Crash of a PZL-Mielec AN-2 in La Paragua

Date & Time: Mar 29, 2007 at 0630 LT
Type of aircraft:
Operator:
Registration:
YV-1953
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
1G238-26
YOM:
1991
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The single engine aircraft was completing a cargo flight from La Paragua to a mining area, carrying a load of food. Shortly after liftoff, the aircraft encountered difficulties to gain height, rolled to the left and crashed upside down. The pilot, sole on board, was slightly injured and the aircraft was damaged beyond repair.

Crash of an Ilyushin II-76TD in Mogadishu: 11 killed

Date & Time: Mar 23, 2007 at 1400 LT
Type of aircraft:
Operator:
Registration:
EW-78849
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Mogadishu - Djibouti City - Minsk
MSN:
10134 05192
YOM:
1991
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
11
Circumstances:
The aircraft was departing Mogadishu on a ferry flight to Minsk with an intermediate stop in Djibouti City, carrying 4 technicians of the operator and 7 crew members who were returning to Belarus after they recovered materials and instruments from another II-76 (EW-78826) that was damaged beyond repair at Mogadishu Airport last March 9. Shortly after takeoff, while in initial climb, the aircraft was hit by a missile that struck the left wing between both engines n°1 and 2. An explosion occurred and the aircraft caught fire. The crew initiated a turn when the left wing detached and crashed in the sea. Out of control, the aircraft crashed on a beach near the airport, killing all 11 occupants.
Probable cause:
Shot down by rebels located on a boat.

Crash of an Airbus A310 in Dubai

Date & Time: Mar 12, 2007 at 0630 LT
Type of aircraft:
Operator:
Registration:
S2-ADE
Flight Phase:
Survivors:
Yes
Schedule:
London - Dubai - Dhaka
MSN:
698
YOM:
1996
Flight number:
BG006
Location:
Region:
Crew on board:
14
Crew fatalities:
Pax on board:
236
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll from Dubai Intl Airport runway 12L, after V1 speed, the crew heard a loud bang then noticed severe vibrations when the nose gear collapsed. The captain abandoned the takeoff procedure and initiated an emergency braking manoeuvre. The aircraft slid on its nose for few hundred metres and came to rest just before the end of the runway, slightly to the left of the centerline. All 250 occupants evacuated safely while the aircraft was damaged beyond repair.
Probable cause:
Failure of the nose gear during the takeoff roll after it impacted a half wheel rim which was broken off during the takeoff from a previous aircraft.

