Crash of an Antonov AN-2 in Astrakhan

Date & Time: May 12, 2010
Type of aircraft:
Operator:
Flight Phase:
Survivors:
Yes
Schedule:
Astrakhan - Astrakhan
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
10
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Shortly after takeoff, while in initial climb, the aircraft suffered an engine failure. The crew attempted an emergency landing when the aircraft stalled and crashed in an open field, bursting into flames. All 12 occupants escaped uninjured while the aircraft was destroyed by a post crash fire.
Probable cause:
Engine failure for unknown reasons.

Crash of a PZL-Mielec AN-2R in Goryachy Klyuch

Date & Time: May 6, 2010 at 1026 LT
Type of aircraft:
Operator:
Registration:
RA-40373
Flight Phase:
Survivors:
Yes
Schedule:
Goryachy Klyuch - Goryachy Klyuch
MSN:
1G222-52
YOM:
1986
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
4120
Aircraft flight cycles:
18409
Circumstances:
Shortly after take off from an open field located in Goryachy Klyuch, Krasnodar krai, while at a height of about 15 metres, the single engine aircraft stalled and crashed on a river shore. Both pilots were injured and the aircraft was damaged beyond repair. The crew was supposed to treat a wooded area with chemical products and the aircraft was carrying about 700 liters of this product at the time of the accident.
Probable cause:
The accident of airplane AN-2 RA-40373 was the result of the nose striking the ground during the execution of a forced landing due to shutdown of the ASz-62IR engine while in the process of taking off, most likely due to ingress of water into the carburetor from the fuel system of the aircraft, which led to the shutdown of the engine.
The cause of the accident was a combination of the following factors:
- Failure to comply with guidelines in part: checking facility for storing and dispensing aviation fuels and lubricants, monitoring and verification of the fuel sludge discharge after refueling for the lack of water and solids;
- Execution of a forced landing straight ahead outside the landing area on difficult terrain, covered with forests, a rugged ravine and a creek.
Final Report:

Crash of an Antonov AN-2R near Saransk

Date & Time: Apr 15, 2010 at 2000 LT
Type of aircraft:
Registration:
RF-00259
Flight Phase:
Survivors:
Yes
Schedule:
Saransk - Saransk
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
While on a crop spraying mission, the engine failed. The crew attempted an emergency landing when the aircraft crashed in an open field located about 20 km from Saransk-Lyambir Airport. There were no casualties but the aircraft was damaged beyond repair. It was reported that the Certificate of Airworthiness and the Certificate of Registration were out of date.
Probable cause:
Engine failure for unknown reasons.

Crash of a Tupolev TU-154M in Smolensk: 96 killed

Date & Time: Apr 10, 2010 at 1041 LT
Type of aircraft:
Operator:
Registration:
101
Flight Type:
Survivors:
No
Schedule:
Warsaw - Smolensk
MSN:
90A-837
YOM:
1990
Flight number:
PLF101
Country:
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
88
Pax fatalities:
Other fatalities:
Total fatalities:
96
Captain / Total flying hours:
3531
Captain / Total hours on type:
2906.00
Copilot / Total flying hours:
1909
Copilot / Total hours on type:
475
Aircraft flight hours:
5142
Aircraft flight cycles:
3907
Circumstances:
On approach to Smolensk Airport in poor weather conditions, crew was forced to make a go-around and approach was abandoned three times. On the fourth approach, at a speed of 260 km/h, aircraft went beyond the minimum safe altitude, hit tree tops, lost its left wing and crashed in a huge explosion. All 96 occupants were killed, among them the President of the Polish Republic Lech Kaczyński and his wife. He was flying to Smolensk to take part to the commemoration of the 70th anniversary of Katyn massacre when Soviet Army killed 20,000 Polish officers. Among the delegation were also members of the Polish Senate and Government; the ex President, the vice-president of low Chamber, the Senate vice-president, the president of the polish central bank, the chief of military staff, the chief of ground forces, the chief of the Air Force, the chief of special forces, the chief of Marines, the personal assistant of President, the chief of National Security, the vice-Minister of Defense and the vice-Minister of Foreign Affairs.
Probable cause:
The immediate cause of the accident was the descent below the minimum descent altitude at an excessive rate of descent in weather conditions which prevented visual contact with the ground, as well as a delayed execution of the go-around procedure. Those circumstances led to an impact on a terrain obstacle resulting in separation of a part of the left wing with aileron and consequently to the loss of aircraft control and eventual ground impact.
Circumstances Contributing to the Accident:
1) Failure to monitor altitude by means of a pressure altimeter during a non-precision approach;
2) failure by the crew to respond to the PULL UP warning generated by the TAWS;
3) attempt to execute the go-around maneuver under the control of ABSU (automatic go-around)
4) Approach Control confirming to the crew the correct position of the airplane in relation to the RWY threshold, glide slope, and course which might have affirmed the crew's belief that the approach was proceeding correctly although the airplane was actually outside the permissible deviation margin;
5) failure by LZC to inform the crew about descending below the glide slope and delayed issuance of the level-out command;
6) incorrect training of the Tu-154M flight crews in the 36 Regiment.
Conducive circumstances
1) incorrect coordination of the crew's work, which placed an excessive burden on the aircraft commander in the final phase of the flight;
2) insufficient flight preparation of the crew;
3) the crew‘s insufficient knowledge of the airplane's systems and their limitations;
4) inadequate cross-monitoring among the crew members and failure to respond to the mistakes committed;
5) crew composition inadequate for the task;
6) ineffective immediate supervision of the 36 Regiment's flight training process by the Air Force Command;
7) failure by the 36 Regiment to develop procedures governing the crew's actions in the event of:
a) failure to meet the established approach criteria;
b) using radio altimeter for establishing alarm altitude values for various types of approach;
c) distribution of duties in a multi-crew flight.
8) sporadic performance of flight support duties by LZC over the last 12 months, in particular under difficult WC, and lack of practical experience as LZC at the SMOLENSK NORTH airfield.
Final Report:

