Casualties unknown

2004-10-30: Beech A36 (N55448) — Downing, MO

Downing, MO, US

On October 30, 2004, a Beech A36 (registration N55448) was involved in an aviation accident near Downing, MO. Investigators recorded the probable cause as: The aircraft entered thunderstorm activity and struck the terrain during a right bank turn, resulting in structural failure and impact. 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 private pilot and two passengers were killed when their aircraft entered thunderstorm activity and struck the terrain, resulting in a post-impact fire.

What happened

At approximately 20:27, an instrument-rated private pilot established radio communications with an air traffic controller at an Air Route Traffic Control Center radar position. During this exchange, the controller provided the current altimeter setting. Shortly thereafter, the controller observed the aircraft enter an area of weather.

At approximately 20:36, the air traffic controller notified the pilot that radar contact had been lost. The pilot did not respond, and no further radio communications were established with the flight. A witness, a commercial pilot, reported seeing the aircraft emerge from clouds, attempt a recovery, strike the ground, and immediately burst into flames.

The accident resulted in 3 fatal injuries to the pilot and two passengers. The aircraft was destroyed upon impact with the terrain and by a post-impact fire.

The investigation

Radar data from the National Track Analysis Program, plotted on Doppler weather radar reflectivity depictions, indicated that the aircraft entered an area of weather consistent with level three to level four thunderstorm activity. While surface observations indicated VFR weather was present, the flight encountered severe convective activity.

An on-scene examination of the wreckage was conducted. Investigators examined a gyroscope and its housing from a flight instrument, which revealed rotational scoring. The turn coordinator was found destroyed, and its face indicated the aircraft was in a right bank turn at the time of the event.

A section of the right wingtip was located near a ground scar, and the navigation light on that wingtip contained green media. The left wing was found detached from the fuselage. An inspection of the control cables showed all breaks were consistent with structural overload. No pre-impact anomalies were detected in the airframe or engine.

Probable cause

The aircraft entered thunderstorm activity and struck the terrain during a right bank turn, resulting in structural failure and impact.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20041103X01745. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.