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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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NTSB Report

June 20, 1993 · Bell 206B · N33EA

Harlem, MT

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
June 20, 1993
Injury Outcomes
1 injury (1 minor injury)
Location
Harlem, MT
Aircraft
Bell 206B
Tail Number
N33EA
Operator
Burney Ray E
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
SEA93LA135

THE HELICOPTER WAS FUELED WITH THE LAST 25 GALLONS OF FUEL FROM THE FUEL TRUCK AND THEN DEPARTED ON A SPRAY DISPERSAL FLIGHT. AT APPROXIMATELY 8 FEET AGL AND 60-70 MPH DURING A SWATH RUN, THE ENGINE ABRUPTLY STOPPED AND THE PILOT ATTEMPTED TO EXECUTE A 'QUICK STOP' DURING WHICH THE HELICOPTER COLLIDED WITH TERRAIN. POST CRASH EXAMINATION REVEALED ONLY A SMALL AMOUNT OF WATER IN THE LOW POINT DRAIN FUEL SAMPLE TAKEN FROM THE FUEL TRUCK. A FUEL SAMPLE TAKEN FROM THE PRESSURE SIDE OF THE HELICOPTER'S AIRFRAME FUEL FILTER SYSTEM REVEALED APPROXIMATELY 20 PERCENT WATER. WHEN THE HELICOPTER'S FUEL TANK WAS DEFUELED, THE OWNER RETRIEVED APPROXIMATELY 2.5 GALLONS OF WATER OUT OF A 40 GALLON QUANTITY.

NTSB Probable Cause

THE IMPROPER REFUELING SYSTEM PROCEDURES WHICH ALLOWED WATER TO CONTAMINATE THE AIRCRAFT FUEL AND THE PILOT'S INADEQUATE PREFLIGHT.

Full Narrative

On June 19, 1993, at approximately 2030 hours mountain daylight time (MDT), a Bell 206B, N33EA, registered to Rotorcraft Partnerships Ltd., and being operated/flown by Ray E. Burney, a certificated commercial pilot, was substantially damaged during an in-flight collision with terrain following a complete power loss while beginning a spray run of chemical over an agricultural field approximately 18 miles south of Harlem, Montana. The pilot, who was ejected from the aircraft during the impact, sustained minor injuries. Visual meteorological conditions prevailed and no flight plan had been filed. The flight, which was for the purpose of chemical dispersion over an agricultural field, was to have been operated in accordance with the requirements set forth in 14CFR137, and originated from a staging point near the accident site. Following the accident, the pilot reported to the investigator in charge that the aircraft was fueled using all the remaining fuel (25 gallons) from the on site fuel truck. The helicopter was serviced with herbicide and then departed for its destination spray site one mile distant. As the helicopter descended to approximately six to ten feet above ground at a speed of 60 to 70 miles per hour, the engine ceased operating. The pilot reported that he attempted to execute a "quick stop" but collided with terrain during which he was thrown out of the aircraft. Post crash on site examination of the wreckage as well as the fuel truck and FBO fuel supplier by FAA inspector James Binion revealed the following: 1) The FBO fuel tanks were checked for water and found free of water. 2) The fuel truck was checked taking a sample from the truck's low point drain. Only a small amount of water was evident with the majority being fuel. 3) Approximately 350 milliliters of fluid was removed from the pressure side of the aircraft's airframe fuel filter and system subsequent to the accident. More than 20% of the fluid (75 milliliters) tested positive using water sensitive paste (refer to photographs 1 and 2). Additionally, the aircraft was defueled by its owner subsequent to salvage. A total of 2.5 gallons of water was recovered from the fuel tank out of an approximate total of 40 gallons of fuel (refer to attached letter of Ken Trovato).

Flight

Event TypeAccident
Event Time20:30 MDT
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell 206B
Tail NumberN33EA
Aircraft CategoryHeli
DamageSubstantial
OperatorBurney Ray E
Operating RulePart 137
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · 250-C20B · Turboshaft · 420
Seats5

People & Injuries

Injury Summary1 injury (1 minor injury)
Fatal0
Serious0
Minor1
Uninjured0
Total1
Crew 1Age 59 · Second Class

Conditions

ConditionsVMC
LightDusk
Wind170° @ 4 kt
CeilingNone
Temperature / Dew Point57
Altimeter0
Observation Time02:29
Weather SourceWFAC

Appendix: Source Data