N9060W

Substantial
None

Piper PA-28-235S/N: 28-10655

Accident Details

Date
Sunday, March 31, 2002
NTSB Number
CHI02LA106
Location
Fulton, IN
Event ID
20020417X00531
Coordinates
40.950027, -86.259437
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
4
Total Aboard
4

Probable Cause and Findings

A loss of engine power due to excessive clearance of the connecting rod bearing resulting in engine seizure. A related factor was the muddy field.

Aircraft Information

Registration
Make
PIPER
Serial Number
28-10655
Engine Type
Reciprocating
Year Built
1965
Model / ICAO
PA-28-235P28B
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
PA-28-235

Registered Owner (Current)

Name
DOYLE THOMAS M
Address
25 RESERVOIR DR
City
NEW CITY
State / Zip Code
NY 10956-6846
Country
United States

Analysis

On March 31, 2002, at 1655 eastern standard time, a Piper PA-28-235, N9060W, piloted by a private pilot, was substantially damaged during a forced landing near Fulton, Indiana. Visual meteorological conditions prevailed at the time of the accident. The flight was operating under the provisions of 14 CFR Part 91 without a flight plan. The pilot and his three passengers did not report any injuries. The flight departed the Randolph County Airport, Winchester, Indiana, at 1600 and the intended destination was the Gary/Chicago Airport, Gary, Indiana.

According to the pilot's written statement, while in cruise flight the constant speed propeller "surged" twice. The pilot reported, "Checked engine gages and noticed [zero] oil pressure." The pilot stated he was using flight following and requested a vector to the nearest airport, which was Fulton County Airport (RCR). The pilot stated he was unable to reach RCR, turned into the wind, and began to look for a field or road to land on. The pilot reported, "Engine began to 'clatter'. Had already reduced throttle to 1/2 and now reduced to idle." The pilot stated that between 500 and 600 feet above ground level (agl) the engine lost complete power. The pilot reported, "Altitude loss became excessive ([approximately] 1,600 feet per min) Pitched down steeply to recover maneuvering speed. Flew between trees in fencerow and landed in muddy corn field [approximately] 150 [feet] from fencerow. Slid sideways [approximately] 125 feet to stop."

Post-accident investigation of the engine revealed the number 5 connecting rod bearing had excessive clearance.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI02LA106