Casualties unknown

Agricultural Airplane Destroyed in Forced Landing Following Gear Collapse (N57616)

Osborne, KS, US

On August 5, 2000, a Piper PA-36-285 (registration N57616) was involved in an aviation accident near Osborne, KS. Investigators recorded the probable cause as: The unsuitable terrain for landing encountered by the pilot during the forced landing. Factors were the failure of the number four piston and cylinder, the soft terrain, and the main landing gear overload and subsequent collapse. 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 2026-06-10Data APIEditorial standards

An agricultural airplane was destroyed after a gear collapse during a forced landing following spraying operations. The pilot sustained fatal injuries. Examination revealed engine failure due to an overstressed intake valve, and seat belt/shoulder harness separations with tensile overload signatures.

Accident Description

An agricultural airplane was destroyed when it impacted terrain during a forced landing following a gear collapse. The airplane was returning from spraying operations when the accident occurred. The wreckage came to rest in a soft farm field of wheat stubble.

Pilot and Restraint System

The pilot was fatally injured in the accident. Examination of the restraint system revealed that the seat belt cable and shoulder harness cable had separated. The separated areas exhibited signatures consistent with tensile overload. The pilot was not wearing a helmet, and the manual control for the shoulder harness inertia reel was found in the unlocked position.

Engine Examination

Post-accident examination of the engine found that the number four cylinder was compromised. A portion of the piston pin was protruding through a hole in the cylinder wall. Examination of the number four piston and intake valve revealed that the valve failed due to overstress. Portions of the piston skirt had fractured and separated from the piston. The fracture surfaces on the piston contained severe mechanical damage that obscured the fracture surface features. One side of the piston skirt exhibited damage consistent with the piston rotating about the piston pin and the connecting rod impacting the skirt.

Additional Findings

No other anomalies were found that could be associated with a preexisting condition.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X21671. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.