N30286

Substantial
Minor

CESSNA T210LS/N: 21059910

Accident Details

Date
Monday, June 14, 2021
NTSB Number
CEN21LA271
Location
Buena Vista, CO
Event ID
20210615103271
Coordinates
38.842200, -106.131100
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
1
Total Aboard
2

Probable Cause and Findings

The partial loss of engine power due to a vane failure in the engine-driven fuel pump.

Aircraft Information

Registration
N30286
Make
CESSNA
Serial Number
21059910
Engine Type
Reciprocating
Year Built
1973
Model / ICAO
T210LC210
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
204 N J ST APT 1
Status
Deregistered
City
IMPERIAL
State / Zip Code
CA 92231
Country
United States

Analysis

On June 14, 2021, about 0700 mountain daylight time, a Cessna T210L, N30286, was substantially damaged when it was involved in an accident near Buena Vista, Colorado. The pilot sustained minor injuries, and the pilot-rated passenger was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that, while the airplane was flying over mountains and near the destination airport, the engine temperature and fuel flow gauges “dropped” immediately, and the engine lost partial power. The pilot reported that the power loss felt as if someone had retarded the throttle, so he “instantly” pushed the throttle in and turned on the auxiliary fuel pump to the “high” position. These actions had no effect on the engine, so the pilot tried to restart the engine, including attempting a hot start, but was unable to do so. The pilot located a flat, treeless area for a forced landing. During the forced landing the landing gear separated, and the airplane came to a stop upright. The airplane sustained substantial damage to the forward fuselage, firewall, and left outboard wing.

A postaccident examination of the airplane’s engine-driven fuel pump showed that one of the pump’s two carbon vanes had fractured in half. No debris was found in the pump housing. No other preaccident failures or malfunctions were found that would have precluded normal operation of the airplane or engine.

According to the engine manufacturer, operation of the pump with a severed vane would likely cause fuel cavitation, which would cause a drop in pump outlet pressure and could result in a gradual decrease in engine rpm.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN21LA271