Country
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Mato Grosso

Crash of a Boeing 737-241 near São José do Xingu: 12 killed

Date & Time: Sep 3, 1989 at 2045 LT
Type of aircraft:
Operator:
Registration:
PP-VMK
Flight Phase:
Survivors:
Yes
Schedule:
São Paulo – Marabá – Belém
MSN:
21006
YOM:
1975
Flight number:
RG254
Country:
Crew on board:
6
Crew fatalities:
Pax on board:
48
Pax fatalities:
Other fatalities:
Total fatalities:
12
Captain / Total flying hours:
6928
Captain / Total hours on type:
980.00
Copilot / Total flying hours:
884
Copilot / Total hours on type:
442
Aircraft flight hours:
33373
Circumstances:
Following a wrong flight preparation and erroneous computer setting regarding the route, the crew computerized 027° instead of 270°. After takeoff from Marabá Airport at 1725LT, the crew was cleared to climb to FL290 and maintained heading of 270° for 40 minutes. The flight was then cleared to descend to FL200 by Belém ACC. However, the crew failed to find navigational aids and lost radio contact. Course was changed to 090 degrees as the aircraft further descended down to FL40. The crew then followed a river, heading 165 degrees. Because of the sunset and haze the pilot's had difficulty navigating. Also, they failed to establish radio contact on several frequencies and failed to find navaids in the area. After the crew found the NDB, both engines stopped due to fuel exhaustion. The captain elected to make an emergency landing when the aircraft crashed in the jungle about 60 km from São José do Xingu. Rescue teams arrived on site 44 hours later. 42 occupants were injured while 12 passengers were killed. The aircraft was destroyed. It appeared that the computerized flight plan used a four digit representation of the magnetic bearing with the last digit being a tenth of a degree without any decimal separator. A course of '027.0' was presented as '0270'.
Probable cause:
A. Human Factor
1) Physiological aspect - Did not contribute to the accident.
2) Psychological aspect - The following psychological variables contributed to the accident:
a) Misleading perception - In the reading of the plan and incorrect heading insertion by the commander.
b) Reinforcement - In the reading and incorrect heading insertion by the co-pilot and heading conference placed by the commander.
c) Marginal attention and level of attention - The non-recognition of conditions that would mean being far from the objective: request for "VHF bridge" when other aircraft were talking normally with the Control; "reception" of commercial stations, and non-receipt of destination NDB, etc.
d) Predisposition - Maintaining the urge to go to the established objective (Belém).
e) Predisposition duration - Maintenance of FL040 for a long time.
f) Reinforcement of predisposition - Reception of boundaries when selecting Belem's radio frequencies.
g) Attention Fixing - Permanent search for headings, radio contacts or river contours, as an alternative, to reach the fixed goal.
h) Blocks - Delays in identifying the initial headings error and plotting itself in navigation.
i) Geographical position error.
B. Material Factor - Did not contribute to the accident.
C. Operational Factor
1) Poor supervision - Inadequate graphical representation of the Computer Flight Plan.
2) Poor cockpit coordination - No supervision of cockpit activities. Actions were not supervised, but imitated.
3) Poor support staff - Lack of radio contact by the operator's Flight Coordination with the aircraft in flight, after the significant landing delay in Belém, thus breaking the chain of events of the accident.
4) Pilot aspect characterized by environmental influence - Difficulties of visualization due to sunset and dry fog: Radio aid markings received from great distances, originating from the ionospheric propagation of electromagnetic waves.
5) Pilot aspect characterized by poor planning - Lack of route letters to cross the flight plan information.
6) Pilot aspect characterized by poor judgment - Inadequate evaluation and use of radio-navigation equipment, resulting in the pursuit of markings without causing tuning and identification.
7) Pilot aspect characterized by other operational factors - Operational doctrine firming.
Final Report:

