N6584B

Substantial
None

CESSNA T210MS/N: 21062791

Accident Details

Date
Friday, April 24, 2009
NTSB Number
WPR09LA214
Location
Hanford, CA
Event ID
20090424X12414
Coordinates
36.215278, -119.588607
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
4
Total Aboard
4

Probable Cause and Findings

A loss of engine power during descent due to fuel starvation as a result of the pilot's improper fuel management. Contributing to the accident was the pilot's failure to use the correct fuel flow performance chart.

Aircraft Information

Registration
N6584B
Make
CESSNA
Serial Number
21062791
Engine Type
Reciprocating
Year Built
1978
Model / ICAO
T210MC210
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
XXX
Status
Deregistered
City
NONE
State / Zip Code
OK 73125
Country
United States

Analysis

On April 24, 2009, about 1425 Pacific daylight time, a Cessna T210M, N6584B, impacted the terrain during a forced landing on rough terrain about five miles southeast of Hanford, California. The commercial pilot and his three passengers were not injured, but the airplane, which was owned and operated by the pilot, sustained substantial damage. The 14 Code of Federal Regulations Part 91 personal pleasure flight, which departed North Las Vegas Airport about two and one-half hours prior to the accident, was being operated in visual meteorological conditions. The flight was en route to Vacaville, California. No flight plan had been filed.

According to the pilot, while en route to Vacaville, he noticed that the fuel quantity was getting lower than he was comfortable with, so he elected to divert into Hanford Municipal Airport to take on some additional fuel. During his descent into Hanford, the engine lost power, and he was unable to get it restarted. He therefore executed an engine-out forced landing in an open field. During the landing roll the airplane's wing came in contact with the rough terrain. A post-accident inspection of the airplane by a Federal Aviation Administration (FAA) Inspector found that there was eight gallons of fuel in the left wing tank, but the right wing tank was empty. Further discussions with the pilot determined that he had the right tank selected when the engine quit, and although he attempted a restart sequence, he did not select the left tank at any time during the restart attempt.

According to the pilot, prior to the time he purchased the airplane (about seven years before the accident) it underwent a RAM Aircraft Supplemental Type Certificate (STC) engine conversion, increasing its output to 310 horsepower, and changing its performance and fuel flow figures. The pilot further stated that until about two weeks before the accident, when his current maintenance provider gave him a copy of the RAM conversion performance charts, he did not realize there was a fuel flow difference between the original/standard engine and the RAM conversion. Although he had the RAM charts, the pilot continued to use the performance/fuel flow charts that came with the aircraft at the time of the aircraft's manufacture, and in so doing, on the accident flight he ended up with less fuel remaining than he expected for the time that he had been airborne.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR09LA214