Crash of an ATR42-320 in Puerto Ordaz: 17 killed

Date & Time: Sep 13, 2010 at 1023 LT
Type of aircraft:
Operator:
Registration:
YV1010
Survivors:
Yes
Schedule:
Porlamar - Puerto Ordaz
MSN:
371
YOM:
1994
Flight number:
VCV2350
Country:
Crew on board:
4
Crew fatalities:
Pax on board:
47
Pax fatalities:
Other fatalities:
Total fatalities:
17
Captain / Total hours on type:
1574.00
Copilot / Total flying hours:
1083
Copilot / Total hours on type:
483
Aircraft flight hours:
27085
Aircraft flight cycles:
29603
Circumstances:
Following two uneventful flights to Santiago Mariño and Maturín, the aircraft departed Porlamar on a flight to Puerto Ordaz with 47 passengers and a crew of four on board. While descending to Puerto Ordaz, at an altitude of 13,500 feet and at a distance of 79 km from the destination, the crew reported control difficulties. After being prioritized, the crew was instructed for an approach and landing on runway 07. At 1021LT, the crew reported his position at 3,000 feet and 28 km from the destination Airport. Two minutes later, the message 'mayday mayday mayday' was heard on the frequency. The aircraft went out of control and crashed in an industrial area located about 9 km short of runway, bursting into flames. Three crew members and 14 passengers were killed while 34 other occupants were injured, 10 seriously.
Probable cause:
The most probable cause for the occurrence of the accident was the malfunction of the centralized crew warning system (CCAS/CAC) with erroneous activation of the flight loss of lift warning system.
The following contributing factors were identified:
- Poor crew resources management,
- Loss of situational awareness,
- Inadequate coordination during the decision-making process to deal with abnormal situations in flight,
- Ignorance of the loss of lift warning system.
- Inadequate handling of flight controls.
Final Report:

Crash of a Beechcraft 350 Super King Air near Uribe: 6 killed

Date & Time: Sep 7, 2010 at 2306 LT
Operator:
Registration:
FAC-5747
Flight Phase:
Survivors:
No
Site:
MSN:
FL-454
YOM:
2005
Location:
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
The twin engine aircraft was engaged in a reconnaissance and survey mission over the southern Colombia territory, carrying six crew members. At 2306LT, the last radio contact was recorded with the crew. In unknown circumstances, while cruising at an altitude of 10,600 feet, the aircraft impacted terrain near Uribe. The wreckage was found four days later, on September 11. The aircraft was totally destroyed and all six occupants were killed.

Crash of an Embraer ERJ-145LU in Vitoria da Conquista

Date & Time: Aug 25, 2010 at 1440 LT
Type of aircraft:
Operator:
Registration:
PR-PSJ
Survivors:
Yes
Schedule:
São Paulo – Vitoria da Conquista
MSN:
145-351
YOM:
2000
Flight number:
PTB2231
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
35
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4400
Captain / Total hours on type:
3100.00
Copilot / Total flying hours:
1373
Copilot / Total hours on type:
813
Circumstances:
While approaching Vitoria da Conquista Airport runway 15, the crew failed to realize his altitude was too low. On short final, the aircraft impacted a small mound located few metres short of runway threshold. On impact, both main landing gears were torn off. The aircraft slid on runway for about 300 metres then veered off runway to the left and came to rest in a grassy area some 35 metres left of the runway with the right engine on fire. All 38 occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
The following factors were identified:
- During the approach, the flight crew's attention was focused on the characteristics of the geographical relief and presence of birds, reducing their awareness as to the maintenance of the approach slope.
- The group culture of maintaining a low angle of approach led the crew to choose the runway aspect instead of the VASIS as a reference for the approach, making them susceptible to various types of spatial illusion.
- Taking into account copilot's report that he was not succeeding in correcting the aircraft glide path relative to the runway, one may suppose that he was not applying the appropriate amplitude for such correction.
- The physical characteristics of the runway 15 (the active one) contributed to a wrong perception of the ideal glide path. The pronounced acclivity of the runway, its width (narrower than the runways on which the crew was accustomed to operate), and the low terrain near the threshold, caused in the pilots a perception that they were above the ideal approach slope, leading them to seek correction, which resulted in an angle of approach below the ideal one.
- For the flight in question, the company chose two pilots who had never operated in SBQV. A crewmember with previous experience in the locality would have a higher level of awareness in relation to the specific characteristics of the aerodrome.
- No company publications were found that could provide the pilots with guidance on the specifics of SBQV, capable of helping with the management of the risks associated with the operation in that aerodrome.
Final Report:

