Casualties unknown

1998-10-28: Cessna 152 (N25037) — Douglasville, GA

Douglasville, GA, US

On October 28, 1998, a Cessna 152 (registration N25037) was involved in an aviation accident near Douglasville, GA. Investigators recorded the probable cause as: Failure of the no. 1 cylinder exhaust valve guide due to erosion, which resulted in separation of the exhaust valve head, loss of engine power, and collision with a power pole during a forced landing on unsuitable terrain. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 8 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 aircraft experienced engine power loss during flight and conducted a forced landing in a field, during which it struck a power pole and came to rest on a pile of railroad ties. Postcrash examination found erosion and separation of the exhaust valve components, though the cause of the erosion was not determined.

Incident Overview

During a flight, the engine lost power, prompting the pilot to attempt a forced landing in an open field. During the landing, the aircraft collided with a power pole and subsequently came to rest on top of a pile of railroad ties. The specific aircraft type, registration, operator, and location were not disclosed in the report.

Postcrash Examination

A postcrash examination of the engine revealed significant damage to the number 1 cylinder exhaust valve assembly. The valve guide and valve stem were eroded. Further inspection showed that the valve guide had partially separated due to progressive cracking, and the valve head had separated from the stem. The reason for the erosion of the valve stem and guide could not be determined from the examination.

Engine Maintenance History

The engine had accumulated 2,225 flight hours since its last major overhaul. During that overhaul, the valves and valve guides were replaced with new parts. The manufacturer's recommended time between overhauls for this engine model is 2,400 flight hours, meaning the engine was still within the recommended service interval at the time of the incident.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X11315. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.