Casualties unknown

1998-10-28: Piper PA-32R-300 (N8554C) — Roswell, GA

Roswell, GA, US

On October 28, 1998, a Piper PA-32R-300 (registration N8554C) was involved in an aviation accident near Roswell, GA. Investigators recorded the probable cause as: A loss of engine power due to the failure of the number five connecting rod assembly as a result of fatigue cracks that were initiated in areas of galling. A factor 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.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

A commercial pilot reported a sudden loss of engine oil pressure and vibration, leading to a forced landing on a highway. The aircraft struck two vehicles and caught fire, injuring the pilot seriously and fatally injuring the driver. Post-crash examination revealed a fractured connecting rod with fatigue cracks.

Incident Overview

While transiting the Atlanta area, a commercial pilot reported a sudden loss of engine oil pressure and a subsequent severe vibration to Atlanta Approach Control. Approach Control vectored the flight toward Dekalb-Peachtree Airport for an emergency landing. Due to the loss of power, the pilot was unable to maintain altitude and was forced to land on a highway.

Emergency Landing and Collision

The pilot left the airplane in the cruise configuration and landed with the wheels and flaps retracted. Upon landing, the aircraft slid on the road, contacting a Jeep Cherokee, then impacting a Mazda 626. After the impact with the Mazda, the aircraft and the automobile caught fire, destroying both. The pilot sustained serious injuries, while the driver of the automobile was fatally injured.

Engine Examination

During a post-crash disassembly of the engine, the number five connecting rod was found fractured through the rod shoulder. A metallurgical examination revealed that the connecting rod had fatigue cracks originating at or near areas of galling. Connecting rods are routinely re-used following inspections for evidence of galling. The engine had operated to within about 60 hours of its recommended time between overhauls, with the broken rod installed.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X11196. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.