Casualties unknown

2012-08-17: Cirrus SR22 — Poznań Ławica (EPPO), PL

Poznań Ławica (EPPO), PL

On August 17, 2012, a Cirrus SR22 was involved in an aviation accident near Poznań Ławica (EPPO), PL. Investigators recorded the probable cause as: The pilot reduced fuel flow to the value indicated in the POH while maintaining disproportionately high manifold pressure, leading to rough engine operation. This summary draws on records from the Polish State Commission on Aircraft Accidents Investigation (PKBWL); 8 related events involving the same aircraft type or operator are linked below.

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

On 17 August 2012, a Cirrus SR22 experienced rough engine operation after the pilot adjusted the fuel mixture per the POH but maintained high manifold pressure. The pilot returned to Poznań-Ławica and landed safely. Investigation attributed the issue to the incorrect mixture setting.

Incident Overview

On 17 August 2012, a Cirrus SR22 operated by a single professional pilot with a Commercial Pilot License (CPL(A)) experienced an in-flight engine irregularity shortly after departing from Poznań-Ławica Airport (EPPO). The pilot, who had accumulated approximately 1200 flight hours including 300 hours on type, was conducting a cross-country flight.

Sequence of Events

After reaching cruise altitude, the pilot performed a mixture leaning procedure in accordance with the Pilot's Operating Handbook (POH) to achieve an economy cruise setting. Immediately after leaning, the engine began running rough. In response, the pilot enriched the mixture, initiated a descent, and returned to the departure airport. As no further anomalies occurred, a normal landing was executed without incident.

Investigation Findings

Post-flight analysis of the engine monitor data revealed no abnormalities. A subsequent in-depth analysis involving a service station in Schönhagen, Germany, determined that the pilot had reduced the fuel flow to the value specified in the POH while simultaneously maintaining a disproportionately high manifold pressure. This combination caused the engine to run unevenly. The pilot had aimed to achieve a turbine inlet temperature (TIT) of 1600°F or lower, which the operator had recommended as an additional verification step rather than a target parameter. The investigation classified the pilot's action as a piloting technique error that did not pose a safety risk, noting that the pilot's decision to return and land given the concerning symptoms was correct.

Cause

The incident was caused by the pilot reducing fuel flow to the POH-indicated value while maintaining a disproportionately high manifold pressure, leading to rough engine operation.

Preventive Actions

Following the incident, the pilot received additional training on thermodynamic parameter dependencies for engines. The event was discussed during a periodic safety meeting of the operator's flight department.

Probable cause

The pilot reduced fuel flow to the value indicated in the POH while maintaining disproportionately high manifold pressure, leading to rough engine operation.

Investigation report by the Polish State Commission on Aircraft Accidents Investigation (PKBWL). Original record: https://pkbwl.gov.pl/raporty/2012-1001/. This page is a structured re-presentation; facts and quotes are in the Panstwowa Komisja Badania Wypadkow Lotniczych (PKBWL), Poland.