N210GE

Destroyed
Minor

CESSNA P210NS/N: P21000655

Accident Details

Date
Tuesday, March 8, 2022
NTSB Number
CEN22LA137
Location
Englewood, CO
Event ID
20220309104753
Coordinates
39.551230, -104.853880
Aircraft Damage
Destroyed
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
2
Uninjured
0
Total Aboard
2

Probable Cause and Findings

A total loss of engine power on short final for reasons that could not be determined based on the available evidence.

Aircraft Information

Registration
Make
CESSNA
Serial Number
P21000655
Engine Type
Reciprocating
Model / ICAO
P210NC210
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
6
FAA Model
P210N

Registered Owner (Current)

Name
LEIMBACH KEITH
Address
32803 UPPER BEAR CREEK RD
City
EVERGREEN
State / Zip Code
CO 80439-7827
Country
United States

Analysis

On March 8, 2022, at 1417 mountain standard time, a Cessna P210N airplane, N210GE, was destroyed when it was involved in an accident near Englewood, Colorado. The pilot and flight instructor both sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The airplane was established on the instrument landing system (ILS) approach to runway 35R as it approached Centennial Airport. The tower controller subsequently instructed them to sidestep to runway 35L. This required the pilot to extend the glide path because the runway arrival thresholds are offset. However, as the pilot attempted to increase engine power, he realized that it was not responding. Attempts to restore engine power by activating the auxiliary fuel pump and changing fuel tanks were not successful. Unable to glide to the runway, the flight instructor executed a forced landing about 1/2-mile short of the runway.

The airplane landed in the grass median area between traffic lanes of an interstate highway and came to rest on a steel-cable safety barrier. A postimpact fire ensued.

The airplane sustained impact damage to the forward fuselage and both wings. The postimpact fire consumed portions of the fuselage, cockpit/cabin area, and right wing. Postrecovery airframe and engine examinations did not reveal any anomalies consistent with an inability of the fuel-injected engine to produce rated power. However, examination of the airframe fuel system was hindered by the extent of the fire damage.

The airplane was equipped with two wing fuel tanks each capable of holding about 44 gallons of useable fuel. The airplane was also equipped with an auxiliary fuel tank, located in the aft baggage compartment, capable of holding about 30 gallons of fuel. Automatic Dependent Surveillance – Broadcast (ADS-B) data revealed that the accident flight was 1 hour and 48 minutes in duration. The pilot’s operating handbook indicated that the expected fuel consumption was 18 – 20 gallons per hour during cruise flight. Accordingly, the expected fuel consumption for the flight would be approximately 36 gallons. The pilot reported that the flight departed with 118 gallons of fuel onboard. The airplane was equipped with two wing fuel tanks each capable of holding about 44 gallons of useable fuel. The airplane was also equipped with an auxiliary fuel tank, located in the aft baggage compartment, capable of holding about 30 gallons of fuel.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN22LA137