Crash of a Gulfstream G200 in Belo Horizonte

Date & Time: Sep 7, 2020 at 1826 LT
Type of aircraft:
Operator:
Registration:
PR-AUR
Flight Type:
Survivors:
Yes
Schedule:
Belo Horizonte - Belo Horizonte
MSN:
140
YOM:
2006
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing a local training flight at Belo Horizonte-Pampulha Airport, consisting of touch-and-go maneuvers. After landing on runway 13, the pilot-in-command decided to abort the takeoff. Unable to stop within the remaining distance, the aircraft overran, lost its landing gear and came to rest near a concrete block. All three occupants evacuated, among them the captain was slightly injured.

Crash of an Embraer EMB-121A Xingu in Tegará da Serra: 2 killed

Date & Time: Jun 14, 2020 at 0840 LT
Type of aircraft:
Registration:
PT-MBV
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Tangará da Serra – Goiânia
MSN:
121-053
YOM:
1982
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
607
Captain / Total hours on type:
41.00
Copilot / Total flying hours:
425
Aircraft flight hours:
4453
Circumstances:
Four minutes after takeoff from Tengará da Serra Airport Runway 20, while climbing, the twin engine airplane entered an uncontrolled descent. One minute later, it crashed with a high angle of attack in a cornfield, bursting into flames. The airplane disintegrated on impact and both occupants were killed.
Probable cause:
One should not rule out the hypothesis of a possible malfunction of the aircraft's angle-of-attack control system, considering that the records related to the provision of the calibration service (a necessary condition for the proper functioning of the referred system, and prescribed in the aircraft's maintenance manual) were not identified in the pertinent
control documents.
Final Report:

Crash of a Comp Air CA-8 in Campo Verde: 1 killed

Date & Time: Apr 13, 2020 at 1232 LT
Type of aircraft:
Operator:
Registration:
PP-XLD
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Campo Verde – Vera Cruz
MSN:
038SSW624
YOM:
2004
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
628
Captain / Total hours on type:
3.00
Circumstances:
After takeoff from Campo Verde-Luiz Eduardo Magalhães Airport, while climbing, the airplane entered a high pitch angle. The pilot initiated a sharp turn to the left when control was lost. The airplane dove into the ground and crashed in an open field, some 900 metres from the takeoff point, bursting into flames. The pilot, sole on board, was killed.
Probable cause:
The exact cause of the accident could not be determined. However, it is believed that the pilot may have encountered an unexpected situation that he was unable to manage due to his relative low experience.
Final Report:

Crash of a Beechcraft C90GT King Air near Caieiras: 1 killed

Date & Time: Dec 2, 2019 at 0602 LT
Type of aircraft:
Registration:
PP-BSS
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Jundiaí – Campo de Marte
MSN:
LJ-1839
YOM:
2008
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
6000
Captain / Total hours on type:
211.00
Circumstances:
The pilot departed Jundiaí-Comandante Rolim Adolfo Amaro Airport at 0550LT on a short transfer flight to Campo de Marte, São Paulo. While descending to Campo de Marte Airport, he encountered poor weather conditions and was instructed by ATC to return to Jundiaí. Few minutes later, while flying in limited visibility, the twin engine airplane impacted trees and crashed in a wooded area located in Mt Cantareira, near Caieiras. The aircraft was destroyed by impact forces and a post crash fire and the pilot, sole on board, was killed.
Probable cause:
The accident was the consequence of the combination of the following factors:
- Attention – undetermined.
It is likely that the pilot has experienced a lowering of his attention in relation to the available information and the stimuli of that operational context in face of the adverse conditions faced.
- Attitude – a contributor.
It was concluded that there was no reaction to the warnings of proximity to the ground (Caution Terrain) and evasive action to avoid collision (Pull Up), a fact that revealed difficulties in thinking and acting in the face of an imminent collision condition, in which the aircraft was found.
- Adverse meteorological conditions – a contributor.
The clouds height and visibility conditions did not allow the flight to be conducted, up to SBMT, under VFR rules.
- Piloting judgment – a contributor.
The attempt to continue with the visual flight, without the minimum conditions for such, revealed an inadequate assessment, by the pilot, of parameters related to the operation of the aircraft, even though he was qualified to operate it.
- Perception – a contributor
The ability to recognize and project hazards related to continuing flight under visual rules, in marginal ceiling conditions and forward visibility, was impaired, resulting in reduced pilot situational awareness, probable geographic disorientation, and the phenomenon known as " tunnel vision''.
- Decision-making process – a contributor.
The impairment of the pilot's perception in relation to the risks related to the continuation of the flight in marginal safety conditions negatively affected his ability to perceive, analyze, choose alternatives and act appropriately due to inadequate judgments and the apparent fixation on keeping the flight under visual rules, which also contributed to this occurrence.
Final Report:

