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(fragments)
• 08.40 – the second group of RSRB rescuers went to Sochi Seaport to take and
transport the bodies (fragments) and the airplane wreckage in co-operation with the Russian
Ministry of Emergencies , Sochi Seaport and other departments.
The two teams worked until 18 h 30 min (Moscow time) jointly with the other ministries and
departments.
• 04.05.2006 - 07.30 - a group of RSRB rescuers and ATB personnel was sent to
Sochi seaport to continue the search-and-rescue work jointly with the Ministry of Emergency of
Russia, Sochi seaport and the other departments, and to transport the bodies (fragments) and the
airplane wreckage.
• 05.05.2006 - 08.30 – a group of RSRB rescuers and 4 ATB people were sent to
Sochi seaport to continue the search-and-rescue work jointly with the Ministry of Emergency of
Russia, Sochi seaport and the other departments, and to transport the bodies (fragments) and the
airplane wreckage.
• 06.05.2006 - 08.30 – a group of RSRB rescuers and 3 ATB people were sent to
Sochi seaport to continue the search-and-rescue work jointly with the Ministry of Emergency of
Russia, Sochi seaport and the other departments, and to transport the bodies (fragments) and the
airplane wreckage.
Airplanes of the Ministry of Emergency were also involved in the search-and-rescue work.
• Be-200ChS airplane, No. 3276, performed visual observation of the accident area
and determined the borders and direction of propagation of the airplane fuel and wreckage. This
information was used to direct the boats in the search area.
The airplane performed two flights:
- 04.05.06 takeoff at 11.07 landing at 12.32;
- 05.05.06 takeoff at 10.16 landing at 11.27.
• Ka-32 helicopter, No. 31088 – performed visual observation of the accident area
and the area of wreckage drift to the North-West and directed the boats collecting the bodies
(fragments) and the wreckage.
The helicopter performed four flights:
- 03.05.06 takeoff at 17.49, landing at 18.50;
- 04.05.06 takeoff at 07.31, landing at 09.50;
- 05.05.06 takeoff at 08.12, landing at 10.37;
- 06.05.06 takeoff at 09.32, landing at 11.42.
• Mi-8MTV helicopter No. 32755 performing a flight from Rostov to Sochi,
worked in the accident area on 03.05.06 from 13:30 to 14:30.
23
1.16 Tests and Research
In the course of investigation of the accident to the A320 EK-23009, Airbus specialists performed
mathematic simulations of the accident flight.
In the course of the mathematic simulation, the final stage of the accident flight was split into two
segments: the autopilot flight segment (up to the moment when the autopilot was disengaged) and
the manual flight segment.
The pilot control inputs, flight control surface deflections, power plant and autopilot modes were
set in accordance with the values registered by the A320 EK-32009’s FDR. The results obtained
showed a high convergence in the mathematical simulation parameters with the values registered
by the FDR in the accident flight (see Attachment 3).
Analysis of the results obtained showed that the autopilot was working in accordance with its
established logic, and the airplane movement was completely determined by deflection of the
control surfaces and the engine mode. The aerodynamic and propulsion performance
characteristics of A320 EK-32009 conformed to those of the type. There was no external
influence on the airplane.
In the period from 25.06.2006 to 07.07.2006 experiments on A320 flight simulators were
conducted.
The research was performed on the following A320 simulators:
- Motion Full Flight Simulator (FFS) A-320, manufactured by CAE, MFR’s PART No. 35-
181-MA002RV1-01 SERIAL No. 2RV1-470 2003. FLIGHT COMP (UNIT FC) 35181-
MA184900.38.2.845 AEROFLOT TRAINING CENTRE (Sheremetyevo);
- Motion Full Flight Simulator (FFS) FFS A-320, manufactured by CAE, MFR’s PART No.
35-181-MA002RJJ-01 SERIAL No. 2RJJ-479 2003г. FLIGHT COMP (UNIT FC)
MA184900.22.2.845 AIRBUS A320 FFS (Toulouse, France);
- Research Fixed Simulator (FS) «ENGINEERING SIMULATOR Airbus» (Toulouse,
France);
- Research Fixed Simulator (FS) «IRON BIRD», fitted with an actual flight control system,
including its mechanical parts (Toulouse, France).
In total the research took the following time:
- on FFS – 12 hours
- on FS – 18 hours.
The following people were involved in the research: Airbus test pilots, a test pilot from the Flight
Research Institute, Armavia and Aeroflot pilots, as well as pilot-inspectors from the CAA RA
and FTOA of Russia.
There were two video cameras installed in the simulator cabins shooting all the experiments. In
　
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