N9120Q

Substantial
Minor

Dixon RV-4S/N: 2278

Accident Details

Date
Friday, September 9, 2005
NTSB Number
CHI05CA259
Location
Grafton, IL
Event ID
20051005X01586
Coordinates
39.002223, -90.432220
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The loss of engine power due to contamination of the fuel system, gascolator and carburetor inlet screen. A factor to the accident was the soybean crop.

Aircraft Information

Registration
Make
DIXON
Serial Number
2278
Engine Type
Reciprocating
Year Built
1995
Model / ICAO
RV-4RV4
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
RV 4

Registered Owner (Current)

Name
RICHEY JOHN D
Address
280 N 18TH ST
City
BATESVILLE
State / Zip Code
AR 72501-3103
Country
United States

Analysis

On September 9, 2005, at 1350 central daylight time, a Dixon RV-4, N9120Q, piloted by a private pilot, was substantially damaged during a forced landing following a loss of engine power near Grafton, Illinois. Visual meteorological conditions prevailed at the time of the accident. The personal flight was operating under the provisions of 14 Code of Federal Regulations (CFR) Part 91 without a flight plan. The pilot sustained minor injuries. The flight departed Batesville Regional Airport (BVX), Batesville, Arkansas, at 1200 and was enroute to Whiteside County Airport (SQI), Rock Falls, Illinois.

The pilot reported that after passing the St. Louis metropolitan area the engine "started missing" and eventually "went dead". The pilot stated that he performed a forced landing into a soybean field and nosed over during the landing rollout.

The pilot told a Federal Aviation Administration (FAA) inspector that he had descended to 2,000 feet mean sea level in order to avoid the St. Louis Class B airspace. The pilot reported that after passing St. Louis he started to initiate a climb when the engine began running rough. The pilot stated that he switched fuel tanks, checked the magnetos, and applied carburetor heat to no avail.

The engine was test run during a post-accident examination. The engine started and ran at idle for a period of five minutes with no anomalies. The engine subsequently ran at 2,100 rpm with no anomalies. The gascolator and carburetor inlet screen were contaminated with fragments of a red fabric-like substance, according to the mechanic who examined the airplane after the accident. The red fragments were similar to a shop-cloth or scotch-brite abrasion pad.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI05CA259