Crash of a Boeing 737-73V in San Andrés: 2 killed

Date & Time: Aug 16, 2010 at 0147 LT
Type of aircraft:
Operator:
Registration:
HK-4682
Survivors:
Yes
Schedule:
Bogotá – San Andrés
MSN:
32416/1270
YOM:
2002
Flight number:
ARE8250
Country:
Crew on board:
6
Crew fatalities:
Pax on board:
125
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
7643
Captain / Total hours on type:
343.00
Copilot / Total flying hours:
1900
Copilot / Total hours on type:
800
Aircraft flight hours:
23485
Circumstances:
The aircraft departed Bogotá-El Dorado Airport at 0007LT on a night schedule service to San Andres Island, carrying 125 passengers and a crew of six. While approaching San Andres-Gustavo Rojas Pinilla Airport, the crew encountered poor weather conditions. Due to heavy rain falls, the crew was informed by ATC that the visibility dropped to 4 km. On short final, flaps were selected down to 30° then the autopilot system was deactivated. After passing 500 feet on approach, the captain repeated the procedures in case of a go-around would be needed due to windshear conditions. Shortly later, the copilot shouted 'go-around' but half a second later, the airplane impacted ground 49 metres short of runway. On impact, the undercarriage and both engines were torn off. The aircraft slid for few dozen metres before coming to rest, broken in three. Two passengers were killed while 129 other occupants were injured, nine seriously.
Probable cause:
Execution of the flight below the angle of approach, due to a misjudgment of the crew, believing to be much higher, leading the aircraft to fly a typical trajectory of a 'black hole' illusion, which was experienced during the night-time approach to a runway with low contrast surrounded in bright focused lights, aggravated by bad weather of heavy rain.
Final Report:

Crash of a Piper PA-42-1000 Cheyenne 400LS in Mercedes

Date & Time: Aug 13, 2010 at 1530 LT
Type of aircraft:
Operator:
Registration:
LQ-BLU
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Mercedes - La Plata
MSN:
42-5527037
YOM:
1987
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4294
Captain / Total hours on type:
390.00
Copilot / Total flying hours:
2827
Copilot / Total hours on type:
14
Aircraft flight hours:
1526
Circumstances:
During the takeoff roll on runway 19 at Mercedes Airport, the twin engine aircraft deviated to the right then to the left. Control was lost and the aircraft veered off runway to the left, lost its undercarriage and came to rest in bushed with its left wing partially torn off. All four occupants escaped uninjured while the aircraft was damaged beyond repair. Both passengers were Ricardo Casal, Minister of Justice and Security, and Maria del Carmen Falbo, Attorney.
Probable cause:
Loss of control during takeoff following the crew's decision to perform the operation outside of the procedures established in the flight manual. The overconfidence of the crew as well as the operation of both engines at low regime were considered as contributing factors.
Final Report:

Crash of a Learjet 55C Longhorn in Rio de Janeiro

Date & Time: Aug 12, 2010 at 0926 LT
Type of aircraft:
Operator:
Registration:
PT-LXO
Flight Type:
Survivors:
Yes
Schedule:
Rio de Janeiro - Rio de Janeiro
MSN:
55C-135
YOM:
1988
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
17000
Captain / Total hours on type:
500.00
Copilot / Total flying hours:
2800
Copilot / Total hours on type:
49
Circumstances:
The aircraft departed Rio de Janeiro-Santos Dumont Airport on a positioning flight to Rio de Janeiro-Galeão-Antonio Carlos Jobim Airport with three crew members on board. Two minutes after takeoff, while in initial climb, the electrical system of the aircraft suffered a voltage power loss. Several instruments lost their functionality such as TCAS, altimeters and airspeed indicator. In good weather conditions, the captain decided to return to Santos Dumont Airport but did not declare any emergency. After being cleared to descend to 3,000 feet, the crew lost all radio communications. On final approach to runway 02R, most of the instruments failed but the crew continued the approach. The aircraft passed over the runway threshold with an excessive speed of 25 knots and after touchdown, the crew started the braking procedure but the spoilers and the reversers could not be activated. Unable to stop within the remaining distance, the aircraft overran and came to rest in the Guanabara Bay. All three crew members escaped uninjured while the aircraft was damaged repair.
Probable cause:
An error in the assembly was detected in the left generator, which interfered with the D+ terminal signal sent to the voltage regulator. Due to a voltage drop, some of the instruments lost their functionality. The following contributing factors were identified:
- The crew did not follow the emergency procedures;
- The crew decided to return to land at Santos Dumont Airport without considering that the runway length was less than the length required for an emergency landing;
- The speed of the aircraft while passing over the runway threshold was 25 knots above the reference speed;
- The pilots were unable to engage the spoilers or the thrust reversers;
- Wrong attitude from the captain;
- Overconfidence of the crew;
- Emotional load due to an emergency situation;
- Poor assessment of the situation due to high stress associated with decreased situational awareness;
- Poor crew coordination;
- Lack of crew resource management;
- Poor judgment;
- Lack of procedures on the part of the operator.
Final Report:

