N9557G

Substantial
None

Cessna A188B S/N: 18800757

Accident Details

Date
Monday, July 10, 2000
NTSB Number
CHI00LA191
Location
WASHINGTON, KS
Event ID
20001212X21383
Coordinates
39.809440, -97.050010
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

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.

Aircraft Information

Registration
N9557G
Make
CESSNA
Serial Number
18800757
Engine Type
Reciprocating
Model / ICAO
A188B C188
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
PO BOX 108
Status
Deregistered
City
JACKSONVILLE
State / Zip Code
IL 62650
Country
United States

Analysis

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.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI00LA191