N2199N

Substantial
None

CESSNA 140S/N: 12435

Accident Details

Date
Thursday, August 4, 2011
NTSB Number
WPR11LA369
Location
Wilkeson, WA
Event ID
20110804X61104
Coordinates
47.129444, -122.055831
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

A partial loss of engine power during takeoff due to water contamination in the fuel system.

Aircraft Information

Registration
Make
CESSNA
Serial Number
12435
Engine Type
Reciprocating
Year Built
1947
Model / ICAO
140C140
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
140

Registered Owner (Current)

Name
SKYWAGON AERO LLC
Address
108 W 13TH ST
City
WILMINGTON
State / Zip Code
DE 19801-1145
Country
United States

Analysis

On August 4, 2011, at 0830 Pacific daylight time, a Cessna 140, N2199N, collided with trees during a forced landing near Wilkeson, Washington. The airplane sustained substantial damage. The private pilot and one passenger were not injured. The pilot, who was also the registered owner of the airplane, was operating it under the provisions of Title 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed and no flight plan was filed for the local area flight.

The pilot reported in a written statement that he had washed the airplane the day before the accident. Prior to the accident flight, he did an extensive preflight and verified no water was in the fuel. He also verified that the scat tubing was free of moisture. The run up was uneventful and during takeoff, he brought the throttle to takeoff power and released the brakes. The pilot stated that about halfway down the runway, the engine began to lose power and sputter. He verified the fuel selector and carburetor heat positions and then began pumping the throttle. He was unable to sustain engine power and force-landed the airplane into trees.

The pilot reported during a phone conversation following the accident, that when he had washed the airplane on prior occasions, the airplane had experienced momentary power interruptions which he had attributed to residual water.

During the post accident inspection, a Federal Aviation Administration accident coordinator test ran the engine using the airframe fuel system, fuel, and controls. The engine was test run from idle to 2,200 revolutions per minute with no operational anomalies.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR11LA369