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Aviation safety reports, made easier to study

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NTSB Report

May 18, 2002 · Bell 206L-1 · N3894Q

Salem, UT

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
May 18, 2002
Injury Outcomes
3 injuries (1 serious injury, 2 minor injuries)
Location
Salem, UT
Aircraft
Bell 206L-1
Tail Number
N3894Q
Injuries
Serious
Aircraft Damage
Substantial
NTSB Number
DEN02LA044

The helicopter was lifting off from a steel helipad located at the 8,800' msl level when it began turning to the right. The pilot applied left pedal, but the helicopter struck trees and impacted terrain 300 feet from the helipad. The pilot told an FAA inspector he had lost "tail rotor effectiveness." The pilot said there were gusty winds in the area at the time of the accident.

NTSB Probable Cause

a loss of tail rotor effectiveness during takeoff. A contributing factor was the wind gusts.

Full Narrative

On May 18, 2002, at 1449 mountain daylight time, a Bell 206L-1, N3894Q, operated by Classic Helicopters, Inc., of Woods Cross, Utah, was substantially damaged when it collided with trees during takeoff from a mountain top, 3 miles east-southeast of Salem, Utah. The commercial pilot was seriously injured, and two passengers received minor injuries. Visual meteorological conditions prevailed, and no flight plan had been filed for the on-demand, non-scheduled domestic passenger flight being operated under Title 14 CFR Part 135. The flight originated in Bountiful, Utah, approximately 1400 MDT. The helicopter had been chartered by American Telephone and Telegraph (AT&T) to transport personnel to remote repeater antenna sites. It was lifting off from one such site, a steel helipad located on Salem Peak at the 8,800' msl level, when it began turning to the right. The pilot applied left pedal, but the helicopter struck trees and impacted terrain 300 feet from the helipad. The pilot told an FAA inspector he had lost "tail rotor effectiveness." Damage consisted of a severed tail boom, a destroyed main rotor, a broken nose section and Plexiglas, a damaged skid tube, and a punctured fuselage panel. The pilot said there were gusty winds in the area at the time of the accident. This report was modified on May 20, 2005.

Flight

Event TypeAccident
Event Time14:49 MDT
Nearest Airport0nm
Flight Plan FiledCvfr
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell 206L-1
Tail NumberN3894Q
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 135
Engines1
Engine TypeTurboshaft
Engine DetailsRolls-Royce · 250-C28B · Turboshaft · 500
Seats7

People & Injuries

Injury Summary3 injuries (1 serious injury, 2 minor injuries)
Fatal0
Serious1
Minor2
Uninjured0
Total3
Crew 1Age 53 · Second Class · Serious

Conditions

ConditionsVMC
LightDaylight
Wind240° @ 10 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point32 C
Altimeter29.87 inHg
Observation Time21:15
Weather SourceWFAC

Appendix: Source Data