N398MA

Substantial
None

CESSNA T210LS/N: 21061441

Accident Details

Date
Friday, October 25, 2013
NTSB Number
CEN14LA031
Location
Borger, TX
Event ID
20131030X13855
Coordinates
35.700832, -101.393608
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The failure of the No. 4 connecting rod due to inadequate oil lubrication.

Aircraft Information

Registration
N398MA
Make
CESSNA
Serial Number
21061441
Engine Type
Reciprocating
Year Built
1976
Model / ICAO
T210LC210
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SHELTON MAX
Address
2700 ONE COMMERCE SQ
Status
Deregistered
City
MEMPHIS
State / Zip Code
TN 38103
Country
United States

Analysis

On October 25, 2013, about 1130 central daylight time, a Cessna T210L airplane, N398MA, struck a transmission wire and collided with terrain during a forced landing near Borger, Texas. The airplane was substantially damaged. The private pilot and passenger sustained minor injuries. The airplane was owned and operated by a private individual under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed for the flight, which operated on an instrument flight rules flight plan. The flight originated from the Thomas P Stafford Airport (KOJA), Weatherford, Oklahoma, about 1040 and was en route to Santa Fe, New Mexico.

According to a statement provided by the pilot, the flight was uneventful until about one hour after takeoff, when the engine began to surge with intermittent power. The airplane's speed decreased along with the engine's manifold pressure, and oil pressure. While diverting to the Hutchinson Country Airport (BGD), Borger, Texas, the engine stopped producing power and the pilot began gliding the airplane toward the airport. When he determined that the airplane was unable to reach the airport, the pilot selected a field for a forced landing. During the forced landing, the airplane struck a transmission wire and collided with terrain. Substantial damage was sustained to both wings, the fuselage, empennage, left horizontal stabilizer and elevator.

A postaccident examination of the engine was conducted by the NTSB and a technical representative from Continental Motors. The examination found the number four connecting rod separated from its rod journal, and the rod cap melted into the rod journal. The number five rod journal was thermally discolored. No other anomalies were discovered with the engine.

The number four rod cap and cap bolts were examined at Continental Motors' Analytical Department, Mobile, Alabama, under the auspices of the NTSB. All components displayed signatures consistent with the lack of oil lubrication. The examinations did not reveal any abnormalities which would have prevented adequate oil lubrication to the engine components.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN14LA031