other two passengers were not injured. Visual meteorological conditions existed at the time and no flight plan was on file. The personal flight was terminating at the time. FAA inspectors from the Reno Flight Standards District Office responded to the airport, interviewed the pilot, and inspected the aircraft. At the time of the accident, the winds were 190 to 250 degrees at 15 knots, gusting to 23 knots. As the pilot continued his approach to the landing pad in a northeasterly direction, the helicopter yawed to the right and the pilot applied full left pedal and pulled collective. The pilot later told the inspectors that the engine was running fine, and he had experienced "no unusual noise," and that he had "run out of tail rotor." A review of a relative wind chart provided by Bell Helicopter Textron shows that the helicopter's heading during the approach to the pad placed it in an area of the chart where unanticipated right yaw might occur. The chart is appended to this report. The helicopter landed hard and a main rotor blade separated and struck a parked airplane. At the time of the accident the winds were 190 to 250 degrees at 15 knots, gusting to 23 knots. As the pilot continued his approach to the landing pad in a northeasterly direction, the helicopter yawed to the right and the pilot applied full left pedal and pulled collective. The pilot stated that the engine was running fine, and he had experienced 'no unusual noise,' and that he had 'run out of tail rotor.' Review of a relative wind chart shows the helicopter's heading during the approach to the pad placed it in an area of the chart where unanticipated right yaw might occur. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1997_LAX97LA320.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
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