N210GB

Destroyed
Minor

Cessna T210NS/N: T210-63564

Accident Details

Date
Friday, November 16, 2001
NTSB Number
DEN02LA012
Location
Montrose, CO
Event ID
20011121X02284
Coordinates
38.578056, -107.988052
Aircraft Damage
Destroyed
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

the loss of engine power during initial climb for undetermined reason. A factor was the lack of suitable terrain for a forced landing.

Aircraft Information

Registration
N210GB
Make
CESSNA
Serial Number
T210-63564
Engine Type
Reciprocating
Year Built
1979
Model / ICAO
T210NC210
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
BOWEN FLOYD E JR
Address
6730 CLAIM ST
Status
Deregistered
City
PLACERVILLE
State / Zip Code
CA 95667-9037
Country
United States

Analysis

On November 16, 2001, at approximately 1415 mountain standard time, a Cessna T210N, N210GB, was destroyed during a postimpact fire following a power loss and subsequent forced landing near Montrose, Colorado. The private pilot, the sole occupant on the airplane, received minor injuries. The pilot/owner was operating the airplane under Title 14 CFR Part 91. Visual meteorological conditions prevailed for the cross-country personal flight that was originating at the time of the accident. No flight plan had been filed, but the pilot said that his planned destination was Placerville, California.

The pilot said that the first leg of his trip from Kansas City, Kansas, to Placerville, California, was uneventful. He was on the ground at Montrose, Colorado, for approximately 30 minutes for fuel and a rest stop. The pilot said that he departed on runway 31 at approximately 1415, and the takeoff seemed normal. During a telephone conversation, he said that at approximately 1,500 feet above ground level (agl) he reduced the throttle for cruise, reduced the propeller control, and adjusted his fuel mixture. He moved his hand to change a radio frequency when the manifold pressure rapidly dropped to approximately 15 inches of mercury. He switched fuel tanks and turned on the auxiliary fuel pump, believing that there was a vapor lock in the fuel line.

The pilot reported that the engine lost power, and the propeller continued to windmill. He pressed the boost pump switch and pulled the throttle out about an inch. The engine still did not restart; he performed a forced landing to a field. During the landing roll, the airplane crossed a creek, and the nose wheel landing gear collapsed under the airplane. He noticed fire around his feet, and immediately exited the airplane. The airplane was consumed by postimpact fire.

Postaccident investigation of the airframe and the engine by an FAA inspector, as well as an engine and airframe manufacturer representatives revealed no anomalies which might have affected the airplane's performance before the accident. The engine manufacturer’s representative did find that eight spark plugs were very black and sooty, and four spark plugs wet. A witness, who observed the takeoff, said that the airplane trailed dark smoke during its takeoff roll and climb out.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN02LA012