Casualties unknown

2024-06-30: TECNAM, P2006T (SP-LFA) — LOT Flight Academy — Sochaczew, PL

Sochaczew, PL

On June 30, 2024, a TECNAM, P2006T (registration SP-LFA) operated by LOT Flight Academy was involved in an aviation accident near Sochaczew, PL. Investigators recorded the probable cause as: Coolant leak from the cooling system due to a damaged pump shaft seal, resulting in left engine cylinder temperature exceeding limits. This summary draws on records from the Polish State Commission on Aircraft Accidents Investigation (PKBWL); 7 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
Aircraft registered SP-LFA
Aircraft registered SP-LFA. Photo: Nanowski Jakub - EPGD Spotters / Public domain, via Wikimedia Commons

On 30 June 2024, a Tecnam P2006T experienced a coolant leak leading to left engine overtemperature during a training flight. The crew shut down the engine and landed safely at EPPT without further incident.

Event Narrative

On 30 June 2024, a training flight for the Instrument Rating (IR(A)) was conducted using a Tecnam P2006T aircraft, registration SP-LFA, operated by Polska Akademia Lotnicza Sp. z o.o. The crew consisted of an instructor and a student pilot. The flight departed from EPPT airport, performed IFR procedures with an approach at EPMO, and began the return to EPPT.

At approximately 11:10 local time, while cruising at 3,000 feet AMSL, the left engine cylinder temperature (CT) exceeded 120°C. Following the Abnormal/Emergency Procedures from the Standard Operating Procedures, the crew shut down the left engine. At about 11:15, the Crew Alerting System indicated low coolant level. The crew executed the corresponding abnormal procedure. After assessing the situation, they declared PAN PAN to FIS Warszawa, confirmed their intention to continue to EPPT, and notified the airport information service at EPPT. The flight coordinator secured the airport and separated other traffic. The aircraft landed at EPPT at 11:47 without further consequences.

Findings

Examination after the incident revealed that the cooling system pump had a damaged seal on its shaft. The rubber sealing ring had worn out naturally, leading to a coolant leak. This leak caused the left engine cylinder temperature to rise above the normal operating range of 50–120°C.

Cause

The direct cause of the event was a coolant leak and loss of fluid from the cooling system, which resulted in elevated left engine cylinder temperature.

Contributing Factors

A contributing factor was the deterioration of the pump shaft seal due to natural wear of the rubber sealing ring, identified after the pump was disassembled.

Probable cause

Coolant leak from the cooling system due to a damaged pump shaft seal, resulting in left engine cylinder temperature exceeding limits.

Investigation report by the Polish State Commission on Aircraft Accidents Investigation (PKBWL). Original record: https://pkbwl.gov.pl/raporty/2024-0046/. This page is a structured re-presentation; facts and quotes are in the Panstwowa Komisja Badania Wypadkow Lotniczych (PKBWL), Poland.