Plane crash of the Yak-40 in Sheremetyevo. 2000
Plane crash of the Yak-40 in Sheremetyevo. 2000

Plane crash Yak-40 Vologda AP Sheremetyevo

  • Date of the crash: November 09.03.2000, XNUMX

  • Country of the crash: Russia

  • Location of the crash: Airport Moscow (Sheremetyevo)

  • aircraft Brand: Yak-40

  • Registration of aircraft: RA88170

  • Name of air carrier: Vologda Aviation Enterprise

  • Flight: VGV9651 

Chronology of events:

When taking off from Sheremetyevo Airport, immediately after separation from the strip plane, at a speed of 230 km / h and an altitude of no more than 15 meters, the plane fell into the stall, which was followed by a left unmanaged kreneniem. The lack of height has not given the possibility to withdraw from the crew of the airplane mode.

The aircraft collided with the ground in 63 m on the left axis of the strip, at a distance from the start of 1200 m run and was destroyed. Appeared fire was liquidated measures taken. The passengers and crew were killed.

Data on victims:

  • Total on board were people 9: 5 4 crew members and passengers. Total killed 9 people: crew 5, 4 passengers.

Details of the crash:

  • Phase of flight: takeoff

Data on the plane:

  • aircraft Brand: Yak-40

  • Aircraft ID: RA88170

  • Country where registered aircraft: Russia

  • Date of manufacture of the aircraft: 1976

  • Serial number of the aircraft :: 9620847

  • Hours aircraft: 21428

  • The cycles of use of the aircraft: 20497

Flight data:

  • Flight: VGV9651

  • Tour type: Administrative

  • Aviation Company: Vologda Aviation Enterprise

  • The country, which was registered aviation company: Russia

  • I flew from Moscow (Sheremetyevo)

  • Flying in: Kiev (Borispol)

  • Original item: Moscow (Sheremetyevo)

  • A final point: Kiev (Borispol)

Additional information:

Information about the crew:

  • FAC SA Jakushin

  • Copilot EA Magoo

  • Mechanic VG Navolotskaya

  • Flight attendants:

  • EA Yakovleva

  • SG Koriagina


GTSBPVT (National Centre for the "Safety of flights in air transport") in the technical-scientific report on the results of the study of the dynamics takeoff Yak-40D RA88170 noticed that analyzing the similarity of characteristics Yak-40D RA88170, which were obtained in the emergency flight, with the characteristics of Yak -40D RA98114, which produced special, flight tests, it is possible to conclude that the rise Yak-40D RA88170 was performed in the absence of ice on the surface of the wing.

The results of the simulation in GTSBPVT demonstrated that the plane during takeoff operated two such perturbations:

 almost constant disturbance for the whole rise. It represents the heeling moment on the left wing = 1000 kgm that the equivalent of at a wing fuel tanks asymmetry within the boundaries of 100 - 120 kg. This factor is performance, and requires a small flow reserve ailerons (up to 2 - 3 degrees off speed aircraft on the strip).