3 fatalities

In-Flight Cylinder Separation and Fire During Air Taxi Flight Leads to Crash Landing (N4839S)

Kenai, AK, US

On August 14, 1994, a Piper PA-32-260 (registration N4839S) was involved in an aviation accident near Kenai, AK. 3 people were killed. Investigators recorded the probable cause as: INADEQUATE ENGINE MAINTENANCE AND/OR INSPECTION, AND FATIGUE CRACKING OF THE ENGINE CASE, WHICH RESULTED IN EVENTUAL DAMAGE TO THE #3 CYLINDER STUDS/ENGINE THROUGH-BOLTS, SUBSEQUENT SEPARATION OF THE #3 CYLINDER AND PISTON, AND AN IN-FLIGHT FIRE. 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

During a Part 135 on-demand air taxi flight, the No. 3 cylinder and piston separated, causing an in-flight fire and subsequent crash landing near a shoreline. One of four occupants survived; maintenance records noted recent cylinder installation and engine inspection revealed fatigue cracks.

Accident Details

An airplane operating under Part 135 as an on-demand air taxi flight experienced a physical separation of the No. 3 cylinder and piston assembly while in flight. This event led to an in-flight fire. The aircraft subsequently crash landed on terrain near the shoreline of a body of water. Of the four occupants on board, one survived the crash. The surviving passenger was unable to recall the events leading up to the accident.

Maintenance History

Maintenance records indicated that the No. 3 and No. 4 cylinder assemblies had been installed approximately 220 flight hours before the accident. This maintenance was performed without removing the engine from the airplane. No problems with the airframe or engine were recorded following the cylinder change.

Engine Examination

Post-accident inspection of the engine revealed fatigue cracks in the engine case beneath the No. 3 cylinder. Magnified inspection of the case showed wear and deformation damage at the location where the cylinder's holding flange and inner skirt would normally be positioned, consistent with movement of the cylinder relative to the case. Additionally, mechanical damage was evident on the threads of the studs and both through-bolts.

Frequently asked questions

What happened in the 14 Aug 1994 Piper PA-32-260 accident near Kenai, AK?

During a Part 135 on-demand air taxi flight, the No. 3 cylinder and piston separated, causing an in-flight fire and subsequent crash landing near a shoreline. One of four occupants survived; maintenance records noted recent cylinder installation and engine inspection revealed fatigue cracks.

Were there any fatalities in the 14 Aug 1994 Piper PA-32-260 accident?

The accident was fatal, resulting in 3 fatalities.

What aircraft was involved and where did it happen?

The accident on 14 Aug 1994 involved a Piper PA-32-260, registration N4839S, at Kenai, AK.

What was the probable cause of the accident?

INADEQUATE ENGINE MAINTENANCE AND/OR INSPECTION, AND FATIGUE CRACKING OF THE ENGINE CASE, WHICH RESULTED IN EVENTUAL DAMAGE TO THE #3 CYLINDER STUDS/ENGINE THROUGH-BOLTS, SUBSEQUENT SEPARATION OF THE #3 CYLINDER AND PISTON, AND AN IN-FLIGHT FIRE.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001206X01900. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.