CEN13LA310 · Bell Helicopter Textron 206L-1
Corporate Aircraft Services Bell Helicopter Textron 206L-1 · Accident: loss of tail rotor effectiveness while maneuvering
From La Junta, CO to La Junta, CO
Event
- NTSB case
- CEN13LA310
- Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
- Accident
- InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
- Completed
- API-reported fatalities
- 0 · all aircraft and ground
- Ground fatalities
- Unknown
- OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
- General aviation
- WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
- Visual Meteorological Cond
Bell Helicopter Textron 206L-1
- Aircraft type
- Bell 206
- Category
- Helicopter
- RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
- N20Z
- Operator
- Corporate Aircraft Services
- Onboard fatalities
- Unknown
- Route
- From La Junta, COTo La Junta, CO
- Aircraft age
- Not recorded
- Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
- Part 91: General Aviation
- Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
- Maneuvering
- Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
- Loss of tail rotor effectiveness
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Substantial
Cause areas
- Aircraft › Aircraft oper/perf/capability
- Environmental issues › Conditions/weather/phenomena
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The purpose of the flight was to videotape a pipeline corridor. The commercial pilot reported that, while flying over mainly flat rural areas, the helicopter entered an uncommanded left yaw, returned to straight flight for about 1 to 2 seconds, and then entered an uncommanded right yaw that continued until the helicopter impacted the ground. GPS data from the camera used to videotape the pipeline corridor indicated that the helicopter's groundspeed was about 37 knots when it entered the uncommanded left yaw. Weather information from an airport about 5 miles away from the accident site indicated that the helicopter was flying with a tailwind of 11 knots gusting to 16 knots, which resulted in a calculated airspeed of between 22 and 26 knots.
A postaccident examination of the airframe, engine, and control system revealed no evidence of mechanical malfunctions or failures that would have precluded normal operation. The helicopter was operating in a high-power, low-airspeed condition that required the pilot to be especially aware of wind direction to avoid tailwinds, which can result in a loss of control due to a loss of tail rotor effectiveness. Based on the available information, it is likely that the pilot's operation of the helicopter at a low airspeed with a gusting tailwind resulted in the loss of tail rotor effectiveness.
Probable cause
The pilot's inadequate compensation for wind during low-altitude operations, which resulted in a loss of tail rotor effectiveness.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record CEN13LA310
- Event ID
- 20130531X43006
- Case number
- CEN13LA310
- Dataset
- full-current
- Source SHA-256
- 5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
- Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
- Filled from the NTSB case API where the bulk record had no value: investigation status, coordinates. Values present in the bulk record are kept.
- The date is the local date, which is the same as the UTC date the NTSB stores.
- API snapshot SHA-256: 22ec04b7f6b70f8e3578a56628adab7c307db8a5e638d9bbb3a4413216c15624; retrieved 2026-09-15T21:44:06.832Z.