Crash of an Embraer EMB-110P Bandeirante in Juara: 17 killed

Date & Time: Jun 23, 1985
Operator:
Registration:
PT-GJN
Survivors:
No
Schedule:
Juara - Cuiabá
MSN:
110-063
YOM:
1975
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
15
Pax fatalities:
Other fatalities:
Total fatalities:
17
Circumstances:
After takeoff from Juara Airport, while climbing, the crew declared an emergency after the failure of the left engine. The crew was cleared to return and the rescue teams were dispatched at the airport. On final approach, during the last segment, the aircraft went out of control and struck the ground. It veered off runway and collided with an emergency vehicle (fire bombers truck) before coming to rest in flames. All 17 occupants were killed while no one on the ground was injured.
Probable cause:
A left engine faulty fuel injection nozzle caused a blow torch effect, damaging compressor turbine vane ring and causing thermal fatigue and loss of one of the turbine blades. The resulting imbalance ruptured the starting control bypass fuel return.

Crash of a Piper PA-31-310 Navajo in Aripuanã: 8 killed

Date & Time: Sep 24, 1984 at 0730 LT
Type of aircraft:
Registration:
PT-BKB
Flight Phase:
Survivors:
No
Schedule:
Aripuanã – Colíder
MSN:
31-482
YOM:
1969
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
8
Circumstances:
Two minutes after takeoff from Aripuanã Airport runway 18, while climbing, the pilot informed on radio that he lost an engine and was returning. He initiated a left turn when the aircraft lost height and crashed in a wooded area located 6 km from the airfield, bursting into flames. The aircraft was totally destroyed and all eight occupants were killed, among them seven journalists covering the official visit of the Governor of Mato Grosso in the region.
Probable cause:
Engine failure for unknown reasons.

Crash of a Britten-Norman BN-2A-9 Islander in Cuiabá: 9 killed

Date & Time: Mar 30, 1980
Type of aircraft:
Operator:
Registration:
PT-JSC
Flight Phase:
Survivors:
No
MSN:
695
YOM:
1973
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
After takeoff from Cuiabá-Marechal Rondon Airport, while climbing, the twin engine airplane struck a hill and crashed few km from the airport. All nine occupants were killed.

Crash of a Douglas C-47-DL in Rondonópolis

Date & Time: Jan 29, 1973
Operator:
Registration:
PP-SQA
Survivors:
Yes
MSN:
4742
YOM:
1942
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed upon landing at Rondonópolis Airport in unknown circumstances. There were no casualties.

Crash of a Fairchild C-82A-FA Packet in Serra do Norte: 4 killed

Date & Time: Oct 28, 1970
Type of aircraft:
Registration:
PT-DNZ
Flight Phase:
Flight Type:
Survivors:
No
MSN:
10219
YOM:
1948
Country:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
Crashed in unknown circumstances near Serra do Norte, while on a cargo flight. All four crew members were killed.

Crash of a Curtiss C-46A-50-CU Commando in Barra do Bugres: 13 killed

Date & Time: Aug 12, 1965 at 0700 LT
Type of aircraft:
Operator:
Registration:
PP-BTH
Flight Phase:
Survivors:
No
Schedule:
Cuiabá – Porto Velho
MSN:
30571
YOM:
1944
Country:
Crew on board:
4
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
13
Captain / Total flying hours:
7857
Captain / Total hours on type:
1357.00
Copilot / Total flying hours:
2816
Copilot / Total hours on type:
1516
Aircraft flight hours:
27761
Circumstances:
The aircraft departed Cuiabá-Marechal Rondon Airport at 1021 GNT, for Porto Velho with an IFR flight plan. At the outskirts of Barra do Bugres about 30 minutes after take-off, the aircraft turned back towards Cuiabá with its left engine on fire. While over Buracao, its left wing and engine broke away from the fuselage and it crashed to the ground out of control. All 13 occupants were killed.
Probable cause:
The cause of the accident was a structural failure. Bolts of the No. 8 cylinder, left engine, fractured. Contributing factors were defective fire detection and fire extinguishing systems.
Final Report: