ASN Wikibase Occurrence # 264068
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information.
If you feel this information is incomplete or incorrect, you can
submit corrected information.
Date: | Monday 14 June 2021 |
Time: | 07:00 LT |
Type: | Cessna T210L Turbo Centurion |
Owner/operator: | Wandsneider Physician Services LLC |
Registration: | N30286 |
MSN: | 21059910 |
Year of manufacture: | 1973 |
Total airframe hrs: | 3470 hours |
Engine model: | Continental TSIO-520-H6B |
Fatalities: | Fatalities: 0 / Occupants: 2 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Buena Vista, Chaffee County, CO -
United States of America
|
Phase: | Manoeuvring (airshow, firefighting, ag.ops.) |
Nature: | Private |
Departure airport: | Broomfield-Rocky Mountain Metropolitan Airport, CO (BJC/KBJC) |
Destination airport: | Leadville Airport, CO (LXV/KLXV) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The pilot reported that the airplane was over mountains and near the destination airport when the engine temperature and fuel flow gauges “dropped' and the engine lost partial power. The pilot pushed the throttle in and turned on the auxiliary fuel pump to the “high' position, but those actions had no effect on the engine power. The pilot troubleshot the loss of power; however, there was no change. The pilot then 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. How the carbon vane fractured was not determined. The severed fuel pump vane likely resulted in fuel cavitation, a drop in pump outlet pressure, a gradual decrease in engine rpm, and subsequent partial loss of engine power.
Probable Cause: The partial loss of engine power due to a vane failure in the engine-driven fuel pump.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | CEN21LA271 |
Status: | Investigation completed |
Duration: | 2 years and 3 months |
Download report: | Final report |
|
Sources:
NTSB CEN21LA271
https://flightaware.com/live/flight/N30286 Location
Revision history:
Date/time | Contributor | Updates |
16-Jun-2021 13:43 |
Captain Adam |
Added |
28-Jul-2021 19:48 |
aaronwk |
Updated [Time, Destination airport, Source, Damage, Narrative, Category] |
21-Sep-2023 12:48 |
ASN Update Bot |
Updated [[Time, Destination airport, Source, Damage, Narrative, Category]] |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation