Unrecoverable Spin During Flight Testing Leads to Aircraft Crash in Uherské Hradiště

Casualties unknown • Uherské Hradiště, CZ

A PS-28 Cruiser entered an unrecoverable spin during intentional spin testing, resulting in the aircraft crashing into a residential garden.

What happened

On June 17, 2013, a PS-28 Cruiser, registration OK-PSA, was conducting flight testing to verify its certification specifications for the CS-LSA category. The testing program, managed by Czech Sport Aircraft a.s., involved performing intentional spins to ensure safe recovery procedures for pilot training.

During the second flight of the day, the pilot initiated a left spin at approximately 10,331 ft. Following two rotations, the pilot attempted a standard recovery using rudder and elevator inputs. However, the aircraft failed to respond to these standard procedures. In an attempt to break the rotation, the pilot increased engine power, which likely transitioned the aircraft into a flat spin. During this phase, the engine subsequently failed, with data showing a sharp drop in engine RPM, fuel pressure, and oil pressure.

Despite further uncoordinated control inputs and the deployment of an anti-spin parachute, the rotation could not be arrested. The pilot eventually exited the aircraft via parachute at approximately 3,000 ft. The aircraft continued its uncontrolled descent, ultimately impacting a garden in the Mařatice district of Uherské Hradiště. The aircraft sustained heavy damage, but no injuries were reported on the ground.

The investigation

The ÚZPLN investigation examined the flight data recorder (FDR), engine monitoring systems (EMS), and electronic flight instrument system (EFIS) parameters. The investigators reviewed the aircraft's configuration, including recent structural changes to the fuel tanks designed to prevent fuel sloshing during high-G maneuvers. The investigation also analyzed the pilot's flight maneuvers, the effectiveness of the anti-spin parachute, and the circumstances surrounding the engine failure during the flat spin.

Probable cause

The investigation determined that the primary cause was the inability to recover from the left spin, likely due to insufficient rudder moment to stop the rotation at the aircraft's maximum weight and aft center of gravity. This was compounded by the transition into a flat spin following the use of engine power, which led to an engine failure—potentially caused by centrifugal forces disrupting fuel supply—and subsequent uncoordinated control inputs that failed to arrest the rotation.

Frequently asked questions

What happened in the 2013-06-17 PS-28 Cruiser accident near Uherské Hradiště, CZ?

A PS-28 Cruiser entered an unrecoverable spin during intentional spin testing, resulting in the aircraft crashing into a residential garden.

What aircraft was involved and where did it happen?

The accident on 2013-06-17 involved a PS-28 Cruiser, registration OK-PSA, at Uherské Hradiště, CZ.

What was the probable cause of the accident?

The investigation determined that the primary cause was the inability to recover from the left spin, likely due to insufficient rudder moment to stop the rotation at the aircraft's maximum weight and aft center of gravity. This was compounded by the transition into a flat spin following the use of engine power, which…

Investigation report by the Czech Air Accidents Investigation Institute (UZPLN). Original record: https://uzpln.gov.cz/incident/340. This page is a structured re-presentation; facts and quotes are in the Ustav pro odborne zjistovani pricin leteckych nehod (UZPLN), Czech Republic.

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