Engine failure and tailpipe fire involving Airbus A321 at Geneva Airport

Casualties unknown • Genève Aéroport (LSGG), GE, CH

An Airbus A321 experienced an engine failure and tailpipe fire during its approach to Geneva, leading to an emergency stop on a taxiway and passenger evacuation.

What happened

On 20 February 2001, a Swissair Airbus A321-111, registration HB-IOC, was operating a scheduled commercial flight from London Heathrow to Geneva. During the cruise phase at FL290, the flight and cabin crews heard a loud bang. While engine parameters initially appeared normal, the situation deteriorated during the descent into Geneva.

As the aircraft approached runway 05, the crew noted increasing and fluctuating vibrations and Exhaust Gas Temperature (EGT) in the right-hand engine. A loss of engine power occurred, requiring corrective rudder input. During the landing and flare, a crew member positioned near the runway observed flames emanating from the engine. Following the landing, an "ENG #2 OIL FILTER CLOGGED" warning illuminated, prompting the crew to shut down the right engine.

Upon instruction from Geneva Apron, the aircraft stopped on a taxiway. The crew discharged both engine fire extinguisher bottles, and the fire brigade arrived to cool the engine. Once the fire was extinguished and the engine cooled, the captain directed passengers to disembark via stairs on the taxiway. There were no injuries among the 85 passengers or 7 crew members.

Probable cause

The incident was caused by the mechanical failure of bearing number 4 in the number 2 engine, which subsequently damaged the high-pressure turbine blade tips.

Frequently asked questions

What happened in the 2001-02-19 AIRBUS INDUSTRIE A321-111 accident near Genève Aéroport (LSGG), GE, CH?

An Airbus A321 experienced an engine failure and tailpipe fire during its approach to Geneva, leading to an emergency stop on a taxiway and passenger evacuation.

What aircraft was involved and where did it happen?

The accident on 2001-02-19 involved a AIRBUS INDUSTRIE A321-111, registration HB-IOC, at Genève Aéroport (LSGG), GE, CH.

What was the probable cause of the accident?

The incident was caused by the mechanical failure of bearing number 4 in the number 2 engine, which subsequently damaged the high-pressure turbine blade tips.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/1798_e.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.

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