N1439V

Substantial
None

CESSNA R172K S/N: R1722191

Accident Details

Date
Saturday, August 26, 1995
NTSB Number
BFO95LA089
Location
LISBON, OH
Event ID
20001207X04174
Coordinates
40.770145, -80.760566
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

Loss of oil, where an oil filter adapter had separated from the crankcase cover, due to stripped threads that were caused or allowed by inadequate maintenance or inspection, which resulted in oil exhaustion and subsequent loss of engine power. A factor relating to the accident was: the airplane encountered uneven terrain during a forced landing.

Aircraft Information

Registration
N1439V
Make
CESSNA
Serial Number
R1722191
Engine Type
Reciprocating
Model / ICAO
R172K C172
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
EGGLESTON KEVIN
Address
1605 TOWER DR
Status
Deregistered
City
MOORE
State / Zip Code
OK 73160-6763
Country
United States

Analysis

On August 26, 1995, at 1912 eastern daylight time, a Cessna R172K, N1439V, lost engine power and made a forced landing in an open field at Lisbon, Ohio. The certificated commercial pilot, the sole occupant, was not injured. The airplane sustained substantial damage. Visual meteorological conditions prevailed for the flight, no flight plan was filed. The local flight originated from East Liverpool, Ohio, and was conducted under 14 CFR 91.

The pilot reported that he was operating the airplane over the fairgrounds, towing a banner, when he noted a complete loss of oil pressure. He stated that when he tried to return to the airport, the engine lost power and he made a forced landing in a freshly mown hay field. The pilot reported that the airplane was damaged when it went over a drop off during the forced landing/landing roll.

The airplane was examined after the accident by the Federal Aviation Administration (FAA) Inspector. The examination revealed that the oil filter adapter separated from the boss of the crankcase cover. According to the FAA, about 80% of the threads in the crankcase cover boss were stripped.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# BFO95LA089