Casualties unknown

Engine Connecting Rod Fatigue Leads to Forced Landing and Post-Impact Fire (N80237)

Houstonia, MO, US

On September 18, 2004, a Cessna 172M (registration N80237) operated by Kenneth T. Conlee was involved in an aviation accident near Houstonia, MO. Investigators recorded the probable cause as: Fatigue cracking of the number 4 connecting rod at the forging parting plane, which initiated at multiple sites and extended through approximately 60% of the wall thickness. 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 airplane cartwheeled during a forced landing in a bean field after engine power loss. Investigation revealed fatigue cracking in the number 4 connecting rod, which originated at the forging parting plane.

Incident Overview

The airplane sustained impact and fire damage when it cartwheeled during a forced landing following a loss of engine power. According to the pilot, approximately 30 minutes into the flight, he heard a "clunk," after which the engine stopped running and the propeller was not windmilling. The pilot attempted to restart the engine without success. During an off-airport landing attempt in a bean field, the right wing contacted the ground, causing the airplane to cartwheel, and a post-impact fire ensued.

Engine Examination

Inspection of the engine revealed that the piston and piston pin on the number 4 cylinder were separated from the connecting rod. A metallurgical examination of the number 4 connecting rod determined that the piston pin end of the rod was fractured and the fractured ends were deformed inward. The fractured surface exhibited an area typical of a fatigue crack that originated at the forging parting plane on the exterior surface. The fatigue origin areas contained ratchet marks, indicating that fatigue cracking initiated at multiple sites and extended through approximately 60% of the wall thickness.

Maintenance History

The engine, a Lycoming O-320-E2D, was overhauled on August 11, 2003, at an engine total time of 3,918.7 hours. The engine had accumulated approximately 70 hours since the overhaul. Maintenance records indicate that during the overhaul, the connecting rods were magnafluxed, rebushed, checked for alignment, and reinstalled. The connecting rods were the original engine rods.

Probable cause

Fatigue cracking of the number 4 connecting rod at the forging parting plane, which initiated at multiple sites and extended through approximately 60% of the wall thickness.

Frequently asked questions

What happened in the 18 Sept 2004 Cessna 172M accident near Houstonia, MO?

An airplane cartwheeled during a forced landing in a bean field after engine power loss. Investigation revealed fatigue cracking in the number 4 connecting rod, which originated at the forging parting plane.

What aircraft was involved and where did it happen?

The accident on 18 Sept 2004 involved a Cessna 172M, registration N80237, operated by Kenneth T. Conlee, at Houstonia, MO.

What was the probable cause of the accident?

Fatigue cracking of the number 4 connecting rod at the forging parting plane, which initiated at multiple sites and extended through approximately 60% of the wall thickness.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20040929X01527. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.