Casualties unknown

1994-05-05: Air Tractor AT-402 (N91966) — Sikeston, MO

Sikeston, MO, US

On May 5, 1994, an Air Tractor AT-402 (registration N91966) was involved in an aviation accident near Sikeston, MO. Investigators recorded the probable cause as: Failure of one compressor blade due to high cycle fatigue, which then resulted in further compressor and turbine blade damage in the engine, leading to a total loss of engine power. 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

Immediately after takeoff, a total loss of engine power occurred, and the airplane pitched nose down, contacting terrain off the left side of the runway. Investigation revealed a compressor blade failure due to high cycle fatigue, leading to further engine damage.

Incident Overview

The pilot reported that immediately after takeoff, a total loss of engine power occurred and the airplane pitched nose down. The airplane then contacted the terrain off the left side of the runway. At the time of the incident, the airplane was loaded with 340 gallons of a Prowl herbicide/water mixture, which spilled upon impact.

Inspection Findings

Post-incident inspection of the engine revealed a failure of one compressor blade. This failure was determined to have occurred due to high cycle fatigue. The initial compressor blade failure subsequently resulted in further damage to additional compressor and turbine blades within the engine.

Operational Circumstances

The airplane had been loaded with 340 gallons of a Prowl herbicide/water mixture for agricultural application. The mixture spilled when the airplane contacted the terrain. No further details regarding the specific aircraft type, registration, or pilot information were provided in the investigation source.

Probable cause

Failure of one compressor blade due to high cycle fatigue, which then resulted in further compressor and turbine blade damage in the engine, leading to a total loss of engine power.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001206X01229. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.