CEN09FA012 · Bell 206 L-4
Helicopters Bell 206 L-4 · Accident: loss of control in flight while maneuvering
From William P. Hobby Airport (HOU) to William P. Hobby Airport (HOU)
Event
- NTSB case
- CEN09FA012
- 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
- 2 · 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 206 L-4
- 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
- N6ZV
- Operator
- Helicopters
- Onboard fatalities
- Unknown
- Route
- From William P. Hobby Airport (HOU), Houston, TXTo William P. Hobby Airport (HOU), Houston, TX
- 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 control in flight
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Destroyed
Cause areas
- Aircraft › Aircraft oper/perf/capability
- Not determined › Not determined
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
**This report was modified on June 28, 2010, and May 11, 2015. Please see the public docket for this accident to view the original report.**
The news helicopter was en route to cover a breaking news story. Witnesses saw the helicopter flying approximately 350 feet above the ground when it nosed over and entered a sharp 70-degree bank and dove towards the ground. The helicopter was equipped with a video camera. Analysis of the video revealed a "small perturbation in yaw (nose towards the left) followed by a return back to the right of equal magnitude." The perturbation was "no larger or faster" than other yaw motions seen previously during the flight. About two seconds later, the helicopter began a slow, smooth roll to the right and the ground was no longer visible. The helicopter came down through trees at a 72-degree impact angle. The right skid was embedded in the ground at a 25-degree angle. Both main rotor blades bore evidence of tree strikes. The clevis ends of the pitch change tubes remained attached to their respective horns. The pitch and collective control rods remained attached to their linkages, and the linkages were attached to their respective servos. Flight control continuity was established between the control rods and the servos but could not be established beyond the servos because of impact forces and a postcrash fire. One tail rotor blade was straight and the other blade was bent 90 degrees to the plane of rotation. There was no evidence of a main rotor blade strike against the horizontal stabilizer, synchronized elevator, or finlets or tail boom. Tail rotor continuity was established. Examination of the engine revealed the Pg line was only finger tight. Later pressure testing of the Pg line disclosed no leaks. The transmission, main drive shaft, and freewheeling unit were disassembled and inspected. No anomalies were noted.
The autopsy of the pilot identified areas of moderate to severe (up to 85 to 90 percent) occlusion of the coronary arteries and a small area of scar in the cardiac muscle, but the significance of these findings to the accident could not be conclusively determined. Although it is clear that the pilot had significant coronary disease, which placed him at risk for an acute coronary event, there is no way to determine, on the basis of the available evidence, whether the pilot actually suffered such an event during the accident flight.
The observations from witnesses, analysis of the wreckage and impact evidence, and test results indicated a loss of control occurred. However, the investigation could not determine the reason for the loss of control.
Probable cause
A loss of control for undetermined reasons.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record CEN09FA012
- Event ID
- 20081013X24743
- Case number
- CEN09FA012
- 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. 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: 2544b5854e313c02705a1a51a3da814cd7713a2c684aceb97de8b7d16894140d; retrieved 2026-09-13T19:33:15.790Z.