Casualties unknown

Engine Failure Results in Forced Landing and Impact with Airport Fence (N4142F)

Indianapolis, IN, US

On June 9, 2000, a Piper PA-28-181 (registration N4142F) was involved in an aviation accident near Indianapolis, IN. Investigators recorded the probable cause as: The improper in-flight decision of the pilot not to land at the nearest airport at the first loss of engine power. Factors to the accident were fuel exhaustion, the excessive fuel flow, and the airport perimeter fence. 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

During cruise, the engine quit multiple times, culminating in a forced landing during which the aircraft struck the perimeter fence of the destination airport. Post-accident examination found no fuel in the fuel system.

Accident Sequence

The flight originated from Greenwood Municipal Airport (HFY) in Greenwood, Indiana, with a planned round trip to Waukegan Regional Airport (UGN) in Waukegan, Illinois. While in cruise flight approximately 10 miles from the destination airport, the engine ceased operation. The pilot successfully restarted the engine by switching to the alternate fuel tank. Subsequently, the engine experienced two more power losses before becoming unable to restart. The final power loss occurred about 2 miles from the destination airport. The pilot initiated a forced landing but was unable to reach Runway 19, and the aircraft impacted the airport perimeter fence during the approach.

Fuel Consumption Calculations

According to the pilot, he planned for a fuel consumption rate of 10 gallons per hour, yielding an estimated endurance of 4 hours and 48 minutes. The total trip duration, recorded by the pilot's GPS unit, was 3 hours and 52 minutes. The aircraft's Hobbs meter indicated 3.9 hours had elapsed since initial departure from HFY. The pilot reported an engine cruise setting of 2,350 rpm with mixture leaned at cruising altitude. The Pilot Operating Handbook for the aircraft specifies a fuel flow of 9.5 gallons per hour at 65% maximum power, with a maximum usable fuel capacity of 48 gallons. Using the 48-gallon capacity and the 3.9-hour flight time, the calculated fuel flow is approximately 12.307 gallons per hour.

Post-Accident Findings

Following the accident, investigators examined the fuel system. No fuel was found in the fuel strainer bowl, the fuel line leading to the carburetor, or the fuel filter located on the electric fuel pump. The pilot reported that the first engine power interruption occurred approximately 10 miles north of the destination airport. Notably, Post-Air Airport (7L8) in Indianapolis, Indiana, is located 8.1 nautical miles from the destination airport at a magnetic bearing of 028.4°.

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Frequently asked questions

What happened in the 9 Jun 2000 Piper PA-28-181 accident near Indianapolis, IN?

During cruise, the engine quit multiple times, culminating in a forced landing during which the aircraft struck the perimeter fence of the destination airport. Post-accident examination found no fuel in the fuel system.

What aircraft was involved and where did it happen?

The accident on 9 Jun 2000 involved a Piper PA-28-181, registration N4142F, at Indianapolis, IN.

What was the probable cause of the accident?

The improper in-flight decision of the pilot not to land at the nearest airport at the first loss of engine power. Factors to the accident were fuel exhaustion, the excessive fuel flow, and the airport perimeter fence.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X21176. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.