FTW93LA219

NTSB accident investigation · Aero Commander 100 · Vidor, TX · July 27, 1993

Accident · No injuriesLimited investigationFinal report
Date
July 27, 1993, 08:30 local (13:30 UTC)
Place
Vidor, TX
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N4134XAero Commander 100
Weather
Visual (VMC) · Day
Status
Completed · report September 13, 1994
Report
Approved by Office Director
FAA report
19930727030849A
Case key
18799

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

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.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine power(total) - mech failure/malfCruise
Mixture control,cable - separationCause
Throttle/power lever,linkage - not securedCause
Maintenance,installation - improperOther maintenance personnelCause
Forced landingDescent - emergency
On ground/water encounter with terrain/waterLanding - roll
Terrain condition - none suitableFactor
Terrain condition - ditch
Nose overLanding - roll

Analysis

During the forced landing in a field, following a total loss of engine power, the airplane hit a ditch and nosed over coming to rest up right. Examination of the controls by federal aviation administration inspectors revealed that the mixture control cable had separated and the throttle power lever linkage retainer was missing. An overhauled carburetor was installed on may 5, 1993.

Factual narrative

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.

Aircraft

Registration
N4134X
Reported as
Aero Commander 100
Category
Airplane
Serial number
233
Airframe hours
3,922
Engine
Lycoming O-320-A2B, 150 horsepower, reciprocating
Damage
Substantial damage
Flight
Other work use · Part 91
Registered owner
Chenault, Bryan E.
Airworthiness certificate
Standard, Normal
Last inspection
Annual · January 17, 1993
Departed
LCH · Lake Charles, LA
Destination
BMT · Beaumont, TX

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
62
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
4,000 total · 144 in this make and model · 3,500 as pilot in command · 208 in the last 90 days · 78 in the last 30 days · 7 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
300° at 3 knots
Visibility
7 statute miles
Lowest ceiling
None
Temperature
82 °F, dew point 79 °F
Altimeter
29.00 inHg
Observed at
BPT, 10 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.