LAX04LA261 · Eurocopter France AS350 B2
Eurocopter France AS350 B2 · Accident: loss of control in flight during initial climb
From Grand Canyon West Airport (1G4) to Las Vegas, NV
Event
- NTSB case
- LAX04LA261
- 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
- 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
Eurocopter France AS350 B2
- Aircraft type
- Eurocopter AS350
- 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
- N91MH
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Grand Canyon West Airport (1G4), Peach Springs, AZTo Las Vegas, NV
- 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
- Initial climb
- 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
- Substantial
Cause areas
- Pilot in command › Collective, improper use of
- Pilot in command › Rotor RPM, not maintained
- Pilot in command › Wrong runway, selected
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The helicopter settled to the ground hard while in the initial takeoff sequence from a helipad for a sightseeing tour flight. The pilot reported he was departing toward the southwest. During takeoff, about 20 knots of indicated airspeed, he detected the helicopter was not climbing. He noticed the main rotor rpm was decaying; he attempted to increase the rpm by lowering the collective, which was unsuccessful. As the helicopter started to yaw to the left, the pilot unsuccessfully tried to stop the left yaw by applying right pedal. The low rotor speed warning horn activated prior to the helicopter impacting the ground. Two videotapes were recovered from the helicopter's-on-board video recording system and sent to the Safety Board vehicle recorders division for readout. The video recorder group observed the helicopter takeoff in a downwind condition, as the bushes were observed blowing in the same direction as the takeoff path. The engine was installed in a test cell and operated for over 2 hours, and it was found to meet all normal parameters and engine performance specifications.
Probable cause
The pilot's selection of downwind takeoff direction and improper use of the collective control prior to reaching translational lift, which resulted in a settling with power condition and a collision with the ground. Also causal was the pilot's failure to maintain main rotor rpm.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record LAX04LA261
- Event ID
- 20040714X00976
- Case number
- LAX04LA261
- 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: 62c08ca0f59f0fa8d815785b35b3bc234d8ccf148beec5092903e4ef5cd72457; retrieved 2026-09-18T15:22:19.678Z.