Crash of a De Havilland DHC-2 Beaver III in Headcorn: 1 killed

Date & Time: Mar 11, 2007 at 1600 LT
Type of aircraft:
Operator:
Registration:
OY-JRR
Flight Phase:
Survivors:
Yes
Schedule:
Headcorn - Headcorn
MSN:
1632
YOM:
1966
Location:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
932
Captain / Total hours on type:
27.00
Circumstances:
The pilot was conducting flights for the purpose of parachute operations; these flights are known colloquially as ‘lifts’. On the previous day, he had conducted 13 lifts, of which eleven were to an altitude of 12,000 ft and two to an altitude of 5,500 ft or less. On the day of the accident the pilot recorded that he took off for the first lift at 0927 hrs. The aircraft, with nine parachutists aboard, climbed to 12,000 ft and landed at 0946 hrs. There followed three flights of an average 18 minute duration, between each of which the aircraft was on the ground for no more than 7 minutes. The last of these flights landed at 1100 hrs, after which the aircraft uplifted 230 ltr of Jet A1 fuel. The aircraft utilised the main runway, Runway 29, for each of these flights. The surface wind had freshened from the south and the pilot requested the use of the shorter Runway 21. The air/ground radio operator refused this request because he believed that the pilot had not been checked out to use this runway, as required by the Headcorn Aerodrome Manual. Accordingly, the pilot approached a nominated check pilot who agreed to observe his next flight. The check pilot briefed the pilot of OY-JRR on the procedures for using the short runway, emphasising the need to make an early decision to abort the takeoff if necessary. The check pilot stated that the pilot of OY-JRR performed a thorough pre-takeoff check using the full checklist available in the cockpit and that the subsequent flight was entirely satisfactory. Following the check flight the aircraft took off again at 1148 hrs and flew a further five flights, each separated by periods that ranged between 7 and 36 minutes. The check pilot observed several of these flights, all of which were from Runway 21, and most appeared to proceed normally. He and another witness noticed that on one occasion the climb gradient after takeoff appeared shallower than normal, but they believed that the wind speed had decreased at this time. The pilot recorded that the aircraft was refuelled again after landing at 1443 hrs, this time uplifting 266 ltr of fuel. The next takeoff was at 1447 hrs and having climbed to 12,000 ft again the aircraft landed at 1521 hrs. The accident occurred on the pilot’s eleventh flight of the day. Prior to the flight the aircraft was refuelled with a further 100 ltr at 1555 hrs. Shortly before 1605 hrs the aircraft taxied to Runway 21. It appeared to accelerate normally but at no time was the tail seen to rise in its usual manner prior to becoming airborne. Onboard, the experienced jump-master noticed that the aircraft was passing the aerodrome refuelling installation and several aircraft parked close to the runway, beyond the intersection of Runway 21 with Runway 29. He was aware that the aircraft had now passed the point where it would normally become airborne. Almost simultaneously, he heard the pilot shout “Abort”. One of the parachutists shouted to the other occupants “Brace - Brace, everyone on the floor”. The aircraft stopped abruptly when its left wing and cockpit collided with a camouflaged F100 fighter aircraft which was parked as a museum exhibit to the left of the southern edge of Runway 21. The occupants of the cabin were able to vacate the aircraft with mutual assistance. Members of the aerodrome fire service extinguished a small fire, which had started in the area of the engine, and other witnesses helped the occupants to move away from the aircraft. The pilot, however, remained unconscious in the cockpit. He was attended subsequently by paramedics and taken to hospital, where he succumbed to his injuries.
Probable cause:
The pilot’s training was probably adequate for the normal and abnormal circumstances envisaged by his instructor. However, the pilot was not familiar with the handling or performance characteristics of the aircraft during takeoff with the flaps in the UP position and consequently he may not have identified that the aircraft was in the wrong configuration for takeoff. The design authority for this type considered that this configuration was “outside the normal flight envelope” and had produced no performance charts or procedures for its use. In such circumstances, it is essential that the pilot follows the published procedures and positively ensures that the aircraft is correctly configured for takeoff.
Final Report:

Crash of a Comp Air CA-8 in Cali

Date & Time: Mar 8, 2007 at 0653 LT
Type of aircraft:
Operator:
Registration:
N2411B
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Cali – Medellín
MSN:
S2000
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed shortly after take off from Cali-Alfonso Bonilla Aragón Airport, bound for Medellín. Both occupants were injured while the aircraft was damaged beyond repair.

