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Aviation safety reports, made easier to study

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NTSB Report

May 22, 1997 · Garlick UH-1H · N95NW

Lolo, MT

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
May 22, 1997
Injury Outcomes
No injuries (1 uninjured)
Location
Lolo, MT
Aircraft
Garlick UH-1H
Tail Number
N95NW
Operator
Northwest Helicopters
Injuries
None
Aircraft Damage
Substantial
NTSB Number
SEA97LA119

The pilot reported that his fuel gauge showed 150 lbs of fuel remaining and he decided to move a large stump prior to landing. As he was hovering about 150 feet over the stump waiting for the stump to be hooked up, the helicopter suddenly lost power. He made a tight spiral down to the service landing area, but landed very hard.

NTSB Probable Cause

Fuel exhaustion due to the pilot's failure to refuel.

Full Narrative

On May 22, 1997, approximately 1130 mountain daylight time, N95NW, a Bell UH-1H, sustained substantial damage when it lost power and landed hard near Lolo, Montana. The commercial pilot was not injured. The flight was conducted in visual meteorological conditions with no flight plan filed. The flight had departed the same area about 1010. The pilot reported that the fuel gauge showed 150 pounds and he decided to remove a large stump to the slash pile prior to landing. The stump was situated approximately 40 feet from the service landing area. As he was hovering about 150 feet over the stump waiting for the stump to be hooked up, the helicopter suddenly lost power. He made a tight spiral down to the service landing area, but landed very hard. The operator reported no mechanical malfunctions and listed the engine failure as "fuel exhaustion". An FAA inspector who inspected the wreckage, stated that a total of about 1 and 1/2 gal of fuel was drained from the tanks.

Flight

Event TypeAccident
Event Time11:30 MDT
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftGarlick UH-1H
Tail NumberN95NW
Aircraft CategoryHeli
DamageSubstantial
OperatorNorthwest Helicopters
Operating RulePart 133
Engines1
Engine TypeTurboshaft
Engine DetailsLycoming · T53-L-13B · Turboshaft · 1400
Seats2

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 50 · Third Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
CeilingNone
Temperature / Dew Point70 F / 0 C
Altimeter29.00 inHg
Weather SourcePILO

Appendix: Source Data