Casualties unknown

Emergency Landing After Engine Failure Results in Gear Collapse (N4593)

Chamerlain, SD, US

On July 25, 1984, a Grumman G-164A (registration N4593) was involved in an aviation accident near Chamerlain, SD. Investigators recorded the probable cause as: The engine cylinder separated due to improperly torqued stud bolts, which allowed an over-stress condition to exist on a few studs that were properly torqued. 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 2026-07-04Data APIEditorial standards

An aircraft experienced an engine failure and emergency landing on a narrow road. The landing gear touched down on a soft shoulder, causing gear failure and substantial damage. Investigation found the engine cylinder separated due to improperly torqued stud bolts.

Incident Overview

A pilot executed an emergency landing on a narrow road following an engine failure. During the landing, one of the landing gear touched down on the soft shoulder of the road. The landing gear subsequently failed, and the aircraft sustained substantial damage.

Engine Examination

Post-incident examination of the engine revealed that a cylinder had separated from the engine. The separation was caused by improperly torqued stud bolts. This condition allowed an over-stress condition to exist on a few studs that were properly torqued, leading to the cylinder failure.

Damage Assessment

The aircraft incurred substantial damage as a result of the landing gear collapse. No further details on the extent of damage were provided.

Investigation Findings

The investigation determined that the root cause of the engine failure was the improper torquing of stud bolts, which led to the cylinder separation. No other contributing factors were identified in the source material.

Probable cause

The engine cylinder separated due to improperly torqued stud bolts, which allowed an over-stress condition to exist on a few studs that were properly torqued.

Frequently asked questions

What happened in the 25 Jul 1984 Grumman G-164A accident near Chamerlain, SD?

An aircraft experienced an engine failure and emergency landing on a narrow road. The landing gear touched down on a soft shoulder, causing gear failure and substantial damage. Investigation found the engine cylinder separated due to improperly torqued stud bolts.

What aircraft was involved and where did it happen?

The accident on 25 Jul 1984 involved a Grumman G-164A, registration N4593, at Chamerlain, SD.

What was the probable cause of the accident?

The engine cylinder separated due to improperly torqued stud bolts, which allowed an over-stress condition to exist on a few studs that were properly torqued.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001214X40291. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.