N8161V

Substantial
Minor

CESSNA A150M S/N: A1500548

Accident Details

Date
Saturday, July 31, 1993
NTSB Number
DEN93LA092
Location
GALVESTON, TX
Event ID
20001211X12903
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

THE DISCONNECTION OF THE THROTTLE LINKAGE AND THE RESULTANT POWER LOSS. A FACTOR WAS THE LACK OF SUITABLE TERRAIN FOR THE FORCED LANDING.

Aircraft Information

Registration
N8161V
Make
CESSNA
Serial Number
A1500548
Engine Type
Reciprocating
Year Built
1974
Model / ICAO
A150M C150
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
AG FLIGHT INC
Address
PO BOX 573
Status
Deregistered
City
THORNTON
State / Zip Code
CA 95686
Country
United States

Analysis

On July 31, 1993, at approximately 1100 central daylight time, a Cessna A150M, N8161V, was substantially damaged when it struck power lines and impacted terrain one half mile west of Scholes Field, Gavelston, Texas. The pilot received minor injuries. Visual meteorological conditions prevailed and no flight plan was filed for this personal flight.

The pilot obtained a full weather briefing at 0858 from the Conroe, Texas, Flight Service Station (FSS), but elected not to file a flight plan. According to his accident report, he performed an airplane preflight inspection and ascertained that both fuel tanks were filled to capacity. The engine developed "normal power" on takeoff and in cruise but after a 40 minute flight, the engine lost power. The pilot advised Galveston Unicom of the situation and reported his position as approximately two to three miles northwest of the airport. The airplane struck power lines one half mile west of the airport, impacted terrain, and came to rest inverted. Two witnesses to the accident submitted written statements (see exhibits attached).

According to the report submitted by the Federal Aviation Administration (FAA) inspector who examined the airplane on August 3, 1993, "The throttle linkage was disconnected from the throttle shaft arm (at) the carburetor...The (castellated nut and cotter pin) could not be located. Inspection of the carburetor arm disclosed a wear pattern of a washer having been placed between the arm and throttle linkage ball type rod end. There was no indication that this wear pattern was recently made, and showed no signs of recent 'working' of the two surfaces." Examination of the airplane's maintenance records indicated compliance with Airworthiness Directive (AD) 86-24-07 which called for the replacement of the existing retention nut with a castellated nut and cotter key; however, a maintenance sign off could not be located in either the aircraft or engine log books.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN93LA092