Casualties unknown

Forced Landing Following Fuel Leak and Possible Fuel Exhaustion (N6303C)

Prescott, AZ, US

On September 17, 2000, a Piper PA-28-161 (registration N6303C) was involved in an aviation accident near Prescott, AZ. Investigators recorded the probable cause as: An improper engine installation by other maintenance personnel that resulted in a fuel leak at the main fuel line fitting to the carburetor and subsequent fuel exhaustion during cruise flight. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 4 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-07-04Data APIEditorial standards

A pilot made a forced landing after the engine lost power, later revealing a fuel leak at the carburetor fitting. The pilot reported running out of fuel, but no fuel was found at the scene, and a long-term leak was discovered.

Incident Overview

A pilot executed a forced landing in an open field after experiencing a loss of engine power. The aircraft collided with desert shrubs and came to rest inverted. The pilot had refueled to maximum tank capacity before departure and calculated an en route time of 4 hours 15 minutes to the planned refueling stop. Approximately 4 hours 10 minutes into the flight, while near the destination airport, the engine ceased operation.

Pilot Actions

Contacting the local tower, the pilot reported being out of fuel and intending to land on a highway. To avoid oncoming traffic, the pilot maneuvered and ultimately landed in a brush-covered field.

Post-Landing Examination

Responding personnel observed no fuel odor or visible fuel on the aircraft or ground. Mechanical continuity within the engine was established during an examination. With the fuel pump activated, a fuel leak was identified at the fuel line fitting where it enters the carburetor. The leak rate, with only the boost pump on, was measured at one drop per minute. Heavy fuel staining was noted on the carburetor bowl below the bowl seal gasket, around the line fitting, and on induction hoses directly below. The stain residue was thick and consistent with a long-term leak.

Maintenance History

Review of maintenance logbooks revealed that the engine had been reinstalled after an overhaul approximately eight days prior to the flight. A subsequent ground run using a remote fuel source attached to the left wing's fuel fitting showed no discrepancies at full power.

Aircraft Fuel Specifications

According to the manufacturer, the aircraft holds 48 gallons of fuel, of which 4 gallons are unusable. The Airplane Flight Manual's range/cruise performance charts indicate a best power fuel consumption of 9.0 gallons per hour at 65 percent power and 10.5 gallons per hour at 75 percent power. Endurance at 65 percent power is listed as 5.5 hours.

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Frequently asked questions

What happened in the 17 Sept 2000 Piper PA-28-161 accident near Prescott, AZ?

A pilot made a forced landing after the engine lost power, later revealing a fuel leak at the carburetor fitting. The pilot reported running out of fuel, but no fuel was found at the scene, and a long-term leak was discovered.

What aircraft was involved and where did it happen?

The accident on 17 Sept 2000 involved a Piper PA-28-161, registration N6303C, at Prescott, AZ.

What was the probable cause of the accident?

An improper engine installation by other maintenance personnel that resulted in a fuel leak at the main fuel line fitting to the carburetor and subsequent fuel exhaustion during cruise flight.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X22016. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.