BELL 206 - B near Mammoth Lakes, CA — 2012-09-19
- Date
- 2012-09-19
- Location
- Mammoth Lakes, CA, USA
- Aircraft
- BELL 206 - B
- Registration
- N222GR
- Category
- Helicopter
- Highest injury
- None
- Fatalities
- 0
- Phase of flight
- Climb
Probable cause
The pilot’s inability to maintain sufficient main rotor rpm while maneuvering in high density altitude conditions, which resulted in a precautionary landing and subsequent rollover.
NTSB narrative
While performing an aerial survey of transmission structures and wires in mountainous terrain at an elevation of about 7,500 feet mean sea level, the pilot initiated a climb to clear a ridge ahead. When he realized that there was no response to an increase in collective, and, with the torque nearing 100 percent, he chose to maneuver the helicopter left of a set of wires, avoid approaching terrain, and establish an approach for a precautionary landing to a dirt road. The pilot reported that, during the approach, he was unable to arrest the helicopter's descent, and, at the same time, he heard a noise that he assumed was the low rotor rpm warning. The helicopter subsequently impacted terrain just short of the road, rolled over on its left side, and was consumed by the postcrash fire. A postaccident examination of the airframe and engine revealed no mechanical anomalies that would have precluded normal operation. At the time of the accident, the nearest weather reporting facility, which was located 10.5 miles west of the accident site, reported wind at 4 knots, gusting to 14 knots, and a temperature of 24 degrees C. The calculated density altitude for the conditions was about 9,742 feet, which would have affected the helicopter's climb performance.
Analysis
- Primary failure mode
- Engine power loss
- First missed decision gate
- Pilot could have considered density altitude in preflight planning.
NTSB coding
Evidence available
- Photos
- 15 docket documents
Docket documents15
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- Release of Aircraft Wreckage, NTSB Form 6120.15form
- FAA inspector's interview with pilot-in-commandinterview
- Statement of Party Representatives to NTSB Investigationinterview
- Witness statementsinterview
- Excerpts from maintenance recordsother
- Weather Dataother
- Photo 1 - view #1 of accident sitephotos
- Photo 2 - view #2 of accident sitephotos
- Photo 3 - view #3 of accident sitephotos
- Photo 4 - view #4 of accident sitephotos
- FAA inspector's report of initial engine examinationreport
- Rolls-Royce engine investigation reportreport
- Standard Aero Investigation Trip Reportreport
- Standard Aero permission to use Investigation Trip Reportreport
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