Casualties unknown

Fuel Exhaustion Leads to Hard Landing After Engine Failure (N3692M)

Walls, MS, US

On June 24, 1997, a Piper PA-28-181 (registration N3692M) was involved in an aviation accident near Walls, MS. Investigators recorded the probable cause as: The poor in-flight planning by the pilot for her failure to divert to an alternate airport after recognizing that a low fuel quantity state existed when preflight and in-flight planning revealed sufficient fuel for the 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 experienced engine failure due to fuel exhaustion caused by a carburetor malfunction with excessive fuel flow and a leak, resulting in a hard landing in a field.

Flight History

The flight departed with full fuel tanks for a planned duration of 4 hours 33 minutes. Three hours and 36 minutes into the flight, approximately 49 nautical miles from the destination airport, the pilot requested to descend to 3,500 feet. According to the performance chart, the descent should have begun at 41.5 nautical miles. About 9 minutes later, the pilot noted that the fuel gauges were indicating low and descended to 1,800 feet. The flight continued for approximately 14 more minutes, after which the engine sputtered. The pilot repositioned the fuel selector and informed the air traffic controller, who vectored the airplane toward a nearby airport. Shortly thereafter, about 4 hours after takeoff, the engine quit completely. Unable to land at the vectored airport, the pilot selected a field, resulting in a hard landing.

Postcrash Examination

Examination of the airplane after the accident revealed fuel exhaustion. The carburetor was tested, and near the power setting used by the pilot during the cruise portion, the fuel flow was found to be 3.0 pounds per hour higher than expected. This was attributed to a failed spring inside the carburetor. The carburetor was 20 years and 4 months old and had never been overhauled since manufacture, although no mandatory requirement for overhaul existed. Additional examination of the carburetor showed evidence of a fuel leak due to one loose carburetor bowl-to-body screw.

Maintenance Background

The airplane had been inspected 5 days and 12 hours earlier in accordance with a 100-Hour inspection. However, the carburetor was not further examined during that inspection.

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Frequently asked questions

What happened in the 24 Jun 1997 Piper PA-28-181 accident near Walls, MS?

A pilot experienced engine failure due to fuel exhaustion caused by a carburetor malfunction with excessive fuel flow and a leak, resulting in a hard landing in a field.

What aircraft was involved and where did it happen?

The accident on 24 Jun 1997 involved a Piper PA-28-181, registration N3692M, at Walls, MS.

What was the probable cause of the accident?

The poor in-flight planning by the pilot for her failure to divert to an alternate airport after recognizing that a low fuel quantity state existed when preflight and in-flight planning revealed sufficient fuel for the flight. Contributing to the accident was the inadequate 100-Hour inspection of the airplane by…

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001208X08199. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.