No fatalities

Helicopter pilot performs emergency landing after collective pitch lock (N2756F)

Chamblee, GA, US

On October 10, 1984, a Bell 206B (registration N2756F) operated by Dooley Helicopter Inc. was involved in an aviation accident near Chamblee, GA. No fatalities were reported. Investigators recorded the probable cause as: The pilot's inability to move the collective pitch lever due to a sudden lockup, despite subsequent mechanical inspection revealing no apparent system failure. 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 2026-06-20Data APIEditorial standards

A helicopter pilot experienced a complete lockup of the collective control during descent, forcing an emergency landing despite remedial attempts and subsequent mechanical inspection.

What happened

During a routine flight operation, the pilot initiated a descent phase when he encountered a sudden and total failure of the aircraft's primary lift control. The collective pitch lever became completely locked in place, rendering it impossible to adjust rotor blade angles regardless of the physical force applied. Despite exerting considerable pressure on the controls, the pilot was unable to move the collective in either an upward or downward direction.

Recognizing the critical nature of the situation, the pilot attempted several remedial actions to restore control authority. These efforts included checking associated systems and trying various mechanical interventions to free the stuck mechanism. None of these attempts were successful. With no further options available to regain normal flight control, the pilot executed an emergency landing. The landing itself was described as uneventful, suggesting that the aircraft touched down without sustaining significant structural damage or causing injury.

The investigation

Following the incident, a thorough mechanical examination of the helicopter was conducted to determine the root cause of the control failure. Investigators performed a complete inspection of the collective hydraulic system, which is typically responsible for transmitting pilot inputs to the rotor mechanism. Despite the severity of the in-flight failure, the post-accident analysis failed to disclose any evidence of a hydraulic leak, pump failure, or mechanical obstruction within the system components.

Findings

The primary finding was the unexplained lockup of the collective control during flight. The pilot's inability to move the lever despite significant force indicates a sudden seizure rather than a gradual degradation. The subsequent lack of findings in the hydraulic system suggests that the failure may have been intermittent, related to a transient mechanical binding, or caused by an issue not evident during the static post-accident inspection. The successful execution of an emergency landing highlights the pilot's ability to manage a critical system failure under pressure.

Safety message

This incident underscores the importance of immediate and decisive action when faced with uncommanded control lockups. Pilots should be prepared to execute emergency procedures swiftly when primary flight controls become unresponsive, as remedial actions may not always restore functionality.

Probable cause

The pilot's inability to move the collective pitch lever due to a sudden lockup, despite subsequent mechanical inspection revealing no apparent system failure.

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Frequently asked questions

What happened in the 10 Oct 1984 Bell 206B accident near Chamblee, GA?

A helicopter pilot experienced a complete lockup of the collective control during descent, forcing an emergency landing despite remedial attempts and subsequent mechanical inspection.

Were there any fatalities in the 10 Oct 1984 Bell 206B accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 10 Oct 1984 involved a Bell 206B, registration N2756F, operated by Dooley Helicopter Inc., at Chamblee, GA.

What was the probable cause of the accident?

The pilot's inability to move the collective pitch lever due to a sudden lockup, despite subsequent mechanical inspection revealing no apparent system failure.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001214X41267. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.