Casualties unknown

Pilot Forced Landing After Engine Power Loss (N8501H)

Tuckerman, AR, US

On February 25, 2005, a Grumman G-164A (registration N8501H) was involved in an aviation accident near Tuckerman, AR. Investigators recorded the probable cause as: The pilot's forced landing due to sudden engine power loss caused by a cracked number nine cylinder head on the radial engine. 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 2026-06-19Data APIEditorial standards

A pilot with 10,000 hours experienced sudden engine power loss while maneuvering and executed a forced landing in a field where the aircraft nosed over.

What happened

The pilot, who held a total of 10,000 flight hours, was operating the aircraft during a maneuvering phase when the engine abruptly lost power. In response to the mechanical failure, the pilot initiated an emergency forced landing procedure targeting a nearby open field.

During the subsequent landing roll, the aircraft's main landing gear sank deeply into the muddy terrain. This loss of ground support caused the airplane to nose over, ultimately coming to rest in an inverted position on the ground.

The investigation

A thorough examination of the radial engine was conducted following the accident. The inspection revealed a significant structural failure within the powerplant. Specifically, the number nine cylinder head was found to be cracked in the area between both sparkplugs.

Findings

The sudden loss of engine power during the maneuvering phase was directly linked to the mechanical defect identified in the radial engine. The cracked cylinder head compromised the engine's ability to maintain power output, necessitating the emergency landing. The muddy conditions of the landing site contributed to the severity of the ground impact and the final inverted position of the aircraft.

Probable cause

The pilot's forced landing due to sudden engine power loss caused by a cracked number nine cylinder head on the radial engine.

Frequently asked questions

What happened in the 25 Feb 2005 Grumman G-164A accident near Tuckerman, AR?

A pilot with 10,000 hours experienced sudden engine power loss while maneuvering and executed a forced landing in a field where the aircraft nosed over.

What aircraft was involved and where did it happen?

The accident on 25 Feb 2005 involved a Grumman G-164A, registration N8501H, at Tuckerman, AR.

What was the probable cause of the accident?

The pilot's forced landing due to sudden engine power loss caused by a cracked number nine cylinder head on the radial engine.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20050328X00365. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.