N381J

Substantial
None

Cessna 172PS/N: 17274183

Accident Details

Date
Monday, August 19, 2002
NTSB Number
CHI02LA255
Location
Buffalo City, WI
Event ID
20020829X01478
Coordinates
44.251667, -91.858612
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The malfunction of the seat positioning system for undetermined reasons, which resulted in the loss of directional control. A factor to the accident was the descending embankment.

Aircraft Information

Registration
Make
CESSNA
Serial Number
17274183
Engine Type
Reciprocating
Year Built
1980
Model / ICAO
172PC172
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
172P

Registered Owner (Current)

Name
US AVIATION GROUP LLC
Address
4850 SPARTAN DR
City
DENTON
State / Zip Code
TX 76207-4547
Country
United States

Analysis

On August 19, 2002, at 1110 central daylight time, a Cessna 172P, N381J, piloted by an airline transport pilot, sustained substantial damage while performing a takeoff from a gravel road near Buffalo City, Wisconsin. Visual meteorological conditions prevailed at the time of the accident. The business flight was operating under the provisions of 14 CFR Part 91 without a flight plan. The pilot reported no injuries. The flight was originating at the time of the accident and had the intended destination of Winona, Minnesota.

According to the pilot's written statement, "On take off, after applying full power and rolling for about 20 to 30 feet, the seat slid back full aft preventing me from reaching the rudder pedals. Therefore I could not maintain the directional control nor I could bring the plane to a stop. I tried to pull the seat forward but it was locked aft and the seat belt & shoulder harness prevented me to move forward. I pulled the power back- the plane had already veered to the left in an embankment 15 [feet] deep."

An inspector with the Federal Aviation Administration (FAA) and a representative of the Cessna Aircraft Company conducted post accident examinations of the airplane. The seat positioning system was a dual latch pin design. The seat tracks had light wear markings, the seat base and attachment feet were worn and the vertical supports of the seat base flexed inboard and outboard approximately 0.20 inches. The seat moved freely along the tracks and the latch pins engaged the pinholes along the tracks. The seat could be twisted (racked) resulting in the outboard latch pin engaging a pinhole and the failure of the inboard latch pin to engage a pinhole. If the seat was displaced in the forward direction, both latch pins engaged a pinhole.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI02LA255