N2KD

Substantial
Minor

Cessna T210JS/N: T210-0436

Accident Details

Date
Saturday, July 3, 2004
NTSB Number
DEN04CA096
Location
Cheyenne, WY
Event ID
20040810X01183
Coordinates
41.150833, -106.452499
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

the detachment of the nut and bolt that attaches the throttle control cable to the fuel induction due to improper maintenance. Contributing factors were the fiber optics wire, fence, and ditch, and the unavailability of suitable terrain on which to make a forced landing.

Aircraft Information

Registration
Make
CESSNA
Serial Number
T210-0436
Engine Type
Reciprocating
Year Built
1969
Model / ICAO
T210JC210
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
T210J

Registered Owner (Current)

Name
ELLIOTT FRANK F
Address
7435 35TH ST W
City
MOJAVE
State / Zip Code
CA 93501-7304
Country
United States

Analysis

On July 3, 2004, at 1341 mountain daylight time, a Cessna T210J, N2KD, co-registered to and operated by the pilot, was substantially damaged when it collided with a fence and drainage ditch during an off-airport forced landing at Cheyenne, Wyoming. The private pilot, the sole occupant on board, received minor injuries. Visual meteorological conditions prevailed, and no flight plan had been filed for the personal flight being operated under Title 14 CFR Part 91. The flight originated from Sycamore Strip (9F9), Fort Worth, Texas, approximately 1120 central daylight time, and was en route to Cheyenne (CYS).

In a telephone interview, the pilot said that after an uneventful flight from Texas, he was cleared to land on runway 30. While on final approach, the engine lost power and he made a forced landing in a field 1-1/2 mile short of the runway. The airplane struck a fiber optics cable, then touched down in the field, went through a fence, and struck a 3-foot wide, 2-1/2-foot deep irrigation ditch. The landing gear was sheared, and the nose gear penetrated the cabin floor. The bottom half of the engine cowling was crushed, the left wing tip was torn off, the engine mounts were broken, and the vertical stabilizer was dented. A similar accounting was given in his written statement to the Federal Aviation Administration (copy attached).

Post-accident examination by an FAA airworthiness inspector revealed that the bolt and nut that attaches the throttle control cable to the fuel induction was missing. Examination of the aircraft maintenance records revealed on April 1, 2004, the engine was removed from the airframe and inspected for metal contamination. Engine removal would necessitate detaching the throttle control cable from the fuel induction. The engine was reinstalled and a 100-hour/annual inspection was accomplished.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN04CA096