Crash of a Britten Norman BN-2A-3 Islander in Aldeia Pikany: 5 killed

Date & Time: Dec 4, 2013 at 1130 LT
Type of aircraft:
Operator:
Registration:
PT-WMY
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Aldeia Pikany – Novo Progresso
MSN:
314
YOM:
1974
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
530
Captain / Total hours on type:
58.00
Circumstances:
Shortly after takeoff from The Pikany Indian Reserve Airfield, while in initial climb, the twin engine aircraft lost height, collided with trees and crashed in a wooded area located on km from the airstrip. The aircraft was destroyed and all five occupants were killed, among them Indian Kayapo who were flying to Novo Progresso to have urgent care.
Probable cause:
The following factors were identified:
- The utilization of an aircraft not included in the Operating Specifications and of a runway neither registered nor approved, with a pilot who did not have the amount of hours necessary nor specific training, disclose a culture based on informal practices, which led to operation below the minimum safety requirements.
- It is possible that the pilot forgot to verify the quantity of fuel in the tanks of the aircraft before takeoff.
- The lack of specific training for the pilot and for the coordinator who, possibly, assumed the function of instructor may have compromised their operational performance during the preparation and conduction of the flight, since they were not effectively prepared for the activity.
- It is possible that the pilot failed to comply with the prescriptions of the legislation relatively to the minimum amount of fuel required for the flight leg. The operation of the aircraft by a pilot with expired qualifications and without the required training goes against the prescriptions at the time, but it was not determined whether this pilot (coordinator) was in the aircraft controls at the moment of the accident. The transport of a cylinder onboard the aircraft also configures flight indiscipline, since it goes against the legislation which prohibits the transport of such material.
- The lack of training of the differences may have contributed to the forgetting to verify the fuel tanks, a procedure that is prescribed in the aircraft manual. Likewise, lack of training may have deprived the pilots from acquiring proficiency for the operation of the aircraft in a single engine condition.
- The fact of conducting a flight to provide assistance in an emergency situation may have contributed to the pilot having forgotten to check safety parameters, such as the amount of fuel necessary.
- The pilot’s intention to earn his operational promotion may have stimulated him excessively, to the point of disregarding the minimum safety requirements for the operation. In addition, the emergency nature of the flight request possibly added to the motivation of the pilot and the coordinator.
- It is possible that, due to having little total experience either both of flight and in the aircraft, the pilot lost control of the aircraft when faced with the situation of in-flight engine failure after the takeoff.
- It is possible that the pilot and the coordinator prioritized the emergency requirement of the situation, failing to evaluate other aspects relevant for the safety of the flight, such as planning, for example.
- The lack of control on the part of the company’s management in relation to the flights operating outside of the main base allowed the pilot and the base manager to conduct a flight without the operating sector authorization. The lack of supervision of the air transport service provision by the contracting organizations allowed the company to provide services without the minimum conditions required by the legislation. Such conditions exposed the passengers to the risks of an irregular operation.
Final Report:

Crash of a Swearingen SA227AC Metro III in Riberalta: 8 killed

Date & Time: Nov 3, 2013 at 1556 LT
Type of aircraft:
Operator:
Registration:
CP-2754
Survivors:
Yes
Schedule:
Trinidad - Riberalta
MSN:
AC-721B
YOM:
1989
Flight number:
AEK025
Location:
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
16
Pax fatalities:
Other fatalities:
Total fatalities:
8
Circumstances:
Following an uneventful flight from Trinidad, the crew started the descent to Riberalta Airport in poor weather conditions with a visibility reduced to 3 km due to rain falls. After touchdown on wet runway 14, the aircraft was unable to stop within the remaining distance. It overran, collided with obstacles and came to rest upside down, bursting into flames, some 300 metres short of runway 32 threshold. Ten people were rescued while eight passengers were killed. The aircraft was totally destroyed. The exact circumstances of the accident remains unclear.

Crash of a De Havilland DHC-8-202 near Acandí: 4 killed

Date & Time: Oct 5, 2013 at 0100 LT
Registration:
N356PH
Flight Phase:
Survivors:
Yes
Site:
Schedule:
Panama City - Panama City
MSN:
502
YOM:
1997
Location:
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
The aircraft departed Panama City-Marcos A. Gelabert Airport in the evening on an anti-narcotic survey flight over Colombia, carrying four passengers and two pilots, five US citizens and one Panamanian. En route, while cruising along the border between Panama and Colombia, the aircraft collided with trees and crashed on the slope of a wooded mountain, bursting into flames. All four passengers were killed and both pilots were seriously injured.

