Ground collision with a Fokker F27 in Edinburgh

Date & Time: Feb 2, 2008 at 2115 LT
Type of aircraft:
Operator:
Registration:
TC-MBG
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Edinburgh - Coventry
MSN:
10459
YOM:
1971
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4080
Captain / Total hours on type:
2745.00
Circumstances:
The aircraft was scheduled to operate a night cargo flight from Edinburgh to Coventry. The weather conditions at Edinburgh Airport were wintry with snowfall, which required the aircraft to be de-iced. Shortly after both engines had been started, the commander signalled to the marshaller to remove the Ground Power Unit (GPU) from the aircraft, which was facing nose out from its stand, down a slight slope. As the marshaller went to assist his colleague to remove the GPU to a safe distance prior to the aircraft taxiing off the stand, the aircraft started to move forward slowly, forcing them to run to safety. The flight crew, who were looking into the cockpit, were unaware that the aircraft was moving. It continued to move forward until its right propeller struck the GPU, causing substantial damage to the GPU, the propeller and the engine. The ground crew were uninjured. No cause as to why the aircraft moved could be positively identified.
Probable cause:
The aircraft moved forward inadvertently after engine start, causing its right propeller to strike a GPU. Possible explanations include that the parking brake was not set, the chocks had slipped from the nosewheel, or the chocks were removed prematurely. There was insufficient evidence to determine which of these scenarios was the most likely. Contributory factors were: the aircraft was facing down a slight downslope, the ramp was slippery due to the weather conditions and the flight crew increased engine speed to top up the pneumatic system pressure. The airport operator’s instructions contained in MDD 04/07 required aircraft facing nose-out on North Cargo Apron stands to be towed onto the taxiway centreline, prior to starting engines. Had these instructions been complied with, the accident would probably have been avoided.
Final Report:

Crash of a Britten-Norman BN-2A-26 Islander in Anguilla

Date & Time: Feb 2, 2008 at 1420 LT
Type of aircraft:
Operator:
Registration:
VP-AAG
Flight Type:
Survivors:
Yes
Schedule:
Anguilla - Sint Maarten
MSN:
88
YOM:
1969
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4217
Captain / Total hours on type:
693.00
Circumstances:
The commander intended to fly the BN-2 Islander aircraft from Anguilla Wallblake International Airport (AXA) to the neighbouring island of St Maarten (SXM) to await cargo inbound on another flight. The cabin of the aircraft was configured for cargo operations with no passenger seats fitted, as the only other planned occupant was the operator’s Chief Engineer, who would be sitting beside the commander in the right hand seat. However, the commander asked the operator if he could take a family member with him to SXM. The operator agreed and an extra seat was fitted. Witnesses stated that the commander appeared "rushed" prior to departure. The commander stated that he partially carried out the normal pre-flight inspection. He then started the engines. Before taxiing he realised that the nose landing gear chocks were still in place so he shut down the left hand engine, removed and stowed the chocks and then restarted the left engine. The aircraft took off from runway 10 at 14:15 hrs. At between 100 ft and 150 ft the commander initiated a left turn but after some initial movement the ailerons jammed. When he discovered that he was unable to straighten the ailerons he attempted to return to land on runway 10. The other flight controls did not appear to be restricted. With the ailerons jammed, the aircraft continued to turn to the left, losing altitude as it flew over a settlement to the north of the aerodrome, until pointed directly at the Air Traffic Control tower, causing the Air Traffic Control Officer (ATCO) to abandon the tower. The commander judged that the aircraft was too fast and high to attempt a landing and therefore initiated a go-around, applying full power. He continued the left turn, losing height and speed to position the aircraft for another approach but, as the aircraft descended over the northern edge of the runway, its left wing struck the perimeter fence. On impact the aircraft spun about its vertical axis with its wings level and continued sliding sideways on its right side for approximately 80 ft before coming to rest facing north-west.
Probable cause:
The commander was probably distracted from his normal duties whilst arranging additional seating to accommodate the second passenger. He did not complete the requisite pre-flight check or the subsequent check of full and free movement of the flight controls, either of which would have revealed an obstruction to proper operation of the ailerons.
Final Report:

Serious incident with a Boeing 747-2D7B in Lomé

Date & Time: Feb 2, 2008
Type of aircraft:
Operator:
Registration:
N527MC
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Lomé - Amsterdam
MSN:
22471/504
YOM:
1981
Flight number:
GTI014
Location:
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Shortly after take off from Lomé international Airport, while on a cargo flight to Amsterdam, the crew declared an emergency and was cleared for an immediate return. The approach and landing were considered as normal and the aircraft returned safely to the apron. While all three crew members were uninjured, the aircraft was damaged beyond repair due to bulkhead destruction.
Probable cause:
It appears that the cargo shifted shortly after rotation and destroyed the bulkhead and several others structural parts inside the airplane.

