Crash of a Shaanxi Y-8B in Colombo: 5 killed

Date & Time: Aug 15, 2002 at 1235 LT
Type of aircraft:
Operator:
Registration:
CR-873
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Colombo - Colombo
MSN:
07 08 02
YOM:
1993
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
The crew departed Colombo-Ratmalana Airport for a local post maintenance test flight as one of the engine has been changed. During climbout, an engine caught fire. The crew was cleared to return for an emergency landing when the engine exploded and separated from the aircraft. Out of control, the airplane crashed in an open field, bursting into flames. All five crew members were killed. It was reported that the engine that caught fire was not the one that has been changed.
Probable cause:
Engine fire and explosion for unknown reasons.

Crash of a PZL-Mielec AN-2R in Sladky Liman: 2 killed

Date & Time: Aug 8, 2002 at 1920 LT
Type of aircraft:
Operator:
Registration:
RA-33322
Flight Phase:
Flight Type:
Survivors:
No
MSN:
1G225-41
YOM:
1987
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
In the evening, a pilot and a technician took off for a local flight. After liftoff, at a height of about 10 metres, the aircraft rolled to the left and impacted the concrete support of a power line then crashed 38 metres further, bursting into flames. Both occupants were killed.
Probable cause:
It was determined that both occupants were intoxicated at the time of the accident. They took off while the ailerons were still locked. Poor flight preparation.

Crash of A Embraer EMB-820C Navajo in Fernandópolis: 1 killed

Date & Time: Jul 28, 2002 at 1630 LT
Registration:
PT-ETT
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Fernandópolis - Fernandópolis
MSN:
820-093
YOM:
1979
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
1
Aircraft flight hours:
3834
Circumstances:
The twin engine aircraft departed Fernandópolis Airport in the afternoon on a panoramic flight over the city with five passengers and one pilot on board. At this time, the visibility was poor due to fog down to 40 metres above the ground. Shortly after takeoff, the pilot lost control of the airplane that crashed, bursting into flames. A passenger was killed while five other occupants were injured, two seriously. The aircraft was destroyed.
Probable cause:
It was determined that the pilot was not qualified to pilot such type of aircraft. Investigations revealed he did not have any licence nor medical documents to prove he was able to conduct such flight with such aircraft. A poor flight planning and a poor evaluation of the weather conditions were considered as contributing factors.
Final Report:

Crash of an Ilyushin II-86 in Moscow: 14 killed

Date & Time: Jul 28, 2002 at 1525 LT
Type of aircraft:
Operator:
Registration:
RA-86060
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Moscow - Saint-Petersburg
MSN:
51483203027
YOM:
1983
Country:
Region:
Crew on board:
16
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
14
Aircraft flight hours:
18363
Circumstances:
The aircraft was leaving Moscow on a ferry flight to St Petersburg following a charter flight from Sochi. On board were 16 crew members, among them 10 employees of the company. Two seconds after takeoff from runway 07L, while climbing to a height of about 200 metres, the stabilizers trimmed to the full up position of 12°. The aircraft nosed up and reached a super critical angle of attack. The crew attempted to regain control by pushing the control column forward but the aircraft stalled and crashed in a huge explosion about 700 metres past the runway end. Two stewardesses were injured while 14 other occupants were killed.
Probable cause:
The cause could not be determined with certainty due to the almost complete destruction of the main and reserve stabilizer control system units as a result of the fire on the ground and lack of information on the primary and backup stabilizer control systems on the flight data recorder, and the lack of crew comments on the cockpit voice recorder. The accident of IL-86 RA-86060 could be caused by an electrical failure in the stabilizer control system, which led to the reverse control response when controlling the stabilizer from the main system or inadequate actions of one of the pilots, expressed in pressing and holding the "pitch up" stabilizer switch on the control column.

Crash of an Antonov AN-26 in Kinshasa

Date & Time: Jul 26, 2002
Type of aircraft:
Operator:
Registration:
9Q-CMC
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Kinshasa - Tshikapa
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
15
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll at Kinshasa-N'DJili Airport, the captain realized he could not make it so he decided to reject takeoff. While initiating an emergency braking procedure, the nose gear collapsed, followed shortly later by both main landing gears. The aircraft slid on its belly and came to rest on the runway. All 21 occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
It is believed that the total weight of the aircraft was above MTOW.

