Country
code

Republic of Yakutia (Sakha)

Crash of an Ilyushin II-76MD in Mirny: 11 killed

Date & Time: Nov 1, 2009 at 0849 LT
Type of aircraft:
Registration:
RF-76801
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Mirny – Irkutsk – Chita
MSN:
00934 95866
YOM:
1989
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
11
Circumstances:
The four engine aircraft departed Mirny on a positioning flight to Chita with an intermediate stop in Irkutsk, carrying four passengers and a crew of seven on behalf of the Russian Ministry of the Interior. Shortly after takeoff by night, the aircraft rolled to the right to an angle of 90° then crashed at a speed of 364 km/h some 1,893 metres past the runway end. The aircraft was totally destroyed and all 11 occupants were killed. The accident occurred 59 seconds after takeoff.
Probable cause:
The day before the accident, the aircraft arrived in Mirny following a cargo flight, delivering various goods. After landing, the crew activated the electrical locking system for the rudder and the ailerons, and the 'lock on' light came on in the cockpit panel. In the morning of the accident, prior to takeoff, the crew followed the pre-takeoff checklist and deactivated the electrical locking system, but the 'lock on' light remained illuminated. Considering this as a false alarm, the captain decided to take off and proceeded with a manuel control of the ailerons. The left aileron moved normally while the right aileron got locked because of the locking mechanism. During the takeoff roll, because the four engine were not in full power mode, there was no sound alarm about the aileron locked mechanism. The aircraft deviated to the right and after lift off, it rolled to the right to angle of 8°. The pilot-in-command elected to counteract the banking but this maneuver was limited due to the right aileron locked mechanism. The aircraft continued to roll to the right to an angle of 90° until control was lost.

Crash of a PZL-Mielec AN-2T in Pokrovsk: 3 killed

Date & Time: Apr 30, 2009 at 2325 LT
Type of aircraft:
Operator:
Registration:
RF-00842
Flight Type:
Survivors:
No
Schedule:
Krasnoyarsk - Lensk - Yakutsk
MSN:
1G195-55
YOM:
1980
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The crew was completing a positioning flight from Krasnoyarsk to Yakutsk with an intermediate stop in Lensk. The intended destination was in fact Prokovsk located about 70 km southwest of Yakutsk but the airfield was not suitable for night movements. On approach to Yakutsk-Magan Airport, the crew continued to Prokovsk where several cars were parked along the runway with their lights ON. Due to low visibility caused by night and snow falls, the crew was unable to establish a visual contact with the ground and two approaches were missed. During a third attempt to land, the aircraft collided with pine trees and power cables and crashed in an open field, bursting into flames. All three occupants were killed.
Probable cause:
The decision of the crew to land on an airfield that was not equipped for night movements.

Crash of a PZL-Mielec AN-2TP near Sangar

Date & Time: Nov 18, 2005 at 1407 LT
Type of aircraft:
Operator:
Registration:
RA-02252
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
Schedule:
Sangar – Segyan-Kyuel – Sangar
MSN:
1G234-06
YOM:
1989
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
10
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft was engaged in an ambulance flight from Sangar to Segyan-Kyuel and back. Because of poor weather the flight was delayed a couple of hours. At ETD, weather conditions at Sangar Airport was as follows: visibility more than 10 km, scattered clouds at 800 metres, overcast at 3,000 metres, temperature -22° C, dewpoint -23° C, pressure 765 mm Hg. Weather forecast en route included a few stratocumulus clouds between 1,400 and 1,700 metres, significant altostratus clouds between 2,700 and 3,500 metres. The mountainous area over which the Antonov was to fly moderate orographic turbulence was present in the layer from 900 to 1,700 meters, and possible downdrafts on the lee side of ridge in the same altitude range. These conditions were not reported to the crew. Then medical equipment with a weight of 400 kg and passengers arrived at the airport by ambulances. The captain expected seven passengers, but three additional passengers had arrived, without having tickets. The names were added to the passenger list and the copilot arranged the payment of the fare. No seats were available for two passengers, so they had to sit on some hand luggage in the aisle. At 04:46 UTC the aircraft departed from Sangar and climbed towards the mountainous terrain. The highest point along the route was at an elevation of 1,976 metres. The minimum safe altitude was 2,515 metres. The pilot climbed VFR and maintained visual separation from the snow-covered mountains. At an altitude of 1,300 metres the Antonov entered an area with strong turbulence. The aircraft was caught in a downdraft. In an attempt to stop the plane from descending further, power was added to nominal, then to the takeoff power. With rising terrain it was impossible to continue. The pilot decided to carry out a 180° turn to the left over downsloping terrain. This brought the plane downwind with a 30° bank instead of the recommended 20°. As a result, the rate of descent increased and after it rolled to an angle of 120°, the left lower wing contacted a cliff. The aircraft lost speed and crashed on the snow covered mountain. All 12 occupants were rescued, among them four were seriously injured. The aircraft was destroyed.
Probable cause:
The following findings were identified:
- The crew carried out a flight at a height lower than the minimum safe altitude,
- Incorrect estimation by the crew of the prevailing situation, which led to a late decision to return to the airport of departure under the conditions of orographic turbulence and airspace limited by mountains,
- Deficiencies in the flight instructions at the airport Of Sangar, due to the absence a.o. of an altitude diagram of the route of flight, which would have shown that it was impossible for the airplane, according to its technical flight characteristics, to gain enough height within 10 km after takeoff,
- The incorrect weather forecast along the flight course, in which the orographic turbulence was not provided,
- The erroneous actions of the crew in the process of the downwind turn with a bank angle of 30° while carrying out the delayed decision to return to the airport of departure, leading to an increase in the vertical rate of descent.

