Tail rotor blade failure leads to Bell 47 crash near Mittelhäusern

Casualties unknown • Mittelhäusern, BE, CH

A Bell 47 G 3 B helicopter experienced a catastrophic tail rotor failure during engine idling, resulting in the death of the pilot.

What happened

On December 29, 1966, an Agusta Bell 47 G 3 B helicopter, registration HB-XCD, was performing field landing training near Mittelhäusern, Switzerland. The flight proceeded normally, and the pilot successfully completed a landing at approximately 16:15 local time. During the period following the landing, while the engine was running at idle, a loud noise was heard accompanied by a violent jolt that caused both cabin doors to fly open. The pilot immediately observed that the tail rotor had detached from the aircraft.

The investigation

Investigators examined the aircraft's maintenance history and identified a previous incident on April 13, 1966. During a mountain rescue mission at the Rottal glacier, the tail rotor had struck hard snow. While the tail rotor blades were inspected and the strike indicators were replaced, the blades themselves remained in service. Laboratory analysis of the broken blade revealed that the fracture was caused by material fatigue, a condition typical of blades that have previously impacted water, snow, or similar substances.

Findings

  • The primary cause of the accident was the fatigue failure of a tail rotor blade.
  • A previous strike against snow in April 1966 had introduced structural damage to the blades.
  • There was a conflict between manufacturer instructions regarding blade replacement: Agusta technical bulletin No. 97 mandated the replacement of both blades if strike indicators showed any bending, whereas Bell Helicopter Service Bulletin No. 1435 B allowed for continued use if no visible damage was found on skid-equipped helicopters.
  • Although the blades were inspected by technical staff, non-visible deformations persisted, leading to abnormal stresses that eventually caused the fatigue fracture.

Probable cause

The accident was caused by the fatigue failure of a tail rotor blade following a previous impact with snow, exacerbated by conflicting manufacturer maintenance instructions regarding the necessity of blade replacement after a strike.

Frequently asked questions

What happened in the 1966-12-29 COSTRUZIONI AERONAUTICHE GIOVANNI AGUSTA S.P.A. AB47G-3B accident near Mittelhäusern, BE, CH?

A Bell 47 G 3 B helicopter experienced a catastrophic tail rotor failure during engine idling, resulting in the death of the pilot.

What aircraft was involved and where did it happen?

The accident on 1966-12-29 involved a COSTRUZIONI AERONAUTICHE GIOVANNI AGUSTA S.P.A. AB47G-3B, registration HB-XCD, at Mittelhäusern, BE, CH.

What was the probable cause of the accident?

The accident was caused by the fatigue failure of a tail rotor blade following a previous impact with snow, exacerbated by conflicting manufacturer maintenance instructions regarding the necessity of blade replacement after a strike.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/369.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.

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