N3440

Substantial
None

STEARMAN AIRCRAFT C3-BS/N: 104

Accident Details

Date
Saturday, September 20, 2008
NTSB Number
SEA08LA206
Location
Stevenson, WA
Event ID
20081003X17553
Coordinates
45.693054, -121.884445
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 fuel starvation from a piece of disintegrating gasket material that was blocking the fuel jet. Also causal was the failure of maintenance personnel to verify the condition of the gaskets when the carburetor was examined prior to installation on the engine.

Aircraft Information

Registration
Make
STEARMAN AIRCRAFT
Serial Number
104
Engine Type
Reciprocating
Year Built
1927
Model / ICAO
C3-BST3
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
3
FAA Model
C2

Registered Owner (Current)

Name
WESTERN ANTIQUE AEROPLANE & AUTOMOBILE MUSEUM
Address
1600 AIR MUSEUM RD
City
HOOD RIVER
State / Zip Code
OR 97031-9800
Country
United States

Analysis

On September 20, 2008, at 0945 Pacific daylight time, N3440, a Stearman C3-B, collided with a tree during a forced landing near Stevenson, Washington. The pilot was operating the airplane under the provisions of 14 Code of Federal Regulations Part 91. The airplane sustained substantial damage; the airline transport pilot, the sole occupant, was not injured. Visual meteorological conditions prevailed, and no flight plan was filed.

The pilot reported that he had completed a cross-country flight to reenact the airmail route, and was part of a flight of two flying down the Columbia River. During the flight, the pilot had applied carburetor heat, but the engine lost power. He attempted to restart the engine, was unsuccessful, and then performed a forced-landing in a field. During the landing roll, the airplane collided with a tree and sustained substantial damage. The pilot reported that he purchased the engine and carburetor that were manufactured in about 1945, and when he purchased them, they were in new condition.

Post accident examination of the carburetor showed that a piece of gasket material had entered into the main fuel jet. The gasket material was removed and the carburetor operated normally.

Prior to installation of the carburetor onto the engine, it was inspected and bench tested by a maintenance facility. According to the facility, the carburetor tested within the specified limits and was installed on the accident airplane engine where it operated for 110 hours prior to the accident. The carburetor was not disassembled prior to the installation because it appeared to be in pristine condition. The facility indicated that in the future they will disassemble all older parts to check the components that might deteriorate over time.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA08LA206