Casualties unknown

1997-04-12: Cessna T210N (N5310A) — Vichy, MO

Vichy, MO, US

On April 12, 1997, a Cessna T210N (registration N5310A) was involved in an aviation accident near Vichy, MO. Investigators recorded the probable cause as: failure of the pilot to properly follow the missed approach procedure and maintain the minimum descent altitude (MDA) during night/IFR flight. 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

An aircraft departed Butler, PA, and attempted a VOR approach in low visibility. The pilot descended below approach minimums and crashed about half a mile northwest of the airport.

Flight and Weather Information

The aircraft was fueled to capacity and departed Butler, Pennsylvania, at approximately 1652 Eastern Daylight Time. Before departure, the pilot was advised that the destination weather consisted of 1/4 mile visibility in fog, a 200-foot overcast ceiling, and wind from 350 degrees at 6 mph. The airport elevation was 1,148 feet.

Approach and Descent

The approach minimums for the VOR Runway 22 approach were a minimum descent altitude (MDA) of 1,500 feet, with a required ceiling of 400 feet and prevailing visibility of 3/4 mile. The pilot continued the approach and descended below these minimums.

Passenger Account

A passenger, who survived the accident, reported that the airport was covered with fog. The passenger observed the altimeter indicating 1,300 feet mean sea level (msl) and stated that the pilot then applied power and turned toward the north. The missed approach procedure called for climbing to 2,700 feet msl, then turning right direct to the VIH VOR/DME and holding.

Impact and Wreckage Inspection

The airplane struck trees and came to rest approximately 1/2 mile northwest of the airport. The crash site elevation was about 1,125 feet. Post-impact inspection of the wreckage revealed that full flaps had been selected and the landing gear was extended. Go-around flaps were set at 20 degrees. The three propeller blades exhibited chordwise gouges and scratches, and the tips showed forward twisting. No anomalies were found in the engine or airframe.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001208X07671. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.