Crash of a Tupolev TU-154M in Longyearbyen: 141 killed

Date & Time: Aug 29, 1996 at 1022 LT
Type of aircraft:
Operator:
Registration:
RA-85621
Survivors:
No
Site:
Schedule:
Moscow - Longyearbyen
MSN:
86A742
YOM:
1986
Flight number:
VKO2801
Country:
Region:
Crew on board:
11
Crew fatalities:
Pax on board:
130
Pax fatalities:
Other fatalities:
Total fatalities:
141
Captain / Total flying hours:
6232
Captain / Total hours on type:
1940.00
Copilot / Total flying hours:
19538
Copilot / Total hours on type:
10177
Circumstances:
Vnukovo Airlines flight VKO2801 departed Moscow-Vnukovo Airport at 04:44 UTC bound for Longyearbyen Airport on the Norwegian archipelago of Svalbard. It was a chartered flight with workers and their families to coal mining towns on Svalbard. The flight was uneventful until the start of the descent. Before radio contact with Longyear Information, the crew went through the detailed landing procedure for runway 10. At 09:56, the crew were cleared to start the descent. A little later, the crew received additional information consisting of runway in use 28, wind 230 degrees at 16 knots, visibility more than 10 km, rain showers, clouds: few at 1500 feet, scattered at 2000 feet and broken at 4000 feet, temperature +5°C, dewpoint -0°C and QNH 1005 hPa. (Later changed to 1006 hPa). The crew tried to request runway 10 for landing twice, but the request was not understood as such by Longyear Information due to language difficulties. When the flight was overhead the ADV beacon, at 10:15 hrs, the crew reported their position to Longyear Information and entered the base turn with a bank angle of 22 degrees. At 10:16 hrs, the aircraft came out of this turn on magnetic heading 160 degrees. During the right turn to the base turn, a malfunction occurred in the electric trimming mechanism, which was corrected by the crew. At 10:17, the crew started the turn to bring the aircraft out on the magnetic inbound course 300 degrees, as prescribed by the approach chart. The distance from the airport at this moment was 14 NM (25.9 km), as prescribed by the approach chart, but the lateral deviation from the outbound magnetic course 155 degrees from ADV was 2 NM (3.7 km) to the left. At 10:18, after the radio altimeter aural warning had been activated twice, the co-pilot took the controls and, after 6 seconds, turned the autopilot pitch channel off by 'overriding' it. From then on until the impact, the flight continued in autopilot mode in the roll channel, and in manual mode in the pitch channel. The aircraft passed through the localizer centerline and when the turn had been completed, the aircraft rolled out on a magnetic heading of 290 degrees. At this time, there was a discussion within the crew as to whether or not the final turn had been made at the correct time. The discussion led to the roll out of the turn to final approach and a corrective turn to the right to magnetic heading 306 degrees. At this point, the aircraft was 14.7 NM (27.4 km) from the airport, 2.8 km to the right of the approach centerline, maintaining an altitude of 5000 feet (1520 m ) and the crew increased the flap setting to 28 degrees. The airspeed was reduced to approx. 330 km/hr (180 kts). Instead of intercepting the centerline, the crew continued the flight on the right side, more or less paralleling the localizer course with minor heading changes. At 10:20 the flight made a corrective turn, resulting in a track close to 300 degrees. At this point, the lateral deviation from the approach centerline was 3.7 km to the right. During this corrective turn, the aircraft started descending. At 10:21, the crew made yet another corrective turn to the right. At 10:22:05, the aircraft started turning towards the left. The distance to the airport was 8 NM (14.8 km). On this part of the final approach, the aircraft apparently entered an area of strong turbulence created by the proximity to the mountains. The GPWS then activated 9 seconds before impact. The crew reacted to this by applying power and initiating a pitch-up. At 10:22:23, 7.7 NM (14.2 km) from the airport at an altitude of 2975 feet (907 m), the aircraft collided with the top of the mountain Operafjellet 3.7 km to the right of the approach centerline. All 141 occupants were killed, most of them employees of a local carbon mine and their family members.
Probable cause:
The following findings were reported:
1) There is no Russian procedure for offset localizer approaches modifying the required rule to set the landing course on the HSI.
2) The course selected on both HSIs was 283° even though the approach course is 300°. This setting does not affect the indication of the CDI. However, the CDI was pointing to 283° on the dial, which is 17° to the left of the approach course, giving a visual impression of wind drift to the left and therefore giving a possible reason for a heading correction to the right.
3) The navigator in a stressed and overloaded working situation most probably followed the rule setting the landing course 283° on the GPS in OBS mode instead of the approach course 300°.
4) The crew was not fully aware of the status of an AFIS officer in comparison with the authority of a Russian air traffic controller with the result that the crew accepted safety information from the AFIS officer as orders.
5) The crew had limited knowledge of the English language with the consequence that they had problems communicating their intentions to the AFIS officer.
6) The navigator was overloaded with tasks leaving little time for rechecking his work, thereby setting the scene for making mistakes.
7) The pilots did not monitor the work of the navigator sufficiently.
8) Leaving the communication with AFIS to the navigator during the approach was not according to the normative documents.
9) Due to the workload of the navigator, the decision of the co-pilot to transfer the responsibility of controlling the aircraft laterally to him, was inappropriate.
10) The crew resource management of the PIC was not satisfactory.
11) When the crew had made the decision to carry out the approach to runway 28, a new approach briefing was not accomplished.
12) The crew made the proper correction for the wind drift, but did not try to intercept the outbound track from ADV with the consequence that they overshot the approach centerline turning inbound.
13) Seemingly confusing indications on the HSIs in the base turn caused the crew to become uncertain of the aircraft position in relation to the LLZ 28 centerline. In this situation, the crew showed a lack of situational awareness.
14) The two pilots did not have the approach chart in front of them at all times during the approach making it difficult for them to maintain situational awareness.
15) The crew did not know of the possibility to check the position of the aircraft in relation to the localizer centerline by the VDF service available.
16) On final approach the crew probably put too much emphasis on the indications displayed on the GPS.
17) The crew started descent in a mountainous area without firm and positive control of the lateral navigation demonstrated by the disagreement within the crew as to whether to correct to the left or right.
18) In spite of the uncertainty within the crew as to whether they were approaching correctly or not, they continued instead of abandoning the approach and climbing to a safe altitude to solve the problem.
Final Report:

