Casualties unknown

Engine Vibration and Partial Power Loss Lead to Crash Landing (N3413R)

Ardmore, OK, US

On September 2, 1994, a Cessna 182L (registration N3413R) operated by Soloman W. Ward was involved in an aviation accident near Ardmore, OK. Investigators recorded the probable cause as: THE PARTIAL LOSS OF POWER DUE TO A CYLINDER HEAD SEPARATION. FACTORS WERE THE LACK OF SUITABLE TERRAIN FOR THE FORCED LANDING AND THE LOW CEILING. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

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

An aircraft experienced severe engine vibration and partial power loss while VFR-on-top. After an IFR descent, it struck wires and crash-landed inverted in a pasture, damaging the left wing spar, horizontal stabilizer, and a separated cylinder head.

Event Summary

While operating VFR-on-top for approximately 10 minutes, the aircraft's engine began producing a severe vibration and partial power was lost. The pilot declared an emergency and received weather conditions and a heading to the Industrial Air Park (ADM) in Ardmore, Texas, from Flight Service. The pilot then contacted Fort Worth Center and initiated an IFR descent through the clouds.

Descent and Landing

Upon exiting the clouds at about 400 feet above ground level, the aircraft was unable to maintain altitude. During the continued descent, it struck electrical wires and made a crash landing into a small mowed pasture. The airplane rolled approximately 300 feet before entering a vast depression, passed through a persimmon thicket, and came to rest inverted.

Damage Examination

An examination of the aircraft revealed damage to the left wing spar and left horizontal stabilizer. Additionally, a cylinder head had separated from the barrel.

Frequently asked questions

What happened in the 2 Sept 1994 Cessna 182L accident near Ardmore, OK?

An aircraft experienced severe engine vibration and partial power loss while VFR-on-top. After an IFR descent, it struck wires and crash-landed inverted in a pasture, damaging the left wing spar, horizontal stabilizer, and a separated cylinder head.

What aircraft was involved and where did it happen?

The accident on 2 Sept 1994 involved a Cessna 182L, registration N3413R, operated by Soloman W. Ward, at Ardmore, OK.

What was the probable cause of the accident?

THE PARTIAL LOSS OF POWER DUE TO A CYLINDER HEAD SEPARATION. FACTORS WERE THE LACK OF SUITABLE TERRAIN FOR THE FORCED LANDING AND THE LOW CEILING.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001206X02244. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.