Crash of an Antonov AN-12BP near Mexico City: 3 killed

Date & Time: Apr 21, 2010 at 2050 LT
Type of aircraft:
Operator:
Registration:
UP-AN216
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Cebu City - Angeles City
MSN:
4 020 01
YOM:
1964
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The aircraft departed Cebu City on a cargo flight to Angeles City, carrying six crew members and a load of various goods on behalf of UPS. En route, a short circuit occurred in the electrical system, followed by one or more engine failure. The crew elected to divert to the nearest airport. Unfortunately, this was not possible and the captain attempted an emergency landing in a paddy field. The aircraft came to rest on an embankment and was destroyed by a post impact fire. Three crew members were killed while three others were seriously injured.
Probable cause:
In flight short-circuit on the electrical system for unknow reasons.

Crash of an Antonov AN-12B in Heglig

Date & Time: Jan 4, 2010 at 0910 LT
Type of aircraft:
Operator:
Registration:
ST-AQQ
Flight Type:
Survivors:
Yes
Schedule:
Khartoum – Heglig
MSN:
9 3 465 04
YOM:
1969
Flight number:
MGG100
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7050
Captain / Total hours on type:
6000.00
Copilot / Total flying hours:
10038
Copilot / Total hours on type:
7050
Aircraft flight hours:
36190
Circumstances:
The four engine aircraft departed Khartoum Airport at 0738LT on a cargo flight to Heglig, carrying four crew members and a load consisting of 13 tons of various goods. On final approach to Heglig Airport, the aircraft was too low. It collided with obstacles and a concrete block located 16 metres short of runway threshold and housing an element of the approach light system. The aircraft bounced, nosed down and landed nose first 52 metres further. After a course of 183 metres, a tyre on the right main gear burst. The captain instructed the flight engineer to activate the reverse thrust systems but the flight engineer did not check the power levers. The aircraft veered off runway to the left, lost its left main gear and came to rest. All four occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
Wrong approach configuration, causing the aircraft to land short of runway.
The following factors were identified:
- The flight engineer unlocked props I, II, III at throttle position < 20 degrees UPRT and No IV engine at 40 degrees UPRT,
- Unrectification of nose wheel and main landing gear crack as recommended by the manufacturer.

Crash of an Antonov AN-12BK in Brazzaville: 6 killed

Date & Time: Aug 26, 2009 at 0500 LT
Type of aircraft:
Registration:
TN-AIA
Flight Type:
Survivors:
No
Schedule:
Pointe-Noire – Brazzaville
MSN:
6 3 446 07
YOM:
1966
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
The aircraft departed Pointe-Noire Airport at 0400LT on a cargo flight to Brazzaville, carrying one passenger, five crew members and a load consisting of food, one minibus and three cars. On final approach by night to Brazzaville-Maya Maya Airport, at an altitude of about 2,000 feet, the four engine aircraft went out of control and crashed near Nganga Lingolo, 11 km short of runway 05. The aircraft was totally destroyed and all six occupants were killed.

Crash of an Antonov AN-12B in Luxor: 5 killed

Date & Time: Feb 20, 2009 at 0418 LT
Type of aircraft:
Operator:
Registration:
S9-SVN
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Kisangani – Entebbe – Luxor – Mykolaiv
MSN:
6 3 443 10
YOM:
1966
Flight number:
LFT1015
Location:
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
20000
Copilot / Total flying hours:
6397
Aircraft flight hours:
11692
Aircraft flight cycles:
6451
Circumstances:
The four engine aircraft was transferred from Kisangani to Mykolaiv, Ukraine, for maintenance purposes. Two enroute stops were scheduled in Entebbe and Luxor. Ar 0417LT, the crew was cleared for takeoff. The aircraft started rolling on runway 02 for takeoff but it kept rolling on it till it reached its end. The aircraft continued rolling in the sand drifting from the runway centerline to the right, crossing a service road and eventually crashing into a military zone located 500 metres from the runway end. The aircraft crashed into one of the buildings inside the military unit causing complete destruction of the building. The right wing also crashed into another building putting the aircraft on fire and forcing the aircraft to turn right. The aircraft kept moving forward the military unit fence (next to Tiba-Luxor road) and stopped there, crashing in its way into oil barrel. The accident resulted in the total destruction and fire of the aircraft and the fatality of its crew but no further injuries.
Probable cause:
The following factors were identified:
- Lack of available thrust which corresponded to the power of only two engines running during take off run,
- Lack of authorized maintenance of the aircraft,
- The uncoordinated crew actions in the critical situation (both pilots had previously flown as captains). The lack of coordination is confirmed by the braking trails left by the main landing gear at the end of RWY -02, based on FCOM instructions, and in case of rejected takeoff attempt, the crew had to set the throttles to idle, lower the nose gear to reach the runway and then use the propellers for braking (releasing them from the stops). Also, to reduce the roll and to maintain the direction they were to use the nose wheel steering and wheel brakes as well as emergency braking if needed. Actually the crew did neither of the above procedures, except using the main wheel brakes.
Final Report:

Crash of an Antonov AN-12BP in Sharjah

Date & Time: Jan 2, 2009 at 0751 LT
Type of aircraft:
Operator:
Registration:
S9-SAM
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
3341408
YOM:
1963
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll, the left main gear collapsed. The aircraft sank on the runway, causing the left wing and the engine n°1 to contact the runway surface. All six crew members escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
Left main gear collapsed during the takeoff roll for unknown reasons.

