N969RJ

Substantial
None

Cessna 210C S/N: 210-58164

Accident Details

Date
Wednesday, December 13, 2000
NTSB Number
DEN01LA022
Location
BOULDER, CO
Event ID
20010110X00074
Coordinates
40.020832, -105.250816
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

Total loss of engine power due to fuel contamination (water), and failure of the pilot to have the airplane completely refueled. A factor was unsuitable terrain on which to make a forced landing.

Aircraft Information

Registration
N969RJ
Make
CESSNA
Serial Number
210-58164
Engine Type
Reciprocating
Year Built
1963
Model / ICAO
210C C210
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
MURO JIMMIE E
Address
8198 BRIAR RIDGE DR
Status
Deregistered
City
CASTLE ROCK
State / Zip Code
CO 80104-8218
Country
United States

Analysis

On December 13, 2000, approximately 1415 mountain standard time, a Cessna 210C, N969RJ, was substantially damaged when it collided with terrain during a forced landing at Boulder, Colorado. The commercial pilot, the sole occupant aboard, was not injured. Visual meteorological conditions prevailed, and no flight plan had been filed for the ferry flight being conducted under Title 14 CFR Part 91. The flight had originated from the Boulder Municipal Airport immediately prior to the accident.

The airplane had sat dormant for almost 8 years, and extensive checks and servicing were performed to prepare it for the ferry flight to Centennial Airport where it was scheduled to undergo an annual inspection. FAA issued a ferry permit. According to the pilot's accident report, the airplane was parked in a heated hangar the night before the ferry flight. When he preflighted the airplane the next morning, "a little water" was found in the gascolator and only "a tiny amount" was found in the right wing sump. He chose not to have the fuel drained and the airplane serviced with fresh fuel. He later told a local newspaper that he had drained the fuel system and thought he had removed all the water, "but apparently it was not enough." The pilot was unsuccessful in trying to start the engine. After it was preheated, the engine started. He performed "an extended time warm up and extended pretakeoff run-up. All things were normal."

The pilot took off on runway 8L. As he was climbing through 350 to 400 feet agl, the engine lost "complete power." He enriched the mixture and turned the auxiliary fuel pump first to LOW, then to HIGH. Power returned momentarily, then the engine quit again. The pilot did not have a chance to switch fuel tanks, but concentrated instead on the forced landing. The airplane "skimmed the tops of hills, went through a fence, nosed over, and tumbled 2 or 3 times." The propeller separated from the engine, which was torn from the airframe, the vertical stabilizer was crushed, and both wings were bent.

On February 8, 2001, the airplane and engine were examined at Beegles Aircraft Services in Greeley, Colorado. A Teledyne Continental Motors representative removed the top of the fuel manifold, but was unable to dislodge the plunger. It was eventually forced out with a screwdriver. Ice had locked the plunger in position, and ice was noted in the chamber under the screen.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN01LA022