Casualties unknown

Propeller Blade Separation Shortly After Rotation Due to Damaged Retention Nut (N4235D)

Kent, WA, US

On August 18, 1987, a Beech G35 (registration N4235D) was involved in an aviation accident near Kent, WA. Investigators recorded the probable cause as: The separation of the blade from the hub was the result of the use of the severely damaged blade retention nut in the overhauled propeller. 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

Shortly after rotation, a propeller blade separated from the aircraft, followed by the hub assembly and remaining blade. The pilot landed straight ahead on the remaining runway. The hub had been overhauled 7 hours before. Metallurgical examination found a severely damaged blade retention nut caused the separation.

Accident Overview

Shortly after rotation during takeoff, a propeller blade separated from the aircraft. The remaining propeller hub assembly and the other blade also subsequently fell from the aircraft. The pilot was able to land the aircraft straight ahead on the remaining runway.

Maintenance History

The propeller hub had undergone overhaul just 7 hours before the accident.

Investigation Findings

Metallurgical examination of the propellers and hub assembly revealed that the separation of the blade from the hub was the result of the use of a severely damaged blade retention nut in the overhauled propeller.

Probable cause

The separation of the blade from the hub was the result of the use of the severely damaged blade retention nut in the overhauled propeller.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001213X31940. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.