Casualties unknown

2004-05-17: Beech A36 (N4550S) — Robert G. Snyder — Morrisville, NC

Morrisville, NC, US

On May 17, 2004, a Beech A36 (registration N4550S) operated by Robert G. Snyder was involved in an aviation accident near Morrisville, NC. Investigators recorded the probable cause as: The failure of the engine for undetermined reasons resulting in the aircraft colliding with powerlines and the ground during the subsequent 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 flight from Daytona Beach to Wilmington and then Raleigh-Durham ended with an engine loss on approach. The pilot reported a problem and lost engine power seconds later. Wreckage showed severed fuel lines at wing roots but no other anomalies.

Flight Details

The flight departed Daytona Beach International Airport en route to Wilmington International Airport, where the passengers were to deplane. Before taking off from Daytona Beach, the pilot performed a visual inspection of the airplane, checked the fuel tanks, and verified that they were full. Two passengers stated that the flight from Daytona Beach to Wilmington lasted approximately two and a half hours.

Upon arriving in Wilmington, the pilot did not shut down the engine. He deplaned the passengers and continued the flight to Raleigh-Durham International Airport. The pilot established radio contact with the FAA Raleigh Approach Control and was provided flight following service for the flight.

Incident Sequence

When the flight arrived within range of the destination airport, the pilot was given radar vectors to the final approach course for runway 23L. A review of radar data showed that when the airplane was 1.37 miles from the runway, it was about 800 feet mean sea level. At the same time, the pilot reported to the controller that he had a problem. Seconds later, the pilot reported that he had lost his engine. This was the last radio transmission from the pilot.

Wreckage and Examination

Examination of the accident site revealed two broken power lines located along the wreckage path. The main wreckage was located inverted in a creek 4,800 feet on an extended centerline on the approach side for runway 23L. Postcrash examination and testing of the aircraft structure, flight controls, systems, engine, and propeller showed no evidence of precrash anomalies. The fuel lines were found severed at the wing roots.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20040524X00640. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.