Casualties unknown

2007-12-08: Cessna T210N (N5431C) — Henry D. Garretson — Bloomfield, KY

Bloomfield, KY, US

On December 8, 2007, a Cessna T210N (registration N5431C) operated by Henry D. Garretson was involved in an aviation accident near Bloomfield, KY. Investigators recorded the probable cause as: the pilot exceeded the design stress limits of the airplane, which resulted in the in-flight break up. Contributing to the accident was the pilot's loss of control in-flight due to spatial disorientation. 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

Radar data shows an airplane descending at 650 ft/min, turning north with a maximum bank of 40-50 degrees, then exceeding structural cruise speed by 20 knots before breaking up. Weather suggests possible entry into instrument conditions.

Radar Data

Review of recorded radar data indicated that the airplane was heading northwest toward its destination airport while descending through an altitude of 6,800 feet mean sea level (msl) at a consistent rate of approximately 650 feet per minute. At that point, the airplane began a shallow turn to the north. Approximately 32 seconds later, the airplane continued turning and descending at a steady rate, reaching a maximum bank angle between 40 and 50 degrees. The airplane exceeded its structural cruise speed by 20 knots calibrated airspeed, which was 13 knots below the never exceed speed. Trajectory calculations showed that the airplane broke apart about 5 seconds after reaching that speed. The debris field was oriented in a southeasterly direction and was located close to the last three radar returns.

Weather

A weather study based on available data at the time of the accident indicated that the airplane was likely in visual meteorological conditions until just before the breakup. However, with cloud tops reaching 13,000 feet, the possibility existed that the airplane entered instrument meteorological conditions.

Wreckage Examination

All fracture surfaces examined on the wreckage displayed features consistent with static overload. No evidence of metal fatigue was found on any of the examined surfaces.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20071218X01970. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.