Crash of a Casa 212 Aviocar 200 in Long Apung: 3 killed

Date & Time: Jan 26, 2008 at 0936 LT
Type of aircraft:
Operator:
Registration:
PK-VSE
Flight Type:
Survivors:
No
Schedule:
Tarakan – Long Apung
MSN:
412/92N
YOM:
1993
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
21019
Captain / Total hours on type:
14234.00
Copilot / Total flying hours:
16849
Copilot / Total hours on type:
16849
Aircraft flight hours:
11750
Aircraft flight cycles:
13749
Circumstances:
On 26 January 2008, a Casa 212-200 aircraft, registered PK-VSE, was being operated by PT. Dirgantara Air Service as a cargo charter flight from Tarakan Airport to Long Apung Airport. There were 3 persons on board; two pilots and one aircraft maintenance engineer/load master. The aircraft was certified as being airworthy prior to departure. The aircraft departed from Tarakan at 0011 UTC (08:11 local time), and the estimated time arrival at Long Apung was 0136. At 0411 the pilot of another aircraft received a distress signal and informed air traffic services at Tarakan. Searchers subsequently found the aircraft wreckage at an elevation of 2,766 feet, about 3.4 NM from Long Apung Airport. The coordinates of the accident site were 01° 39.483′ S and 115° 00.265′ E near Lidung Payau Village, Malinau, East Kalimantan. The accident site was on the left downwind leg of the runway 35 circuit.
Probable cause:
The following findings were identified:
• The aircraft was certified as being airworthy prior to departure.
• All crew members held appropriate and valid flight crew licenses.
• The pilots continued flight into instrument meteorological conditions.
• The aircraft impacted terrain in controlled flight.
• The cargo was not adequately restrained.
Causes:
The crew did not appear to have awareness of the aircraft’s proximity with terrain until impact with terrain was imminent. The pilot attempted to continue the flight in instrument meteorological
conditions, below the lowest safe altitude.
Final Report:

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

Date & Time: Jan 25, 2008
Type of aircraft:
Operator:
Registration:
EK-11660
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Brazzaville – Pointe-Noire
MSN:
5 3 432 09
YOM:
1965
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft departed Brazzaville on a cargo flight to Pointe-Noire, carrying six crew members and a load of various goods. Following a normal landing, the crew vacated the runway and while approaching the apron, they lost control of the aircraft that collided with a parked Boeing 727-246 registered 9L-LEF and operated by Canadian Airways Congo. All six crew members on board the AN-12 were injured, both pilots seriously. Both aircraft were damaged beyond repair. The Boeing 727 was empty at the time of the ground collision.
Probable cause:
It is believed that the loss of control was the consequence of a brakes failure.

Crash of a Rockwell Aero Commander 500B in Tulsa: 1 killed

Date & Time: Jan 16, 2008 at 2243 LT
Operator:
Registration:
N712AT
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Tulsa - Oklahoma City
MSN:
500-1118-68
YOM:
1961
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
4373
Captain / Total hours on type:
695.00
Aircraft flight hours:
17888
Circumstances:
The commercial pilot departed on a night instrument flight rules flight in actual instrument meteorological in-flight conditions. Less than 2 minutes after the airplane departed the airport, the controller observed the airplane in a right turn and instructed the pilot to report his altitude. The pilot responded he thought he was at 3,500 feet and he thought he had lost the gyros. The pilot said he was trying to level out, and when the controller informed the pilot he observed the airplane on radar making a 360-degree right turn , the pilot said "roger." Three minutes and 23 seconds after departure the pilot said "yeah, I'm having some trouble right now" and there were no further radio communications from the flight. The on scene investigation disclosed that both wings and the tail section had separated from the airframe. All fractures of the wing and wing skin were typical of ductile overload with no evidence of preexisting failures such as fatigue or stress-corrosion. The deformation of the wings indicated an upward failure due to positive loading. No anomalies were noted with the gyro instruments, engine assembly or accessories
Probable cause:
The pilot's loss of control due to spatial disorientation and the pilot exceeding the design/stress limits of the aircraft. Factors contributing to the accident were the pilot's reported gyro problem, the dark night conditions , and prevailing instrument meteorological conditions.
Final Report:

Crash of a Cessna 208B Super Cargomaster in Columbus: 2 killed

Date & Time: Dec 5, 2007 at 0651 LT
Type of aircraft:
Operator:
Registration:
N28MG
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Columbus - Buffalo
MSN:
208B-0732
YOM:
1999
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
1310
Captain / Total hours on type:
200.00
Aircraft flight hours:
9936
Aircraft flight cycles:
9033
Circumstances:
The cargo flight was departing on its fourth flight leg of a five-leg flight in night instrument conditions, which included a surface observation of light snow and a broken ceiling at 500 feet above ground level (agl). One pilot who departed just prior to the accident flight indicated that moderate snow was falling and that he entered the clouds about 200 feet agl. The accident airplane's wings and tail were de-iced prior to departure. Radar track data indicated the accident flight was about 45 seconds in duration. An aircraft performance radar study indicated that the airplane reached an altitude of about 1,130 feet mean sea level (msl), or about 400 feet above ground level, about 114 knots with a left bank angle of about 29 degrees. The airplane descended and impacted the terrain at an airspeed of about 155 knots, a pitch angle of -16 degrees, a left roll angle of 22 degrees, and a descent rate of 4,600 feet per minute. The study indicated that the engine power produced by the airplane approximately matched the engine power values represented in the pilot's operating handbook. The study indicated that the required elevator deflections were within the available elevator deflection range, and that the center-of-gravity (CG) position did not adversely affect the controllability of the airplane. The study indicated that the load factor vectors, the forces felt by the pilot, could have produced the illusion of a climb, even when the airplane was in a descent. The inspection of the airframe and engine revealed no anomalies that would have precluded normal operation.
Probable cause:
The pilot's failure to maintain aircraft control and collision avoidance with terrain due to spatial disorientation. Contributing to the accident were the low cloud ceiling and night conditions.
Final Report:

Crash of an Antonov AN-12TB in Khartoum: 2 killed

Date & Time: Nov 8, 2007 at 0807 LT
Type of aircraft:
Operator:
Registration:
ST-JUA
Flight Type:
Survivors:
Yes
Schedule:
Khartoum - Juba
MSN:
3 3 411 10
YOM:
1963
Flight number:
JUC700
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Aircraft flight hours:
11787
Aircraft flight cycles:
7220
Circumstances:
The four engine aircraft departed Khartoum-Haj Yusuf Airport at 0759LT on a cargo flight to Juba, carrying four crew members and a load of 11 tons of various goods. After takeoff, while climbing, the crew reported the failure of the engine n°3 and was cleared to return for an emergency landing. After touchdown, the aircraft went out of control, veered off runway and came to rest in the military area of the airport, bursting into flames. All four crew members were injured while two people on the ground were killed. The aircraft was destroyed by a post crash fire.
Probable cause:
Failure of the engine n°3 during initial climb following a bird strike.

Crash of an Antonov AN-26 near Tripoli

Date & Time: Oct 31, 2007
Type of aircraft:
Operator:
Registration:
5A-DOZ
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
MSN:
125 04
YOM:
1982
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances in a desert area near Atoqah. There were no injuries but the aircraft was destroyed in the accident.

Crash of an Ilyushin II-76TD in Bamako

Date & Time: Oct 31, 2007
Type of aircraft:
Operator:
Registration:
5A-DNQ
Flight Type:
Survivors:
Yes
MSN:
00434 54641
YOM:
1984
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Upon landing at Bamako-Senou Airport, the nose gear collapsed. The aircraft was damaged beyond repair and all six crew members evacuated safely. The exact date of the mishap remains unknown, somewhere in October 2007.