Casualties unknown

2007-10-02: KAMAN AEROSPACE CORPORATION K-1200 (HB-ZEH) — Illgau, SZ, CH

Illgau, SZ, CH

On October 2, 2007, a KAMAN AEROSPACE CORPORATION K-1200 (registration HB-ZEH) was involved in an aviation accident near Illgau, SZ, CH. Investigators recorded the probable cause as: The accident is due to a turbine failure at a height from which it was not possible to successfully carry out autorotation. The distinctive signs of a turbine failure had not been addressed consistently. This summary draws on records from the Swiss Transportation Safety Investigation Board (STSB / SUST).

Sourcesthe Swiss Transportation Safety Investigation Board (STSB / SUST)Primary reportUpdated 1785034239Data APIEditorial standards

On 2 October 2007, a K-1200 K-MAX helicopter (HB-ZEH) operated by Eagle Helicopter AG suffered a turbine failure near Strit, Illgau, Switzerland. The accident was attributed to the failure occurring at a height from which successful autorotation was not possible; warning signs were not adequately addressed.

Aircraft and Operator

The accident involved a K-1200 K-MAX helicopter, registration HB-ZEH. This type is a single-engine heavy-lift helicopter known for its external load capabilities. The aircraft was operated by Eagle Helicopter AG, and its maintenance was entrusted to RUAG Aviation.

Accident Circumstances

On 2 October 2007, the helicopter was conducting a flight in the area of Strit, within the municipality of Illgau in the canton of Schwyz, Switzerland. The local time was Central European Summer Time (UTC+2). During the flight, the engine, a Honeywell T5317A-1 turbine, experienced a failure. The helicopter was at an altitude from which a successful autorotation—the emergency landing technique without engine power—could not be accomplished.

Investigation Findings

The Swiss Accident Investigation Board (SUST) investigated the accident under the provisions of Annex 13 to the International Civil Aviation Organization (ICAO) convention. The investigation included a detailed examination of the wreckage, the engine, and its accessories. The fuel control unit, oil pump, starter/generator, and the N1 accessory drive gearbox were inspected. The examination revealed damage to the bevel gear teeth and bearing wear. The cause of the turbine failure was determined to be a mechanical issue that led to a loss of engine power. The investigation also found that the distinctive signs indicating an impending turbine failure—such as those from the chip detection system—had not been addressed consistently.

Probable Cause

According to the final report, the accident was caused by a turbine failure at a height from which it was not possible to successfully carry out autorotation. Additionally, the distinctive signs of a turbine failure had not been addressed consistently.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/2142_d.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.