N3944Y

Substantial
Serious

CESSNA 210DS/N: 21058444

Accident Details

Date
Tuesday, August 10, 2021
NTSB Number
CEN21LA371
Location
West Fargo, ND
Event ID
20210811103685
Coordinates
46.903989, -96.929787
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

A total loss of engine power due to fuel starvation.

Aircraft Information

Registration
Make
CESSNA
Serial Number
21058444
Engine Type
Reciprocating
Year Built
1964
Model / ICAO
210DC210
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
210D

Registered Owner (Current)

Name
BROWN PELICAN AVIATION LLC
Address
7605 PARK DR
City
RALSTON
State / Zip Code
NE 68127-3943
Country
United States

Analysis

On August 10, 2021, about 1545 central daylight time, a Cessna 210D airplane, N3944Y, was substantially damaged when it was involved in an accident near West Fargo, North Dakota. The pilot was seriously injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

Witnesses stated that the pilot performed a go-around after an attempt to land on runway 18. During the go-around, the airplane banked right and the engine “cut out.” The airplane impacted a field west of the runway and sustained substantial damage to the fuselage, wings, and empennage.

An on-scene examination of the airplane by a Federal Aviation Administration inspector revealed that the fuel selector was in the left tank position. There was about 8 gallons of fuel in the left wing fuel tank and no useable fuel in the right wing fuel tank. The right wing sustained impact damage, but there was no evidence of fuel on the ground at the accident site. There was no evidence of a fuel leak or fuel staining on the airplane.

A subsequent examination of the engine and fuel system revealed no anomalies that would have precluded normal operation. Examination of the fuel system found about 1/8 ounce of fuel in the fuel system forward of the fuel selector. The fuel system lines and components were intact, secure, and did not exhibit any evidence of leakage. The fuel vent system was unobstructed. The fuel selector operated through its detents without anomaly.

An ohmmeter was used to check resistances of both fuel senders when their float arms were positioned at the top and bottom mechanical stops. The approximate resistance values for the left fuel sender bottom stop was 28 ohms, the right fuel sender bottom stop was 38 ohms. According to the aircraft manufacturer, the fuel senders’ minimum resistance value should be 33.5 ohms +/- 2 ohms.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN21LA371