Crash of a Tupolev TU-154B-2 in Grozny

Date & Time: Dec 25, 1993 at 1229 LT
Type of aircraft:
Operator:
Registration:
RA-85296
Survivors:
Yes
Schedule:
Moscow - Grozny
MSN:
78A296
YOM:
1978
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
165
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Following an uneventful flight from Moscow, the crew completed the approach to Grozny in poor weather conditions. The aircraft landed nose first, causing it to be torn off. The aircraft slid on the ground for few dozen metres before coming to rest. All 172 occupants evacuated safely while the aircraft was written off.

Crash of a Tupolev TU-134A in Sukhumi

Date & Time: Aug 14, 1982 at 1809 LT
Type of aircraft:
Operator:
Registration:
CCCP-65836
Flight Phase:
Survivors:
Yes
Schedule:
Sukhumi - Moscow-Vnukovo
MSN:
17113
YOM:
1974
Flight number:
SU974
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
76
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
17003
Aircraft flight cycles:
10406
Circumstances:
At 1808LT, the crew was cleared for takeoff from Sukhumi-Babushara runway 02. During the takeoff run, 26 seconds after it started to roll, at a speed of 195 km/h, the crew sighted a Let L-410M entering the runway. Registered CCCP-67191, the Let L-410 was engaged in a scheduled service (flight SU73G) to Kutaisi with two pilots and nine passengers on board. The captain of the Tupolev decided to abandon the takeoff maneuver and initiated an emergency braking procedure. Spoilers were deployed and revers systems were activated. He elected to turn to the left to reach an exit taxiway. In the same time, the crew of the Let saw the Tupolev coming from their right and increased engine power to move forward. Seven seconds after the crew of the Tupolev rejected takeoff, at a speed of 216 km/h, the right wing of the Tupolev struck the Let that was destroyed upon impact. The Tupolev rolled for about 514 meters then veered off runway to the left and came to rest 48 meters to the left of its centerline. All 82 people on board the TU-134 escaped uninjured while all 11 people on board the Let were killed.
Probable cause:
It was determined that the collision was the consequence of a series of errors made by the crew of the Let L-410 who failed to follow ATC and ground controllers instructions regarding taxiing procedures prior to takeoff, which led them to enter the runway when he was not authorized to do so. A poor management in flights organization at Sukhumi Airport remains a contributing factor as well as few procedures violation on the part of ATC and ground controllers, among others concerning the use of a non-standard phraseology which may create confusion to the crew.

