Engine Failure Due to Connecting Rod Fatigue Results in Forced Landing

Casualties unknown • Des Moines, IA, US

An aircraft experienced a total engine failure shortly after takeoff due to severe mechanical wear. The pilot executed a forced landing on private property, resulting in significant airframe damage.

What happened

The incident occurred shortly after the aircraft departed the airport and reached a cruise altitude of 3,500 feet mean sea level. During this phase of flight, the engine began to shudder violently. The pilot initiated a 180-degree course reversal to return to the departure airport but reported to air traffic control that visibility was obstructed because oil had been smeared across the aircraft's exterior surfaces.

After completing the turn, the engine lost all power. The pilot attempted a forced landing on a nearby farm. Upon contact with the lip of a fencerow, the landing gear separated from the airframe. The aircraft then traveled through a barbed wire fence, where the wings sustained damage from striking fence posts.

The investigation

A metallurgical examination was conducted on the failed engine components to determine the root cause of the mechanical failure. The analysis revealed that two connecting rods had failed due to high-stress fatigue. Additionally, three cam followers were found to have heads that were severely worn and suffered from heavy spalling damage.

Findings

The primary factor in this accident was the engine failure caused by internal component degradation. The severe wear of the cam followers and the subsequent fatigue failure of the connecting rods led to a total loss of power. This mechanical failure necessitated an emergency landing on unprepared terrain, which resulted in further damage to the aircraft structure.

Probable cause

The engine's total loss of power due to high-stress fatigue failure of two connecting rods and severe wear with heavy spalling damage to three cam followers.

Frequently asked questions

What happened in the 1984-07-30 Piper PA32R300 accident near Des Moines, IA?

An aircraft experienced a total engine failure shortly after takeoff due to severe mechanical wear. The pilot executed a forced landing on private property, resulting in significant airframe damage.

What aircraft was involved and where did it happen?

The accident on 1984-07-30 involved a Piper PA32R300, registration N1654H, at Des Moines, IA.

What was the probable cause of the accident?

The engine's total loss of power due to high-stress fatigue failure of two connecting rods and severe wear with heavy spalling damage to three cam followers.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001214X40414. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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