Crash of a Canadair RegionalJet CRJ-100SE in Moscow

Date & Time: Feb 13, 2007 at 1637 LT
Operator:
Registration:
N168CK
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Moscow - Berlin
MSN:
7099
YOM:
1996
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
9100
Copilot / Total flying hours:
2679
Copilot / Total hours on type:
68
Aircraft flight hours:
3814
Aircraft flight cycles:
1765
Circumstances:
The crew was completing a positioning flight from Moscow to Berlin for maintenance purposes. After the crew was cleared to start up the engines, the aircraft was towed to the deicing pad where the crew requested a two-step deicing procedure. The deicing was completed at 1618LT and the crew was cleared for takeoff at 1636LT. After a course of 1,500 metres on runway 06 in snow falls, the pilot-in-command started the rotation when the aircraft rolled left and right. The right wing struck the ground, the aircraft went out of control, got inverted and crashed in a snow covered area located 450 metres further and 35 metres to the right of the runway. All three crew members escaped with minor injuries while the aircraft was destroyed. At the time of the accident, weather conditions were as follow: wind from 130 at 10 knots, horizontal visibility 1,000 metres in snow falls, vertical visibility 300 feet, OAT -6° and dewpoint at -7°.
Probable cause:
Loss of control at liftoff due to a loss of lift caused by a stall consecutive to an excessive accumulation of ice/frost on the critical surfaces despite the aircraft had been deiced/anti-iced prior to takeoff. The following findings were identified:
- The aircraft was deiced in a two-step procedure - deicing with Type I then anti-icing with Type IV. The treatment was completed at 1618LT, 19 minutes prior to the accident,
- At the time of the accident, there were moderate to strong snow falls at the airport,
- The crew did not receive the full meteorological bulletin prior to departure and failed to determine the correct holdover time,
- Referring to the actual weather conditions, the crew failed to proceed with a second deicing/anti-icing procedure,
- Lack of adequate check by crew members and/or the airline representatives regarding the quality of the anti-icing treatment,
- The crew failed to comply with AFM relating to the actual weather conditions,
- The takeoff was started at a speed that was 12 knots below the reference speed, increasing the stall condition with leading edges that were slightly contaminated with frost/ice.
Final Report:

Crash of a Piper PA-31T Cheyenne II in Zweibrücken: 1 killed

Date & Time: Feb 12, 2007 at 1020 LT
Type of aircraft:
Operator:
Registration:
N160TR
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Zweibrücken – Split – Athens
MSN:
31-7920036
YOM:
1979
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The pilot departed Zweibrücken Airport on a flight to Athens with an intermediate stop in Split as the aircraft should be delivered to its new owner based in Greece. After takeoff from runway 21 at Zweibrücken Airport, while in initial climb, the aircraft deviated to the left while the standard departure route was a straight climb until 7 nm. The pilot was contacted by ATC and reported problems. Shortly later, the altitude of the aircraft fluctuated from 1,500 to 3,200 feet and again, the pilot was contacted by ATC to check the situation. Few seconds later, the aircraft entered an uncontrolled descent and crashed in an open field located in Rieschweiler, about 6 km northeast of the airport. The aircraft was totally destroyed upon impact and the pilot, sole on board, was killed. It was reported that, prior to departure, the pilot encountered difficulties to close the main cabin door and had to be shown how to operate it. A member of the FBO staff then asked the pilot if he should explain the aircraft's avionics and, after the pilot replied yes, went on to describe how to operate the RNAV system. The pilot then had difficulty in starting the right engine and was directed to the 'ignition switch' on the overhead panel.

