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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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September 9, 2002 · Cessna A188B · N4919Q

Dexter, MO

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 9, 2002
Injury Outcomes
No injuries (1 uninjured)
Location
Dexter, MO
Aircraft
Cessna A188B
Tail Number
N4919Q
Operator
Randal Laverne Douglass
Injuries
None
Aircraft Damage
Substantial
NTSB Number
CHI02LA282

The agricultural airplane impacted a cotton field during a forced landing. Examination of the engine revealed that the number two connecting rod was fractured. The fracture surface was consistent with a fatigue fracture. The engine exceed the manufacture's time to be overhauled by 283 hours.

NTSB Probable Cause

The fatigue fracture of the connecting rod, the recommended engine overhaul not performed by the company, and the low altitude flight.

Full Narrative

On September 9, 2002, at 1020 central daylight time, a Cessna A188B, N4919Q, piloted by a commercial pilot, was substantially damaged on impact with terrain. The pilot performed a forced landing while applying pesticide on a cotton field near Dexter, Missouri. Visual meteorological conditions prevailed at the time of the accident. The 14 CFR Part 137 agricultural flight was not operating on a flight plan. The pilot was uninjured. The flight originated from Dexter Municipal Airport, Dexter, Missouri, at 0850. The pilot reported that the engine experienced a total loss of engine power while turning to change course for another pass over the field. The airplane was powered by a Teledyne Continental Motors (TCM) IO-520-D32B, serial number 282977-R, engine. The engine accumulated a total time of 1,983 hours. The manufacturer's recommended time to be overhauled for the engine was 1,700 hours. The engine was removed from the airframe and shipped to TCM, Mobile, Alabama, for a disassembly examination under the supervision of the National Transportation Safety Board. The examination revealed that the number two connecting rod was fractured at the journal area. The fracture surface was noted to have beach marks. The Federal Aviation Administration and TCM were parties to the investigation.

Flight

Event TypeAccident
Event Time10:20 CDT
Nearest Airport0nm
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCessna A188B
Tail NumberN4919Q
Aircraft CategoryAir
DamageSubstantial
OperatorRandal Laverne Douglass
Operating RulePart 137
Engines1
Engine TypeReciprocating
Engine DetailsTeledyne Continental · IO-520-D32B · Reciprocating · 300
Seats1

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 29 · Second Class · None

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility8 sm
CeilingNone
Temperature / Dew Point70 F
Altimeter30.13 inHg
Observation Time14:55
Weather SourceWFAC

Appendix: Source Data