Crash of a Cessna 550 Citation II in Maraú: 5 killed

Date & Time: Nov 14, 2019 at 1417 LT
Type of aircraft:
Registration:
PT-LTJ
Flight Type:
Survivors:
Yes
Schedule:
Jundiaí – Maraú
MSN:
550-0225
YOM:
1981
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
8000
Captain / Total hours on type:
2500.00
Copilot / Total flying hours:
350
Copilot / Total hours on type:
25
Aircraft flight hours:
6978
Aircraft flight cycles:
6769
Circumstances:
The aircraft took off from the Comandante Rolim Adolfo Amaro Aerodrome (SBJD), Jundiaí - SP, to the Barra Grande Aerodrome (SIRI), Maraú - BA, at about 1458 (UTC), in order to carry out a private flight, with two pilots and eight passengers on board. Upon arriving at the destination Aerodrome, at 1717 (UTC), the aircraft made an undershoot landing on runway 11, causing the main and auxiliary landing gear to burst. The airplane moved along the runway, dragging the lower fuselage and the lower wing, leaving the runway by its left side, and stopping with the heading lagged, approximately, 210º in relation to the landing trajectory. Afterwards, there was a fire that consumed most of the aircraft. The aircraft was destroyed. One crewmember and four passengers suffered fatal injuries and the other crewmember and four passengers suffered serious injuries.
Probable cause:
Contributing factors.
- Control skills – a contributor
The inadequate performance of the controls led the aircraft to make a ramp that was lower than the ideal. This condition had the consequence of touching the ground before the runway’s threshold.
- Attention – undetermined
During the approach for landing, the commander divided his attention between the supervision of the copilot's activities and the performance of the aircraft's controls. Such circumstances may have impaired the flight management and limited the reaction time to correct the approach ramp.
- Attitude – undetermined
The report that the commander took two photographs of the runway and of the Aerodrome with his cell phone, during the wind leg, reflected an inadequate and complacent posture in relation to his primary tasks at that stage of the flight, which may have contributed to this occurrence.
- Communication – undetermined
As reported by the commander, the low tone and intensity of voice used by the copilot during the conduct of callouts, associated with the lack of use of the head phones, limited his ability to receive information, which may have affected his performance in management of the flight.
- Crew Resource Management – a contributor
The lack of proper use of CRM techniques, through the management of tasks on board, compromised the use of human resources available for the operation of the aircraft, to the point of preventing the adoption of an attitude (go-around procedure) that would avoid the accident, from the moment when the recommended parameters for a stabilized VFR approach are no longer present.
- Illusions – undetermined
It is possible that the width of the runway, narrower than the normal for the pilots involved in the accident, caused the illusion that the aircraft was higher than expected, for that distance from the thrashold 11 of SIRI, to the point of influence the judgment of the approach ramp. In addition, the fact that the pilot was surprised by the geography of the terrain (existence of dunes) and the coloring of the runway (asphalt and concrete), may have led to a false visual interpretation, which reflected in the evaluation of the parameters related to the approach ramp.
- Piloting judgment – a contributor
The commander's inadequate assessment of the aircraft's position in relation to the final approach ramp and landing runway contributed to the aircraft touching the ground before the thrashold.
- Perception – undetermined
It is possible that a decrease in the crew's situational awareness level resulted in a delayed perception that the approach to landing was destabilized and made it impossible to correct the flight parameters in a timely manner to avoid touching the ground before the runway.
- Flight planning – undetermined
It is possible that, during the preparation work for the flight, the pilots did not take into account the impossibility of using the perception and alarm system of proximity to the ground that equipped the aircraft, and the inexistence of a visual indicator system of approach ramp at the Aerodrome.
- Other / Physical sensory limitations – undetermined
The impairment of the hearing ability of the aircraft commander, coupled with the lack of the use of head phones, may have interfered with the internal communication of the flight cabin, in the critical phase of the flight.
Final Report:

