Russia

The pilot was completing a crop-spraying mission when the engine failed. He attempted an emergency landing when the aircraft collided with power cables and crashed in a field located about 20 km southeast of Primorsko-Akhtarsk, bursting into flames. The aircraft was destroyed by a post crash fire and the pilot was injured.

The crew was completing a positioning flight from Krasnoyarsk to Yakutsk with an intermediate stop in Lensk. The intended destination was in fact Prokovsk located about 70 km southwest of Yakutsk but the airfield was not suitable for night movements. On approach to Yakutsk-Magan Airport, the crew continued to Prokovsk where several cars were parked along the runway with their lights ON. Due to low visibility caused by night and snow falls, the crew was unable to establish a visual contact with the ground and two approaches were missed. During a third attempt to land, the aircraft collided with pine trees and power cables and crashed in an open field, bursting into flames. All three occupants were killed.

On take off roll at dusk during heavy snow falls, the aircraft veered off runway to the left and collided with a snow mound (1,2 meter high). The nose gear was torn off while both main gears collapsed. All occupants escaped uninjured while the aircraft was damaged beyond repair. It was used for the Far East Command.

45 seconds after takeoff, while climbing, the aircraft stalled and crashed in a snow covered field. The pilot and all 10 skydivers escaped uninjured while the aircraft was damaged beyond repair.

Shortly after take off from Pskov Airport, while climbing to a height of about 50-70 metres, the crew encountered engine problems and elected to make an emergency landing. The aircraft lost height and crashed in a snow covered field located near the airport and came to rest. All 13 occupants escaped uninjured while the aircraft was damaged beyond repair. All passengers were skydivers (paratroopers) from the Marine Corps.

The aircraft was dispatched to Makhachkala to deliver troops, military equipments and cargo with 7 crew members on board. Ready for the next trip to Nizhny Novgorod, the crew was cleared to taxi to the holding point of runway 14. At that time, the visibility was poor due to the night and foggy conditions. Another Ilyushin II-76MD registered RA-76827 was on approach to runway 14 with 25 passengers and a crew of six on board. On final approach, the navigator informed the crew that the headlights should be switched on but no actions was taken. In a visibility lower than 800 metres, the aircraft landed slightly to the left of the runway centerline. After touchdown, the left wing impacted the cockpit of the II-76 awaiting at the holding bay. While RA-76827 suffered only minor damaged and that no one on board was injured, all four crew members in the cockpit of RA-76825 were killed while three other occupants were injured.

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.

On September 13, 2008 an Aeroflot –Nord flight crew (Captain and copilot), were conducting a scheduled domestic passenger flight n°AFL821 on a B737-505 aircraft, registration VP-BKO, from Moscow (Sheremetyevo, UUEE) to Perm (Bolshoye Savino, USPP). Apart from the two-member flight crew there were 4 flight attendants and 82 passengers on board, which makes a total of 88 people, including 66 citizens of the Russian Federation, 8 citizens of Azerbaijan, 1 citizen of Byelorussia, 1 of Germany, 1 of Italy, 1 of China, 1 of Latvia, 1 of Turkey, 1 of Uzbekistan, 5 citizens of Ukraine and 2 of France. According to the load sheet, the aircraft payload (cargo and passengers) was 8079 kg. The takeoff weight was ~54000 kg (with the max TOW of 60554 kg), the CG was at 20.61 % MAC, which was within the B-737-500 FCOM limitations. The calculated landing weight was 49700 kg (with the maximum of 49895 kg), and the CG was at 21.9 % MAC, which was also within the B737-500 FCOM limitations. The pre-flight briefing was conducted in due time and in compliance with the standard procedures. All the crew members passed medical check at the medical office of Aeroflot – Russian Airlines on September 13, 2008 at 1948 hrs and got permissions to fly. On the basis of the dispatch information (aircraft condition, aeronautical information, weather information, aircraft load data and operational flight plan) the PIC at 1955 hrs made a decision to fly. The takeoff was performed at 2113 without delay. The climb and level flight at FL290, 9,100 metres were conducted without any deviations. At 2245 hrs the crew started descent from the flight level to waypoint Mendeleyevo (940 MN). After passing over Mendeleyevo, in compliance with the Perm Approach Control instruction, the aircraft flew via the outer marker (705 PX) of Runway 21 which is the initial approach fix (IAF) for Runway 21 (heading 212° magnetic). After passing over the RWY with heading 110° M, the crew, following the Controller’s instruction, turned right for back course and started maneuvering for ILS approach to Runway 21. After the base turn, approaching the landing course at 600 m with both autopilot and autothrottle disengaged, the aircraft started climbing up to 1300 m, rolled 360° over the left wing and collided with the ground. The aircraft was totally destroyed and partly burnt in the ground fire. All passengers and crew members on board died due to the ground impact. The accident occurred at 2310 hrs 12.4 km from aerodrome reference point (ARP) of Perm Airport, azimuth 60° M. Accident site elevation is 153 m.

While performing an aerial photography mission, the engine failed. The crew attempted an emergency landing and reduced his altitude when the aircraft collided with trees and crashed in a field, coming to rest upside down. The wreckage was found a day later about 50 km from Osinovy Mys. All four occupants were injured.

During the takeoff roll, at a speed of 32 knots, the engine n°1 (a Soloviev D-30KU-154-II) exploded. The crew abandoned the takeoff procedure and started an emergency braking manoeuvre. The aircraft was stopped on the main runway and all 112 occupants evacuated safely. The aircraft was considered as damaged beyond repair as several compressor elements punctured the engine n°1 nacelle, hit the fuselage and n°2 engine structure. A fire erupted on the left engine and destroyed the nacelle and a part of APU as well.