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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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March 29, 1989 · Piper PA-16 · N5368H

Danville, GA

Overview

Report Status
Probable Cause
Event Type
Accident
Date
March 29, 1989
Injury Outcomes
No injuries (1 uninjured)
Location
Danville, GA
Aircraft
Piper PA-16
Tail Number
N5368H
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ATL89LA118

THE PLT REPORTED THAT THE ENGINE BEGAN TO LOSE PWR (RPM) DURING CRUISE AS IF IT WAS EXPERIENCING 'A BAD CASE OF CARB ICE'. THE PLT APPLIED CARB HEAT AFTER THE ENGINE LOST OVER 300 RPM. THE ENGINE CONTINUED TO LOSE PWR AND THE PLT ELECTED TO MAKE A PRECAUTIONARY LDG IN AN OPEN FIELD. THE FIELD WAS UNEVEN, AND THE PLT FOUND THAT HE COULD NOT BRAKE THE AIRPLANE TO A STOP BEFORE COLLIDING WITH A FENCE. TOTAL ELAPSED TIME FROM THE INITIAL PWR LOSS TO LDG WAS ONLY 2 TO 3 MINUTES, ACCORDING TO THE PLT. EXAM OF THE ENGINE REVEALED BLACK, SOOTY DEPOSITS ON THE FIRING ENDS OF THE SPARK PLUGS. ACCORDING TO ICING PROBABILITY CURVES, CONDITIONS WERE FAVORABLE FOR THE FORMATION OF MODERATE ICING AT CRUISE PWR. THE AIRPLANE WAS STC'D TO OPERATE ON AUTOGAS, AND WAS FUELED WITH A MIX OF 100LL AVGAS AND AUTO GAS.

NTSB Probable Cause

THE PILOT DELAYED IN APPLYING CARBURETOR HEAT AFTER THE ENGINE BEGAN TO LOSE POWER, AND HIS SELECTION OF UNSUITABLE TERRAIN FOR A PRECAUTIONARY-LANDING SITE.

Full Narrative

THE PLT REPORTED THAT THE ENGINE BEGAN TO LOSE PWR (RPM) DURING CRUISE AS IF IT WAS EXPERIENCING 'A BAD CASE OF CARB ICE'. THE PLT APPLIED CARB HEAT AFTER THE ENGINE LOST OVER 300 RPM. THE ENGINE CONTINUED TO LOSE PWR AND THE PLT ELECTED TO MAKE A PRECAUTIONARY LDG IN AN OPEN FIELD. THE FIELD WAS UNEVEN, AND THE PLT FOUND THAT HE COULD NOT BRAKE THE AIRPLANE TO A STOP BEFORE COLLIDING WITH A FENCE. TOTAL ELAPSED TIME FROM THE INITIAL PWR LOSS TO LDG WAS ONLY 2 TO 3 MINUTES, ACCORDING TO THE PLT. EXAM OF THE ENGINE REVEALED BLACK, SOOTY DEPOSITS ON THE FIRING ENDS OF THE SPARK PLUGS. ACCORDING TO ICING PROBABILITY CURVES, CONDITIONS WERE FAVORABLE FOR THE FORMATION OF MODERATE ICING AT CRUISE PWR. THE AIRPLANE WAS STC'D TO OPERATE ON AUTOGAS, AND WAS FUELED WITH A MIX OF 100LL AVGAS AND AUTO GAS.

Flight

Event TypeAccident
Event Time10:45 EST
Nearest Airport0nm N
Runway0
Runway Length0
Runway Width0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-16
Tail NumberN5368H
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-235-C1 · Reciprocating · 115
Seats4

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 17 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind140° @ 9 kt
Visibility12 sm
CeilingNone
Temperature / Dew Point63 F
Altimeter30.00 inHg
Observation Time15:52
Weather SourceWFAC

Appendix: Source Data