Forced Landing Following Loss of Aileron Control

Casualties unknown • Glen Allan, MS, US

A pilot performed an emergency forced landing in a field after the aircraft became uncontrollable due to mechanical failure in the left aileron control assembly.

What happened

While surveying a field for potential future work, the pilot experienced a loss of control of the aircraft. In response to the loss of controllability, the pilot selected an emergency landing area and executed a forced landing in a field. During the landing sequence, the left wing struck the ground, causing the aircraft to cartwheel and sustain significant structural damage.

The pilot was not injured during the event.

The investigation

An examination of the aircraft focused on the left aileron control mechanism. Investigators found that the bolt used to secure the left aileron to the control surface had separated from the assembly. Upon removal of the aileron, the missing bolt was located within the inter-structure of the wing area.

Further inspection of the bolt assembly revealed that the bolt connecting the forward end of the control rod to the bell crank was too short; it failed to protrude sufficiently through the nylon lock nut. Additionally, the investigation determined that the rod-end bearing was seized and unable to move.

Probable cause

The loss of control was caused by a failure in the left aileron control assembly, specifically involving a bolt that separated from the control surface and a short bolt at the bell crank connection, compounded by a seized rod-end bearing.

Frequently asked questions

What happened in the 1999-06-19 Cessna A188B accident near Glen Allan, MS?

A pilot performed an emergency forced landing in a field after the aircraft became uncontrollable due to mechanical failure in the left aileron control assembly.

What aircraft was involved and where did it happen?

The accident on 1999-06-19 involved a Cessna A188B, registration N53198, operated by Michael Lewis, at Glen Allan, MS.

What was the probable cause of the accident?

The loss of control was caused by a failure in the left aileron control assembly, specifically involving a bolt that separated from the control surface and a short bolt at the bell crank connection, compounded by a seized rod-end bearing.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X18926. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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