Casualties unknown

2019-01-16: ROBINSON HELICOPTER COMPANY R44 (HB-ZDW) — Luzern-Beromünster Flugplatz (LSZO), LU, CH

Luzern-Beromünster Flugplatz (LSZO), LU, CH

On January 16, 2019, a ROBINSON HELICOPTER COMPANY R44 (registration HB-ZDW) was involved in an aviation accident near Luzern-Beromünster Flugplatz (LSZO), LU, CH. 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
Aircraft registered HB-ZDW
Aircraft registered HB-ZDW. Photo: Peter Gronemann from Switzerland / CC BY 2.0, via Wikimedia Commons

On 16 January 2019, a Robinson R44 helicopter experienced an engine failure during initial climb. The pilot executed an autorotation back to the airport, but the helicopter tipped over after landing on soft ground. All four occupants were uninjured.

Accident Overview

On 16 January 2019, at 11:29 local time, a Robinson R44 Raven I helicopter, registration HB-ZDW, experienced an engine failure shortly after departing from Luzern Beromünster Airport (LSZO). The helicopter was on a private VFR flight with one pilot and three passengers. During the initial climb, the pilot perceived a sudden left yaw, followed by a low rotor RPM warning. The pilot immediately lowered the collective and initiated an autorotation, turning back towards the airfield.

Flight History

After routine pre-flight preparations, the pilot started the engine and allowed it to warm up with carburetor heat fully open. A hover check revealed no anomalies. At 11:26, the pilot began the takeoff on runway 33. During the climb check, the pilot again fully opened the carburetor heat to compensate for reduced heating when pulling collective. The helicopter reached about 2800 ft MSL (650 ft above aerodrome elevation) and 70 kt when the engine failed. The pilot autorotated back to the airfield, touching down approximately 100 meters past the threshold of the glider runway 33. The left skid sank into soft ground, causing the helicopter to rotate 90 degrees left, tip over onto its right side, and come to rest on its side. All occupants exited unaided and uninjured. The helicopter was substantially damaged.

Technical Findings

Post-accident examination found no pre-existing malfunctions that could have caused the engine failure. The fuel system functioned correctly, and no water or contamination was detected. Laboratory analysis of fuel showed a mixture of AVGAS 100LL with a small amount of unleaded automotive gasoline, within allowable limits. The engine was test-run and operated within normal parameters. The ignition switch showed high wear but remained functional; wiring was intact. The investigation could not determine the cause of the engine failure. Carburetor icing was considered unlikely because carburetor heat had been fully applied.

Outcome

The pilot successfully performed an autorotation and returned to the airport, but the helicopter tipped over during the landing roll due to soft ground. The cause of the engine failure remains undetermined.

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