Engine power loss during takeoff leads to autorotative landing in Osiek

Casualties unknown • Osiek / Brodnica, PL

A pilot of a Xenon 2 RST autogyro was forced to perform an emergency autorotative landing near Osiek after experiencing a significant engine power loss during takeoff.

What happened

On August 13, 2016, at approximately 16:30 local time, a pilot initiated a takeoff from a landing strip located approximately 150 meters south of the runway in Osiek, Poland. The flight was planned to proceed from Osiek to the Toruń Aero Club airfield (EPTO). The takeoff proceeded normally until the aircraft reached an altitude of approximately 300 ft AGL.

After roughly two minutes of operation at takeoff power, the pilot experienced a significant loss of engine power. To avoid obstacles, the pilot executed an emergency landing via autorotation, altering the flight path approximately 40 degrees to the left of the original takeoff heading. The Xenon 2 RST landed in a cornfield at the edge of a meadow with minimal forward speed. The pilot sustained no injuries.

The investigation

The investigation focused on the sudden loss of engine performance during the climb phase. Following the incident, the aircraft was moved to a hangar in Osiek. Local police conducted a breathalyzer test on the pilot, which returned a negative result for alcohol. The pilot was found to be fully qualified, with 1,280 flight hours logged on this specific aircraft type.

Post-incident inspections of the aircraft revealed minor damage, including a slight bend in the landing gear and a cracked landing light cover. The engine was subsequently sent to the manufacturer for a detailed examination. During testing, the engine operated normally without any detectable malfunctions, and the manufacturer issued a certificate of airworthiness for its continued use.

Findings

  • The primary cause of the incident was a significant loss of engine power during the climb.
  • The manufacturer was unable to determine the specific cause of the power loss, as the engine functioned correctly during subsequent testing.
  • Meteorological conditions were clear with no cloud cover and winds from 270 degrees at 3–5 m/s; weather conditions did not contribute to the event.

Probable cause

The incident was caused by a significant reduction in engine power during the takeoff climb, the underlying cause of which could not be identified by the manufacturer during subsequent testing.

Frequently asked questions

What happened in the 2016-08-13 Xenon 2 RST accident near Osiek / Brodnica, PL?

A pilot of a Xenon 2 RST autogyro was forced to perform an emergency autorotative landing near Osiek after experiencing a significant engine power loss during takeoff.

What aircraft was involved and where did it happen?

The accident on 2016-08-13 involved a Xenon 2 RST, at Osiek / Brodnica, PL.

What was the probable cause of the accident?

The incident was caused by a significant reduction in engine power during the takeoff climb, the underlying cause of which could not be identified by the manufacturer during subsequent testing.

Investigation report by the Polish State Commission on Aircraft Accidents Investigation (PKBWL). Original record: https://pkbwl.gov.pl/raporty/2016-2130/. This page is a structured re-presentation; facts and quotes are in the Panstwowa Komisja Badania Wypadkow Lotniczych (PKBWL), Poland.

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