Crash of a PZL-Mielec AN-2TP near Amakinskaya

Date & Time: Oct 9, 2003
Type of aircraft:
Operator:
Registration:
RA-01440
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Olenek - Amakinskaya
MSN:
1G231-20
YOM:
1988
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The single engine airplane departed Olenek on a cargo flight to Amakinskaya (Aykal) with two pilots on board and a load consisting of five fuel drums for a total weight of 900 kilos. While cruising at an altitude of 1,150 metres, the engine exploded and stopped. The crew elected to carry out an emergency landing in a field located 49 km north of Amakinskaya-3 Airport. On landing, the aircraft hit small trees and crashed. Both pilots escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
The engine failure was the consequence of a fatigue fracture on the n°1 cylinder.

Crash of an Antonov AN-3T near Sangar

Date & Time: May 16, 2003 at 1321 LT
Type of aircraft:
Operator:
Registration:
RA-05881
Flight Phase:
Survivors:
Yes
Schedule:
Sangar – Yakutsk
MSN:
2218-18-01
YOM:
2002
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
11
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
En route from Sangar to Yakutsk-Magan Airport, while cruising at an altitude of 1,000 metres in snow falls, the engine failed. The aircraft lost height and the crew attempted an emergency landing when the aircraft struck trees and crashed in a swampy and wooded area located 45 km from Sangar. All 13 occupants were injured and the aircraft was damaged beyond repair.
Probable cause:
Failure of the engine in flight after melted snow and ice entered the engine air intake. The following contributing factors were identified:
- The crew failed to feather the propeller after the engine failed, causing high drag,
- The crew modified his route and continued the prescribed altitude,
- Weather conditions were poor and did not allow to fly under VFR mode,
- Lack of ATC assistance.

Crash of an Antonov AN-26B in Ust-Kuyga

Date & Time: Dec 27, 2002
Type of aircraft:
Operator:
Registration:
RA-26053
Flight Type:
Survivors:
Yes
Schedule:
Yakutsk - Ust-Kuyga
MSN:
109 09
YOM:
1981
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
17609
Aircraft flight cycles:
9649
Circumstances:
Following an uneventful cargo flight from Yakutsk, the crew started the approach to Ust-Kuyga on a polar night with an OAT of -51° C. On final approach, at a distance of 1,150 metres from the runway threshold, the aircraft deviated to the right by 150 metres. The captain was instructed by ATC to initiate a go-around but he decided to continue the approach. Unstable, the aircraft's speed dropped to 210 km/h and on the last segment, it lost height, causing the right main gear to struck the runway surface. On impact, the right main gear was torn off, followed shortly later by the nose gear. Out of control, the aircraft slid for few dozen metres before coming to rest. All six occupants escaped uninjured and the aircraft was damaged beyond repair.
Probable cause:
The following findings were identified:
- Wrong approach configuration on part of the crew,
- The aircraft was unstable on approach,
- The approach' speed of 210 km/h was insufficient (20 km/h below the prescribed speed),
- On the last segment, the aircraft rolled to the right following improper actions from the crew,
- The crew failed to initiate a go-around and ignored ATC instructions,
- The configuration adopted by the crew resulted in the aircraft making a deliberate descent to the right of the approach pattern.

