N761SZ

Substantial
Serious

CESSNA T210MS/N: 21062493

Accident Details

Date
Monday, December 12, 2016
NTSB Number
WPR17LA036
Location
Mecca, CA
Event ID
20161212X85310
Coordinates
34.066665, -115.970000
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The total loss of engine power due to fuel starvation during approach, which necessitated a gear-up landing on unsuitable terrain.

Aircraft Information

Registration
N761SZ
Make
CESSNA
Serial Number
21062493
Engine Type
Reciprocating
Year Built
1978
Model / ICAO
T210MC210
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
RL EQUIPMENT AND SERVICES LLC
Address
PO BOX 526
Status
Deregistered
City
CRIPPLE CREEK
State / Zip Code
CO 80813-0526
Country
United States

Analysis

On December 11, 2016, about 1815 Pacific standard time, a Cessna T210M, N761SZ, sustained substantial damage when it was involved in an accident near Mecca, California. The pilot sustained serious injuries. The airplane was being operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that he had the fuel tanks filled before departing for the cross-country flight, and he confirmed they were full during the preflight inspection. The pilot reported that he had to change his intended flight route due to weather. During the flight, the fuel meter indicated a flow rate of between 12 and 15 gallons per hour. When the pilot had the destination in sight and was descending for the approach, he noted that both fuel tank gauges were reading just below 1/4 tank and that the fuel totalizer was showing about 22 gallons were remaining. He then switched from the right to the left tank. Subsequently, the engine lost all power. The pilot was unable to restart the engine, so he chose to conduct a gear-up landing on hilly terrain about 10 miles east of the destination airport, resulting in substantial damage to the forward fuselage.

The airplane was examined about 1 month after the accident. The fuel line between the right header tank and selector valve had separated during impact. An unspecified amount of fuel was found in the wing tanks. Examination and testing of the fuel gauges and floats revealed no anomalies that would have precluded normal operation. No residual fuel was found in the gascolator. A small amount of fuel was found in the fuel pump and fuel manifold valve. There was no evidence of preimpact mechanical malfunctions or failures of the engine or airframe that would have precluded normal operation.

The engine manufacturer estimated that, assuming the fuel tanks were full at takeoff and using the time elapsed from takeoff to the loss of engine power and the fuel burn rate during the flight, it is likely that the fuel tanks had 10 to 15 gallons of fuel in them at the time of the accident.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR17LA036