Crash of a Cessna 208B Grand Caravan in Manaus

Date & Time: Sep 16, 2019 at 1225 LT
Type of aircraft:
Operator:
Registration:
PT-MHC
Flight Phase:
Survivors:
Yes
Schedule:
Manaus - Maués
MSN:
208B-0543
YOM:
1996
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
22800
Captain / Total hours on type:
14150.00
Copilot / Total flying hours:
947
Copilot / Total hours on type:
791
Circumstances:
The single engine airplane departed Manaus-Eduardo Gomes Airport Runway 29 in heavy rain falls as weather conditions deteriorated shortly prior to takeoff. After liftoff, while in initial climb, the airplane lost altitude and crashed in a dense wooded area located 600 metres past the runway end. The aircraft was destroyed by impact forces and all 10 occupants were injured, among them six seriously. At the time of the accident, weather conditions were poor with heavy rain falls, turbulence and windshear.
Probable cause:
The accident was the consequence of the combination of the following factors:
- Control skills – undetermined.
While facing adverse conditions, the use of controls may have been inappropriate for the situation and may have contributed to the aircraft not being able to maintain a positive climb rate.
- Attitude – undetermined.
Familiarization with the region may have led to an attitude, on the part of the PIC, of minimizing the importance of analyzing adverse weather conditions, to the detriment of compliance with the minimum limits established by the company in its manuals.
- Training – undetermined.
It is possible that, due to possible inadequate training, the SIC did not identify the critical situation that arose shortly after the take-off in time to assist the PIC in maintaining flight control.
- Tasks characteristics – undetermined.
The characteristics present in the type of operation, compliance with schedules without the possibility of delays, due to the runway closing period, may have favored the self imposed pressure on the part of the PIC, leading him to operate with reduced safety margins.
- Adverse meteorological conditions – a contributor.
The conditions at the time of the take-off contributed to the aircraft not being able to maintain the flight with a positive climb rate. The probable occurrence of Windshear determined that the trajectory of the aircraft was modified until its collision with the ground.
- Crew Resource Management – undetermined.
On the part of the SIC, no assertive attitude was perceived in the sense of alerting the PIC that those conditions were not favorable for takeoff. Thus, the crew decided to carry out the take-off despite the company's SOP.
- Organizational culture – undetermined.
The company encouraged compliance with the legs even though, within the planning of flights, there was not an adequate margin of time to absorb any delays. This culture may have influenced the PIC's decision-making, which, despite encountering adverse conditions, chose to take off, since the short time on the ground in the intermediate locations did not allow room for delays.
- Emotional state – undetermined.
The reports indicated that the PIC felt pressured to perform the take-off even in the weather conditions found on the day of this occurrence. Also, according to the interviewees, this pressure would be related to the fulfillment of the flight schedule and the need to keep to the scheduled times. In this way, it is possible that their assessment of the performance of the flight was influenced by the stress resulting from the pressure to complete the flight within the expected time, given the closing time of the runway for works.
- Flight planning – a contributor.
The flight planning was not carried out properly, considering that the planned schedules and routes would end after the closing time of the SBEG runway for works, provided for in the NOTAM. This meant that there was little time to adjust the legs, increasing the workload and stress in the cabin.
- Decision-making process – a contributor.
There was a wrong assessment of the meteorological conditions, which contributed to the decision of performing it in an adverse situation.
- ATS publication– undetermined.
The TWR-EG did not inform, before the take-off, of the changes in the significant weather conditions that were occurring at the terminal, which could have contributed to the PIC's decision-making.
Final Report:

Crash of an Embraer EMB-121A1 Xingu II in Campinas

Date & Time: Apr 2, 2019 at 2315 LT
Type of aircraft:
Registration:
PT-FEG
Survivors:
Yes
Schedule:
Sorocaba - Palmas
MSN:
121-057
YOM:
1982
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The twin engine airplane departed Sorocaba-Estadual Bertram Luiz Leupolz Airport at 2300LT on a flight to Palmas, Tocantins, carrying three passengers and a crew of two. Few minutes after takeoff, the crew encountered technical difficulties and was cleared to divert to Campinas-Viracopos Airport. On final, he realized he could not make it so he attempted an emergency landing in a prairie located about 6 km short of runway 15 threshold. The wreckage was found less than a km from the Jardim Bassoli condominium and all five occupants, slightly injured, were evacuated. The aircraft was damaged beyond repair.

Crash of a Cessna 208 Caravan I near Caracaraí

Date & Time: Feb 9, 2019 at 1040 LT
Type of aircraft:
Operator:
Registration:
PR-RTA
Survivors:
Yes
Schedule:
Manaus - Caracaraí
MSN:
208-0380
YOM:
2004
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The single engine floatplane departed Manaus-Eduardo Gomes Airport on a charter flight to the area of the Xeriuini River near Caracaraí, carrying eight passengers and two pilots bound for a fish camp. Due to the potential presence of obstacles in the river due to low water level, the crew decided to land near the river bank. After landing, the left wing impacted a tree and the aircraft rotated to the left and came to rest against trees on the river bank. All 10 occupants evacuated safely and the aircraft was damaged beyond repair.
Probable cause:
The following findings were identified:
- Attention,
- Judgment,
- Perception,
- Management planning,
- Decision making processes,
- Organization processes,
- Support systems.
Final Report:

Crash of a Cessna 525 CitationJet M2 in Fazenda Fortaleza de Santa Terezinha: 4 killed

