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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 14, 2008 · Hughes 369FF · N530R

Kekaha, HI

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
May 14, 2008
Injury Outcomes
No injuries (1 uninjured)
Location
Kekaha, HI
Aircraft
Hughes 369FF
Tail Number
N530R
Operator
Smoky Mountain Helicopters
Injuries
None
Aircraft Damage
Substantial
NTSB Number
LAX08LA139

The helicopter pilot reported that he was conducting long-line operations when he heard a loud "popping" sound and moments later the helicopter's engine lost power. The pilot released the long line with its cargo and performed an autorotation to the ground. The helicopter landed hard and the main rotor blades severed the tail boom. Postaccident examination of the helicopter revealed no discrepancies that would have prevented normal engine operation. The engine was removed from the helicopter, placed in an engine test cell, and started. It was taken through a series of timed accelerations and decelerations where it performed to production test standards. The reason for the loss of engine power was not determined.

NTSB Probable Cause

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

Full Narrative

On May 14, 2008, approximately 1140 Hawaiian standard time, a Hughes 369FF, N530R, was substantially damaged during a hard landing following an autorotation to ground subsequent to a loss of engine power near Kekaha, Hawaii. The commercial pilot, the sole occupant on board, was not injured. Inter-Island Helicopters was operating the helicopter under 14 Code of Federal Regulations Part 133. Visual meteorological conditions prevailed for the local, long line operations. The flight originated from a temporary helicopter pad, approximately 20 minutes before the accident. The pilot reported that he was conducting long line operations when he heard a loud "popping" sound, and moments later, the engine lost power. The pilot released the long line with its cargo, and performed an autorotation to the ground. The helicopter landed hard, and the main rotor blades severed the tail boom. Postaccident examination of the helicopter by a Federal Aviation Administration (FAA) inspector and the engine manufacturer revealed no discrepancies that would have prevented normal engine operation. On July 9, 2008, the engine was placed in an engine run test cell at the manufacturer's facility in Indianapolis, Indiana. The engine was started, and taken through a series of timed accelerations and decelerations where it performed to Production Test Standards. The reason for the loss of engine power was not determined.

Flight

Event TypeAccident
Event Time11:40 HST
Nearest Airport0nm
Flight Plan FiledVFR
Flight Plan ActivatedYes
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHughes 369FF
Tail NumberN530R
Aircraft CategoryHeli
DamageSubstantial
OperatorSmoky Mountain Helicopters
Operating RulePart 133
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · 250-C30 · Turboshaft · 425
Seats5

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 32 · Second Class · None

Conditions

ConditionsVMC
LightDaylight
Wind180° @ 8 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point64 F
Altimeter30.02 inHg
Observation Time21:56
Weather SourceWFAC

Appendix: Source Data