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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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April 29, 1982 · Bell 206L · N16959

New York City, NY

Overview

Report Status
Preliminary report
Event Type
Accident
Date
April 29, 1982
Injury Outcomes
No injuries (6 uninjured)
Location
New York City, NY
Aircraft
Bell 206L
Tail Number
N16959
Operator
Island Helicopter
Injuries
None
Aircraft Damage
Substantial
NTSB Number
NYC82FA083

THE FLT DEPARTED THE 34TH STREET HELIPORT ON A LOCAL SIGHTSEEING FLT TO THE STATUE OF LIBERTY & RETURN. AS THE FLT CROSSED LOWER MANHATTAN, ABOUT 1/4 MI FROM THE EAST RIVER, THE PLT HEARD THE LOW RPM AUDIO SIGNAL. HE LOWERED THE COLLECTIVE & ROTOR RPM RETURNED TO THE GREEN. WHILE TURNING TO THE EAST RIVER THE GENERATOR-OUT & ENG-OUT LIGHTS' ILLUMINATED. THE FLOATS WERE INFLATED & THE HELICOPTER CONTACTED THE WATER IN A LEVEL ATTITUDE. THE NOSE THEN CONTACTED THE WATER & THE CHIN BUBBLE BROKE. WATER ENTERED THE HELICOPTER & IT ROLLED RIGHT TO AN INVERTED POSITION. INVESTIGATIONDISCLOSED THAT THE FILTER LINE BETWEEN THE COMPRESSOR SCROLL & THE POWER CONTROL UNIT HAD BROKEN AT THE FILTER END. A VISUAL EXAMINATION OF THE FAILED PC LINE & THE B-NUT FITTING DISCLOSED THAT THE FRACTURE OCCURRED AT THE OUTBOARDEND OF THE FERRUL.

Full Narrative

THE FLT DEPARTED THE 34TH STREET HELIPORT ON A LOCAL SIGHTSEEING FLT TO THE STATUE OF LIBERTY & RETURN. AS THE FLT CROSSED LOWER MANHATTAN, ABOUT 1/4 MI FROM THE EAST RIVER, THE PLT HEARD THE LOW RPM AUDIO SIGNAL. HE LOWERED THE COLLECTIVE & ROTOR RPM RETURNED TO THE GREEN. WHILE TURNING TO THE EAST RIVER THE GENERATOR-OUT & ENG-OUT LIGHTS' ILLUMINATED. THE FLOATS WERE INFLATED & THE HELICOPTER CONTACTED THE WATER IN A LEVEL ATTITUDE. THE NOSE THEN CONTACTED THE WATER & THE CHIN BUBBLE BROKE. WATER ENTERED THE HELICOPTER & IT ROLLED RIGHT TO AN INVERTED POSITION. INVESTIGATIONDISCLOSED THAT THE FILTER LINE BETWEEN THE COMPRESSOR SCROLL & THE POWER CONTROL UNIT HAD BROKEN AT THE FILTER END. A VISUAL EXAMINATION OF THE FAILED PC LINE & THE B-NUT FITTING DISCLOSED THAT THE FRACTURE OCCURRED AT THE OUTBOARDEND OF THE FERRUL.

Flight

Event TypeAccident
Event Time11:45 EDT
Nearest Airport0nm N
Runway0
Runway Length0
Runway Width0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell 206L
Tail NumberN16959
Aircraft CategoryHeli
DamageSubstantial
OperatorIsland Helicopter
Operating RulePart 91
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · 250-C20B · Turboshaft · 420
Seats7

People & Injuries

Injury SummaryNo injuries (6 uninjured)
Fatal0
Serious0
Minor0
Uninjured6
Total6
Crew 1Age 24 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind350° @ 17 kt
Visibility15 sm
CeilingNone
Temperature / Dew Point14 C / 0 C
Altimeter30.00 inHg
Observation Time11:52

Appendix: Source Data