Date & Time: Nov 26, 2018 at 0830 LT
Type of aircraft:
Operator:
Registration:
PP-OEG
Survivors:
No
Schedule:
Belo Horizonte - Fazenda Fortaleza de Santa Terezinha
MSN:
525-0849
YOM:
2014
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
11000
Captain / Total hours on type:
522.00
Circumstances:
The twin engine airplane was completing a flight from Belo Horizonte-Pampulha-Carlos Drummond de Andrade to the Fortaleza de Santa Terezinha Farm (Fazenda Fortaleza de Santa Terezinha) located in Várzea da Palma, Jequitaí, Minas Gerais. On board were three passengers and one pilot. On final approach to runway 20, during the last segment, the airplane collided with a metallic water irrigation system. The pilot initiated a go around procedure when he lost control of the airplane that veered to the left, impacted the ground and crashed in a field located to the left of the runway, about 600 metres from the initial impact, bursting into flames. The aircraft was totally destroyed by impact forces and a post crash fire and all four occupants were killed, among them Mr. Adolfo Geo, owner of the Brazilian group ARG Ltd active in food, oil and construction. He was accompanied by his wife Margarida Janete Geo.
Probable cause:
The following factors were identified:
- Airport infrastructure – a contributor.
It was found that the irrigation pivot, at the point where the collision took place, was impairing the gauge of the approach surface as described in Ordinance 957/GC3, of 09JUL2015, which provided for restrictions on objects projected into the airspace that could adversely affect the safety or regularity of air operations.
- Piloting judgment – a contributor.
The final approach was carried out below the ideal approach ramp, allowing the collision against the pivot, located in the alignment of the runway.
- Perception – undetermined.
It is possible that the PIC, when approaching for the landing, did not notice the irrigation pivot and, therefore, collided with the obstacle.
- Flight planning – a contributor.
There was no prior coordination with the farm employees, in a timely manner so that the irrigation pivot could be repositioned to a safe location in relation to the flight trajectory on the final landing approach.
Final Report:

Crash of a Honda HA-420 HondaJet in Foz do Iguaçu

Date & Time: Sep 24, 2018 at 1342 LT
Type of aircraft:
Operator:
Registration:
PR-TLZ
Survivors:
Yes
Schedule:
Curitiba – Foz do Iguaçu
MSN:
420-00068
YOM:
2017
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5600
Captain / Total hours on type:
77.00
Copilot / Total flying hours:
660
Copilot / Total hours on type:
14
Circumstances:
The airplane departed Curitiba-Afonso Pena Airport at 1240LT on an executive flight to Foz do Iguaçu, carrying one passenger and two pilots. Following an uneventful flight, the crew started the descent to Foz do Iguaçu-Cataratas Airport. The aircraft was stabilized and landed on wet runway 32. After touchdown, the crew encountered difficulties to stop the aircraft that overran and came to rest into a ravine. All three occupants evacued safely and the aircraft was damaged beyond repair.
Probable cause:
The following findings were identified:
- The approach was considered stabilized;
- The required landing distance of 6,431t (1,960m) was compatible for the operation, since the LDA of runway 32 at SBFI was 7,201ft (2,195m);
- There was no evidence of malfunction of the aircraft brake system that could have caused the runway excursion;
- At the time of landing, the runway was wet with a significant amount of water on the pavement;
- The estimated deceleration corresponded to what would be expected on a very wet runway (> 3mm of water) with hydroplaning of the tires at higher speeds;
- The friction and macrotexture measurements had normal parameters and did not contribute to the aircraft's poor deceleration;
- The characteristics of the precipitation over threshold 14 associated with the large variations in wind direction and intensity were consistent with the windshear phenomenon, resulting from a microburst;
- The PR-TLZ sensors did not detect the occurrence of windshear during the landing approach;
- A sudden increase in the calibrated speed that peaked at 32kt altered the aircraft's lift and, consequently, reduced the tires' grip on the ground, resulting in poor braking in the parts where the ground speed was lower;
- The speedbrakes were not extended during the run after landing, contrary to what was prevised in the AFM;
- The aircraft ran the full length of the runway, overpassed its limits and crashed into a ravine;
- There was a windshear alert issued about 30 seconds after the landing of the PRTLZ by an aircraft that was at the threshold 32;
- The aircraft had substantial damage; and
- The crewmembers and the passenger left unharmed.
Contributing factors:
- Control skills – undetermined
Despite the low contribution of the speedbrakes to the reduction of the landing distance, this device represents a deceleration resource through aerodynamic drag that should not be neglected, especially during landing on wet runways, and could have contributed to avoiding runway excursion.
- Adverse meteorological conditions – a contributor
The large variation in wind intensity peaked at 32 kt. This variation lasted 13 seconds and raised the indicated speed from 76 kt to 108 kt. Considering that the speed of 108 kt was very close to the VREF (111 KCAS), it can be stated that this phenomenon altered the aircraft's lift and, consequently, reduced the tires' grip on the ground, leading to poor braking.
Final Report: