N86851

Substantial
None

Bellanca 14-13 S/N: 1213

Accident Details

Date
Friday, March 28, 1997
NTSB Number
LAX97LA134
Location
OROVILLE, CA
Event ID
20001208X07586
Coordinates
39.500778, -121.670143
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

a loss of engine power due to connecting rod bolt failure. The reason for the bolt failure was not determined. A contributing factor was the presence of trees in the emergency landing path.

Aircraft Information

Registration
Make
BELLANCA
Serial Number
1213
Engine Type
Reciprocating
Year Built
1946
Model / ICAO
14-13
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
14-13

Registered Owner (Current)

Name
NUTTER MICHAEL S
Address
4443 PARADISE AVE W
City
UNIVERSITY PLACE
State / Zip Code
WA 98466-1023
Country
United States

Analysis

On March 27, 1997, at 1825 hours Pacific standard time, a Bellanca 14-13, N86851, owned and operated by the pilot, experienced a loss of engine power while cruising at 3,500 feet mean sea level near Oroville, California. According to the pilot, the sequence of events started when his "perfect running engine" suddenly began knocking and vibrating. Moments later, all engine power was lost. The commercial pilot attempted to land on a nearby road. During the approach the airplane collided with a tree, and the airplane was substantially damaged. The pilot was not injured. Visual meteorological conditions prevailed during the personal flight, and no flight plan was filed. The flight originated from Redding, California, at 1750.

The pilot and the Federal Aviation Administration (FAA) coordinator inspected the airplane, manufactured in 1946, and the Franklin engine. The FAA reported observing several holes in the upper portion of the engine case in the vicinity of the number 6 cylinder. The largest hole was about 0.75 inches wide by 2.0 inches long. The FAA reported it appeared as though something was trying to get out from inside the engine.

An additional examination of the engine revealed that both of the number 6 connecting rod bolts were broken and the rod cap was crushed and fragmented. According to the owner, the rod bolts had been in service for about 1,185 hours. The engine's total time was about 2,350 hours.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX97LA134