No fatalities

31 Dec 2008: CESSNA T210M — Fort Collins, CO

Fort Collins, CO, United States

On 31 Dec 2008, a CESSNA T210M was involved in an aviation accident near Fort Collins, CO. No fatalities were reported. Investigators recorded the probable cause as: A total loss of engine power due to fuel starvation as a result of the pilot's failure to select the fullest tank before landing. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

A pilot experienced a total loss of engine power on final approach after selecting the left fuel tank, which contained less than four gallons, while the right tank held 25 gallons. The subsequent road landing resulted in a wing striking a road sign.

Accident Overview

The pilot departed on a cross-country flight with 89 gallons of usable fuel on board. Four hours and 20 minutes after engine start, while on final approach, the airplane's engine lost total power. Unable to reach the runway, the pilot elected to land on a nearby road. During the rollout, the airplane's left wing impacted a road sign, resulting in substantial damage.

Fuel Management

According to information downloaded from the airplane's fuel computer, the airplane had consumed 60.2 gallons of fuel at the time of the loss of engine power. An examination of the airplane after the accident revealed that the right fuel tank contained approximately 25 gallons of fuel. The left tank contained residual fuel; however, it had been compromised during the accident. Fuel calculations indicate that the left tank would have contained less than four gallons when the loss of engine power occurred. The pilot reported that he approached to land with the fuel selector in the left tank position. The airplane's before-landing checklist states that the fullest tank is to be selected before landing. In addition, a required placard on the fuel selector states that the fullest tank is to be selected for takeoff and landing.

Post-Accident Examination

Following the accident, an engine run was performed with the right fuel tank selected. No anomalies were noted during the engine run.

Contributing factors

Incorrect use/operationPilot