Crash of an Antonov AN-22A in Moscow: 3 killed

Date & Time: Jun 2, 1980
Type of aircraft:
Operator:
Registration:
CCCP-09311
Flight Type:
Survivors:
Yes
Schedule:
Damascus - Moscow
MSN:
043481251
YOM:
1974
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
On approach to Moscow, a fault accumulator caused a fire in the well of the main right gear, while the aircraft was 28 km from Vnukovo on a flight to Sheremetievo. When the fire was detected, the crew decided to divert to Vnukovo Airport (VKO). Electric power was switched from the main system to the emergency one when the aircraft was flying at a height of 3,400 meters some 8 km from VKO. But the emergency system failed also at an altitude of 2,500 meters on approach, leaving the aircraft without any electric power. The crew attempted a emergency belly landing in a field when the aircraft collided with obstacles and a drainage ditch before coming to rest in flames. Three crew members were killed while three others were injured.
Probable cause:
Fire in the right main wheel well.

Crash of a Tupolev TU-104B in Moscow: 59 killed

Date & Time: Mar 17, 1979 at 1948 LT
Type of aircraft:
Operator:
Registration:
CCCP-42444
Survivors:
Yes
Schedule:
Moscow - Odessa
MSN:
9 2 10 01
YOM:
1959
Flight number:
SU1691
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
114
Pax fatalities:
Other fatalities:
Total fatalities:
59
Captain / Total hours on type:
32.00
Aircraft flight hours:
24356
Aircraft flight cycles:
14118
Circumstances:
Five seconds after takeoff from runway 01 at Moscow-Vnukovo Airport, while in initial climb, a fire alarm activated in the cockpit panel, informing the crew about a fire in the left engine. The crew declared an emergency, continued to climb and was cleared to return. Following several turns, the crew started an approach to runway 01 by night and marginal weather conditions. On final, the airplane descended below the MDA until it struck the ground at a speed of 350 km/h and crashed in flames in a snow covered field located along a wooded area, 1,548 meters short of runway 01. 58 passengers and a stewardess were killed while 61 other occupants were injured. The aircraft was destroyed.
Probable cause:
It was determined that the fire alarm that activated in the cockpit was false and not related to an engine fire. Analysis revealed that the temperature of the left engine compartment increased to 253° C due to the disconnection of a pipe coupled to the anti-icing system. The accident was the consequence of the combination of several wrong decisions on part of the flying crew and the following factors:
- The approach was completed by night and icing conditions in a single engine configuration,
- The total weight of the aircraft was 10,201 kg above the maximum weight allowed for landing,
- The approach was completed with a tailwind component,
- Excessive approach speed,
- Premature descent resulting in a collision with ground after passing MDA,
- Lack of crew interaction and coordination,
- The navigator failed to inform the captain about the decision height fixed at 120 meters,
- The approach was completed with the GPWS deactivated,
- The copilot failed to monitor the instruments properly, which contributed to the deviation of the airplane to the right during the last sequence until it lost altitude and impacted the ground.

Crash of an Ilyushin II-18E in Verkhnyaya Khava: 111 killed

Date & Time: Mar 6, 1976 at 0058 LT
Type of aircraft:
Operator:
Registration:
CCCP-75408
Flight Phase:
Survivors:
No
Schedule:
Moscow - Yerevan
MSN:
186 0092 01
YOM:
1966
Flight number:
SU909
Country:
Region:
Crew on board:
11
Crew fatalities:
Pax on board:
100
Pax fatalities:
Other fatalities:
Total fatalities:
111
Aircraft flight hours:
21587
Aircraft flight cycles:
9082
Circumstances:
While cruising by night at an altitude of 7,800 metres, the electrical system failed, causing several instruments to fail, among them gyros. Control was lost and the airplane entered a dive and eventually crashed in a nose-down angle of 70° in an open field located 150 metres from the village of Verkhnyaya Khava, about 50 km northeast of Voronezh. Some debris of the airplane were found at a depth of 14 meters. It disintegrated on impact and all 111 occupants were killed.
Probable cause:
The 36 volts electrical system failed in flight, causing the automatic pilot system to fail as well as instruments such as gyros. Investigations were unable to determine the exact cause of the electrical system's failure. While flying by night and in a visibility reduced by clouds, the crew was unable to have visual references and lost control of the airplane after suffering a spatial disorientation.

