N2229B

Substantial
None

LUSCOMBE 8A S/N: 6656

Accident Details

Date
Thursday, September 6, 1990
NTSB Number
CHI90LA259
Location
LEBANON, IL
Event ID
20001212X24222
Coordinates
38.600921, -89.809082
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

the loss of engine power for undetermined reasons while executing a go-around with insufficient runway remaining for a forced landing. A factor in the accident was the structures at the end of the runway that the pilot was attempting to avoid. This report was modified on February 9, 2005.

Aircraft Information

Registration
Make
LUSCOMBE
Serial Number
6656
Engine Type
Reciprocating
Year Built
1949
Model / ICAO
8A L8
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
8A

Registered Owner (Current)

Name
B & G FLYING SERVICE
Address
700 AIRPORT RD
City
CLANTON
State / Zip Code
AL 35045-2966
Country
United States

Analysis

On September 6, 1990, at 1845 CDT, a Luscombe 8A, N2229B, operated by an airline transport pilot, was substantially damaged when it nosed over during landing roll following an emergency landing at Lebert Flying L Airport, Lebanon, Illinois. The pilot was not injured. The personal flight was conducted under 14 CFR Part 91 and no flight plan was filed. The local flight originated at Lebert Flying L Airport at 1815 CDT. Visual meteorological conditions prevailed at the time of the accident.

A witness who observed the airplane's approach stated that the approach was "hot and high." The pilot stated that he was too high and fast at the landing threshold, that he applied power to execute a go-around, but the engine "popped and quit." He stated that he cycled the carburetor heat to the off position after the engine quit, and also cycled the mixture control during his unsuccessful attempt to restart the engine at low altitude. He stated that when the engine failed to restart he concentrated on landing on the remaining runway. He landed the airplane near the departure end of the runway and applied maximum braking to avoid cement company structures off the end of the runway and the airplane nosed over.

The investigation determined that the carburetor heat control was jammed in the off position and that the carburetor was dislodged from its base. The temperature at the time of the accident was 97° F, and the dew point was 72°.

This report was modified on February 9, 2005.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI90LA259