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July 16, 1999 · Bell OH-58A · N9254R

Bastrop, LA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
July 16, 1999
Injury Outcomes
No injuries (1 uninjured)
Location
Bastrop, LA
Aircraft
Bell OH-58A
Tail Number
N9254R
Injuries
None
Aircraft Damage
Substantial
NTSB Number
FTW99LA191

The helicopter experienced a total loss of engine power due to a contaminated fuel system. Days prior to the accident flight, the refueling truck had been contaminated with water, and the accident helicopter had been filled with the contaminated fuel. The pilot and ground crew became aware of the situation and sumped both the truck and the helicopter. The pilot thought that the helicopter's fuel system was free of the contaminated fuel. During the accident flight, the engine lost power, the pilot initiated an autorotation, and the helicopter impacted pine trees. The FAA inspector observed water and algae in the helicopter's fuel filters. The operator stated that the refueling truck's water filter failed to separate the water from the fuel during the fueling operations. After the accident, the operator installed water/fuel separators in all the refueling trucks in addition to the filters that were already in place as an extra measure of safety.

NTSB Probable Cause

The failure of the refueling truck's filter to separate water resulting in the water contamination in the helicopter's fuel system and subsequent loss of engine power. A factor was the lack of suitable terrain for the forced landing.

Full Narrative

On July 16, 1999, approximately 0834 central daylight time, a Bell OH-58A helicopter, N9254R, was substantially damaged when it impacted terrain during a forced landing following a total loss of engine power near Bastrop, Louisiana. The instrument-rated commercial pilot, sole occupant of the helicopter, was not injured. The helicopter was registered to and operated by North Star Helicopters Inc., of Jasper, Texas. Visual meteorological conditions prevailed for the 14 Code of Federal Regulations Part 137 aerial application flight and no flight plan was filed. The local flight originated from a private staging area near Bastrop, Louisiana. According to the pilot, he had completed his 30th application of arsenal, a chemical used for aerial application flights, and was returning to the staging area. The helicopter was flying at 150 feet agl when the engine power "gradually decreased," and the engine lost total power. The pilot stated that the "ENGINE OUT" warning light illuminated. He initiated an autorotation, during which the helicopter contacted pine trees that were approximately 20 feet tall. The helicopter came to rest on its left side in the pine trees. The tail boom, the left skid, and the main rotor blades were damaged. The FAA inspector, who visited the accident site, reported that the helicopter's fuel system was contaminated with water and algae. He stated that water and algae were found in the helicopter's fuel filters. According to the operator, the refueling truck had been contaminated with water a few days prior to the accident. The accident helicopter was fueled from the contaminated truck. The ground crew and pilot became aware of the situation and sumped the helicopter's fuel tanks and the refueling truck. The pilot thought he had sumped all of the water out of the helicopter's fuel tanks. The pilot took the helicopter on the first flight since the discovery of contamination and experienced the ensuing engine failure. The operator stated that the filter on the refueling truck had failed to separate the water from the fuel during the fueling operations. The operator reported that all of its refueling trucks have since been modified with additional water/fuel separators as an extra measure of safety.

Flight

Event TypeAccident
Event Time08:34 CDT
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell OH-58A
Tail NumberN9254R
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 137
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · C-20B-T63 · Turboshaft · 420
Seats2

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 41 · Second Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility6 sm
CeilingNone
Altimeter30.00 inHg
Observation Time14:53
Weather SourceWFAC

Appendix: Source Data