Crash of a Beechcraft E90 King Air in Bloomington: 2 killed

Date & Time: Jul 21, 2002 at 1026 LT
Type of aircraft:
Operator:
Registration:
N12KA
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Bloomington - Cable Union
MSN:
LW-41
YOM:
1973
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
1740
Captain / Total hours on type:
942.00
Aircraft flight hours:
8643
Circumstances:
The airplane was destroyed by impact forces and post-impact fire when it impacted the terrain about 1/3 mile northeast of the departure end of runway 20 during takeoff. The airplane was cleared for a right turnout after takeoff, but witnesses observed the airplane climb to about 100 feet, veer left, enter a left bank, go inverted, and then impact the terrain in a nose low attitude. The airplane's left and right wings, fuselage, and cockpit were largely consumed by fire. Inspection of the airplane revealed the flaps and landing gear were retracted. There was aileron control continuity from the control yoke to the aileron bellcranks. There was elevator and rudder control cable continuity from the bellcranks at the forward bulkhead to the control surfaces. Inspections of the engines and propellers indicated the right engine and propeller was producing power in the middle to high power range at impact, and the left engine and propeller was producing power in the low to middle range of power at impact. The 60-year old pilot had flown 942 hours in the accident airplane, and was described as a very safety conscious, conservative pilot, who performed very thorough preflights and adhered to all checklists. The 22-year old pilot rated passenger had not received ground or flight instruction in the make and model of the accident airplane. The toxicology reports were negative for all substances tested. There were no remarkable findings in the autopsies.
Probable cause:
The cause of the accident is undetermined.
Final Report:

Crash of a Rockwell Shrike Commander 500S in Fortaleza

Date & Time: Jul 2, 2002 at 1640 LT
Operator:
Registration:
PT-KZD
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
Schedule:
Fortaleza - Fortaleza
MSN:
500-3140
YOM:
1972
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
8000
Captain / Total hours on type:
2900.00
Aircraft flight hours:
9960
Circumstances:
The twin engine aircraft departed Fortaleza-Pinto Martins Airport on a local post maintenance test flight (50 hours), carrying two passengers and one pilot. After takeoff, while climbing to a height of 200 feet, the power on the left engine fluctuated. The pilot modified the position of the fuel selector but the situation did not change. As the aircraft was losing height, the pilot shut down the left engine and feathered its propeller when the aircraft rolled to the left, causing the left wing to struck a concrete wall. Out of control, the aircraft struck the roof of a house, then a second one and eventually crashed on a third residence. All three occupants were injured as well as one people on the ground.
Probable cause:
The fuel pump and the servo-injectors had faults which certainly contributed to the accident as the left engine was not properly supplied with fuel.
Final Report:

Crash of a De Havilland DHC-3 Otter near Lake Cojibo

Date & Time: Jun 30, 2002 at 0900 LT
Type of aircraft:
Operator:
Registration:
C-GUTQ
Flight Phase:
Survivors:
Yes
Site:
MSN:
402
YOM:
1960
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The single engine aircraft departed Lake Cojibo with two passengers, one pilot and a full load of freight, destined for a fishing camp. Weather conditions were good but the OAT was high. After takeoff, the aircraft encountered difficulties to maintain a proper rate of climb due to the high temperature and the weight it was carrying. The pilot entered a valley and while trying to gain height to clear rising terrain, the aircraft struck the top of a mountain and crashed, bursting into flames. All three occupants were injured and the aircraft was destroyed by fire.

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

Date & Time: Jun 27, 2002 at 0806 LT
Type of aircraft:
Operator:
Registration:
RA-84639
Flight Phase:
Survivors:
Yes
Schedule:
Dubovoe - Dubovoe
MSN:
1G191-17
YOM:
1981
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew as engaged in a crop spraying mission in Dubovoe. Shortly after takeoff, while climbing to a height of about 40 metres, the engine lost power. The airplane lost height and the crew attempted to make an emergency landing when the aircraft rolled to the left to an angle of 10-15° then collided with trees and crashed in a wooded area. Both pilots escaped unhurt while the aircraft was damaged beyond repair.
Probable cause:
Loss of engine power following a bird strike. It was determined that the aircraft collided with a bird during initial climb and that the bird came to rest in the carburetor air intake.

Crash of a Beechcraft E18S in Venice

Date & Time: Jun 26, 2002 at 0800 LT
Type of aircraft:
Registration:
N1002C
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Venice - Cancún
MSN:
BA-251
YOM:
1957
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1750
Captain / Total hours on type:
250.00
Aircraft flight hours:
10500
Circumstances:
An airplane impacted the runway shortly after takeoff. According to the pilot, the airplane rolled sharply to the left immediately after liftoff from the runway. The passenger in the back seat stated the airplane banked sharply to the left after takeoff. The pilot then applied right rudder and aileron to stop the roll. Unable to level the airplane with the horizon, the pilot elected to reduce power to idle on both engines and land on the remaining runway. The airplane impacted the runway, slid into the grass and erupted into flames.
Probable cause:
The pilot's improper use of flight controls during takeoff, that resulted in the loss of control during takeoff.
Final Report: