Casualties unknown

2003-11-24: Cessna 340A (N200GC) — Poplar Bluff, MO

Poplar Bluff, MO, US

On November 24, 2003, a Cessna 340A (registration N200GC) was involved in an aviation accident near Poplar Bluff, MO. Investigators recorded the probable cause as: Failure to maintain directional control during landing. Collapse of the nose landing gear, the muddy grass/turf and the berm were contributing factors. 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 twin-engine airplane sustained substantial damage after departing the runway during landing. The pilot reported a loss of right rudder control on short final, but post-accident inspection found no pre-impact anomalies.

Accident Overview

A twin-engine airplane was substantially damaged during a landing attempt on runway 36. The aircraft departed the runway and its nose landing gear collapsed after encountering soft, muddy turf adjacent to the runway. The aircraft subsequently impacted a berm.

Pilot Report

The pilot stated that the flight was normal until short final, just prior to touchdown. He reported wind from 320 degrees at 6 knots. When he attempted to align the nose of the aircraft with the runway for touchdown, he had no right rudder control. The pilot observed that the right rudder pedal was fully deflected to the right and he was unable to move it back to the normal position with his foot.

After touchdown, the aircraft veered to the left. The pilot tried to correct to the right without success. He attempted differential power to maintain runway alignment but was unable. He reduced power to idle and maneuvered as best he could while having no right rudder control. Once the aircraft came to a complete stop, it was shut down.

Post-Accident Inspection

A post-accident inspection confirmed rudder control continuity and brake system integrity. Full rudder travel without restriction or binding was observed. Rudder pedal inputs produced proper, corresponding rudder movement. No anomalies with the nose wheel steering system that could be attributed to a pre-impact malfunction were observed. The brake system appeared intact and operated normally.

Conclusion

The aircraft departed the runway during landing, resulting in substantial damage. The pilot reported a loss of right rudder control prior to touchdown, but no mechanical cause was identified during post-accident inspection.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20031205X02002. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.