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Aviation safety reports, made easier to study

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June 16, 1992 · Beech BE-200 · N32HG

New Castle, DE

Overview

Report Status
Probable Cause
Event Type
Accident
Date
June 16, 1992
Injury Outcomes
4 injuries (4 fatalities)
Location
New Castle, DE
Aircraft
Beech BE-200
Tail Number
N32HG
Operator
Omega Air
Injuries
Fatal
Aircraft Damage
Destroyed
NTSB Number
NYC92FA118

WITNESSES OBSERVED THE AIRPLANE ON A 'NORMAL' FINAL APPROACH, THEN SAW IT DROP 'LOW AND SLOW, RETRACT THE GEAR AND ROLL TO THE LEFT INTO THE TREES.' EXAMINATION OF THE ENGINES REVEALED THAT THE LEFT ENGINE FAILED BECAUSE OF A FATIGUE FAILURE OF A COMPRESSOR TURBINE BLADE. EXAMINATION OF THE RIGHT ENGINE REVEALED NO EVIDENCE OF MALFUNCTION THAT WOULD HAVE PREVENTED THE USE OF FULL POWER. THE AIRCREW WAS EXPERIENCED AND WELL TRAINED. THE RADAR DATA CONFIRMED A DROP IN AIRSPEED JUST BEFORE THE AIRPLANE CONTACTED THE TREES.

NTSB Probable Cause

THE PILOT'S IMPROPER EXECUTION OF AN EMERGENCY PROCEDURE, AFTER AN ENGINE FAILURE, WHICH RESULTED IN A LOSS OF AIRSPEED AND SUBSEQUENT STALL AT AN ALTITUDE TOO LOW FOR RECOVERY. A FACTOR RELATED TO THE ACCIDENT WAS THE FATIGUE FAILURE OF A COMPRESSOR TURBINE BLADE AND THE SUBSEQUENT ENGINE FAILURE.

Full Narrative

WITNESSES OBSERVED THE AIRPLANE ON A 'NORMAL' FINAL APPROACH, THEN SAW IT DROP 'LOW AND SLOW, RETRACT THE GEAR AND ROLL TO THE LEFT INTO THE TREES.' EXAMINATION OF THE ENGINES REVEALED THAT THE LEFT ENGINE FAILED BECAUSE OF A FATIGUE FAILURE OF A COMPRESSOR TURBINE BLADE. EXAMINATION OF THE RIGHT ENGINE REVEALED NO EVIDENCE OF MALFUNCTION THAT WOULD HAVE PREVENTED THE USE OF FULL POWER. THE AIRCREW WAS EXPERIENCED AND WELL TRAINED. THE RADAR DATA CONFIRMED A DROP IN AIRSPEED JUST BEFORE THE AIRPLANE CONTACTED THE TREES.

Flight

Event TypeAccident
Event Time14:47 EDT
Nearest AirportNew Castle County (0nm N)
Runway19
Runway Length7002 ft
Runway Width200 ft
Flight Plan FiledNone
Aircraft FireGrd
Aircraft ExplosionNo

Aircraft

AircraftBeech BE-200
Tail NumberN32HG
Aircraft CategoryAir
DamageDestroyed
OperatorOmega Air
Operating RulePart 91
Engines2
Engine TypeTurboprop
Engine DetailsP&W · PT6A-41 · Turboprop · 850
Seats8

People & Injuries

Injury Summary4 injuries (4 fatalities)
Fatal4
Serious0
Minor0
Uninjured0
Total4
Crew 1Age 57 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind160° @ 10 kt
Visibility15 sm
CeilingNone
Temperature / Dew Point57
Altimeter0
Weather SourcePILO

Appendix: Source Data