N761KK

Substantial
Minor

Cessna T210M S/N: 21062315

Accident Details

Date
Thursday, January 18, 1996
NTSB Number
FTW96LA098
Location
LAS VEGAS, NM
Event ID
20001208X05140
Coordinates
35.590404, -105.219306
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

failure of the throttle cable. A factor relating to the accident was: the lack of suitable terrain for a forced landing.

Aircraft Information

Registration
N761KK
Make
CESSNA
Serial Number
21062315
Engine Type
Reciprocating
Year Built
1977
Model / ICAO
T210M C210
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
TRI STATE AVIATION SERVICES INC
Address
20 TRI STATE RD
Status
Deregistered
City
BERRYVILLE
State / Zip Code
AR 72616-9531
Country
United States

Analysis

On January 18, 1996, at 0730 mountain standard time, a Cessna T210M, N761KK, registered to and operated as a cargo flight by South Aero Inc., under Title 14 CFR Part 135, was substantially damaged during a forced landing near Las Vegas, New Mexico. The commercial pilot sustained minor injuries. Instrument meteorological conditions prevailed, and an IFR flight was filed. The flight originated from Albuquerque, New Mexico, at 0655.

The pilot reported that he had reduced the throttle to begin final descent for an IFR approach to the Las Vegas Municipal Airport, Las Vegas, New Mexico. When he pulled back the throttle, "the throttle control came all the way back with the manifold pressure dropping to zero with the engine idling." Attempts to "push the throttle back in to restore power were unsuccessful." As the aircraft exited the clouds, he "noted that there were no roads" in the vicinity and the terrain appeared to be "rough." Therefore, he decided to make a gear up landing. During the landing to rough terrain the airplane came rest 150 feet from the point of touch down.

An examination of the airplane by the FAA inspector revealed the throttle cable had a big "loop" and moving the throttle from the cockpit had no effect at the fuel control. The engine firewall was damaged, the fuselage and tail were buckled, and the left elevator sustained damaged.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW96LA098