Casualties unknown

1997-05-08: Cessna T210 (N7398M) — Winona, MN

Winona, MN, US

On May 8, 1997, a Cessna T210 (registration N7398M) was involved in an aviation accident near Winona, MN. Investigators recorded the probable cause as: Installation of incorrect pistons (part number 648045 with a compression ratio of 8.5:1 instead of the specified part number 648044 with a compression ratio of 7:1) during the engine overhaul on July 30, 1996. 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 pilot experienced engine power loss and made an uneventful forced landing. Post-flight inspection revealed wrong pistons installed during a previous overhaul.

Incident Summary

About half an hour into the flight, while cruising at 8,000 feet MSL, the engine momentarily missed and then resumed normal operation. Shortly thereafter, the engine power decreased to 20 inches of manifold pressure. The pilot informed Air Traffic Control of the situation and requested vectors to the nearest airport, which was 8 miles away. Despite attempts to re-establish engine power, the pilot was unable to restore full performance. The aircraft reached the airport, but the engine lost all power during the final approach. The pilot executed an uneventful forced landing on the runway.

Engine Inspection Findings

Following the incident, an inspection of the engine revealed that the wrong pistons had been installed during an overhaul performed on July 30, 1996. The specified pistons were part number 648044, which correspond to a compression ratio of 7:1. However, the pistons found installed were part number 648045, which have a compression ratio of 8.5:1. This discrepancy likely contributed to the engine power loss.

Probable cause

Installation of incorrect pistons (part number 648045 with a compression ratio of 8.5:1 instead of the specified part number 648044 with a compression ratio of 7:1) during the engine overhaul on July 30, 1996.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001208X07862. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.