Casualties unknown

1986-01-18: Cessna 310G (N8983Z) — Ragland, AL

Ragland, AL, US

On January 18, 1986, a Cessna 310G (registration N8983Z) was involved in an aviation accident near Ragland, AL. Investigators recorded the probable cause as: The in-flight separation of the horizontal tail surfaces while the aircraft was circling in low overcast conditions. 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 training aircraft experienced in-flight separation of its horizontal tail surfaces while circling in low overcast conditions. The student pilot had no instrument experience, and the flight duration matched the aircraft's total endurance.

What happened

An aircraft was observed circling overhead in low overcast skies with sputtering engines before a catastrophic structural failure occurred. During this phase of flight, the horizontal tail surfaces separated from the airframe. The debris field was extensive, with the tail components coming to rest approximately 450 feet from the main wreckage in mountainous terrain.

The flight had been airborne for approximately 3.6 hours. This duration coincided exactly with the aircraft's total flight endurance from takeoff, suggesting the engines were operating at or near their operational limits. The pilot involved was a student who possessed no instrument flying experience, yet was conducting operations in conditions that required such proficiency.

The investigation

Examination of the accident site revealed the significant separation of the horizontal tail surfaces from the main fuselage. The location of the debris, scattered across difficult mountainous terrain, indicated a loss of control following the structural failure. The sputtering engines noted prior to the separation suggest potential mechanical distress or fuel system issues contributing to the flight's termination.

Findings

The accident involved a student pilot with no instrument experience operating in low overcast conditions. The aircraft had been flying for its maximum endurance time of 3.6 hours. The primary failure mode was the in-flight separation of the horizontal tail surfaces, which led to the loss of the aircraft in mountainous terrain.

Probable cause

The in-flight separation of the horizontal tail surfaces while the aircraft was circling in low overcast conditions.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20010110X00104. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.