Crash of a De Havilland DHC-6 Twin Otter 310 in Bili

Date & Time: Jan 3, 1995
Operator:
Registration:
P2-IAA
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Bili - Bili
MSN:
244
YOM:
1969
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was engaged in a local training flight at Bili Airfield. During the takeoff roll on a grassy airstrip, the crew lost control of the airplane that veered off runway, lost its undercarriage and came to rest. Both pilots escaped uninjured and the aircraft was damaged beyond repair.

Crash of a Lockheed C-130B Hercules in Trinidad

Date & Time: Dec 31, 1994
Type of aircraft:
Operator:
Registration:
TAM-67
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Trinidad - Trinidad
MSN:
3581
YOM:
1960
Country:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing a local training at Trinidad-Jorge Heinrich Arauz Airport. Upon takeoff, the aircraft lost height and crash landed by the runway. All four occupants escaped uninjured while the aircraft was damaged beyond repair. It is believed that the loss of control occurred at liftoff while the crew was attempting a 3-engine takeoff.

Crash of a Piper PA-46-350P Malibu in Rochester: 3 killed

Date & Time: Dec 22, 1994 at 1152 LT
Registration:
N133MA
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Rochester - Guntersville
MSN:
46-22133
YOM:
1993
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
2500
Captain / Total hours on type:
96.00
Aircraft flight hours:
106
Circumstances:
The airplane departed on runway 31 in instrument meteorological conditions (IMC) and turned right to a heading of 090°. Radar contact (arts tag) was acquired about 1 to 2 miles north of the airport. Reportedly, the arts tag would typically be acquired as the airplane climbed through an altitude of about 700 feet agl. Subsequently, the airplane crashed about 2 miles north of the airport. A witness reported hearing a loud engine noise before the plane crashed. The wreckage path was oriented along a westerly heading and over an area of about 380 feet. There was evidence of an in-flight breakup. An outboard portion of the right wing was found about 150 feet from the main impact crater. An examination revealed the right wing had failed near the production seam. The right spar exhibited features 'typical of an upward bending overstress separation.' Examination revealed no other evidence of preimpact aircraft or engine malfunction. The airplane's gross weight was estimated to be about 4,696 pounds; its max limit was 4,300 pounds. The pilot's logbook indicated that he had flown only 2 instrument approaches in the previous 14 months. All three occupants were killed.
Probable cause:
Failure of the pilot to maintain control of the airplane, while climbing in instrument meteorological conditions (IMC) after takeoff. Factors related to the accident were: fog, low ceiling, the pilot's lack of recent instrument experience, and the excessive gross weight of the airplane.
Final Report:

Crash of a Fokker F27 Friendship 600 in Guayaramerín

Date & Time: Dec 22, 1994 at 0700 LT
Type of aircraft:
Operator:
Registration:
CP-2165
Flight Phase:
Survivors:
Yes
Schedule:
Guayaramerín – San Joaquín
MSN:
10592
YOM:
1979
Country:
Crew on board:
4
Crew fatalities:
Pax on board:
36
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll on runway 17, at a speed of 107 knots, the right engine lost power. The crew decided to abandon the takeoff procedure and initiated an emergency braking procedure. Unable to stop within the remaining distance (runway 17 is 1,995 metres long), the aircraft overran, rolled for 120 metres and eventually collided with trees. All 40 occupants were rescued, among them six passengers were injured. The aircraft was damaged beyond repair.
Probable cause:
A filter located on a fuel line connected to the right engine was clogged, causing a momentary failure of the engine.

Crash of a Rockwell Sabreliner 40R in Buenos Aires

Date & Time: Dec 21, 1994 at 0422 LT
Type of aircraft:
Registration:
N747E
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
282-22
YOM:
1964
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll by night, after V1 speed, the crew elected to rotate but the aircraft failed to respond. The captain abandoned the takeoff procedure and initiated an emergency braking maneuver. Unable to stop within the remaining distance, the aircraft overran, lost its undercarriage and came to rest few dozen metres further. Both pilots escaped uninjured and the aircraft was damaged beyond repair.
Probable cause:
It was determined that the total weight of the aircraft was above MTOW and the CofG was out of permissible limits.

