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Aviation safety reports, made easier to study

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NTSB Report

February 8, 1989 · Cessna T210L · N81859

Melbourne, FL

Overview

Report Status
Probable Cause
Event Type
Accident
Date
February 8, 1989
Injury Outcomes
1 injury (1 minor injury)
Location
Melbourne, FL
Aircraft
Cessna T210L
Tail Number
N81859
Operator
Stambaugh S Air Service
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
MIA89GA082

THE ACFT WAS BEING FERRIED TO MELBOURNE BY A CONTRACTOR TO THE US MARSHALS SERVICE. BEFORE DEPARTURE INSPECTION AND ENGINE RUN-UP REVEALED A 500-600 RPM MAGNETO DROP; THE LEFT TANK WAS 3/4 FULL AND THE RIGHT TANK HAD APPROX 15 GALLONS OF FUEL, ACCORDING TO GAUGES. THE PLT HAD WORK DONE THAT REDUCED THE MAG DROP TO 200-250 RPM. THE PLT REPORTED THAT WHILE ON A 3-MILE FINAL TO RWY 4 AT MELBOURNE, THE ENGINE QUIT. HE SAID HE SWITCHED THE SELECTOR TO THE OTHER TANK. THE ACFT COLLIDED WITH TREES AND THE GROUND DURING A FORCED LANDING. THE FUEL SELECTOR WAS FOUND IN THE LEFT TANK POSITION. NO FUEL SYSTEM LEAKS WERE EVIDENT. FURTHER EXAMINATION REVEALED 3 OZ OF FUEL IN THE RT TANK; THE LEFT TANK CONTAINED 25 GALLONS BUT APPEARED TO BE 3/4 FULL. THE RT FUEL GAUGE WAS ACCURATE AND THE LEFT READ LOW WHEN TESTED. THE RT MAG DROP WAS 700 RPM DRG A TEST-RUN. THE RT MAG IMPULSE SPRING WAS BROKEN, ALLOWING INTERNAL TIMING TO VARY.

NTSB Probable Cause

FAILURE OF THE PILOT TO ACCURATELY DETERMINE FUEL QUANTITY PRIOR TO DEPARTURE FOLLOWED BY HIS FAILURE TO OPERATE THE ENGINE ON THE FULLEST FUEL TANK RESULTING IN A FUEL TANK BEING RUN DRY RESULTING IN ENGINE FAILURE WHILE ON SHORT FINAL APPROACH AT HIS DESTINATION.

Full Narrative

THE ACFT WAS BEING FERRIED TO MELBOURNE BY A CONTRACTOR TO THE US MARSHALS SERVICE. BEFORE DEPARTURE INSPECTION AND ENGINE RUN-UP REVEALED A 500-600 RPM MAGNETO DROP; THE LEFT TANK WAS 3/4 FULL AND THE RIGHT TANK HAD APPROX 15 GALLONS OF FUEL, ACCORDING TO GAUGES. THE PLT HAD WORK DONE THAT REDUCED THE MAG DROP TO 200-250 RPM. THE PLT REPORTED THAT WHILE ON A 3-MILE FINAL TO RWY 4 AT MELBOURNE, THE ENGINE QUIT. HE SAID HE SWITCHED THE SELECTOR TO THE OTHER TANK. THE ACFT COLLIDED WITH TREES AND THE GROUND DURING A FORCED LANDING. THE FUEL SELECTOR WAS FOUND IN THE LEFT TANK POSITION. NO FUEL SYSTEM LEAKS WERE EVIDENT. FURTHER EXAMINATION REVEALED 3 OZ OF FUEL IN THE RT TANK; THE LEFT TANK CONTAINED 25 GALLONS BUT APPEARED TO BE 3/4 FULL. THE RT FUEL GAUGE WAS ACCURATE AND THE LEFT READ LOW WHEN TESTED. THE RT MAG DROP WAS 700 RPM DRG A TEST-RUN. THE RT MAG IMPULSE SPRING WAS BROKEN, ALLOWING INTERNAL TIMING TO VARY.

Flight

Event TypeAccident
Event Time17:51 EST
Nearest AirportMelbourne Regional (0nm N)
Runway4
Runway Length3002 ft
Runway Width100 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCessna T210L
Tail NumberN81859
Aircraft CategoryAir
DamageSubstantial
OperatorStambaugh S Air Service
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsContinental · TSIO-520-H4A · Reciprocating · 285
Seats6

People & Injuries

Injury Summary1 injury (1 minor injury)
Fatal0
Serious0
Minor1
Uninjured0
Total1
Crew 1Age 55 · First Class

Conditions

ConditionsIMC
LightDaylight
Wind30° @ 10 kt
Visibility6 sm
CeilingBroken clouds 800 ft
Temperature / Dew Point0 C / 0 C
Altimeter30.00 inHg
Observation Time22:50
Weather SourceWFAC

Appendix: Source Data