Casualties unknown

2000-03-22: Cessna 310C (N3311H) — Cedar City, UT

Cedar City, UT, US

On March 22, 2000, a Cessna 310C (registration N3311H) was involved in an aviation accident near Cedar City, UT. Investigators recorded the probable cause as: The failure of the right engine mixture control cable, which prevented the pilot from restarting the engine. Contributing factors were the pilot's failure to follow procedures by not feathering the right propeller, the rough terrain, and the high vegetation. 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 instructor shut down the right engine for single-engine practice. Restart attempts failed due to a mixture control cable failure. The propeller was not feathered, and left engine power was insufficient. A gear-down landing was made in rough, brush-covered desert terrain. Two airfields were within 5 miles.

Incident Overview

A flight instructor intentionally shut down the right engine of the airplane to practice single-engine flight. Subsequent attempts to restart the engine were unsuccessful; later examination determined that the mixture control cable had failed. The pilot did not feather the right engine, and reported that the left engine was providing insufficient power to maintain flight. The instructor executed a gear-down landing in rough, brush-covered desert terrain.

Flight Details

According to the owner of the airplane, the practice engine shutdown was performed at 9,500 feet mean sea level, approximately 3,800 feet above the terrain. The owner stated that the practice maneuver was not initiated over a landing airfield, but that two airfields were available within 5 miles of that location.

Performance Considerations

The airplane's Owner's Manual performance section indicates that the single-engine best rate of climb ranges from 50 feet per minute to 250 feet per minute, depending on altitude and outside air temperature. A representative from the manufacturer noted that a non-feathered propeller would reduce the rate of climb by approximately 400 feet per minute, and that having the landing gear extended would reduce it an additional 300 feet per minute.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X20621. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.