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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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June 4, 1982 · Beech 65-90 · N190BT

Wichita, KS

Overview

Report Status
Preliminary report
Event Type
Accident
Date
June 4, 1982
Injury Outcomes
No injuries (3 uninjured)
Location
Wichita, KS
Aircraft
Beech 65-90
Tail Number
N190BT
Operator
Midwest Piper Flight
Injuries
None
Aircraft Damage
Substantial
NTSB Number
MKC82FA095

THE PLT DETECTED A LOSS OF ENG TORQUE AT ABOUT ROTATION AIRSPEED ABOUT 1700 FT DOWN THE RWY & THE TAKEOFF WAS ABORTED. THE ACFT SLID INTO A DITCH OFF THE END OF THE RWY COLLAPSING THE MAIN GEAR. A FUNCTIONAL CHECK OF THE RIGHT ENG FUEL PUMP, P/N4V146R002, SER.#JX241439D, MANUFACTURED BY SPERRY VICKERS SHOWED THAT AT HIGH PUMP SPEED FUEL FLOW WAS INTERMITTENT. DISASSEMBLY OF THE PUMP REVEALED THAT THE ROTOR DRIVE SERRATIONS ON THE MAIN ROTOR DRIVE SHAFT, P/N330205,WERE WORN TO THE POINT THAT THE ROTOR WOULD SLIP ON THE SHAFT AT HIGH PUMP SPEEDS.

Full Narrative

THE PLT DETECTED A LOSS OF ENG TORQUE AT ABOUT ROTATION AIRSPEED ABOUT 1700 FT DOWN THE RWY & THE TAKEOFF WAS ABORTED. THE ACFT SLID INTO A DITCH OFF THE END OF THE RWY COLLAPSING THE MAIN GEAR. A FUNCTIONAL CHECK OF THE RIGHT ENG FUEL PUMP, P/N4V146R002, SER.#JX241439D, MANUFACTURED BY SPERRY VICKERS SHOWED THAT AT HIGH PUMP SPEED FUEL FLOW WAS INTERMITTENT. DISASSEMBLY OF THE PUMP REVEALED THAT THE ROTOR DRIVE SERRATIONS ON THE MAIN ROTOR DRIVE SHAFT, P/N330205,WERE WORN TO THE POINT THAT THE ROTOR WOULD SLIP ON THE SHAFT AT HIGH PUMP SPEEDS.

Flight

Event TypeAccident
Event Time17:46 CDT
Nearest AirportColonel James Jabara (0nm N)
Runway36
Runway Length2800 ft
Runway Width40 ft
Flight Plan FiledIFR
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBeech 65-90
Tail NumberN190BT
Aircraft CategoryAir
DamageSubstantial
OperatorMidwest Piper Flight
Operating RulePart 135
Engines2
Engine TypeTurboprop
Engine DetailsP&W · PT-6A-6 · Turboprop · 500
Seats3

People & Injuries

Injury SummaryNo injuries (3 uninjured)
Fatal0
Serious0
Minor0
Uninjured3
Total3
Crew 1Age 25 · First Class

Conditions

ConditionsVMC
LightDaylight
Wind90° @ 5 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point15 C / 0 C
Altimeter30.00 inHg

Appendix: Source Data