Barcelona - Kaliningrad

On October 1, 2008 at 11:18 PM, Barcelona - Kaliningrad experienced a crash involving Boeing 737-300, operated by KD Avia - Kaliningrad Avia, with the event recorded near Kaliningrad Kaliningrad oblast.

The flight was categorized as scheduled revenue flight and the reported phase was landing (descent or approach) at a airport (less than 10 km from airport) crash site.

144 people were known to be on board, 0 fatalities were recorded, 144 survivors were identified or estimated. This corresponds to an estimated fatality rate of 0.0%.

Crew on board: 6, crew fatalities: 0, passengers on board: 138, passenger fatalities: 0, other fatalities: 0.

The listed crash cause is human factor. The accident aircraft Boeing 737-3Y0 EI-DON, was operated by KD Avia on a flight from Kaliningrad, Russia to Barcelona, Spain and return. Flight KD793 to Barcelona was uneventful. The return flight, KD794, departed at 16:18 with 138 passengers and six crew members on board. The copilot was Pilot Flying, the captain was Pilot Monitoring. The en route part of the flight was uneventful. As the flight was descending to Kaliningrad at night in heavy rains and with gusty crosswind. During the descent flaps were first selected at 1° and thereafter to 5°. As the flaps were transitioning to this position, a flap asymmetry warning caught the attention of the crew. At 19:00 hours the captain took over control and selected flaps to 2°, the position at which there was no asymmetry warning. The crew then contacted the controller at Kaliningrad and reported that they had flap problems. As the descent was continued, the copilot performed the necessary calculations for a landing with flaps at 2°. At 19:09 the cabin crew was warned to prepare for a high-speed landing. Using the QRH to work the flap issue, the co-pilot activated the 'flap inhibit' and 'gear inhibit' switches. This "incorrect" action effectively disconnected the ground-proximity warning system (GPWS). At 19:11 it was established that the landing speed would be Vref +30, leading to a planned landing speed of 161 knots. At 19:14 the Landing Gear Warning Horn sounded due to the combination of power and flaps setting with the fact that the landing gear had not been selected down. This warning was cancelled by the crew. When the engine power was reduced to idle, the Landing Gear Warning Horn sounded again. This time the crew did not pay attention to the warning and continued to land. The airplane performed a gear up landing, sliding for 1440 m before coming to rest on the runway. The flap asymmetry issue was caused by a faulty Flap Position Transmitter. The flaps had extended to the commanded position, but the system incorrectly detected an asymmetry issue. This issue had occurred previously on EI-DON. The sensor had been replaced prior to departure from Kaliningrad that same day.

Aircraft reference details include registration EI-DON, MSN 23812/1511, year of manufacture 1988.

Geospatial coordinates for this crash are approximately 54.7065°, 20.4937°.