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Lufthansa Flight 2904

14 Sept 1993 · Warsaw Chopin Airport, Warsaw, Poland

Airbus A320-211 · Overshot runway due to pilot error

From Frankfurt Main Airport (FRA) to Warsaw Chopin Airport (WAW)

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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.