Casualties unknown

Pilot Encounters Windshear, Control Wheel Breaks During Go-Around (N4075R)

Austin, NV, US

On March 16, 1992, a Piper PA-32-300 (registration N4075R) operated by Galen M. Reimer was involved in an aviation accident near Austin, NV. Investigators recorded the probable cause as: THE PILOT'S LOSS OF CONTROL DUE TO THE FAILURE OF HIS CONTROL WHEEL DURING AN ATTEMPTED GO AROUND. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-07-04Data APIEditorial standards

During a go-around after encountering windshear and a downdraft on short final, the left-side plastic control wheel broke in half. The aircraft hit the ground hard and veered off the runway. Inspection showed no crack existed at the last annual inspection per AD 69-22-2.

Incident Details

According to the pilot, while on short final to the airstrip, the aircraft encountered a windshear and downdraft. The pilot added power to initiate a go-around. During this maneuver, the plastic control wheel on the left side of the cockpit broke into two sections at its midpoint. The aircraft then struck the ground hard and veered off the runway.

Pilot Actions

The pilot stated that after the left control wheel failed, he attempted to control the aircraft by grabbing the wheel on the right side of the cockpit. However, the aircraft hit the ground and he lost directional control.

Maintenance History

The plastic control wheels installed in this model are subject to a recurring Airworthiness Directive (AD 69-22-2). This AD mandates repetitive dye penetrant inspections at each annual inspection to detect cracks in the center of the wheel. Review of the maintenance records showed that the control wheel had been inspected in accordance with the AD at the last annual inspection.

Examination Findings

A microscopic examination of the fracture face revealed no evidence of dye penetrant. This indicates that the crack did not exist at the time of the last inspection.

Conclusion

The investigation documented the sequence of events and the results of the post-accident examination. No probable cause was determined from the available information.

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Frequently asked questions

What happened in the 16 Mar 1992 Piper PA-32-300 accident near Austin, NV?

During a go-around after encountering windshear and a downdraft on short final, the left-side plastic control wheel broke in half. The aircraft hit the ground hard and veered off the runway. Inspection showed no crack existed at the last annual inspection per AD 69-22-2.

What aircraft was involved and where did it happen?

The accident on 16 Mar 1992 involved a Piper PA-32-300, registration N4075R, operated by Galen M. Reimer, at Austin, NV.

What was the probable cause of the accident?

THE PILOT'S LOSS OF CONTROL DUE TO THE FAILURE OF HIS CONTROL WHEEL DURING AN ATTEMPTED GO AROUND.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X14324. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.