Casualties unknown

Engine Failure and Forced Landing Results in Nose-Over During Off-Airport Landing (N2725G)

Gillette, WY, US

On September 6, 2004, a Cessna 182 (registration N2725G) was involved in an aviation accident near Gillette, WY. Investigators recorded the probable cause as: improper engine overhaul performed by the mechanic which resulted in the fractured exhaust valve and subsequent partial loss of engine power. Contributing to the accident was the lack of suitable terrain for a forced landing. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-07-04Data APIEditorial standards

During cruise, the engine ran rough with grinding metal sounds and violent shaking. The pilot shut down and attempted a forced landing in a plowed field, where a nose wheel rut impact separated the tire, causing the airplane to nose over and sustain substantial damage.

The Incident

The pilot reported that while in cruise flight, the engine began to run rough. Shortly thereafter, he heard sounds of grinding metal and the engine started shaking violently. He shut the engine down and initiated a forced landing to a plowed field.

Forced Landing and Damage

During the forced landing, the nose wheel impacted a small rut, which caused the nose landing gear tire to separate from the assembly. The airplane nosed over, resulting in substantial damage to the aircraft.

Engine Examination

An internal examination of the engine revealed that the number 3 piston, piston rings, tension springs, and the number 3 exhaust valve head had fragmented into numerous pieces. These pieces were found in the oil sump. The crankcase halves showed impact damage in areas aft of the number 4 piston and forward of the number 3 piston. The top inside of the number 3 cylinder head exhibited multiple impact marks, including a 7/8-inch long, 1/8-inch wide, and 1/8-inch deep indentation at one of the spark plug openings, and a 1/2-inch long, 1/8-inch wide, and 1/8-inch deep indentation at the area of the exhaust valve seat. These marks were consistent with a valve head edge impact. The number 3 exhaust valve seat was missing.

Additional Findings

The number 3 exhaust valve stem was removed and examined. Fractures observed on the valve stem were consistent with an overload failure. The number 3 exhaust valve guide showed elongating distortion. Examination of the crankshaft, camshaft, other cylinders, pistons, valves, and valve springs revealed no pre-existing failures. No evidence of the number 3 exhaust valve seat was found among the fractured pieces in the engine. Examination of the remaining airplane systems revealed no anomalies.

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Frequently asked questions

What happened in the 6 Sept 2004 Cessna 182 accident near Gillette, WY?

During cruise, the engine ran rough with grinding metal sounds and violent shaking. The pilot shut down and attempted a forced landing in a plowed field, where a nose wheel rut impact separated the tire, causing the airplane to nose over and sustain substantial damage.

What aircraft was involved and where did it happen?

The accident on 6 Sept 2004 involved a Cessna 182, registration N2725G, at Gillette, WY.

What was the probable cause of the accident?

improper engine overhaul performed by the mechanic which resulted in the fractured exhaust valve and subsequent partial loss of engine power. Contributing to the accident was the lack of suitable terrain for a forced landing.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20040908X01357. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.