N4134X

Substantial
None

AERO COMMANDER 100 S/N: 233

Accident Details

Date
Tuesday, July 27, 1993
NTSB Number
FTW93LA219
Location
VIDOR, TX
Event ID
20001211X12925
Coordinates
30.119352, -94.000953
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

CONTROL CABLE SEPARATION DUE TO THE THROTTLE POWER LEVER LINKAGE NOT BEING SECURED BY RETAINER RESULTANT FROM IMPROPER INSTALLATION. A FACTOR WAS A LACK OF SUITABLE TERRAIN FOR THE FORCED LANDING.

Aircraft Information

Registration
N4134X
Make
AERO COMMANDER
Serial Number
233
Engine Type
Reciprocating
Model / ICAO
100 VO10
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
CHENAULT E BRYAN
Address
1465 FU TURA
Status
Deregistered
City
BEAUMONT
State / Zip Code
TX 77706
Country
United States

Analysis

On July 27, 1993, at approximately 0830 central daylight time, an Aero Commander 100, N4134X, sustained substantial damage near Vidor, Texas, following a forced landing due to a loss of engine power. The commercial pilot was not injured. Visual meteorological conditions prevailed for the pipeline patrol flight.

During telephone interviews, conducted by the investigator in charge with the pilot and operator, the following information was revealed. The flight departed Lake Charles, Louisiana, and was en route with a final destination of Beaumont, Texas. During cruise flight at approximately 500 feet above the ground, there was a total loss of engine power. A forced landing was made to a wet field. During the landing roll, the nose wheel hit a ditch and the airplane nosed over, coming to rest up right.

Examination of the airplane by the Federal Aviation Administration inspectors revealed that the throttle mixture control cable was separated at the carburetor, the retainer for the cable was missing, and the control arm was in the shutoff position.

According to the maintenance records, which were reviewed by the investigator in charge, an overhauled carburetor was installed on May 5, 1993. On July 13, 1993, the carburetor heat control cable had been adjusted.

The airplane was released to the owner's representative following the investigation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW93LA219