Crash of a Beechcraft 200C Super King Air off East Bay Cay: 1 killed

Date & Time: Feb 6, 2007 at 1842 LT
Operator:
Registration:
VQ-TIU
Flight Phase:
Survivors:
Yes
Schedule:
East Bay Cay - Grand Turk
MSN:
BL-131
YOM:
1988
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
8500
Captain / Total hours on type:
394.00
Aircraft flight hours:
24578
Aircraft flight cycles:
31684
Circumstances:
The aircraft was parked on the small apron at North Caicos Airport while the pilot went home to collect some personal items. One of the intended passengers saw the aircraft arrive. He remained in the vicinity until the pilot returned, and reported that the aircraft was unattended in the intervening time. When the pilot returned, four of the five passengers were gathered near the aircraft, and the last passenger arrived soon afterwards. The pilot, a local man well-known to the passengers, appeared to be his normal self and in good spirits. As most inter-island travel in the TCI is by air, the passengers were also familiar with the operator’s aircraft and used to travelling by air. Some had flown frequently on VQ-TIU. The pilot supervised embarkation and gave an emergency briefing. One passenger reported that the pilot made a mobile telephone call, which he presumed to be to Air Traffic Control (ATC) at Providenciales to notify them of the proposed flight. Prior to seating himself at the controls, the pilot told the passengers that they may expect some turbulence. The aircraft taxied onto the runway at its eastern end and along its length for a departure from Runway 08. It was about one hour after sunset and outside the airport’s normal operating hours, so there were no ATC personnel on duty. The runway lights were operated by the operator’s station manager. The aircraft took off at 1840 hrs. Soon after takeoff the aircraft was seen to start a turn to the right, which was consistent with its routing to Grand Turk, some 54 nm to the south-east. However, the aircraft reached a relatively large angle of bank and started to descend. The descent continued until it crashed with significant forward speed into an area of very shallow water. The aircraft broke up on impact, with the fuselage section coming to rest nearly inverted but comparatively intact. All those on board survived the impact sequence with varying degrees of injury. However, the pilot died before he could receive specialist medical treatment.
Probable cause:
The investigation identified the following causal factors:
1. The aircraft adopted an excessive degree of right bank soon after takeoff. This led to a descending, turning flight path which persisted until the aircraft was too low to make a safe recovery.
2. The pilot probably became spatially disoriented and was unable to recognise or correct the situation in time to prevent the accident.
The investigation identified the following contributory factors:
1. The environmental conditions were conducive to a spatial disorientation event.
2. The pilot had probably consumed alcohol prior to the flight, which made him more prone to becoming disorientated.
3. The flight was operated single-pilot when two pilots were required under applicable regulations. The presence of a second pilot would have provided a significant measure of protection against the effects of the flying pilot becoming disoriented.
Final Report:

Crash of a PZL-Mielec AN-2R in Narsarsuaq

Date & Time: Feb 4, 2007
Type of aircraft:
Operator:
Registration:
LY-AJG
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Vágar - Reykjavik - Kulusuk - Narsarsuaq
MSN:
1G178-48
YOM:
1977
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On take off from Narsarsuaq Airport, the single engine aircraft was caught by strong winds, veered off runway and collided with a bank. Both left wings were damaged while the undercarriage were torn off. Both pilots escaped uninjured while the aircraft was damaged beyond repair. A snow storm was approaching Narsarsuaq at the time of the accident.

Crash of a Fokker 100 in Pau: 1 killed

Date & Time: Jan 25, 2007 at 1124 LT
Type of aircraft:
Operator:
Registration:
F-GMPG
Flight Phase:
Survivors:
Yes
Schedule:
Pau - Paris
MSN:
11362
YOM:
1991
Flight number:
AF7775
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
50
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
6135
Captain / Total hours on type:
2948.00
Copilot / Total flying hours:
6295
Copilot / Total hours on type:
287
Aircraft flight hours:
28586
Aircraft flight cycles:
34886
Circumstances:
Following a normal takeoff acceleration on runway 13 at Pau-Pyrénées Airport, the pilot-in-command started the rotation when the aircraft immediately rolled to the left. Then it rolled to the right and to the left again, lost height, struck the ground and bounced. At a speed of about 160 knots, the crew reduced the engine power when the aircraft rolled to the right of the runway, struck the perimeter fence then collided with a truck driving along a road. Upon touchdown, both main landing gears were torn off and the aircraft slid on its belly before coming to rest in an open field located 535 metres past the runway end. All 54 occupants evacuated safely while the aircraft was damaged beyond repair. The truck's driver was killed while his colleague was seriously injured.
Probable cause:
The accident resulted from a loss of control caused by the presence of ice contamination on the surface of the wings associated with insufficient consideration of the weather during the stopover, and by the rapid rotation pitch, a reflex reaction to a flight of birds.
Contributing factors:
- Limited awareness within the aviation community regarding the risks associated with the icing on the ground and changes in the performance of the aircraft involved in this phenomenon;
- The sensitivity of small aircraft not equipped with burners to the effects of ice on the ground;
- Insufficient awareness of the crew of procedures for the tactile verification of the condition of the surfaces in icing conditions and the lack of implementation by the operator of an adapted organization;
- The ordinary aspect of the flight including the weather encountered, which was not likely to incite the crew to particular vigilance.
Final Report: