Casualties unknown

2024-07-23: Embraer - ERJ190-200-200LR (SP-LNB) — PLL LOT — Na trasie LSZH - EPWA, PL

Na trasie LSZH - EPWA, PL

On July 23, 2024, an Embraer - ERJ190-200-200LR (registration SP-LNB) operated by PLL LOT was involved in an aviation accident near Na trasie LSZH - EPWA, PL. Investigators recorded the probable cause as: Malfunction of the Flap/Slat Control System. This summary draws on records from the Polish State Commission on Aircraft Accidents Investigation (PKBWL); 5 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-LNB
Aircraft registered SP-LNB. Photo: Janusz Jakubowski from Warsaw, Poland / CC BY 2.0, via Wikimedia Commons

On 23 July 2024, an Embraer E195LR (SP-LNB) experienced a SLAT FAIL message after departure from Zurich. The crew followed procedures and continued to Warsaw, landing safely with adequate fuel reserves.

Event Sequence

On 23 July 2024, after departure from Zurich Airport (ZRH), an Embraer E195LR (registration SP-LNB) was climbing in FLAP 1 configuration and before acceleration began, a SLAT FAIL message appeared. In accordance with the SLAT/FLAP FAILURE procedure, the crew consulted the Quick Reference Handbook (QRH) and executed the required checklist. Despite completing all prescribed actions, the malfunction persisted. The crew then assessed the limitations from the QRH and evaluated fuel consumption with flaps and slats in the 1+3 position. They decided to continue the flight to the intended destination, Warsaw Chopin Airport (EPWA). The remainder of the flight proceeded without further issues, and after landing, the remaining fuel was 2100 kg.

Relevant Information

The QRH operational limitations allowed continued flight at altitudes no higher than FL200 and required landing approaches at Vref FULL + 20. For the SLAT/FLAP FAILURE condition, the calculated required landing distance was 1390 meters. The aircraft was flown with flaps and slats in the 1+3 position and at speeds below 230 knots. Fuel analysis showed that the available fuel was sufficient for safe continuation to the destination while maintaining the minimum required diversion reserve of 1800 kg.

Conclusions

The investigating commission determined that the actions taken were in accordance with established procedures and that no safety threat occurred. The cause of the incident was a malfunction of the Flap/Slat Control System.

Probable cause

Malfunction of the Flap/Slat Control System.

Investigation report by the Polish State Commission on Aircraft Accidents Investigation (PKBWL). Original record: https://pkbwl.gov.pl/raporty/2024-0068/. This page is a structured re-presentation; facts and quotes are in the Panstwowa Komisja Badania Wypadkow Lotniczych (PKBWL), Poland.