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:

Crash of a Beechcraft C90B King Air in Ipumirim: 1 killed

Date & Time: Sep 15, 2018 at 1200 LT
Type of aircraft:
Operator:
Registration:
PR-RFB
Flight Phase:
Survivors:
No
Schedule:
Florianópolis – Chapecó
MSN:
LJ-1546
YOM:
1999
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The pilot departed Florianópolis-Hercílio Luz Airport at 1100LT on a flight to Chapecó. Following an uneventful flight, the pilot initiated the descent to Chapecó-Serafim Enoss Bertasco Airport but encountered marginal weather conditions with limited visibility. While descending under VFR mode, the aircraft collided with trees and crashed in a dense wooded area located in Ipumirim, some 50 km east of Chapecó Airport, bursting into flames. The aircraft was destroyed by impact forces and a post crash fire and the pilot, sole occupant, was killed.
Probable cause:
Controlled flight into terrain.
Contributing factors.
- Attitude - contributed
The fact that the pilot continued the descent visually, not performing the instrument approach according to the IFR flight plan, denoted disregard of the real risks of this action. Thus, his attitude contributed to the inappropriate approach that culminated in the collision with the ground.
- Adverse weather conditions - contributed
Despite the aerodrome presenting ceiling and visibility conditions favorable for visual flight at the time of the accident, it was verified that there was dense fog covering the entire region near the impact site and, therefore, the IFR rules, which determined a minimum altitude of 5,000 ft, should have been observed.
- Emotional state - undetermined
Some events in the pilot's personal life were negatively affecting his emotional state. In addition, the pilot appeared to be more introspective in the period leading up to the accident.
Thus, it is possible that his performance was impaired due to his emotional state.
- External influences - undetermined
The pilot was possibly experiencing difficult events in his personal life. These events could have negatively affected his emotional state.
Thus, the pilot's way of thinking, reacting and performance at work may have been impacted by factors external to work.
- Motivation - undetermined
The pilot intended to return home because he would be celebrating his birthday and that of his stepdaughter.
The audio recording of the pilot's telephony with the GND-FL, shows that he insisted to accelerate his take-off, denoting a possible high motivation focused on fulfilling his eagerness to accomplish the flight. This condition may have influenced the flight performance.
- Decision making process - contributed
The choice to continue the descent without considering the IFR rules, based on an inadequate judgment of the meteorological conditions, revealed the pilot's difficulties to perceive, analyze, choose alternatives and act adequately in that situation.
Final Report:

Crash of a Beechcraft A100 King Air in Itapaci

Date & Time: Sep 6, 2018 at 0830 LT
Type of aircraft:
Operator:
Registration:
PT-LJN
Survivors:
Yes
Schedule:
Goiânia – Ceres
MSN:
B-121
YOM:
1972
Location:
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The twin engine airplane departed Goiânia-Santa Genoveva Airport at 0810LT on a charter flight to Ceres, carrying nine passengers and one pilot. En route, it was decided to change the itinerary and to land in Itapaci where there was no suitable terrain for landing. On final approach, the aircraft impacted ground, lost its undercarriage and veered to the right. It collided with a fence and made a 180 turn before coming to rest. All 10 occupants evacuated safely and the aircraft was damaged beyond repair. On board was the candidate for governor of the state of Goiás and his campaign team.
Probable cause:
The pilot intentionally changed his routing for Itapaci where the landing zone was not approved for flight operations. During the landing, the plane struck the ground before the planned zone and crashed. The pilot violated the rules established by the authority.
Final Report:

Crash of a Beechcraft C90GTi King Air in Vila Rica

Date & Time: Sep 5, 2018 at 1120 LT
Type of aircraft:
Registration:
PR-GVJ
Flight Type:
Survivors:
Yes
Schedule:
Belo Horizonte – Confresa
MSN:
LJ-2145
YOM:
2017
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The twin engine airplane departed Belo Horizonte-Pampulha-Carlos Drummond de Andrade Airport at 0820LT on a private flight to Confresa, carrying five passenger and one pilot. While descending to Confresa, the pilot decided to fly directly to the farm of the owner (Fazenda Angola) located in Vila Rica, about 80 km northeast of Confresa Airport. On final approach, the aircraft was too low when it struck the surface of a lake then its bank. On impact, the undercarriage were torn off and the aircraft crash landed and came to rest on its belly. There was no fire. All six occupants were injured, one seriously. The aircraft was damaged beyond repair.
Probable cause:
The pilot descended too low on approach to an umprepared terrain.
Contributing Factors:
- Attitude,
- Command application,
- Pilot judgment,
- Decision making process,
- Lack of adherence to regulations established by the authority of Brazilian civil aviation.
Final Report:

Crash of a Beechcraft C90GTi King Air in Campo de Marte: 1 killed

Date & Time: Jul 29, 2018 at 1810 LT
Type of aircraft:
Operator:
Registration:
PP-SZN
Survivors:
Yes
Schedule:
Videira – Campo de Marte
MSN:
LJ-1910
YOM:
2008
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
While approaching Campo de Marte Airport by night following an uneventful flight from Videira, the crew encountered technical problems with the landing gear and was cleared to complete two low passes over the runway to confirm visually the problem. While performing a third approach, the twin engine airplane rolled to the left then overturned and crashed inverted about 100 metres to the left of runway 30, bursting into flames. Six occupants were injured and one pilot was killed.