Casualties unknown

Engine Failure Leads to Ditching in Hilo Bay (N4193)

Hilo, HI, US

On November 10, 1991, a Beech D18S (registration N4193) operated by Tomy International was involved in an aviation accident near Hilo, HI. Investigators recorded the probable cause as: THE AIRCRAFT'S LACK OF SINGLE ENGINE PERFORMANCE TO MAINTAIN ALTITUDE AFTER THE ENGINE LOST POWER. FACTORS RELATED TO THE ACCIDENT WERE: DISPLACEMENT/MECHANICAL INTERFERENCE WITHIN THE ACCESSORY DRIVE GEAR SYSTEM OF THE LEFT ENGINE, FAILURE OF THE LEFT 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 2026-06-10Data APIEditorial standards

An aircraft experienced left engine power fluctuations and subsequent loss of power, leading to a ditching in Hilo Bay. Post-accident examination revealed a failed accessory gear drive shaft and mechanical interference within the gear system.

Engine Failure and Ditching

Approximately 45 miles from landing, the left engine's revolutions per minute (RPM) began to fluctuate. When the aircraft was about 15 miles from landing, the engine lost power completely. The pilot reported that the aircraft could not maintain altitude. Unable to reach the runway, he ditched the aircraft in Hilo Bay, approximately one-quarter mile from shore and 1.5 miles from the airport.

Post-Recovery Examination

After the aircraft was retrieved, the airframe and left engine were examined. The accessory gear drive shaft was found to have failed in torsional overload. Inside the accessory gear case, an area of gouging and abrasion was located directly in front of the starter gear. The left magneto, fuel pump, and propeller governor were driven by the accessory drive gear.

Deep impressions were noted on approximately 70% of the gear teeth, with material displacement and gouging evident. There was evidence that the collector drive floating gear may have moved forward and contacted the engine case. Additionally, there was evidence of mechanical interference within the accessory drive gear system.

Weight at Time of Accident

The aircraft's gross weight at the time of the accident was about 9,108 pounds.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X18473. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.