Crash of an Antonov AN-74 in Ivanovo

Date & Time: Mar 30, 2010 at 1400 LT
Type of aircraft:
Operator:
Registration:
RA-74017
Flight Phase:
Survivors:
Yes
Schedule:
Ivanovo - Moscow
MSN:
471 95 015
YOM:
2004
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Just after liftoff, at a height of about 3 meters, left engine thrust reverser deployed. The takeoff procedure was aborted but the aircraft veered off runway and came to rest in a field with the cockpit partially separated. All five occupants were injured, both pilots seriously. The aircraft was damaged beyond repair. Configured in a VIP version, it was used by the FSB's Director Nikolai Patrushev and flying back to Moscow at the time of the accident.
Probable cause:
The thrust reverser deployed accidentally on the left engine after rotation due to inappropriate maintenance.

Crash of a Tupolev TU-204-100 in Moscow

Date & Time: Mar 22, 2010 at 0235 LT
Type of aircraft:
Operator:
Registration:
RA-64011
Flight Type:
Survivors:
Yes
Schedule:
Hurghada - Moscow
MSN:
14507413640
YOM:
1993
Flight number:
TUP1906
Country:
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5388
Captain / Total hours on type:
1868.00
Copilot / Total flying hours:
1973
Copilot / Total hours on type:
979
Aircraft flight hours:
18335
Aircraft flight cycles:
4795
Circumstances:
The aircraft was returning to Moscow on a ferry flight after passengers have been dropped off in Hurghada. On approach to Moscow-Domodedovo Airport, the visibility was low due to foggy conditions. Horizontal visibility on runway 14L threshold was 1,300 meters and vertical visibility was 200 feet. In flight, the flight computer failed and the crew continued the approach below minimums. Despite he was not able to establish a visual contact with the runway, the captain continued the approach and failed to initiate a go-around procedure. The aircraft descended below the glide, impacted trees and crashed in a dense wooded area located 1,450 metres short of runway. All eight occupants were injured, three seriously. The aircraft was destroyed.
Probable cause:
The crew performed an approach in below-minima weather conditions for an airplane with a defective flight computer. The crew failed to initiate a go-around procedure while unable to establish a visual contact with the runway.
Contributing factors were:
- Insufficient training of the crew to perform approaches at or near weather minimums,
- Lack of control over the activities of the crew, which led to poor resource management (CRM) of the captain,
- Failure of the flight control computer system, which led to an increase in the allowed weather minima of the aircraft,
- Failure of captain to divert to another airport,
- Failure of captain to decide about a missed approach when there was visual contact with the approach lights,
- Failure of the co-pilot to call for a missed approach,
- Unsatisfactory interaction in the crew, resulting in a descent below safe altitude.
Final Report:

Crash of a Technoavia SM-92T Turbo Finist in Kalachevo: 8 killed

Date & Time: Dec 13, 2009 at 1100 LT
Operator:
Registration:
RA-0257G
Flight Phase:
Survivors:
No
Schedule:
Kalachevo - Kalachevo
MSN:
02-005
YOM:
1997
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
8
Captain / Total flying hours:
4658
Captain / Total hours on type:
98.00
Aircraft flight hours:
536
Aircraft flight cycles:
1378
Circumstances:
The single engine was completing local skydiving sorties at Kalachevo Airport, about 24 kkm south of Chelyabinsk. Shortly after takeoff, while climbing to a height of about 100 metres, the aircraft stalled and crashed in a snow covered field located 1,5 km north of the airfield. The aircraft was totally destroyed upon impact and all 8 occupants were killed.
Probable cause:
The accident was the consequence of a stall during initial climb due to the combination of the following factors:
- Violation of the climb procedures regarding the speed,
- Flight performances were not met as the aircraft was operated for skydiving purposes but not intended for such type of flight,
- The total weight of the aircraft was above the MTOW,
- The aircraft was not equipped with a system that could inform the pilot of the imminence of a stall,
- The aircraft stalled at a relative low altitude that could not allow the pilot to expect recovery.
Final Report:

Ground accident of an Ilyushin II-76MD in Ivanovo

Date & Time: Nov 7, 2009
Type of aircraft:
Operator:
Registration:
RA-86894
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
00134 32977
YOM:
1981
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
6200
Circumstances:
The crew lined up on runway and was cleared for takeoff. Power was added on all four engine and the crew started the takeoff roll when the engine n°3 detached from its pylon, fall on the ground and rolled for about 150 metres before coming to rest. The crew stopped the airplane and evacuated safely. The aircraft was damaged beyond repair.
Probable cause:
The engine n°3 detached during the takeoff roll for unknown reasons.

Crash of a Tupolev TU-142MZ in the Tatar Strait: 11 killed

Date & Time: Nov 6, 2009 at 2119 LT
Type of aircraft:
Operator:
Registration:
55 red
Flight Type:
Survivors:
No
Schedule:
Mongokhto AFB - Mongokhto AFB
MSN:
0 60 41 75
YOM:
1990
Country:
Region:
Crew on board:
11
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
11
Circumstances:
Following a training flight over the Okhotsk Sea, the four engine was returning to its base at Mongokhto AFB. While descending by night, the aircraft crashed in the Tatar Strait between the Island of Sakhalin and the Sikhote-Alin region. Some debris were found about 15 km off Sadinga Cape. All 11 occupants were killed.

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.