N77068

Substantial
None

CESSNA 120S/N: 11522

Accident Details

Date
Friday, September 19, 2008
NTSB Number
MIA08LA196
Location
Jesup, GA
Event ID
20081007X11157
Coordinates
31.553888, -81.882499
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

An oil starvation-induced catastrophic engine failure due to the improper installation of the crankshaft expansion plug during engine overhaul.

Aircraft Information

Registration
N77068
Make
CESSNA
Serial Number
11522
Engine Type
Reciprocating
Year Built
1946
Model / ICAO
120C120
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
WARREN VIRGIL P III
Address
261 PIERCE AVE
Status
Deregistered
City
MACON
State / Zip Code
GA 31204-2419
Country
United States

Analysis

On September 19, 2008, at 1100 eastern daylight time, a Cessna 120, N77068, incurred substantial damage during a force landing in an open field near Jesup, Georgia. Visual meteorological conditions prevailed and a flight plan was filed for the Title 14 Code of Federal Regulations Part 91, personal flight. The pilot and the passenger were not injured.

The pilot stated that he planned a flight from the Macon Downtown Airport, Macon, Georgia to the Jekyll Island Airport, Jekyll Island, Georgia. They departed at about 0945. The flight went uneventful for the first hour of the estimated 2 hour flight. About an hour and twenty minutes into the flight, an opaque film began to accumulate on the windshield. Engine oil was leaking from the forward right engine cowling area. Within a minute, forward visibility was severely restricted and he had to rely on the instruments for level flight while referring out the side window for visual reference. There were no abnormal indications from the engine instrumentations. The nearest airport was too far away and the pilot elected to land in a clear field within gliding distance. The pilot approached the open field in a slip; the windshield was covered with oil. He lost visual reference as he recovered from the slip to land; estimating the flare for the touchdown. The airplane landed hard and bounced, which separated the right wheel assembly from the gear. The airplane’s right gear dug in on the second contact with the ground, resulting in the airplane coming to an abrupt stop in a nose low and tail high position. The pilot and passenger removed their four point restraint system and exited the airplane on their own.

A wreckage examination a Federal Aviation Administration inspector revealed the engine oil was leaking from the front section of the engine crankcase, behind the propeller flange. Upon removal of the propeller and spinner, the forward crankshaft expansion plug was observed dislodged from it seating, allowing pressurized oil to escape from the forward end of the crankshaft. The pilot/owner stated the airplane’s engine was overhauled 39 flight hours prior to the accident.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA08LA196