Casualties unknown

Hard Landing and Rollover During Practice Autorotation (N305FD)

Lancaster, CA, US

On June 23, 2004, a Bell 206B (registration N305FD) was involved in an aviation accident near Lancaster, CA. Investigators recorded the probable cause as: The pilot's misjudged autorotative flare and the flight instructor's delayed remedial action and inadequate supervision of the flight. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-07-04Data APIEditorial standards

A helicopter conducting a practice 180-degree autorotation landed hard, bounced, and rolled onto its right side. The pilot reported insufficient engine power to recover. Engine teardown found no anomalies; fuel control and governor tested within specifications.

Accident Details

During a practice 180-degree autorotation, a helicopter landed hard, bounced, spun around, struck the ground again, and rolled over onto its right side. The accident occurred in the context of routine training maneuvers.

Pilot Statements

The pilot-undergoing-instruction (PUI) reported that after rolling out onto final approach at 400 feet AGL, he leveled the helicopter, rolled in throttle, and initiated a flare at about 70 feet AGL. At approximately 50 feet AGL, he leveled the flare because the helicopter "did not feel like it was building energy" and the flare seemed less effective. Rotor rpm was at 100 percent. The PUI stated there appeared to be insufficient engine power to recover, so he leveled the aircraft and raised the collective. The low rotor horn sounded shortly thereafter.

Procedures

The Los Angeles City Fire Department "flare autorotations" procedure describes that at approximately 75 feet, the pilot should begin a smooth cyclic flare, leveling the ship with quick but smooth cyclic movement, with expected altitude loss but leveling by 10 feet.

Engine and Fuel Control Tests

An engine teardown was conducted with no anomalies found. The fuel control and governor were bench tested and performed to specifications.

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Frequently asked questions

What happened in the 23 Jun 2004 Bell 206B accident near Lancaster, CA?

A helicopter conducting a practice 180-degree autorotation landed hard, bounced, and rolled onto its right side. The pilot reported insufficient engine power to recover. Engine teardown found no anomalies; fuel control and governor tested within specifications.

What aircraft was involved and where did it happen?

The accident on 23 Jun 2004 involved a Bell 206B, registration N305FD, at Lancaster, CA.

What was the probable cause of the accident?

The pilot's misjudged autorotative flare and the flight instructor's delayed remedial action and inadequate supervision of the flight.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20040712X00950. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.