Crash of an Antonov AN-24RV in Yakutsk

Date & Time: Jul 13, 2002 at 1418 LT
Type of aircraft:
Operator:
Registration:
RA-46670
Flight Type:
Survivors:
Yes
Schedule:
Yakutsk - Yakutsk
MSN:
47309601
YOM:
1974
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The Antonov departed Yakutsk on a crew training flight. Two approach and landings were carried out using flap settings of 38 and 15 degrees. During the third approach the captain called for lowering of the landing gear. The flight engineer moved the landing gear handle from neutral into the "retract" position. He did not check for three greens so failed to notice his mistake. Then the captain requested the flaps to be selected at 10 degrees. The Antonov turned to finals, but the crew did not carry out the final approach checks and continued after having obtained landing clearance. Fourteen seconds before touchdown an air traffic controller informed the crew that they should go around because the landing gear was not down. The captain did not hear this because at that moment height and speed were called out by the flight engineer. Five seconds later the controller repeated his warning. One of the crew members heard the call and noticed three reds on the instrument panel. He informed that captain about this, but it was already too late. The captain added takeoff power, but within three seconds the tail struck the runway. The airplane skidded about 1000 metres before coming to rest.
Probable cause:
The accident was caused by the combination of the following factors:
- The erroneous actions of the flight engineer when trying to lower the landing gear,
- Failure of the flight crew to conduct the necessary (final approach) checks,
- The failure by the crew to check and respond to landing gear warning indications,
- The execution of a flight with an incomplete composition of crew, causing additional workload on the flight engineer during the approach (height and speed call outs),
- Late commands to go around by the air traffic controller,
- On the Yak-40 the landing gear handle moves to the opposite direction for retraction and lowering compared to the Antonov 24 (the flight mechanic had more, and recent, flight experience on the Yakovlev 40 jet),
- The large workload and fatigue of the crew during the recent six days before the incident.

Crash of a PZL-Mielec AN-2T near Polyarny

Date & Time: Oct 6, 2001 at 1732 LT
Type of aircraft:
Operator:
Registration:
RA-40480
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Polyarny - Olenek
MSN:
1G224-57
YOM:
1987
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew departed Polyarny Airport on a cargo flight to Olenek. En route, weather conditions worsened with mist, low clouds and icing conditions. The crew decided to return to Polyarny when the engine lost power. Unable to maintain a safe altitude, he attempted an emergency landing when the aircraft crash landed in rough terrain. All three occupants were injured and the aircraft was damaged beyond repair.
Probable cause:
The following contributing factors were identified:
- A possible unpremeditated entry into conditions with severe icing and late decision making by the captain to manoeuvre the aircraft away from the icing area,¨
- A loss of engine power and a subsequent loss of speed due to icing of the carburetor,
- The failure of the captain to remove ice from the propeller blades by changing their pitch mode.

Crash of a PZL-Mielec AN-2T in Kobyay

Date & Time: Apr 23, 2001 at 1745 LT
Type of aircraft:
Operator:
Registration:
RA-01122
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Pokrovsk – Magan – Kobyay – Sangar
MSN:
1G238-04
YOM:
1990
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
11
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
2135
Aircraft flight cycles:
3112
Circumstances:
The aircraft departed Pokrovsk on an ambulance flight to Sangar with intermediate stops in Magan and Kobyay. On approach to Kobyay Airport, the aircraft was too high and its speed was excessive. Rather than initiating a go-around procedure, the captain continued the approach and landed 375 metres pas the runway threshold (the runway length is 600 metres). Unable to stop within the remaining distance, the aircraft overran, collided with various obstacles and came to rest 50 metres further. The crew did not report the incident to the company and decided to take off few minutes later. After liftoff, the aircraft was unable to gain sufficient speed and height. It struck trees and crashed in a snow covered terrain, bursting into flames. All 13 occupants were injured, among them five seriously. The aircraft was destroyed by fire.
Probable cause:
It was determined that the captain was intoxicated at the time of the accident and that he started the mission from Pokrovsk already drunk. He took the decision to take off from Kobyay Airstrip despite the propeller blades have been damaged during the previous overrun.

Crash of a PZL-Mielec AN-2T near Yakutsk: 1 killed

Date & Time: Jul 8, 1998
Type of aircraft:
Operator:
Registration:
RA-02823
Flight Phase:
Survivors:
Yes
Schedule:
Yakutsk – Kobyay – Sangar
MSN:
1G199-48
YOM:
1983
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The aircraft was engaged in a special flight from Yakutsk to Sangar with an intermediate stop in Kobyay, carrying doctors who came to provide care to local populations. Few minutes after takeoff from Yakutsk-Magan Airport, while cruising at an altitude of 1,150 metres at a speed of 180 km/h, the engine started to vibrate and lost power, Also, the oil pressure dropped and the speed decreased. The captain attempted an emergency landing in a swampy area when the aircraft rolled for about 32 metres and nosed over. A passenger was killed and all other occupants were injured, four seriously.
Probable cause:
Engine failure following the failure of the first cylinder and piston due to fatigue.