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Aviation safety reports, made easier to study

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NTSB Report

July 10, 2000 · Cessna A188B · N9557G

Washington, KS

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
July 10, 2000
Injury Outcomes
No injuries (1 uninjured)
Location
Washington, KS
Aircraft
Cessna A188B
Tail Number
N9557G
Injuries
None
Aircraft Damage
Substantial
NTSB Number
CHI00LA191

During an aerial application flight the aircraft engine sustained a loss of power and the pilot performed a forced landing to nearby field. During the landing the aircraft sustained substantial damage. Post-accident examination of the engine revealed that the number-two cylinder connecting rod bearing was in several pieces and the connecting rod bolts were broken. The number-two piston was removed from the cylinder and no anomalies were found with the piston or piston-rings. The cylinder wall was inspected and no scoring was noted.

NTSB Probable Cause

the failure of the number-two connecting rod bearing and the unsuitable terrain for landing encountered by the pilot during the forced landing. A factor to the accident was the rough/uneven field.

Full Narrative

On July 10, 2000, at 1100 central daylight time, a Cessna A188B, N9557G, piloted by a commercial pilot, sustained substantial damage during an in-flight collision with terrain while executing a forced landing following a loss of engine power while maneuvering near Washington, Kansas. Visual meteorological conditions prevailed at the time of the accident. The aerial application flight was operating under the provisions of 14 CFR Part 137 and was not on a flight plan. The pilot, the sole occupant, reported no injuries. The flight departed the pilot's private airstrip near Morrowville, Kansas, at 1000, and was conducting aerial application operations at the time of the accident. According to the pilot's written statement, "Upon completing spraying a feild [field], I heard a different sound in the engine[.] I then noticed power loss and oil smoke coming from the engine compartment." The pilot reported, "I truned [turned] to land on a near by road, but was loosing altitude too fast to complete the trun [turn], so I attempted to land across the road in a feild [field]." Post-accident examination of the engine revealed that the number-two cylinder connecting rod bearing was in several pieces and the connecting rod bolts were broken. The number-two piston was removed from the cylinder and no anomalies were found with the piston or piston-rings. The cylinder wall was inspected and no scoring was noted.

Flight

Event TypeAccident
Event Time11:00 CDT
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCessna A188B
Tail NumberN9557G
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 137
Engines1
Engine TypeReciprocating
Engine DetailsContinental · IO-520-D · Reciprocating · 300
Seats1

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 55 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind20° @ 4 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point19 C / 17 C
Altimeter29.00 inHg
Observation Time15:55
Weather SourceWFAC

Appendix: Source Data