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 near Grossevichi: 98 killed

Date & Time: Dec 7, 1995 at 0308 LT
Type of aircraft:
Operator:
Registration:
RA-85164
Flight Phase:
Survivors:
No
Site:
Schedule:
Yuzhno-Sakhalinsk - Khabarovsk - Ulan-Ude – Novosibirsk
MSN:
76A164
YOM:
1976
Flight number:
KHB3949
Country:
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
90
Pax fatalities:
Other fatalities:
Total fatalities:
98
Captain / Total flying hours:
12225
Captain / Total hours on type:
5054.00
Copilot / Total flying hours:
10294
Copilot / Total hours on type:
1620
Aircraft flight hours:
30001
Aircraft flight cycles:
13801
Circumstances:
En route from Yuzhno-Sakhalinsk to Khabarovsk, while cruising at the assigned altitude of 10,600 metres, about 35 minutes after takeoff, the aircraft rolled to the right, entered an uncontrolled descent and crashed in a mountainous and isolated area located in the Sikhot-Alin Mountain Range. SAR operations were initiated but suspended a day later due to the deterioration of the weather conditions and started again four days later. The wreckage was found 11 days later about 50 km west of Grossevichi. The aircraft disintegrated on impact and all 98 occupants were killed.
Probable cause:
It was determined that the crew selected the left main fuel tank to feed all three engines after takeoff from Yuzhno-Sakhalinsk. During 35 minutes of flight, the automatic pilot system was able to control and counteract the imbalance caused by the fuel consumption on one side only. Eventually, the aircraft started to bank right and the crew reaction to an unexpected situation was non compliant, causing the aircraft to enter an uncontrolled descent.

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

Date & Time: Jan 21, 1995
Type of aircraft:
Operator:
Registration:
UN-85455
Flight Phase:
Survivors:
Yes
Schedule:
Karachi - Almaty
MSN:
80A455
YOM:
1980
Country:
Region:
Crew on board:
12
Crew fatalities:
Pax on board:
105
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll at Karachi-Quaid-e-Azam Airport, at a speed of 270-280 km/h, the pilot-in-command pulled up on the control column to start the rotation but the aircraft failed to respond. The crew decided to abandon the takeoff procedure and initiated an emergency braking procedure. Unable to stop within the remaining distance, the aircraft overran, rolled for about 500 metres then lost its nose gear and came to rest. All 117 occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
It was determined that the crew failed to prepare the flight according to published procedures. The mass and balance sheet was incorrect. At the time of the accident, the total weight of the aircraft was six tons above MTOW and the CofG as too far forward.

Crash of a Tupolev TU-154M near Xi'an: 160 killed

Date & Time: Jun 6, 1994 at 0822 LT
Type of aircraft:
Operator:
Registration:
B-2610
Flight Phase:
Survivors:
No
Schedule:
Xi'an - §Guangzhou
MSN:
86A740
YOM:
1986
Flight number:
WH2303
Location:
Country:
Region:
Crew on board:
14
Crew fatalities:
Pax on board:
146
Pax fatalities:
Other fatalities:
Total fatalities:
160
Aircraft flight hours:
12507
Aircraft flight cycles:
6651
Circumstances:
Twenty-four seconds after takeoff, while climbing, the crew encountered controllability problems. The captain contacted ATC and reported uncommanded rolled left and right up to 30°. The aircraft continued to climb but reached a high angle of attack when it nosed up to 20°, activating the stall warning alarm. The aircraft reached the altitude of 4,717 metres then rolled to the left, pitched down to an angle of 65° and entered an uncontrolled descent. At a speed of 747 km/h, the aircraft descended to the altitude of 2,884 metres in 12 seconds then suffered structural deformation and failure before crashing in an open field located 29 km southeast of Xi'an Airport. The aircraft disintegrated on impact and all 160 occupants were killed.
Probable cause:
It was determined that the loss of control was the consequence of poor maintenance. The previous evening, the autopilot yaw-channel had been erroneously connected to the bank control and the bank-channel to the yaw control, after maintenance was completed at an unapproved facility.

