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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

May 20, 1994 · Bell 206A · N206HS

Ukiah, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
May 20, 1994
Injury Outcomes
2 injuries (2 minor injuries)
Location
Ukiah, CA
Aircraft
Bell 206A
Tail Number
N206HS
Operator
Petersen Dane A
Injuries
Minor
Aircraft Damage
Destroyed
NTSB Number
LAX94LA221

The pilot stated that he was on approach to a ridge line landing zone. He said he was passing through translational lift at 20 knots and 70 feet when a gust of wind induced a loss of tail rotor effectiveness and a resultant loss of directional control. The pilot reported that the helicopter began to spin and he could not regain directional control prior to ground contact. After the impact sequence, a ground fire erupted which consumed the helicopter. The helicopter was an early model Bell 206A and was equipped with the small tail rotor.

NTSB Probable Cause

the pilot's inadequate compensation for the existing wind conditions which resulted in a loss of tail rotor effectiveness event and a subsequent loss of directional control.

Full Narrative

On May 20, 1994, at 1530 Pacific daylight time, a Bell 206A helicopter, N206HS, collided with the ground near Ukiah, California, following a loss of control during a landing approach. The helicopter was operated by the pilot and was on a personal flight. Visual meteorological conditions prevailed and no flight plan was filed for the operation. The helicopter was consumed by a postimpact ground fire. The certificated private pilot and the passenger sustained minor injuries. The flight originated from a private helipad near Piercy, California, about 1445 hours on the day of the accident as a personal flight to a private helipad at the accident site. In a telephone conversation, the pilot stated that he was on approach to a ridge line landing zone. He said he was passing through translational lift at 20 knots and 70 feet above ground when a gust of wind induced a loss of tail rotor effectiveness and a resultant loss of directional control. The pilot reported that the helicopter began to spin and he could not regain directional control prior to ground contact. After the impact sequence, a ground fire erupted which consumed the helicopter. The helicopter was an early model Bell 206A and was equipped with the small tail rotor.

Flight

Event TypeAccident
Event Time15:30 PDT
Nearest AirportPrivate Helipad (0nm)
Runway0
Flight Plan FiledNone
Aircraft FireGrd
Aircraft ExplosionNo

Aircraft

AircraftBell 206A
Tail NumberN206HS
Aircraft CategoryHeli
DamageDestroyed
OperatorPetersen Dane A
Operating RulePart 91
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · 250 C18 · Turboshaft · 317
Seats5

People & Injuries

Injury Summary2 injuries (2 minor injuries)
Fatal0
Serious0
Minor2
Uninjured0
Total2
Crew 1Age 45 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind10 kt, gusting 15 kt
Visibility30 sm
CeilingNone
Temperature / Dew Point70 F / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data