N616X

Substantial
None

BELL 47G S/N: 5015

Accident Details

Date
Thursday, September 21, 1995
NTSB Number
ATL95LA171
Location
UNION CITY, TN
Event ID
20001207X04425
Coordinates
36.419681, -89.050346
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

Failure of a #4 connecting rod bolt, which resulted in engine stoppage and a forced landing.

Aircraft Information

Registration
N616X
Make
BELL
Serial Number
5015
Engine Type
Reciprocating
Model / ICAO
47G B47G
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
KENTUCKY WING & ROTOR INC
Address
PO BOX 355
Status
Deregistered
City
WEST PADUCAH
State / Zip Code
KY 42086-0355
Country
United States

Analysis

On September 21, 1995, about 1415 central daylight time, a Bell 47G, N616X, force landed following an in-flight engine vibration, near Union City, Tennessee. The helicopter was operated by the pilot under the provisions of 14 CFR Part 91, and visual flight rules. Visual meteorological conditions prevailed. A flight plan was not filed for the solo, instructional flight. There were no injuries to the private pilot, and the helicopter was substantially damaged. Origination of the flight was Union City, Tennessee, about ten minutes prior to the accident.

The pilot reported that while enroute to his farm, he noticed a vibration in the flight controls and initiated an autorotation. The pilot stated that he touched down in a flat bean field with forward speed. The skids caught on the beans, the helicopter rolled over, caught fire and burned. The pilot held a private pilot certificate with airplane single engine, multi engine, and instrument ratings. He also had a helicopter solo endorsement.

During the ensuing engine teardown, it was noted that the connecting rod from the #4 cylinder was found separated from the crankshaft with the rod cap wedged between the rod and the case. Only 1 connecting rod bolt was located for the #4 cylinder, and it was located in the cap, with the threads stripped from the bolt. The separation of the rod resulted in the fracture of the camshaft, case cracking, and lifter separation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL95LA171