Crash of a Basler BT-67 in Lobito: 2 killed

Date & Time: Dec 16, 1994 at 0715 LT
Type of aircraft:
Registration:
N96BF
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Lobito - Luanda
MSN:
13321
YOM:
1944
Location:
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The aircraft was engaged in a humanitarian flight from Lobito to Luanda on behalf of the International Committee of the Red Cross, carrying two pilots and a load of 4,6 tons of green beans. After takeoff, while climbing to a height of about 50 feet, the aircraft stalled and crashed by the runway. The aircraft was destroyed and both pilots were killed.
Probable cause:
The exact cause of the accident could not be determined with certainty but it is believed that the loss of control that occurred during initial climb was the consequence of an unexpected shift of the cargo.

Crash of a Learjet 35A in Moscow: 1 killed

Date & Time: Dec 14, 1994 at 2359 LT
Type of aircraft:
Operator:
Registration:
D-CATY
Flight Phase:
Survivors:
Yes
Schedule:
Munich - Moscow - Magnitogorsk
MSN:
35A-114
YOM:
1977
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The twin engine aircraft was engaged in a charter flight from Munich to Magnitogorsk and back, with an intermediate stop in Moscow to pick up a Russian navigator. Shortly after takeoff, at a height of about 15 metres, the aircraft banked left and impacted the ground some 30 metres to the left of the runway. Out of control, it rolled for about 325 metres before coming to rest. A pilot was killed while six other occupants were seriously injured.

Crash of an Antonov AN-8 in Dundo

Date & Time: Dec 6, 1994
Type of aircraft:
Operator:
Registration:
D2-FVA
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Dundo - Luanda
MSN:
0C3450
YOM:
1960
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll at Dundo Airport, the twin engine aircraft deviated to the left after the crew encountered directional control problems. Few seconds later, at a speed of 190 km/h, the aircraft deviated to the right then veered off runway. On rough ground, the aircraft became airborne the struck power cables, stalled and crashed. All six crew members were injured and the aircraft was destroyed.

Crash of a Cessna 208B Caravan I in Oslo: 1 killed

Date & Time: Dec 4, 1994 at 0502 LT
Type of aircraft:
Operator:
Registration:
LN-PBC
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Oslo - Bergen
MSN:
208B-0310
YOM:
1992
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
1676
Captain / Total hours on type:
327.00
Aircraft flight hours:
2193
Circumstances:
The aircraft was completing a cargo flight to Bergen, carrying one pilot and 1,389 kilos of newspapers. Following a night takeoff from runway 19, while climbing in poor weather conditions at an altitude of about 390 metres, the single engine aircraft stalled and crashed in a wooded area located 1,5 km from the airport. The pilot, sole on board, was killed.
Probable cause:
The accident was the consequence of a stall during initial climb to an excessive accumulation of ice on wings and tail as the aircraft had not been deiced prior to departure. The following contributing factors were reported:
- The plane was outdoors for an estimated time of 20 minutes under conditions in which ice could adhere on the surface of the plane's hull, wings and tail surfaces.
- The plane was not de-iced by the pilot prior to departure.
- The company had not developed adequate written instructions for de-icing. The company had no written instructions to prevent icing during ground stay.
- The company had no sufficient equipment available, or added conditions sufficiently organized so that icin accretion be prevented or removed before departure from Gardermoen.
- The plane took off with ice on the surface of the wings and tail surfaces
- Ice on the surface of the wings and tail surfaces reduced flight characteristics in such a degree that the pilot did not manage to gain height after departure and therefore crashed.
Final Report:

Crash of a De Havilland DHC-6 Twin Otter 300 at Rothera Station: 4 killed

Date & Time: Nov 24, 1994 at 0301 LT
Operator:
Registration:
C-GKBD
Flight Phase:
Survivors:
No
Schedule:
Rothera - Terra Nova Bay
MSN:
314
YOM:
1971
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
3984
Captain / Total hours on type:
3414.00
Copilot / Total flying hours:
3180
Copilot / Total hours on type:
448
Circumstances:
The twin engine aircraft departed Rothera Station runway 18 on a charter flight to Terra Nova, carrying two passengers and two pilots. During initial climb, the airplane became unstable and rolled side to side. From a height of about 100 feet, it stalled and crashed on the slope of an iceberg facing the airport, bursting into flames. All four occupants were killed.
Probable cause:
The exact cause of the accident could not be determined with certainty as rescuers and investigators were unable to reach the crash site that was unstable and too dangerous. The stall occurred at a too low altitude to expect recovery.
Final Report: