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ATL05CA003 · Bell 206 B

14 Oct 2004 · Eutaw, AL, United States

Bell 206 B · Accident: loss of engine power while maneuvering

From Eutaw, AL to an unrecorded destination

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Event

NTSB case
ATL05CA003
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
General aviation
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

Bell 206 B

Aircraft type
Bell 206
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
N300HT
Operator
Unknown
Onboard fatalities
Unknown
Route
From Eutaw, ALTo not recorded
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 137: Agricultural
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
Maneuvering · aerial application
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 engine power
Also codedOther events the NTSB coded in the sequence, such as a wire strike after a loss of power. Flight Findings uses them for its kinds of event. Glossary
Fuel exhaustion; Tree(s)
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

  • Fluid, fuel › Exhaustion

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 was conducting a spraying operation in a wooded area in Eutaw, Alabama. The helicopter was refueling for 10-15 minute flights. After the helicopter refueled it departed the staging area, and did not return after 20 minutes. An aerial and ground search was initiated, and the downed helicopter was located approximately three hours after the initial search. Fueling records are not documented by the operator. The pilot did not report any mechanical malfunctions with the helicopter prior to the accident. Examination of the accident site revealed the helicopter lying on its left side. Further examination of the helicopter revealed that the main rotor blades were broken off of the main rotor head, and the fuselage was buckled. During the preparation for a functional check of the engine, fuel was poured into the main fuel tank. After pouring about one gallon fuel into the main tank, an undetermined small amount of jet fuel leaked out of the bottom of the fuel tank. An external source of jet fuel was attached to the engine fuel system and the engine was started and, a functional engine run was accomplished up to 65% power for five minutes. Both the oil and engine temperature instruments were in the normal operating range during the engine run. No mechanical anomalies were found during the engine run.

Probable cause

The pilots inadequate preflight planning of fuel required for the flight that resulted in fuel exhaustion and the subsequent loss of engine power.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record ATL05CA003
Event ID
20041116X01824
Case number
ATL05CA003
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: 82b196ca48922443f7c1e71a14785a9578347efc2526d2ae5934a9a44d065354; retrieved 2026-09-21T19:07:15.662Z.