N61946

Substantial
None

CESSNA 180K S/N: 18052815

Accident Details

Date
Thursday, October 7, 1993
NTSB Number
SEA94LA016
Location
GARFIELD, WA
Event ID
20001211X13666
Coordinates
46.990985, -117.160049
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

CONNECTING ROD BOLT FATIGUE.

Aircraft Information

Registration
Make
CESSNA
Serial Number
18052815
Engine Type
Reciprocating
Year Built
1977
Model / ICAO
180K C180
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
180K

Registered Owner (Current)

Name
STRAIGHT AND LEVEL AEROMEDICAL LLC
Address
451 PARKHILL DR
City
BILLINGS
State / Zip Code
MT 59101-0662
Country
United States

Analysis

On October 7, 1993, at 1200 Pacific daylight time, a Cessna 180K, N61946, lost engine power during cruise flight. The pilot initiated a forced landing to an open area near Garfield, Washington. During the ground roll, the airplane collided with the rough terrain and ground looped. Visual meteorological conditions prevailed at the time and no flight plan was filed. The airplane was substantially damaged and the private pilot and his passenger were not injured. The flight had originated from Spokane, Washington, on October 7, 1993, at 1100 and was en route to Grangeville, Idaho, during a personal flight.

The pilot reported during a telephone interview and subsequent written statement, that while in cruise flight at 500 feet above ground level, the engine began to vibrate and shake. The pilot stated that he immediately shut the engine down and initiated a forced landing. During the ground roll on the rough terrain, the airplane ground looped before coming to a stop.

During the post-crash investigation, it was found that the number three connecting rod was broken. The connecting rod and related assembly were metallurgically examined by the National Transportation Safety Board Materials Laboratory. The metallurgist reported that "The breaking and damage of the No. 3 connecting rod was the result of fatigue fracture of one of the connecting rod bolts." No metallurgical defects could be found to contribute to the initiation of the fracture. Extensive post- separation damage was noted to nearly all of the connecting rod and assembly.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA94LA016