Crash of a Dornier DO228-202K in Viña del Mar: 2 killed

Date & Time: Sep 9, 2013 at 0950 LT
Type of aircraft:
Operator:
Registration:
CC-CNW
Flight Type:
Survivors:
No
Schedule:
Coquimbo - Viña del Mar
MSN:
8063
YOM:
1986
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
15537
Captain / Total hours on type:
12431.00
Copilot / Total flying hours:
10777
Aircraft flight hours:
25012
Circumstances:
The crew departed Coquimbo on a positioning flight to Viña del Mar to pick up passengers who need to fly to a mining area located in Los Perlambres. As the ILS system was inoperative, the crew was forced to complete a non-precision approach to runway 05. The visibility was poor due to foggy conditions. On final approach, while the aircraft was unstable, the crew descended below the MDA until the aircraft collided with power cables and crashed in an open field located about 1,8 km short of runway. The aircraft was destroyed upon impact and both pilots were killed.
Probable cause:
Controlled flight into terrain following the decision of the crew to continue the approach below the MDA without visual contact with the runway until the aircraft impacted ground.
The following contributing factors were identified:
- Failure to apply the concepts of Crew Resource Management (CRM).
- Failure to use checklists.
- Failure to brief the maneuvers to be executed.
- Loss of situational awareness of the crew.
- Failure to keep a sterile cockpit during approach.
- Complacency and overconfidence of the pilots.
- Unstabilized instrument approach.
- Lack and/or non-use of equipment and systems to support the flight.
Final Report:

Crash of a Swearingen SA227DC Metro 23 in Sucre

Date & Time: Aug 20, 2013 at 0847 LT
Type of aircraft:
Operator:
Registration:
CP-2655
Survivors:
Yes
Schedule:
Potosí – Sucre
MSN:
DC-819B
YOM:
1993
Flight number:
AEK228
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
11073
Captain / Total hours on type:
806.00
Copilot / Total flying hours:
1553
Copilot / Total hours on type:
953
Aircraft flight hours:
34860
Circumstances:
Following an uneventful flight from Potosí, the crew started the descent to Sucre-Juana Azurduy de Padilla Airport Runway 05 in good weather conditions. After touchdown, at a speed of about 50 knots, the aircraft deviated to the left then pivoted 90° left, veered off runway and rolled for about 50 metres before coming to rest in a rocky ditch. There was no fire. All 10 occupants evacuated safely and the aircraft was damaged beyond repair.
Probable cause:
Loss of control after landing due to the failure of the nosewheel steering system.
Final Report:

Crash of a Comp Air CA-8 in Sorocaba: 2 killed

Date & Time: May 29, 2013 at 1540 LT
Type of aircraft:
Operator:
Registration:
PP-XLR
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Sorocaba - Jundiaí
MSN:
0204CA8
YOM:
2006
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
Shortly after take off from Sorocaba Airport, while climbing, the pilot encountered technical problems and elected to return. While trying to land in a wasteland, the single engine aircraft crashed in a street and was destroyed by impact forces and a post impact fire. Both occupants were killed as a house was also destroyed.

Crash of a Learjet 60 in Valencia: 2 killed

Date & Time: May 5, 2013 at 1000 LT
Type of aircraft:
Operator:
Registration:
N119FD
Flight Type:
Survivors:
No
Site:
Schedule:
Charallave – Valencia
MSN:
60-029
YOM:
1994
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
On final approach to Valencia-Arturo Michelana Airport in marginal weather conditions, the aircraft crashed in a residential area some 2,055 metres short of runway. The aircraft was totally destroyed by impact forces and a post impact fire and both pilots were killed. A building, several houses and cars were also damaged by fire.

