N3221J

Substantial
None

CESSNA 150G S/N: 15065921

Accident Details

Date
Friday, December 23, 1994
NTSB Number
ATL95LA030
Location
RHINE, GA
Event ID
20001206X02686
Coordinates
31.979625, -83.200378
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 CYLINDER ROCKER SHAFT BOSSES, WHICH RESULTED IN A LOSS OF ENGINE POWER, AND AN EVENTUAL EMERGENCY LANDING.

Aircraft Information

Registration
N3221J
Make
CESSNA
Serial Number
15065921
Engine Type
Reciprocating
Year Built
1966
Model / ICAO
150G C150
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
3240 CAPITAL CIR SW
Status
Deregistered
City
TALLAHASSEE
State / Zip Code
FL 32310-8723
Country
United States

Analysis

On December 23, 1994, at 1400 eastern standard time, a Cessna 150G, N3221J, collided with a ditch during a forced landing at Rhine, Georgia. The commercial pilot and his passenger were not injured. The aircraft was substantially damaged. The aircraft was operated under the provisions of 14 CFR Part 91 by the pilot. Visual meteorological conditions existed at the time, and no flight plan was filed for the personal flight to Columbia, South Carolina. The flight originated in Tallahassee, Florida, at 1230.

The pilot reported that 90 minutes into the flight, the engine began to vibrate, and the engine rpm dropped to 2,100. He checked the magnetos, carburetor heat, and mixture; everything appeared stable. About three minutes later, the rpm dropped to 1,700, and he prepared for an emergency landing. He landed the airplane on a small agricultural landing strip. He was unable to stop the aircraft in the remaining runway, and the aircraft collided with a ditch.

After the accident, the engine was examined by an inspector from the Federal Aviation Administration. He reported that both rocker shaft bosses of the number two cylinder had failed, and were broken away from the cylinder head. He observed no evidence of fatigue on the fracture surfaces. An examination of the maintenance records revealed that Airworthiness Directive 94-05-05, which requires inspection of the rocker shaft bosses, had been complied with. The reason for the rocker shaft boss failures was not determined.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL95LA030