Crash of a Dassault Falcon 20F in Chiclayo

Date & Time: Jun 18, 2010 at 1930 LT
Type of aircraft:
Operator:
Registration:
FAP-300/OB-1433
Flight Type:
Survivors:
Yes
Schedule:
Chiclayo – Lima
MSN:
434
YOM:
1983
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Shortly after takeoff from Chiclayo Airport, while climbing, the crew contacted ATC, reported technical problems and was cleared for an immediate return. On final approach, the crew was forced to make an emergency landing when the aircraft crash landed about 500 metres short of runway. All 8 occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
One of the engine failed during initial climb for unknown reasons.

Crash of a PZL-Mielec M28 Skytruck on Mt Izcaragua: 3 killed

Date & Time: Jun 12, 2010 at 0725 LT
Type of aircraft:
Operator:
Registration:
ENBV-0063
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Valle de la Pascua – La Carlota
MSN:
AJE002-02
YOM:
2000
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The twin engine airplane departed Valle de la Pascua Airport at 0646LT on a flight to La Carlota-General Francisco de Miranda Air Base. At 0722LT, the crew reported his position at 7,000 feet when contact was lost. The wreckage was found the following day at 1700LT in a wooded and hilly terrain located between Mt Izcaragua and Mt Meregoto, about 18 km northeast of La Carlota Airport. The aircraft was destroyed and all three occupants were killed.

Crash of an Embraer EMB-110P Bandeirante in Cascavel

Date & Time: May 19, 2010 at 0510 LT
Operator:
Registration:
PT-GKQ
Flight Type:
Survivors:
Yes
Schedule:
Sorocaba – Cascavel
MSN:
110125
YOM:
1976
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6879
Captain / Total hours on type:
2000.00
Copilot / Total flying hours:
1121
Copilot / Total hours on type:
15
Circumstances:
The twin engine aircraft departed Sorocaba on a cargo flight to Cascavel, carrying two pilots and a load consisting of pharmaceutical materials. On final approach in low visibility due to bad weather conditions and night, the aircraft descended below the glide and impacted the ground 700 metres short of runway 33. On impact, it lost its undercarriage then slid for 150 metres before coming to rest. Both pilots escaped uninjured while the aircraft was damaged beyond repair. Visibility at the time of the accident was 1,200 metres with mist, local patches of fog and ceiling at 100 feet. Cascavel Airport was equipped with an NDB only.
Probable cause:
Controlled flight into terrain after the crew descended too low in IMC conditions. The following contributing factors were identified:
- Visibility was below minimums,
- The crew continued the descent until the aircraft impacted ground and failed to initiate a go-around procedure,
- A probable crew fatigue,
- It is possible that the crew suffered optical illusions,
- Overconfidence on part of the captain,
- The captain did not request any assistance from the copilot during the approach procedure,
- Inexperienced, the copilot did not interfere despite dangerous flight conditions,
- Poor organizational culture,
- Deficiencies in crew training,
- Lack of crew discipline,
- Poor flight planning,
- Lack of supervision on part of the operator,
- The copilot was inexperienced on this type of aircraft.
Final Report:

Crash of a PZL-Mielec AN-28 in Poeketi: 8 killed

Date & Time: May 15, 2010 at 1510 LT
Type of aircraft:
Operator:
Registration:
PZ-TSV
Flight Phase:
Survivors:
No
Schedule:
Godo Olo – Paramaribo
MSN:
1AJ007-10
YOM:
1990
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
8
Circumstances:
En route from Godo Olo to Paramaribo, the twin engine aircraft crashed in unknown circumstances in a wooded area located 5 km northeast from Poeketi. The wreckage was found few hours later and all 8 occupants were killed.