Casualties unknown

2016-08-27: CESSNA, 152 — Urzędów, PL

Urzędów, PL

On August 27, 2016, a CESSNA, 152 was involved in an aviation accident near Urzędów, PL. Investigators recorded the probable cause as: The likely cause of the failure was the loosening of the connecting rod foot nut, resulting in the shearing of the second bolt, disconnecting the connecting rod from the crankshaft at the crank of the third cylinder, which locked the crankshaft-connecting… This summary draws on records from the Polish State Commission on Aircraft Accidents Investigation (PKBWL).

Sourcesthe Polish State Commission on Aircraft Accidents Investigation (PKBWL)Primary reportUpdated 1785092869Data APIEditorial standards

A Cessna 152 experienced a significant power loss and engine vibrations during a training flight near Kraśnik, Poland, on 27 August 2016. The pilot executed a precautionary landing in unprepared terrain with no injuries or aircraft damage.

Incident Overview

On 27 August 2016, a Cessna 152 departed on a training flight from EPLR to EPML. The pilot, holding a valid SEP(L) rating and Class 2 medical, planned the cross-country at an altitude of 2800 ft AMSL under VFR in VMC conditions during the afternoon.

Flight and Engine Failure

Approximately 20 minutes into the flight, near the town of Kraśnik, the pilot observed a substantial loss of engine power accompanied by vibrations. Simultaneously, the oil temperature gauge indicated a sudden rise beyond the maximum allowable limit. The pilot notified FIS Warszawa of the engine problem.

Precautionary Landing

Deciding to perform a precautionary landing, the pilot selected an unprepared field. The landing was successful: the airframe sustained no damage, and the sole occupant—the pilot—was uninjured. Meteorological conditions were not a factor in the event.

Probable Cause

The investigation identified the likely cause of the engine failure: the loosening of the connecting rod foot nut, which led to the shearing of a second bolt. This resulted in the disconnection of the connecting rod from the crankshaft at the crank of the third cylinder, ultimately locking the crankshaft-connecting rod-cylinder assembly.

Investigation report by the Polish State Commission on Aircraft Accidents Investigation (PKBWL). Original record: https://pkbwl.gov.pl/raporty/2016-2257/. This page is a structured re-presentation; facts and quotes are in the Panstwowa Komisja Badania Wypadkow Lotniczych (PKBWL), Poland.