Crash of a Tupolev TU-124V in Moscow: 62 killed

Date & Time: Jan 3, 1976 at 1005 LT
Type of aircraft:
Operator:
Registration:
CCCP-45037
Flight Phase:
Survivors:
No
Schedule:
Moscow - Minsk - Brest
MSN:
2 35 10 02
YOM:
1962
Flight number:
SU2003
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
56
Pax fatalities:
Other fatalities:
Total fatalities:
62
Aircraft flight hours:
17014
Aircraft flight cycles:
14409
Circumstances:
26 seconds after takeoff from runway 24 at Moscow-Vnukovo Airport, while climbing to a height of 200 metres, the crew retracted the landing gear and reduced the engine power to nominal value. Once the altitude of 250 metres was reached, while at a speed of 340 km/h, the airplane entered a right turn when the crew was cleared to climb to 1,500 metres. The crew failed to acknowledge this clearance when seven seconds later, the airplane entered a left turn, nosed down and crashed at a speed of 550 km/h onto a house located 5,400 meters from the runway end and 1,800 metres to the right of its extended centerline. The aircraft and the house were totally destroyed and all 61 occupants were killed as well as one people in the house. Another person on the ground was injured.
Probable cause:
It was determined that both artificial horizons failed during initial climb for undetermined reasons. The combination of this instrument failure and a limited visibility caused the pilots to suffer a spatial disorientation and then a loss of control.

Crash of a Tupolev TU-124V in Karacharovo: 51 killed

Date & Time: Dec 16, 1973 at 1910 LT
Type of aircraft:
Operator:
Registration:
CCCP-45061
Flight Phase:
Survivors:
No
Schedule:
Vilnius - Moscow
MSN:
4 35 14 06
YOM:
1964
Flight number:
SU2022
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
46
Pax fatalities:
Other fatalities:
Total fatalities:
51
Aircraft flight hours:
14903
Aircraft flight cycles:
13832
Circumstances:
The crew was cleared to descent to 5,700 meters when a technical issue occurred on the elevator trim system. The airplane entered a dive and during the descent, the captain was able to regain control at an altitude of 2,000 meters. While flying by night, the gyro failed and the pilot suffered a spatial disorientation. So he lost again control of the airplane that dove into the ground and crashed in a near vertical attitude at a speed of 900 km/h in an open field located about 480 meters from Karacharovo. The aircraft disintegrated on impact and all 51 occupants were killed.
Probable cause:
An electrical short-circuit occurred in the elevator trim system, causing the elevator to be jammed in a down position. In such conditions, the airplane entered a dive and became uncontrollable after the gyro failed as well.

Crash of a Tupolev TU-154 in Moscow

Date & Time: May 7, 1973
Type of aircraft:
Operator:
Registration:
CCCP-85030
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Moscow - Moscow
MSN:
72A030
YOM:
1972
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing a local training mission at Vnukovo Airport. Following four successful touch-and-go manoeuvres, the crew took off again. Just after liftoff, while at a height of 20 meters, the aircraft suffered severe vibrations and went unstable. Shortly later, while climbing to a height of 70 meters, both engines n°1 & 3 lost power simultaneously. The captain decided to make an emergency landing when the aircraft struck tree tops and crashed in flames in a wooded area. All four occupants were slightly injured while the aircraft was destroyed.
Probable cause:
It appears that a technical problem occurred with the slats which deployed in an inappropriate angle after rotation. Nevertheless, the cause of the power loss on two engine remains unknown.

Crash of an Ilyushin II-18V off Sochi: 109 killed

Date & Time: Oct 1, 1972 at 1925 LT
Type of aircraft:
Operator:
Registration:
CCCP-75507
Flight Phase:
Survivors:
No
Schedule:
Sochi - Moscow
MSN:
183 0064 05
YOM:
1963
Flight number:
SU1036
Country:
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
101
Pax fatalities:
Other fatalities:
Total fatalities:
109
Aircraft flight hours:
15718
Aircraft flight cycles:
7899
Circumstances:
Shortly after takeoff from Sochi-Adler Airport, while climbing by night at an altitude of 200 meters, the airplane initiated a right turn according to departure procedures then made a left turn, entered a dive and crashed into the Black Sea, about 10 km offshore. Some debris and dead bodies were found in the evening while the main wreckage sank by a depth of about 1,000 meters. None of the 109 occupants survived the crash and the wreckage was not recovered.
Probable cause:
Due to lack of evidences, the exact cause of the accident could not be determined with certainty. However, the assumption that the loss of control may have been caused by the failure of an instrument or an in-flight collision with migratory birds was not ruled out.