Crash of an Antonov AN-12BK near Al-Taqaddum AFB: 7 killed

Date & Time: Nov 13, 2008 at 1124 LT
Type of aircraft:
Operator:
Registration:
S9-SAO
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Al Asad – Bagdad
MSN:
00 346 908
YOM:
1970
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
The four engine aircraft departed Al Asad AFB at 1102LT on a cargo flight to Baghdad with 7 crew members on board, carrying various goods for the allied forces in Iraq. While cruising at an altitude of 9,000 feet, the engine n°2 failed and caught fire. The crew declared an emergency and reduced his altitude in an attempt to make an emergency landing when the aircraft entered an uncontrolled descent and crashed in a desert area located 22 km southeast of Al-Taqaddum AFB, bursting into flames. All seven occupants were killed.
Probable cause:
Failure of engine n°2 for unknown reasons.

Crash of an Antonov AN-12B in Pointe-Noire

Date & Time: Nov 10, 2008
Type of aircraft:
Registration:
UR-PLV
Flight Type:
Survivors:
Yes
MSN:
4 3 423 08
YOM:
1964
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Few minutes after takeoff from Pointe-Noire Airport, while flying 80 km away, the crew contacted ATC and declared an emergency after a fire erupted in the cargo compartment. The crew was able to return and after landing, the aircraft stopped on the main runway, bursting into flames. All six occupants escaped uninjured while the aircraft was destroyed by fire.
Probable cause:
It is believed that the fire started in the cargo bay near a generator.

Ground accident of an Antonov AN-12BK in Luanda

Date & Time: Sep 29, 2008
Type of aircraft:
Operator:
Registration:
T-311
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
8 3 454 10
YOM:
1968
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
While taxiing to runway 23, the aircraft suffered a right landing gear failure and came to rest. There were no injuries and the aircraft was damaged beyond repair.
Probable cause:
Failure of the right main gear for unknown reasons.

Crash of an Antonov AN-12BK near Malakal: 7 killed

Date & Time: Jun 27, 2008 at 0705 LT
Type of aircraft:
Operator:
Registration:
ST-ARN
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Khartoum – Juba
MSN:
8 3 460 10
YOM:
1968
Country:
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Captain / Total flying hours:
13300
Captain / Total hours on type:
5000.00
Copilot / Total flying hours:
11535
Copilot / Total hours on type:
3300
Aircraft flight hours:
14597
Aircraft flight cycles:
6924
Circumstances:
The aircraft departed Khartoum at 0555LT on a cargo flight to Juba with 8 crew members on board. While cruising at FL170 in bad weather conditions, the engines n° 1 failed. One minute later, the engine n°3 failed as well, followed 40 seconds later by the failure of the engine n°4. The aircraft initiated a descent with a rate of 3,450 feet per minute and reach the altitude of 800 feet three minutes and 40 seconds after the failure of the engine n°1. At an altitude of 600 feet, the crew stabilized the aircraft and elected to restart the three engines but without success. Too low, the aircraft struck trees, lost its left stabilizer and crashed in a prairie 264 metres past the initial impact, bursting into flames. A crew member was rescued while 7 other occupants were killed.
Probable cause:
Loss of control and subsequent ground impact following the failure of engine n°1, 3 and 4.
The following contributing factors were identified:
- The crew entered an area of thunderstorm activity with turbulences and icing conditions,
- Unserviceability or sudden failure of the weather radar,
- Accumulation of ice caused the blockage of the engines air intake assembly,
- Following impact with trees, the aircraft lost parts and the running engine n°2 caused the fire.

Crash of an Antonov AN-12BP in Chelyabinsk: 9 killed

Date & Time: May 26, 2008 at 2011 LT
Type of aircraft:
Operator:
Registration:
RA-12957
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Chelyabinsk - Perm
MSN:
8 3 455 08
YOM:
1968
Flight number:
GIA9675
Country:
Region:
Crew on board:
9
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
9
Aircraft flight hours:
42817
Aircraft flight cycles:
14828
Circumstances:
Following an uneventful cargo flight from Moscow to Chelyabinsk where a load of 9 tons of various goods was deplaned, the aircraft was ferried to Perm. One minute after takeoff from Chelyabinsk Airport runway 09, while climbing in marginal weather conditions, the crew declared an emergency and reported smoke in the cockpit. After being cleared to return, the crew completed a circuit. During a third turn to the left, while in a left bank of 15° and at a speed of 335 km/h, both left engines failed and their propellers autofeathered. About 40 seconds later, the aircraft entered a right turn then descended to the ground and crashed in an open field located 11 km from Chelyabinsk Airport, bursting into flames. The accident occurred 8 minutes after takeoff. The aircraft was totally destroyed and all 9 occupants were killed.
Probable cause:
The accident was the result of a loss of controllability due to the destruction of the aileron control cables while carrying out an emergency approach to Chelyabinsk Airport after smoke spread in the cabin and the cockpit. The destruction of aileron wiring occurred, presumably, in the area of the 23-25 web frames of the cargo hold. The reason for the destruction of the wiring installation has most likely been a significant heating of a control rod located in this zone, made of alloy D16-T, and its subsequent break under tension-load operation. Heating of the control rod could be a consequence of fire of the aircraft's electricity network, in immediate proximity of the control rod. This led smoke to spread in the cargo hold, unexpected triggering of alarm systems, aircraft equipment failures, and the auto-shutdown of two engines. Electrical bunch-conductors, distributors, blocks and aggregates of the aeronautical equipment, located in the 15-25 frames zone (ceiling of the cargo compartment) came under intense attack by fire, resulting in a collision collision with the ground, as a result of which it was impossible to accurately determine the primary origin and reason of the fire.