No fatalities

Main Rotor Blade Strike on Tail Boom During Forced Landing of Robinson R44 Raven HB-ZCU

Selzach, SO, CH

On July 26, 2003, a ROBINSON HELICOPTER COMPANY R44 (registration HB-ZCU) was involved in an aviation accident near Selzach, SO, CH. No fatalities were reported. Investigators recorded the probable cause as: The accident is due to a main rotor blade striking the tail boom at the end of an autorotation. The autorotation was necessary because of engine power loss in cruise. This summary draws on records from the Swiss Transportation Safety Investigation Board (STSB / SUST).

Sourcesthe Swiss Transportation Safety Investigation Board (STSB / SUST)Primary reportUpdated 2026-10-18Data APIEditorial standards

On 26 July 2003, a Robinson R44 Raven helicopter, HB-ZCU, suffered an engine power loss due to a blocked exhaust valve and broken pushrod. During the ensuing autorotation, a main rotor blade struck the tail boom. The three occupants were uninjured.

Accident Overview

On 26 July 2003, at approximately 15:08 local time, a Robinson R44 Raven helicopter, registration HB-ZCU, was involved in an accident near Selzach, in the municipality of Grenchen, Solothurn, Switzerland, about 25 km north of Bern. The helicopter was on a private VFR flight with a pilot and two passengers on board.

Flight History

The flight originated from Sitterdorf at around 11:50. After a stop in Bern for refueling and a subsequent landing at Kernenried BE to exchange passengers, the helicopter departed Kernenried at approximately 14:45. The route took the pilot over several locations before contacting Grenchen control tower to request transit through the control zone towards Biel.

Engine Failure

While cruising at about 4500 ft AMSL and 80 kt, the pilot experienced low-frequency vibrations. The engine rpm gauge fluctuated, and the clutch warning light briefly illuminated. Despite reducing power and speed, the situation worsened. The helicopter began to oscillate abruptly around the vertical axis. As rotor rpm decreased, the low rpm warning light and horn activated, prompting the pilot to perform an autorotation.

Autorotation and Landing

During the autorotation, the pilot informed the tower of the emergency landing. In the final phase, the tail rotor protection skid contacted the ground. The helicopter landed with significant sink rate but negligible forward speed. At that moment, a main rotor blade struck the tail boom. After coming to rest, the pilot shut down the engine and applied the rotor brake. The occupants exited the helicopter uninjured. The helicopter sustained damage, and minor crop damage occurred from oil spillage, which was contained by police.

Cause

The investigation determined that the accident occurred because a main rotor blade struck the helicopter's tail boom at the end of an autorotation. The autorotation was necessitated by a loss of engine power during cruise flight. The engine failure resulted from a blocked exhaust valve in one cylinder and a broken pushrod.

Probable cause

The accident is due to a main rotor blade striking the tail boom at the end of an autorotation. The autorotation was necessary because of engine power loss in cruise. The engine problem occurred due to blockage of an exhaust valve in a cylinder and breakage of the pushrod.

Frequently asked questions

What happened in the 26 Jul 2003 ROBINSON HELICOPTER COMPANY R44 accident near Selzach, SO, CH?

On 26 July 2003, a Robinson R44 Raven helicopter, HB-ZCU, suffered an engine power loss due to a blocked exhaust valve and broken pushrod. During the ensuing autorotation, a main rotor blade struck the tail boom. The three occupants were uninjured.

Were there any fatalities in the 26 Jul 2003 ROBINSON HELICOPTER COMPANY R44 accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 26 Jul 2003 involved a ROBINSON HELICOPTER COMPANY R44, registration HB-ZCU, at Selzach, SO, CH.

What was the probable cause of the accident?

The accident is due to a main rotor blade striking the tail boom at the end of an autorotation. The autorotation was necessary because of engine power loss in cruise. The engine problem occurred due to blockage of an exhaust valve in a cylinder and breakage of the pushrod.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/1964_d.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.