Casualties unknown

2002-12-09: Piper PA-28-161 (N2588Y) — Falcon Executive Aviation — Scottsdale, AZ

Scottsdale, AZ, US

On December 9, 2002, a Piper PA-28-161 (registration N2588Y) operated by Falcon Executive Aviation was involved in an aviation accident near Scottsdale, AZ. Investigators recorded the probable cause as: The pilot's inadequate preflight inspection and failure to refuel the airplane resulting in a loss of engine power due to fuel starvation. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 10 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

An airplane experienced engine power loss during initial climb. The pilot attempted to land on a street, engine briefly recovered, then quit again. He landed in a parking lot, striking a light pole. Fuel exhaustion was indicated.

Event Details

The airplane lost engine power during the takeoff initial climb. The pilot described the power loss as smooth, without vibration or roughness. With insufficient runway remaining, he set up for a landing on a street. During the approach, the engine power returned. He then attempted to turn back to the runway, but the engine quit again. The pilot subsequently landed the airplane in a parking lot, where the left wing struck a light pole.

Preflight Fuel Status

Prior to the accident flight, the airplane had been fueled to the tabs (34 usable gallons) and flown for 2.4 hours by another individual. After that flight, the airplane was rented to the accident pilot. The operator's policy was to fuel their airplanes to the tabs after each flight. The accident pilot reported visually checking the fuel during his preflight and observing that it was "at or slightly below the tabs." He also noted that the fuel gauge readings appeared consistent with his visual observations. An airplane fueler reported that he asked the pilot if he needed fuel, and the pilot responded that he was "good" and did not need any.

Flight and Fuel Management

The pilot departed and switched fuel tank positions every half hour during the flight. The airplane was flown for 2.3 hours from the start of the accident flight until engine power was lost. Post-accident documentation found the fuel selector in the left tank position. Three gallons of fuel were found in the right wing tank, and zero gallons were found in the left wing tank. There was no evidence of fuel leakage or staining on the asphalt under the airplane.

Fuel Consumption Analysis

The airplane had been flown for a total of 4.7 hours after being fueled to the tabs. It burns 6.6 gallons per hour (gph) at 55 percent power. At this power setting, the calculated fuel burn for the two combined flights was 31 gallons, leaving 3 gallons remaining in the tanks. These calculations were based on cruise performance only.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20021211X05596. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.