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Aeroflot Flight 5143

1985 plane crash in the north-central Uzbek SSR


1985 plane crash in the north-central Uzbek SSR

FieldValue
nameAeroflot Flight 5143
occurrence_typeAccident
imageWreckage of CCCP-85311.jpg
captionWreckage of the aircraft
date
summaryHigh-altitude stall, and crash
siteKyzylkum Desert, near Uchkuduk, Uzbek SSR
coordinates
plane1_imageTashkent Airport, 1980s uzbekistan (Cropped).jpg
plane1_captionCCCP-85311, the aircraft involved in the accident
aircraft_typeTupolev Tu-154B-2
operatorAeroflot (Tashkent Aviation Unit)
callsignAEROFLOT 5143
IATASU5143
ICAOAFL5143
tail_numberCCCP-85311
originKarshi Airport
Karshi, Uzbek SSR
stopoverUfa Airport
Ufa, Russian SFSR
destinationPulkovo Airport
Leningrad, Russian SFSR
occupants200
passengers191
crew9
fatalities200
survivors0

Karshi, Uzbek SSR Ufa, Russian SFSR Leningrad, Russian SFSR Aeroflot Flight 5143 was a scheduled domestic passenger flight between the Soviet cities of Karshi and Leningrad with a stopover in Ufa, operated by the Uzbek division of Aeroflot. On July 10, 1985, the Tupolev Tu-154 operating the flight was involved in an aviation accident when it crashed due to a high-attitude stall in the Kyzylkum Desert, near the city of Uchkuduk. The crash resulted in the deaths of all 200 occupants onboard the flight, making it the deadliest accident in the Soviet Union and Uzbekistan and the deadliest crash of Aeroflot's Tu-154s in service.

Aircraft

The Tu-154B-2 registration CCCP-85311 was manufactured at the Aviakor Plant on November 30, 1978. On January 2, 1979, the aircraft was transferred to the Ministry of Civil Aviation, which was given to the Tashkent Aviation Unit of the Uzbek Civil Aviation Directorate. It was powered by three Kuznetsov NK-8U turbofan engines. At the time of the accident, the aircraft accumulated 12,443 flight hours and 5,660 flight cycles.

Accident

The Tu-154 (CCCP-85311) was operating the first leg of the flight from Karshi to Ufa, piloted by the crew of the 219th flight squadron, consisting of commander O. P. Belisov (48), co-pilot A. T. Pozyumsky (48), flight engineer A. S. Mansurov (32), navigator G. N. Argeev (41), with 5 flight attendants onboard the flight. There were 191 passengers onboard the flight, which had consisted of 139 adults and 52 children, which met the standard regulations of 92.2 tonnes. The aircraft took off at 23:00 PM, 4 hours behind the scheduled departure of 19:00; the temperature of Karshi Airport was 33 C. The Tu-154 climbed altitude, following the guidelines of the Aircraft Flight Manual (AFM).

The aircraft gained an altitude of 11,600 m at a speed of 400 kph. The crew had changed the autopilot to gain speed, leading the aircraft to pitch down. The crew pulled the aircraft up, making the Tu-154 on the verge of activating the alarm of the critical angle of attack; suddenly, the alarm had stopped due to a blown fuse. The aircraft then entered the jet flow zone with a weight of 86.5 tonnes; the air temperature of the specified flight path was 16.5 C-change higher than the standard. The Tu-154 suddenly entered a critical angle of attack. This led to disruption in the airflow to the engines, leading to shaking; the flight engineer thought it was a compressor stall and ordered the crew to decrease the speed.

Instead of pushing back the throttle, they both decreased and increased the speed of the aircraft. The captain still continued to hold the altitude. The aircraft had then repeatedly had critical angles of attack; as a result, the engines failed, causing the aircraft’s speed to decrease 290 kph after 1 minute and 17 seconds after the repeated angles of attack, leading the aircraft to lose control and enter a flat spin.

The crew contacted the dispatcher, stating that they were in a flat spin and had no power on the engines.

The aircraft remained in the spin for 2 minutes and 33 seconds, and at 23:46, it impacted the ground in a remote part of the Uchkuduk District, roughly 30 km east of the small town of Kokpatas and 70 km northeast of Uchkuduk itself. All 200 occupants were killed.

Investigation

Official conclusions

CCCP-85311's cockpit voice recorder was severely damaged by the impact. The Ministry of Civil Aviation had concluded the cause of the accident:The cause of the disaster was the aircraft entering a flat spin at cruising altitude with a high flight mass, influenced by a high non-standard outside air temperature, a small angle of attack margin, and engine thrust. Under these flight conditions and the rapidly developing catastrophic situation, the crew made a number of deviations from the requirements of the Flight Operations Manual, lost speed, and was unable to control the aircraft.The Ministry of Civil Aviation revealed that, during the proposal of the Tupolev Design Bureau and the State Research Institute of Civil Aviation, the flight weight of the Tu-154 was increased from 70 tonnes at an altitude of 12,500 meters to 86.5 tonnes for a flight level of 12,100 meters, without taking into account deviations in outside air temperatures from standard ones.

Theories

It is believed that the crew had been exhausted due to the poor resting conditions during the delay at Karshi, which caused the pilots to make inadequate decisions during the ascent and fail to be aware of the situation. This is unconfirmed, as the investigation materials made by the Ministry of Civil Aviation are classified and not published.

References

References

  1. {{ASN accident
  2. "Soviet Database".
  3. (1996). "Aviation Disasters Second Edition". Patrick Stephens Limited.
  4. Ershov, Vasily Vasilyevich. "Раздумья ездового пса".
  5. (2007-08-16). "Особенности поведения и пилотирования магистральных пассажирских самолетов на критических режимах полета - МФАБ".
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