Casualties unknown

Propeller Clamp Failure Prevents Feathering After Engine Malfunction (N4072P)

Atlanta, GA, US

On June 14, 1982, a Piper PA-23-160 (registration N4072P) operated by Mark Hewlett was involved in an aviation accident near Atlanta, GA. Investigators recorded the probable cause as: The right engine propeller retaining clamp failed from high cycle fatigue, preventing feathering of the propeller blade. 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 2026-06-10Data APIEditorial standards

After takeoff, a loud noise and sparks from the right engine prompted an attempted feathering that failed. The aircraft descended into trees and came to rest on a house roof, later catching fire. Investigation found a propeller retaining clamp failed from high cycle fatigue.

Incident Overview

Shortly after takeoff, the aircrew heard a loud noise and observed sparks coming from the right side of the right engine. They attempted to feather the right engine, but it would not respond. Unable to maintain altitude, the aircraft descended into trees. After striking the trees, the aircraft came to rest on the roof of a house. Approximately 5 to 10 minutes after the crash, the aircraft burst into flames. A police officer who had responded and climbed onto the roof was reportedly thrown off by an explosion, sustaining minor injuries.

Examination Findings

An examination of the right engine revealed that one blade of the model HC-82XG propeller did not feather and was free to move. The retaining clamp on this blade was cracked and had a portion missing. A metallurgical examination determined that the clamp had failed from high cycle fatigue. Hartzell Propeller Service Bulletin No. 126, dated December 9, 1980, recommended that this old model clamp be replaced by a new improved type. No other preimpact failures were found.

Probable cause

The right engine propeller retaining clamp failed from high cycle fatigue, preventing feathering of the propeller blade.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20020917X02839. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.