Casualties unknown

2004-10-14: Bell 206 B (N300HT) — Eutaw, AL

Eutaw, AL, US

On October 14, 2004, a Bell 206 B (registration N300HT) was involved in an aviation accident near Eutaw, AL. Investigators recorded the probable cause as: The pilots inadequate preflight planning of fuel required for the flight that resulted in fuel exhaustion and the subsequent loss of engine power. 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 1781061362Data APIEditorial standards

A helicopter conducting spraying operations in Eutaw, Alabama, crashed after a refueling stop. The aircraft was found on its left side with broken main rotor blades and buckled fuselage. Post-accident engine tests revealed no mechanical anomalies, though a small fuel leak was noted.

Accident Overview

A helicopter engaged in aerial spraying operations in a wooded area near Eutaw, Alabama, failed to return from a flight following a refueling stop. The helicopter had been conducting short-duration missions of 10 to 15 minutes. After refueling, the aircraft departed the staging area but did not return within 20 minutes, prompting an aerial and ground search. The downed helicopter was located approximately three hours after the search began.

Examination of the Accident Site

At the accident site, the helicopter was observed lying on its left side. Examination revealed that the main rotor blades had been broken off from the main rotor head, and the fuselage exhibited buckling. The pilot had not reported any mechanical malfunctions with the helicopter prior to the accident.

Post-Accident Engine Functional Check

During preparations for a functional check of the engine, fuel was poured into the main fuel tank. After adding approximately one gallon of jet fuel, an undetermined small amount of fuel leaked from the bottom of the tank. An external source of jet fuel was then connected to the engine fuel system. The engine was started and operated for five minutes at up to 65% power. Both oil and engine temperature instruments remained within normal operating ranges throughout the run. No mechanical anomalies were identified during the engine test.

Additional Information

The operator did not document fueling records. The accident investigation did not determine a specific cause for the crash.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20041116X01824. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.