Casualties unknown

2006-03-14: Bell 206L-1 (N370RL) — Patterson, LA

Patterson, LA, US

On March 14, 2006, a Bell 206L-1 (registration N370RL) was involved in an aviation accident near Patterson, LA. Investigators recorded the probable cause as: The improper installation of an engine fuel line fitting by other maintenance personnel, which resulted in a loose fitting and a loss of engine power during cruise flight. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

A helicopter lost engine power during cruise and made a hard forced landing before being engulfed in flames. Investigation found a loose fuel nozzle B nut lacking required lock wire, linked to improper maintenance the previous evening.

Accident Overview

Approximately five minutes after departing on a Part 135 air taxi cross-country flight, the helicopter experienced a loss of engine power while in cruise flight. The commercial pilot executed a forced landing at an off-airport site characterized by tall vegetation and soft terrain. The helicopter came to rest upright, and the two rear-seat passengers egressed unassisted. Moments later, the helicopter was consumed by fire.

Wreckage and Environmental Conditions

The wreckage path was oriented on a magnetic heading of 225 degrees. Wind at the time was reported from 020 degrees at 12 knots.

Engine Examination

On-site examination revealed that the fuel line to fuel nozzle "B" nut could be turned by hand and was not secured with lock wire, as required. All other fittings and nuts on the engine were found to be secure. A subsequent teardown examination of the engine found no preimpact anomalies.

Maintenance History

Review of maintenance records showed that a 50-hour fuel nozzle inspection had been performed the evening prior to the accident flight. This inspection involved removal, disassembly, cleaning, inspection, reassembly, and reinstallation of the fuel nozzle. An interview with maintenance personnel confirmed that the fuel nozzle installation procedures specified in the engine manufacturer's maintenance manual had not been followed.

Operational Testing

Investigators conducted operational tests on an engine of the same make and model to determine the effect of a loose fuel nozzle "B" nut. The tests demonstrated that a loose nut could cause a substantial loss of power, potentially resulting in a flameout. Further testing indicated that conditions would have been conducive to an in-flight fire.

Fire Origin

Investigators could not determine whether the fire originated in flight or during the ground impact.

Conclusion

The loss of engine power was attributed to the loose fuel nozzle "B" nut, which lacked lock wire due to maintenance personnel not following the manufacturer's procedures. The subsequent fire consumed the helicopter.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20060320X00323. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.