N8203U

Substantial
None

Cessna 172FS/N: 17252103

Accident Details

Date
Thursday, January 20, 2005
NTSB Number
DFW05LA067
Location
Sallisaw, OK
Event ID
20050215X00184
Coordinates
35.438056, -94.802780
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 for undetermined reasons. A contributing factor was the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
N8203U
Make
CESSNA
Serial Number
17252103
Engine Type
Reciprocating
Year Built
1964
Model / ICAO
172FC172
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SPITTLER MICHAEL W
Address
RR 4 BOX 980
Status
Deregistered
City
WAGONER
State / Zip Code
OK 74467-9178
Country
United States

Analysis

On January 20, 2005, approximately 1415 central standard time, a Cessna 172F, single-engine airplane, N8203U, was substantially damaged during a forced landing following a loss of engine power while in cruise flight. The commercial pilot, sole occupant of the airplane, was not injured. Visual meteorological conditions prevailed, and a flight plan was not filed for the personal flight conducted under the provisions of 14 Code of Federal Regulations Part 91. The local flight originated from the Tahlequah Municipal Airport (TQH), near Tahlequah, Oklahoma, at an unknown time, destined for Sallisaw Municipal Airport (JSV) near Sallisaw, Oklahoma.

Despite repeated attempts by the Investigator-In-Charge (IIC), the pilot never returned a completed Pilot Operator Aircraft Accident Report Form (NTSB Form 6120.1/2). However, in a written statement submitted by the pilot to a Federal Aviation Administration (FAA) inspector shortly after the accident, the pilot reported that he was at an altitude of 3,500 feet mean sea level (MSL), approximately 10 miles northeast of Sallisaw, at a low cruise power setting, when "the engine began running rough". The pilot stated that he checked the mixture, fuel selector, magneto switch, and then applied carburetor heat. The engine continued to run rough until "it quit," at approximately 600 ft above ground level (AGL). During the landing roll, the airplane impacted a barbed-wire fence and hit a small tree.

An examination of the airplane by a Federal Aviation Administration (FAA) inspector revealed structural damage to the inboard section of the left wing and flap area, the outboard leading edge of the left wing, the outboard section of the right wing, and the right horizontal stabilizer and elevator. Additional damage to the wing strut, spinner/propeller assembly, and engine cowling was observed.

The reason for the reported loss of engine power could not be determined.

At 1355, the automated weather observing system at JSV, located approximately 3 miles southwest of the accident site, reported wind from 220 degrees at 7 knots, 10 statute miles visibility, a clear sky, temperature 68 degrees Fahrenheit, dew point 39 degrees Fahrenheit, and an altimeter setting of 29.97 inches of Mercury.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DFW05LA067