Crash of a Tupolev TU-154 in Irkoutsk: 125 killed

Date & Time: Jan 3, 1994 at 1207 LT
Type of aircraft:
Operator:
Registration:
RA-85656
Flight Phase:
Survivors:
No
Schedule:
Irkutsk - Moscow
MSN:
89A801
YOM:
1989
Flight number:
BKL130
Country:
Region:
Crew on board:
9
Crew fatalities:
Pax on board:
115
Pax fatalities:
Other fatalities:
Total fatalities:
125
Circumstances:
While preparing the flight, the crew encountered technical problems with the engine n°2 and 17 minutes were necessary to start all three engines. A technical issue occurred with the starter of the engine n°2 and a warning light came on in the cockpit. The crew did not find any corrective actions in the operations manual and as he thought the warning was false, decided to take off. Four minutes after the aircraft departed Irkutsk Airport runway 12, while climbing, the starter located in the engine n°2 failed. Debris scattered around and hydraulic and fuel lines were cut. The crew declared an emergency and was cleared for an immediate return after the engine n°2 caught fire. Unfortunately, the crew was unable to extinguish the fire and the aircraft entered an uncontrolled descent and eventually crashed on farm buildings located about 11 km from the airport. The aircraft disintegrated on impact and all 124 occupants were killed as well as one farmer. Another farmer was seriously injured.
Probable cause:
The commission found that the air starter malfunction occurred when the engine was started due to a structural element of the air conditioning system, probably a fragment of the air-to-air radiator (VVR) splitter of engine n°2, hit under the constant pressure flap. This became possible due to the lack of protection against the ingress of foreign objects from the air lines and the low operational reliability of the VVR. A constant supply of air under pressure from the engines operating at a mode close to the nominal through an open damper led to the starter not switching off and the turbine rotor spinning up to off-design speed with the alarm "Dangerous starter speed" being triggered, which was detected by the flight engineer after starting all the engines. Pressing the starter shutdown button did not turn off the alarm. There were no other signs of failure other than the operation of the warning lamp. The crew, believing that the alarm was false, made the wrong decision to take off, which was a consequence of the unwillingness to act in such a situation due to shortcomings in the regulatory documentation, information support, as well as insufficient information content of the starter's technical condition monitoring system in the cockpit. Laying the mains of all three hydraulic systems through the fire-hazardous compartment of the engine n°2 is a constructive disadvantage of the Tu-154M aircraft.

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-154B in Sukhumi: 108 killed

Date & Time: Sep 22, 1993 at 1830 LT
Type of aircraft:
Operator:
Registration:
4L-85163
Survivors:
Yes
Schedule:
Tbilisi - Sukhumi
MSN:
76A163
YOM:
1976
Country:
Region:
Crew on board:
12
Crew fatalities:
Pax on board:
120
Pax fatalities:
Other fatalities:
Total fatalities:
108
Circumstances:
On final approach to Sukhumi-Babushara Airport, the aircraft was shot down by a surface-to-air missile and crashed near the runway threshold, bursting into flames. 24 people survived while 108 others were killed. All passengers were Georgian soldiers and policeman dispatched to Sukhumi.
Probable cause:
Shot down by a surface-to-air missile fired by Abkhazi separatists.

Crash of a Tupolev TU-154M near Tehran: 131 killed

Date & Time: Feb 8, 1993 at 1416 LT
Type of aircraft:
Operator:
Registration:
EP-ITD
Flight Phase:
Survivors:
No
Schedule:
Tehran - Mashhad
MSN:
91A903
YOM:
1991
Country:
Region:
Crew on board:
12
Crew fatalities:
Pax on board:
119
Pax fatalities:
Other fatalities:
Total fatalities:
131
Circumstances:
The aircraft just departed runway 29R at Tehran-Mehrabad Airport and and continued to climb when it collided with an Iranian Air Force Su-24MK fighter that was preparing to land on runway 29L. Both aircraft entered an uncontrolled descent and crashed on a military depot located 15 km from the airport. All 131 occupants of the TU-154 and both pilots on board the fighter were killed.
Probable cause:
It is believed that the collision was the consequence of a poor coordination between civil and military ATC.