Crash of an Embraer EMB-820C Carajá in Almeirim: 10 killed

Date & Time: Mar 12, 2013 at 2030 LT
Operator:
Registration:
PT-VAQ
Survivors:
No
Schedule:
Belém - Almeirim
MSN:
820-140
YOM:
1986
Location:
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
10
Captain / Total flying hours:
1300
Captain / Total hours on type:
70.00
Circumstances:
The twin engine aircraft departed Belém-Val de Cans-Júlio Cezar Ribeiro Airport at 1907LT on a flight to Almeirim, carrying one pilot and nine employees of a company taking part to the construction of a hydro-electric station in the area. Following an eventful flight at FL85, the pilot started the descent to Almeirim and contacted ground at 2023LT. On final approach by night, the aircraft descended too low, impacted ground and crashed 5 km short of runway, bursting into flames. The aircraft was destroyed and all 10 occupants were killed.
Probable cause:
The following findings were identified:
- The pilot took the risks inherent to that flight when he accepted to be the only crewmember on a night-time flight with an aircraft in which he lacked enough experience. It is therefore considered that the pilot was complacent when he accepted to fly the aircraft under those circumstances, taking the risks associated with the operation.
- The fact that the pilot made a phone call to his father, to tell that he was feeling insecure for conducting the flight, may be considered an indication that he was not confident, and this condition may have influenced negatively his operational performance during the descent procedure.
- It is possible that the motivation of the pilot in making a fast progress in his career contributed to his acceptance of the challenge to operate the flight, even if he was not feeling fully confident.
- It is possible that the characteristics related to the type of flight, regions, time of the day, in addition to the fact that the pilot was flying the aircraft alone for the first time, contributed to an unclear perception of the relevant elements around him, leading him to a mistaken comprehension, which resulted in the deterioration of his ability to foresee the events.
- The operational progress of the pilot in the company was expedited and, therefore, it is possible that for this reason he did not gather the necessary experience for conducting that type of flight.
- It is possible that the way the work was organized within the company, with designation of pilots not readapted in the aircraft for night-time flights without artificial horizon, and for takeoffs with an aircraft weight above the one prescribed in the manual contributed to the event that resulted in the accident.
- It is possible that the prioritization of the financial sector, in detriment of operational safety, contributed to the designation of a single pilot with short experience for transporting nine passengers.
- It is probable that the pilot, during the preparation of the aircraft for landing, allowed the its speed and power to drop to a value below the minima required for maintenance of level flight on the downwind leg.
- It is possible that the location of the runway in an isolated area of the Amazonian jungle region, without visual references in a night-time flight, contributed to the pilot’s difficulty maintaining a sustained flight.
- It is possible that the training done by the pilot in a shortened manner deprived him from the knowledge and other technical abilities necessary for flying the aircraft.
- The decisions of the company operation sector to designate a short-experienced pilot without a copilot for a night flight destined for an aerodrome located in a jungle region without visual reference with the terrain increased the risk of the operation. Therefore, the risk management process was probably inappropriate.
- It was the first time the pilot was flying the aircraft on a night-time flight without a copilot. Since he had only little experience in the aircraft, it is possible that his operational performance was hindered in the management of tasks, weakening his situational awareness.
- It was not possible to determine whether the company chose to dispense with the copilot on account of the need to transport a ninth passenger and, thus, did not consider in a conservative manner the prescription contained in the aircraft airworthiness certificate by designating just one pilot for the flight.
Final Report:

Crash of a Beechcraft B200 Super King Air in Pias: 9 killed

Date & Time: Mar 6, 2013 at 0741 LT
Operator:
Registration:
OB-1992-P
Survivors:
No
Schedule:
Lima - Pias
MSN:
BB-1682
YOM:
1999
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
9
Captain / Total flying hours:
4509
Captain / Total hours on type:
312.00
Copilot / Total flying hours:
994
Copilot / Total hours on type:
425
Aircraft flight hours:
3859
Aircraft flight cycles:
4318
Circumstances:
The twin engine aircraft departed Lima-Jorge Chávez Airport at 0625LT on a charter flight to Pias, carrying two pilots and seven employees of the Peruvian company MARSA (Minera Aurífera Retamas) en route to Pias gold mine. On approach to Pias Airport, the crew encountered limited visibility due to foggy conditions. Heading 320° on approach, the crew descended too low when the aircraft collided with power cables, stalled and crashed on the slope of a mountain located 4,5 km from the airport, bursting into flames. The aircraft was destroyed by impact forces and a post crash fire and all 9 occupants were killed.
Probable cause:
Loss of control following the collision with high power cables after the crew lost visual references during an approach completed in poor weather conditions. The following contributing factors were identified:
- Inadequate meteorological information provided by the Pias Airport flight coordinator that did not reflect the actual weather condition in the area,
- Lack of a procedure card to carry out the descent, approach, landing and takeoff at Pias Airport, considering the visual and operational meteorological limitations in the area,
- The copilot training was limited and did not allow the crew to develop skills for an effective CRM in normal and emergency procedures.
Final Report:

Crash of a Beechcraft King Air C90A in Cândido Mota: 5 killed

Date & Time: Feb 3, 2013 at 2030 LT
Type of aircraft:
Registration:
PP-AJV
Flight Phase:
Survivors:
No
Schedule:
Maringá – São Paulo
MSN:
LJ-1647
YOM:
2001
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total hours on type:
441.00
Aircraft flight hours:
3137
Circumstances:
The twin engine aircraft departed Maringá Airport at 1837LT on a flight to São Paulo, carrying four passengers and one pilot. 35 minutes into the flight, about five minutes after he reached its assigned altitude of 21,000 feet, the aircraft stalled and entered an uncontrolled descent. The pilot was unable to regain control, the aircraft partially disintegrated in the air and eventually crashed in a flat attitude in a field. The aircraft was destroyed and all five occupants were killed.
Probable cause:
The following findings were identified:
- The lack of a prompt identification of the aircraft stall by the captain may have deprived him of handling the controls in accordance with the prescriptions of the aircraft emergency procedures, contributing to the aircraft entry in an abnormal attitude.
- The captain’s attention was focused on the passengers sitting in the rear seats, in detriment of the flight conditions under which the aircraft was flying. This had a direct influence on the maintenance of a poor situational awareness, which may have made it difficult for the captain to immediately identify that the aircraft was stalling.
- There was complacency when the copilot functions were assumed by a person lacking due professional formation and qualification for such. Even under an adverse condition, the prescribed procedure was not performed, namely, the use of the aircraft checklist.
- The fact that the aircraft was flying under icing conditions was confirmed by a statement of the female passenger in the cockpit (CVR). The FL210 (selected and maintained by the captain) gave rise to conditions favorable to severe icing on the aircraft structure. If the prevailing weather conditions are correlated with reduction of speed (attested by the radar rerun), the connection between loss of control in flight and degraded aircraft performance is duly established.
- The rotation of the aircraft after stalling may have contributed to the loss of references of the captain’s balance organs (vestibular system), making it impossible for him to associate the side of the turn made by the aircraft with the necessary corrective actions.
- The non-adherence to the aircraft checklists on the part of the captain, in addition to the deliberate adoption of non-prescribed procedures (disarmament of the starter and “seven killers”) raised doubts on the quality of the instruction delivered by the captain.
- The captain made an inappropriate flight level selection for his flight destined for São Paulo. Even after a higher flight level was offered to him, he decided to maintain FL 210. Also, after being informed about icing on the aircraft, he did not activate the Ice Protection System, as is expressly determined by the flight manual.
- The captain had the habit of making use of a checklist not prescribed for the aircraft, and this may have influenced his actions in response to the situation he was experiencing in flight.
- His recently earned technical qualification in the aircraft type; his inattention and distraction in flight; his attitude of non-compliance with operations and procedures prescribed in manuals; all of this contributed to the captain’s poor situational awareness.
- The flight plan was submitted via telephone. Therefore, it was not possible to determine the captain’s level of awareness of the real conditions along the route, since he did not report to the AIS office in SBMG. In any event, the selection of a freezing level for the flight, considering that the front was moving along the same proposed route, was indication of inappropriate planning.
- The investigation could neither determine the whole experience of the aircraft captain, nor whether his IFR flight experience was sufficient for conducting the proposed flight, since he made decisions which went against the best practices, such as, for example, selecting a flight level with known icing.
- With a compromised situational awareness, the pilot failed to correctly interpret the information available in the aircraft, as well as the information provided by the female passenger sitting in the cockpit, and he chose to maintain the flight level under inadequate weather conditions.
- The lack of monitoring/supervision of the activities performed by the captain allowed that behaviors and attitudes contrary to flight safety could be adopted in flight, as can be observed in this occurrence.
- Apparently, there was lack of an effective managerial supervision on the part of the aircraft operator, with regard to both the actions performed by the captain and the correction of the aircraft problems.
Final Report: