Engine Failure Following Propeller Damage Leads to Emergency Landing in Córdoba

Casualties unknown • Aeródromo Villa Rumipal (Cordoba), AR

A Tecnam P2008-JC experienced an engine shutdown during initial climb, forcing an emergency landing on unpaved terrain in Villa Rumipal, Argentina.

What happened

On December 28, 2023, a Tecnam P2008-JC, registered as LV-FQS, was conducting a general aviation pleasure flight departing from the Villa Rumipal – Primer Teniente Mario Nívoli Aerodrome in Córdoba. During the initial climb phase of the flight, the aircraft's propeller suffered a structural failure where a section of the blade separated. This mechanical failure caused the engine to stop functioning immediately.

Following the loss of engine power, the pilot was forced to perform an emergency landing in an unprepared area near the airfield. While the aircraft sustained significant damage and was destroyed during the impact, there were no fatalities or serious injuries reported among the two occupants on board.

The investigation

The investigation focused on the mechanical integrity of the propeller and the sequence of events leading to the engine shutdown. Investigators examined the aircraft's flight path during the climb and the condition of the propeller at the time of the separation. The inquiry established that the separation of a propeller section was the direct trigger for the engine's cessation of operation.

Probable cause

The engine failure was caused by the structural separation of a propeller section during the initial climb phase.

Frequently asked questions

What happened in the 2023-12-28 TECNAM P2008-JC accident near Aeródromo Villa Rumipal (Cordoba), AR?

A Tecnam P2008-JC experienced an engine shutdown during initial climb, forcing an emergency landing on unpaved terrain in Villa Rumipal, Argentina.

What aircraft was involved and where did it happen?

The accident on 2023-12-28 involved a TECNAM P2008-JC, registration LV-FQS, operated by Aviación General, at Aeródromo Villa Rumipal (Cordoba), AR.

What was the probable cause of the accident?

The engine failure was caused by the structural separation of a propeller section during the initial climb phase.

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