Casualties unknown

2004-06-14: Piper PA 32R-301 (N8451E) — Richard Helminiak — Baxley, GA

Baxley, GA, US

On June 14, 2004, a Piper PA 32R-301 (registration N8451E) operated by Richard Helminiak was involved in an aviation accident near Baxley, GA. Investigators recorded the probable cause as: The mechanical malfunction of the autopilot pitch servo, and the pilot's inability to maintain adequate control pressure to manually retrim the pitch attitude. 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

After disengaging the autopilot, the pilot could not maintain pitch control, leading to uncontrollable gyrations and a collision with trees. Post-accident examination found the autopilot pitch servo only corrected in one direction and the pitch trim servo solenoid was out of specification.

Incident Overview

While flying at 2,300 feet, the pilot disengaged the autopilot. Immediately after disengagement, the pilot could not maintain pitch control, and the airplane entered a series of uncontrollable gyrations. Attempts to regain control were unsuccessful. The airplane subsequently collided with trees approximately five miles west of Baxley Municipal Airport.

Post-Accident Examination

A functional examination of the autopilot assembly after the accident revealed that when the unit was engaged, the pitch servo would only correct the pitch attitude in one direction. Internal examination of the pitch servo disclosed that three transistors had been replaced, and one transistor appeared to be original to the unit. Additionally, a functional check of the pitch trim servo solenoid showed that the unit was not within design specifications.

Pilot Operating Handbook Guidance

According to the pilot operating handbook, if the autopilot is disengaged when opposing mistrim forces are encountered, the pilot may be required to exert control forces in excess of 50 pounds to maintain airplane attitude. The handbook notes that the pilot must maintain this control force while manually retrimming the airplane.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20040616X00819. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.