Casualties unknown

Tail Rotor Blade Separation Due to Fatigue Crack During Cruise Flight (N3893S)

Eugene Is. 313, US

On June 9, 1999, a Bell 412 (registration N3893S) was involved in an aviation accident near Eugene Is. 313. Investigators recorded the probable cause as: Fatigue crack in the tail rotor blade spar. 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

A helicopter experienced a tail rotor blade separation during cruise flight due to a fatigue crack. The pilots regained control and deployed emergency floats before impacting the ocean.

Incident Summary

During cruise flight, one of the tail rotor blades separated from the helicopter. The pilots reported hearing a 'loud bang,' after which the helicopter 'immediately and violently tucked down and left then rolled inverted and [was] spinning to the right.' The flying pilot righted the helicopter, and the non-flying pilot inflated the emergency floats prior to impacting the ocean.

Examination Findings

The outboard section of one of the tail rotor blades was recovered and examined. Investigators found that a fatigue crack had initiated in the spar in an 'area of round-bottomed corrosion pits 0.001 inch deep.' The two tail rotor blades installed on the helicopter had accumulated 4,644 and 4,913 hours, respectively. The tail rotor blades are life limited at 5,000 hours.

Probable cause

Fatigue crack in the tail rotor blade spar

Frequently asked questions

What happened in the 9 Jun 1999 Bell 412 accident near Eugene Is. 313?

A helicopter experienced a tail rotor blade separation during cruise flight due to a fatigue crack. The pilots regained control and deployed emergency floats before impacting the ocean.

What aircraft was involved and where did it happen?

The accident on 9 Jun 1999 involved a Bell 412, registration N3893S, at Eugene Is. 313.

What was the probable cause of the accident?

Fatigue crack in the tail rotor blade spar

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X18996. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.