Casualties unknown

Piper aircraft lands inverted after engine failure (N25SK)

Burlington, CO, US

On July 31, 1996, a Grumman G-164A (registration N25SK) operated by Ron Seelhoff was involved in an aviation accident near Burlington, CO. Investigators recorded the probable cause as: The structural failure of the number 5 cylinder due to cracking, which resulted in an in-flight loss of engine power. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-10Data APIEditorial standards

A pilot returning from agricultural spraying experienced sudden engine power loss, resulting in a forced landing in an alfalfa field where the aircraft overturned.

What happened

The pilot was operating the aircraft during an agricultural application mission. While returning to base after completing a field spraying operation, the engine suddenly lost power without warning. The pilot immediately initiated emergency procedures for a forced landing, selecting an adjacent alfalfa field as the landing site.

During the descent and touchdown sequence, the left main landing gear struck a ditch within the field. This impact caused the aircraft to roll over, coming to rest in an inverted position on its roof. The force of the rollover resulted in significant structural damage to the airframe.

The investigation

An FAA inspector arrived at the scene shortly after the accident to examine the wreckage and the aircraft components. A detailed visual inspection of the engine revealed a critical defect. Investigators identified a distinct crack located on the bottom surface of the number 5 cylinder. This mechanical failure was consistent with the reported sudden loss of power during flight.

Findings

The investigation determined that the primary factor leading to the accident was the structural failure of the engine component. The crack in the cylinder likely caused an immediate and total loss of engine operation, leaving the pilot with no option other than a forced landing. The subsequent impact with the ditch and the resulting rollover were direct consequences of the emergency landing conditions.

Probable cause

The structural failure of the number 5 cylinder due to cracking, which resulted in an in-flight loss of engine power.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001208X06247. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.