Lufthansa Flight 2904
Airbus A320-211 · Overshot runway due to pilot error
From Frankfurt Main Airport (FRA) to Warsaw Chopin Airport (WAW)
Event
- Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
- Accident
- Event fatalities
- 2 · all aircraft and ground
- Ground fatalities
- Unknown
- Occupants
- 70
- Survivors
- 68
- InjuriesFatal: death within 30 days. Serious: over 48 hours in hospital within a week, most broken bones, severe bleeding, nerve or organ damage, or serious burns. Minor: anything less. Glossary
- 56
- OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
- Airline
Airbus A320-211
- Flight
- LH2904
- Aircraft type
- Airbus A320
- Category
- Airplane · from aircraft type
- RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
- D-AIPN
- Operator
- Lufthansa
- Onboard fatalities
- 2
- Route
- From Frankfurt Main Airport (FRA)To Warsaw Chopin Airport (WAW)
Cause areas
- Personnel issues › Action/decision
- Environmental issues › Conditions/weather/phenomena
- Environmental issues › Operating environment
- Organizational issues › Development
From the investigation findings the Wikipedia article reports, sorted into the NTSB's cause areas with AI assistance.
Approximate · Coordinates from the Wikipedia article; not checked against an investigation report.
From the Wikipedia article
Lufthansa Flight 2904 was an Airbus A320 flying from Frankfurt, Germany to Warsaw, Poland that overran the runway at Okęcie International Airport on 14 September 1993.
Incident description
Lufthansa Flight 2904 was cleared to land at Okęcie International Airport Runway 11 and was informed of the existence of wind shear on the approach. To compensate for the crosswind, the pilots attempted to touch down with the aircraft banked slightly to the right and with a speed of about 20 kn faster than usual. According to the manual, this was the correct procedure for the reported weather conditions, but the weather report was not up-to-date. At the moment of touchdown, the assumed crosswind turned out to be a tailwind of approximately 20 kn. With the resulting increased speed, the airplane hit the ground at approximately 170 kn and far beyond the normal touchdown point; its right gear touched down 770 m from the runway threshold. The left gear touched down nine seconds later, 1525 m from the threshold. Only when the left gear touched the runway did the ground spoilers and engine thrust reversers start to deploy, these systems depend on oleo strut (shock absorber) compression. The wheel brakes, triggered by wheel rotation being equal to or greater than 72 kn, began to operate about four seconds later.
The remaining length of the runway (left from the moment when braking systems had begun to work) was too short to enable the aircraft to stop. Seeing the approaching end of the runway and the obstacle behind it, the pilot steered the aircraft off the runway to the right. The aircraft departed the runway at a speed of 72 kn and rolled 90 m before it hit the embankment and an localizer with the left wing. A fire started in the left wing area and penetrated into the passenger cabin. Two of 70 occupants died, the training captain (seated in the right seat) who died on impact and one passenger who was unable to escape because he lost consciousness from the smoke in the cabin.
Investigation and cause
Causes of the accident
The main cause of the accident was the incorrect decisions and actions of the flight crew. Some of these decisions were made based on wind shear information that was received by the crew. The wind shear was produced by the front passing over the airport, accompanied by an intensive variation of wind parameters, as well as heavy rain on the runway itself.
Contributing to the cause was the lack of current wind information at the tower. For that reason, no up-to-date wind information could be transmitted to the crew.
Additional causes involved certain design features of the aircraft. Computer logic prevented the activation of both ground spoilers and thrust reversers until a minimum compression load of at least 6.3 tons was sensed on each main landing gear strut, thus preventing the crew from achieving any braking action by the two systems before this condition was met.
Text from the Wikipedia article “Lufthansa Flight 2904” (revision 1372145921, retrieved 2026-09-18) by its authors, under CC BY-SA 4.0. Extracted as plain text: references, tables, images and some sections are left out. Read the article
Sources
Wikipedia article: Lufthansa Flight 2904
- Article
- Lufthansa Flight 2904
- Revision
- 1372145921 · 2026-08-30 · retrieved 2026-09-18
- Wikidata
- Q468754
- Licence
- Text CC BY-SA 4.0, by the article's authors; Wikidata CC0; town positions GeoNames (CC BY 4.0)
Where each value comes from
- Record
- Wikipedia article "Lufthansa Flight 2904" (page 8107688, revision 1372145921)
- Date
- Wikipedia infobox: date
- Place and country
- Wikipedia infobox: site
- Map position
- Wikipedia article coordinates
- Aircraft, operator and route
- Wikipedia infobox: aircraft type, registration, operator, origin and destination; route airports from the linked airport articles' Wikidata codes (OurAirports)
- Operation
- airline flight number in the infobox
- Fatalities
- Wikipedia infobox: aircraft fatalities
- Ground fatalities
- not stated in the Wikipedia infobox
- Summary
- Wikipedia infobox: summary
Source notes (1)
- Wikipedia · Facts from the Wikipedia article's infobox and coordinates, not checked against an investigation report. Independent review pending.