DFW07LA171 · Bell 206L-1
Bell 206L-1 · Accident: loss of control in flight during takeoff
From Marks, MS to Memphis, TN
Event
- NTSB case
- DFW07LA171
- 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
- 0
- 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
- Charter & commuter
- 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 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
- N90AE
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Marks, MSTo Memphis, TN
- 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 135: Air Taxi & Commuter
- 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
- Takeoff
- First occurrenceThe 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
- Pilot in command › Tail rotor effectiveness, encountered
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The commercial pilot reported that he noted that the wind sock atop the hospital was limp prior to starting the engine. He added that the helicopter was parked on a westerly heading when the patient was loaded aboard the helicopter. The pilot added that he brought the helicopter to a hover, prior to executing a right hovering turn to the right for his planned departure in a northerly heading. The pilot further stated that he initiated a vertical takeoff on a northerly heading to clear the obstacles. The pilot added that "after reaching an altitude that allowed the rotor system to be slightly above the trees, the aircraft began a slow turn to the right." The pilot countered with left anti-torque pedal and the torque increased to 101 percent and he "backed-out on the amount of left pedal input." The pilot then attempted to "nurse the aircraft" at the 100 percent torque indication to avoid an engine over-torque condition. The pilot then lowered the collective as he attempted to remain over the helipad and land. The pilot added that the rate of turn to the right decreased some, but was not totally arrested. The helicopter landed hard while on a left yaw on a grassy area approximately 20-feet short of the helipad. The landing gear collapsed and the helicopter came to rest on its left side. The investigation revealed that the helicopter was within weight and balance limits at the time of the mishap. The helicopter was recovered to a secured location for further investigation. The 3,884-hour helicopter pilot reported having accumulated 83 hours in the last 90-days and 21.3 hours within the last 30-days. The pilot reported that he was familiar with the mission and had operated from the same heliport on previous occasions. Flight and engine control continuity was established. No mechanical discrepancies were found with the helicopter or the powerplant.
Probable cause
The loss of control and hard landing as result of the loss of tail rotor effectiveness. A contributing factor was the prevailing dark night conditions.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record DFW07LA171
- Event ID
- 20070731X01064
- Case number
- DFW07LA171
- Dataset
- historical-pre2008
- Source SHA-256
- 89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
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: cf112f275bb788499a3c3e0fed3ccb5933c6d9a9bdc7ee8c5c5e98ac5890b96a; retrieved 2026-09-18T14:42:55.164Z.