Berlin-Schönefeld

The aircraft departed Berlin-Schönefeld Airport on a local 35-minute sightseeing flight over Berlin with 25 passengers and three crew members on board. Shortly after takeoff, while in initial climb, the pilots encountered technical problems with the right engine and elected to make an emergency landing. The aircraft struck the airport boundary fence then crash landed on its belly with its right wing partially torn off. All 28 occupants escaped uninjured while the aircraft was damaged beyond repair.

The crew was completing a positioning flight from Moscow to Berlin for maintenance purposes. After the crew was cleared to start up the engines, the aircraft was towed to the deicing pad where the crew requested a two-step deicing procedure. The deicing was completed at 1618LT and the crew was cleared for takeoff at 1636LT. After a course of 1,500 metres on runway 06 in snow falls, the pilot-in-command started the rotation when the aircraft rolled left and right. The right wing struck the ground, the aircraft went out of control, got inverted and crashed in a snow covered area located 450 metres further and 35 metres to the right of the runway. All three crew members escaped with minor injuries while the aircraft was destroyed. At the time of the accident, weather conditions were as follow: wind from 130 at 10 knots, horizontal visibility 1,000 metres in snow falls, vertical visibility 300 feet, OAT -6° and dewpoint at -7°.

On 6 July 2001 at 18:46, a Lockheed TriStar operated by the Canadian airline Air Transat took off from runway 18R at Lyon Saint-Exupéry Airport (LYS), France for flight TSC906 to Berlin-Schönefeld Airport (SXF) with 14 crew members and 197 passengers. At 18:50 the crew contacted Marseilles and requested a heading of 350 degrees to avoid the area of active clouds that the crew had noticed on their weather radar. The controller cleared the flight to climb to FL160, at the requested course. The flight was cleared to climb further to FL190 and at 18:55 instructed to turn right to the MOREG reporting point. During the turn towards the reporting point, while the autopilot was connected, the crew saw that they were approaching an active cell. The captain, who was PNF, instructed the copilot to tighten the turn, which reached a 45° bank angle. At 18:56 Marseille transferred the flight to Geneva Control. It was during this first turn to MOREG that the first burst of hail hit the plane for a duration of one to two seconds. Then a second hailstorm struck the plane, with a duration of 10 to 15 seconds. At that moment the captain took control of the aircraft putting the airplane in a 60° bank angle. The plane lost 500 feet altitude. The crew did not declare an emergency but advised ATC of his intention to turn back to Lyon. The captain asked the flight engineer to depressurize the cabin, which was conducted during descent. There was no rapid depressurization. The windshield of the cockpit was badly damaged. The copilot had the best visibility and carried out the final approach and landing at Lyon-Saint Exupery. The plane landed safely at 1916LT and all 211 occupants evacuated safely.

Shortly after takeoff from Mindelheim-Mattsies Airport, while in initial climb, the pilot informed ATC about problems and elected to return. While completing a sharp turn to the right at a relative low altitude, the aircraft stalled and crashed in a field located less than 2 km from the airfield. The aircraft was destroyed and the pilot, sole on board, was killed. The aircraft was operated by Burkhart Grob Luft-und-Raumfahrt later renamed Grob Aerospace.

Interflug flight 102, an Ilyushin Il-62M, was destroyed following a runway excursion accident on takeoff from Berlin-Schönefeld Airport, East Germany. Of the 113 occupants, 21 were killed. At 06:20 hours local time the engines were started. Immediately thereafter, the flight control surfaces were unlocked, a process which, according to the cockpit voice recorder, was not completed. The crew did not carry out the necessary check of the warning panel on the condition of the elevator. While taxiing for departure, the captain checked for the second time the movement of the elevators but failed to notice they were locked. The aircraft was cleared for takeoff from runway 25L and the engines were adjusted to rated power due to the low take-off mass of 113 tons. At 06:28:05 the aircraft reached VR. The captain pulled the control column during VR, but the aircraft did not respond. Four seconds later he called out to abort the takeoff. At this time the aircraft had attained a speed of 293 km/h. Instead of using reverse thrust, the flight engineer shut down all four engines. The speed at this time was 303 km/h and the remaining distance to the end of the runway was about 940 meters. The aircraft rolled over the end of the runway at a speed of 262 km/h and slightly to the left of the centerline. During the emergency braking five tires of the main landing gear had been destroyed. The airaft crossed an excavation pit of 40 cm deep, causing the the right main landing gear to collapse. It then collided with a water tank, concrete piles of the airport fence, a road embankment and six trees. At 06:28:37 the aircraft came to rest and burst into flames. Within two minutes, 82 passengers could be rescued alive from the fuselage, which had been broken into three parts. All 10 crew members survived.

Originally, flight SU892 was a direct service from Minsk to Berlin but due to poor weather at Berlin, the flight was diverted to the alternate Airport of Prague-Ruzyne. Following an uneventful flight from Prague, the crew started the descent to Berlin-Schönefeld Airport. At that time, weather conditions were marginal with limited visibility to 900 meters and a ceiling down to 60 meters. After the crew was cleared for an ILS approach to runway 25L, ATC turned on the runway 25R lighting system while informing all crews that runway 25R was closed to traffic due to work in progress. These transmissions being done in english, a misinterpretation of the situation conducted the crew to continue the approach to runway 25R. On short final, ATC realized the wrong position of the aircraft and instructed the crew to make a left turn to reach the runway 25L approach path. With flaps down at 38° and at a speed of 263 km/h, the captain initiated a left turn and descended below the glide. With a rate of descent of 7 meters per second, the aircraft struck tree tops then stalled and crashed in a wooded area located 3 km short of runway threshold, bursting into flames. Twelve passengers were seriously injured while 70 other people were killed. Two weeks later, two of the survivors died from their injuries.

The approach to Sofia-Vrazhdebna Airport was initiated by night and limited visibility due to snow falls. On short final, the crew descended below the glide when the aircraft struck successively power cables and tree tops and crashed in a wooded area located 4 km short of runway threshold, bursting into flames. The aircraft was destroyed and all 50 occupants were killed.

After touchdown on runway 11 at Warsaw-Okecie Airport, the airplane was unable to stop within the remaining distance. It overran and struck a four meters high embankment. Upon impact, the right wing was torn off and the airplane came to rest in flames. There were no casualties while the aircraft was written off. The aircraft was christened 'Władysław Reymont'.

The approach to Berlin-Schönefeld Airport runway 25L was completed with the autopilot activated. At a height of 120 meters, the crew was supposed to switch off the autopilot but the captain decided to continue in such configuration, using elevator to counter the autopilot. During the last segment, the rate of descent increased to 6-8 meters per second when the airplane struck the runway surface. Upon impact, the left wing was torn off. Out of control, the airplane veered off runway and came to rest upside down in a grassy area, about 400 meters from the initial impact. All 74 occupants were evacuated, eight of them were seriously injured. The aircraft was destroyed.
Photos via www.interflug.biz

The approach to Budapest-Ferihegy Airport runway 31L was initiated in poor weather conditions with limited visibility due to fog. On short final, the pilot-in-command elected to make a go-around when the airplane struck the ground and crashed 1,360 meters short of runway 31L threshold and 120 meters to the left of its centerline. The airplane crashed and burned and all nine crew members who were completing a ferry flight from Berlin-Schönefeld Airport were killed. At the time of the accident, the horizontal visibility was reported to be 300 meters with a 1,500 meters RVR for runway 31L. The vertical visibility was 30 meters.