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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 21, 1989 · Aerospatiale AS350D · N6003S

Waialae Falls, HI

Overview

Report Status
Probable Cause
Event Type
Accident
Date
May 21, 1989
Injury Outcomes
7 injuries (7 minor injuries)
Location
Waialae Falls, HI
Aircraft
Aerospatiale AS350D
Tail Number
N6003S
Operator
Papillion Helicopters
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
LAX89LA197

THE ON-DEMAND AIR TAXI HELICOPTER WAS ON A LOCAL SIGHTSEEING FLT TO WAIALAE FALLS WITH SIX PAX ABOARD. ELEVATION OF THE FALLS WAS ABOUT 3000 FT. AFTER HOVERING AT LOW ALT NEAR THE FALLS, THE PLT BEGAN A PEDAL TURN & BEGAN FORWARD MOVEMENT FOR THE INITIAL CLIMB AWAY FROM THE FALLS. THE MAIN ROTOR RPM DECAYED & THE PLT TURNED BACK TOWARD THE UPPER FALLS, WHERE HE THOUGHT HE COULD LAND. HOWEVER, THE HELICOPTER SETTLED INTO A RAVINE, IMPACTED ROCKS & CAME TO REST. AN EXAM OF THE ENG FUEL CONTROL REVEALED THE MAXIMUM STOP WAS SET AT 93% VERSUS 99% AS SPECIFIED BY THE MANUFACTURER. ALSO, THE GOVERNOR BREAK WAS SET 400 RPM EARLY, THERE WAS NO SEAL ON THE METERING VALVE SLEEVE & THE SAFETY WIRE THRU THE GOVERNOR ADJUSTMENT HAD BEEN CUT & NOT REPLACED.

NTSB Probable Cause

IMPROPER MAINTENANCE/ADJUSTMENT OF THE ENGINE FUEL CONTROL UNIT BY COMPANY MAINTENANCE PERSONNEL, WHICH RESULTED IN A SLIGHT LOSS OF ENGINE POWER, AND FAILURE OF THE PILOT TO MAINTAIN ROTOR RPM, WHILE TURNING AND TAKING OFF FROM A HOVER WITH A RELATIVELY HEAVY GROSS WEIGHT. FACTORS RELATED TO THE ACCIDENT WERE: THE HIGH DENSITY ALTITUDE AND ROUGH/UNEVEN (ROCKY) TERRAIN IN THE EMERGENCY LANDING AREA.

Full Narrative

THE ON-DEMAND AIR TAXI HELICOPTER WAS ON A LOCAL SIGHTSEEING FLT TO WAIALAE FALLS WITH SIX PAX ABOARD. ELEVATION OF THE FALLS WAS ABOUT 3000 FT. AFTER HOVERING AT LOW ALT NEAR THE FALLS, THE PLT BEGAN A PEDAL TURN & BEGAN FORWARD MOVEMENT FOR THE INITIAL CLIMB AWAY FROM THE FALLS. THE MAIN ROTOR RPM DECAYED & THE PLT TURNED BACK TOWARD THE UPPER FALLS, WHERE HE THOUGHT HE COULD LAND. HOWEVER, THE HELICOPTER SETTLED INTO A RAVINE, IMPACTED ROCKS & CAME TO REST. AN EXAM OF THE ENG FUEL CONTROL REVEALED THE MAXIMUM STOP WAS SET AT 93% VERSUS 99% AS SPECIFIED BY THE MANUFACTURER. ALSO, THE GOVERNOR BREAK WAS SET 400 RPM EARLY, THERE WAS NO SEAL ON THE METERING VALVE SLEEVE & THE SAFETY WIRE THRU THE GOVERNOR ADJUSTMENT HAD BEEN CUT & NOT REPLACED.

Flight

Event TypeAccident
Event Time16:00 HST
Nearest Airport0nm N
Runway0
Flight Plan FiledCvfr
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftAerospatiale AS350D
Tail NumberN6003S
Aircraft CategoryHeli
DamageSubstantial
OperatorPapillion Helicopters
Operating RulePart 135
Engines1
Engine TypeTurboshaft
Engine DetailsLycoming · LTS-101 · Turboshaft · 531
Seats7

People & Injuries

Injury Summary7 injuries (7 minor injuries)
Fatal0
Serious0
Minor7
Uninjured0
Total7
Crew 1Age 37 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind90° @ 5 kt
Visibility15 sm
CeilingNone
Temperature / Dew Point64 F / 55
Altimeter30.00 inHg
Observation Time23:55
Weather SourceWFAC

Appendix: Source Data