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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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September 1, 2019 · Hughes 369 D · N54528

Asotin, WA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 1, 2019
Injury Outcomes
No injuries (2 uninjured)
Location
Asotin, WA
Aircraft
Hughes 369 D (1978)
Tail Number
N54528
Injuries
None
Aircraft Damage
Substantial
NTSB Number
WPR19LA249

The pilot of the helicopter reported that he was departing over a river in dark night conditions when, shortly after takeoff, the helicopter yawed severely to the left. He applied full right anti-torque pedal and the helicopter subsequently impacted the water. The helicopter was not examined after the accident, and the reason for the loss of control could not be determined based on the available information.

NTSB Probable Cause

Not determined-Not determined-(general)-(general)-Unknown/Not determined

Full Narrative

On August 31, 2019, about 2217 Pacific daylight time, a Hughes 369D helicopter, N54528, was substantially damaged when it was involved in an accident near Asotin, Washington. The pilot and passenger were not injured. The helicopter was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot reported that he and his passenger departed from a private residence near the Snake River in dark night conditions. The pilot recalled that shortly after lifting off, the helicopter yawed severely to the left. He applied full right anti-torque pedal and the helicopter subsequently impacted the water. He and the passenger egressed the helicopter, which subsequently sank, and were rescued shortly thereafter. The pilot stated that the helicopter had experienced a loss of tail rotor effectiveness, and that the accident was not due to anything he did incorrectly. The mechanic who was repairing the helicopter after the accident reported that the aft tail rotor aft drive flex coupling had sheared. He stated that none of the four tail rotor blades were damaged during the accident sequence. No follow-up examination of the helicopter was performed, and the reason for the loss of control could not be determined.

Flight

Event TypeAccident
Event Time22:17 PDT
Nearest Airport0nm
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHughes 369 D
Tail NumberN54528
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · C-20B · Turboshaft · 420
Seats5

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 42 · First Class · None

Conditions

ConditionsVMC
LightDark Night
WindCalm
CeilingNone
Temperature / Dew Point0 C / 0 C
Altimeter0

Appendix: Source Data