BRANTLY B-2B near Weaverville, CA — 2011-05-27
- Date
- 2011-05-27
- Location
- Weaverville, CA, USA
- Airport
- O54
- Aircraft
- BRANTLY B-2B
- Registration
- N222DW
- Category
- Helicopter
- Highest injury
- Fatal
- Fatalities
- 1
- Phase of flight
- Climb
Probable cause
The student pilot's decision to fly in windy conditions that exceeded his capabilities, which resulted in his subsequent loss of helicopter control. Contributing to the accident was his lack of flight experience in the accident helicopter.
Contributing factors
Contributing to the accident was his lack of flight experience in the accident helicopter.
NTSB narrative
The student pilot’s solo flight endorsement prohibited flight in gusty wind conditions such as those existing at the time of departure along his route of flight and at his planned destination. Additionally, his route of flight would have been over mountainous terrain, which would have further exacerbated the conditions and resulted in updrafts, downdrafts, and turbulence at his flight altitude. A witness, who was located close to the accident site, reported unusually strong wind for the area at the time of the accident. The pilot did not request a weather briefing prior to the flight. The wreckage distribution was consistent with a level impact with trees in the direction of flight. No indications of an in-flight breakup, bird strike, or fire were present, and damage to the main rotor system was consistent with it operating at a high level of rotational energy. The throttle was noted in the closed position, consistent with an autorotation event; however, it is possible the pilot may have closed the throttle just prior to, or during, the impact sequence. The student pilot had received about 120 hours of helicopter flight training over the 3 1/2-year period prior to the accident. (The pilot's flight logbook had been defaced, thus an accurate assessment of his total flight experience was not possible.) During that time, he had used the services of about nine flight instructors, with only the last instructor endorsing him for solo flight about 2 weeks before the accident. The accident flight was most likely his second solo flight in the accident helicopter. Acquaintances and previous instructors recounted that the pilot often exhibited poor decision-making traits, was headstrong, stubborn, and overconfident. Although the pilot performed maintenance and unapproved modifications to the helicopter, the modifications did not appear to have been causal to the accident, and a postaccident examination did not reveal any anomalies with the airframe or engine that would have precluded normal operation.
Analysis
- Primary failure mode
- Human factors
- First missed decision gate
- Pilot should have canceled flight due to strong winds and lack of experience.
NTSB coding
Evidence available
- Photos
- 23 docket documents
Docket documents23
- Evidence Control Formform
- Witness Statementsinterview
- Airframe and Engine Logbook Excerptsother
- Pilot Logbook Excerptsother
- Surface Windsother
- Image 1 - Accident Location Relative to Departure and Arrival Airportsphotos
- Photo 1 – Helicopter During Takeoff of Accident Flight – Provided by Jim Waltersphotos
- Photo 10 – Fuel Servo Venturi Contaminationphotos
- Photo 11 – Left Side of Fuselagephotos
- Photo 12 – Gascolatorphotos
- Photo 13 – Low Fuel Warning Bulbphotos
- Photo 14 – Grease Contamination of Venturi Slotsphotos
- Photo 2 – Helicopter at Accident Sitephotos
- Photo 3 - Helicopter at Accident Sitephotos
- Photo 4 – Main Rotor Blade Remnantsphotos
- Photo 5 – Modified Collective Friction Lockphotos
- Photo 6 - Combination Oil Pressure, Fuel Quantity, and Engine Temperature Gaugephotos
- Photo 7 – Rotor Headphotos
- Photo 8 – Enginephotos
- Photo 9 – Top Spark Plugsphotos
- Airframe and Engine Examination Reportreport
- Fuel Servo Examination Reportreport
- Toxicological Reportreport
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