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Bahia

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 Beechcraft 300 Super King Air in Porto Seguro

Date & Time: Apr 21, 2016 at 1140 LT
Registration:
PT-MCM
Flight Type:
Survivors:
Yes
Schedule:
Rio de Janeiro – Porto Seguro
MSN:
FA-52
YOM:
1985
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
8000
Captain / Total hours on type:
1000.00
Circumstances:
On final approach to Porto Seguro-Terravista Golf Club Airport Runway 15, the twin engine aircraft descended too low, causing the left main gear to impact the ground short of runway threshold. On impact, the left main landing gear was torn off. The aircraft slid on runway for few dozen metres then veered to the left and came to a halt. All 10 occupants evacuated safely and the aircraft was damaged beyond repair.
Probable cause:
The following factors were identified:
- Application of the commands - contributed
There was no effective action on the aircraft controls during the final approach to avoid a brutal impact with the ground prior to the runway threshold.
- Adverse weather conditions - undetermined
It is possible that the aircraft was under the effect of the phenomenon known as windshear, which affected the approach profil and the subsequent impact with the ground short of runway.
- Pilot judgement - contributed
The risks of a possible windshear during the final approach were not adequately considered by the pilot. The decision to proceed for the landing, to the detriment of the alternative recommended by experts to perform a missed approach, proved decisive for the development of the accident.
Final Report:

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 Beechcraft 350 Super King Air in Porto Seguro: 14 killed

Date & Time: May 22, 2009 at 2053 LT
Registration:
PR-MOZ
Flight Type:
Survivors:
No
Schedule:
São Paulo – Porto Seguro
MSN:
FL-237
YOM:
1999
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
12
Pax fatalities:
Other fatalities:
Total fatalities:
14
Captain / Total flying hours:
20000
Captain / Total hours on type:
5000.00
Copilot / Total flying hours:
357
Copilot / Total hours on type:
107
Circumstances:
The twin engine aircraft departed São Paulo-Congonhas Airport at 1831LT on a private flight to Porto Seguro, carrying 12 passengers and two pilots, among them the Brazilian Businessman Roger Wright, his wife, children and grandchildren. On approach to Porto Seguro-Terravista Golf Club Airport, the crew encountered poor weather conditions and the visibility was low due to the night. On final approach to runway 15, the aircraft impacted trees located 900 metres from the runway threshold. The aircraft continued for about 700 metres then struck others trees and crashed 200 metres short of runway, bursting into flames. The aircraft was totally destroyed and all 14 occupants were killed.
Probable cause:
The crew's decision to continue the approach in poor weather conditions following a high motivation to land at destination.
The following contributing factors were identified:
- The crew failed to follow the published procedures,
- The crew did not take the bad weather conditions into consideration and took the decision to land,
- Limited visibility due to rain falls and night,
- Weather conditions affected the perception of the pilots who suffered a loss of situational awareness,
- Poor judgment of the situation and flight conditions on part of the crew,
- The crew continued the approach under VFR mode in IMC conditions,
- The crew carried out an improvised VFR approach via a GPS system,
- Excessive approach speed,
- Poor crew coordination,
- Lack of crew discipline.
Final Report:

Crash of an Embraer EMB-820C Carajá in Lençóis: 2 killed

Date & Time: Mar 31, 2008 at 0630 LT
Operator:
Registration:
PT-VCI
Flight Type:
Survivors:
No
Schedule:
Salvador – Lençóis
MSN:
820-144
YOM:
1986
Location:
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
25000
Captain / Total hours on type:
1769.00
Copilot / Total flying hours:
750
Copilot / Total hours on type:
195
Aircraft flight hours:
7293
Circumstances:
The twin engine aircraft departed Salvador Airport at 0525LT on a cargo flight to Lençóis, carrying two pilots and a load of bank documents. On final approach to Lençóis Airport, the crew encountered limited visibility due to marginal weather conditions. The captain decided to continue the approach and completed a turn to the left when the aircraft crashed 2 km from the runway threshold, bursting into flames. The aircraft was totally destroyed and both pilots were killed.
Probable cause:
The decision of the captain to continue the approach under VFR mode in IMC conditions to an airport that was not suitable for IFR operations. The following contributing factors were identified:
- The lack of ground references may have contributed to the commander's spatial disorientation,
- Although the weather conditions made it impossible to land under VFR conditions, the captain insisted on landing, neglecting IFR procedures,
- The captain ignored the copilot's advice and continued with the approach procedure,
- The captain put the aircraft in an attitude that caused it to stall,
- Poor judgment on part of the captain,
- Despite the implementation of a CRM program, the operator was unable to identify that the captain was violating the published procedures.
Final Report:

Crash of a Rockwell Shrike Commander 500S in São Sebastião do Passé: 4 killed

Date & Time: Mar 14, 2007 at 1355 LT
Operator:
Registration:
PP-SEC
Flight Phase:
Survivors:
No
Schedule:
Petrolina – Salvador
MSN:
500-3094
YOM:
1971
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
6858
Captain / Total hours on type:
2368.00
Aircraft flight hours:
15843
Circumstances:
The twin engine aircraft departed Petrolina Airport at 1221LT on a flight to Salvador, carrying 2 passengers, 2 pilots and a load of bags containing bank documents. At 1332LT, while in cruising altitude, the crew contacted ATC and reported an engine failure. The captain elected to make an emergency landing and reduced his altitude when the aircraft entered a right turn and crashed in a field located in São Sebastião do Passé, about 50 km northwest of Salvador Airport. The aircraft was destroyed upon impact and all four occupants were killed.
Probable cause:
Engine failure in flight following a fuel exhaustion. It was determined that the crew failed to prepare the flight properly and did not calculate the fuel consumption correctly. Investigations determined that the crew calculated a fuel consumption of 100 liters per hour while the true consumption was 120 liters per hour. The following contributing factors were identified:
- Overconfidence on part of the crew,
- Poor organisational culture that affected flight safety,
- Poor flight planning,
- The crew failed to feather the propeller following the engine failure, causing drag and contributing to the loss of control at low height.
Final Report:

Crash of a Britten-Norman BN-2A-21 Islander near Cascalho: 3 killed

Date & Time: Jan 11, 2001 at 1440 LT
Type of aircraft:
Registration:
PT-KNE
Flight Phase:
Survivors:
No
Site:
Schedule:
Paramirim - Paramirim
MSN:
696
YOM:
1973
Location:
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
3886
Captain / Total hours on type:
3263.00
Copilot / Total flying hours:
6088
Copilot / Total hours on type:
23
Circumstances:
The twin engine aircraft departed Paramirim Airport at 1400LT on a 3-hours ore prospecting flight, carrying two pilots and one passenger. En route, weather conditions worsened and the crew apparently decided to return to Paramerim when he encountered atmospheric turbulences and windshear. The aircraft stalled and crashed in a mountainous area. After 17 hours without contact, the aircraft was declared as missing. Its wreckage was found the following day at 1800LT near the summit of Mt Serra Preta, near Cascalho, about 27 km east of Paramirim. The aircraft was destroyed and all three occupants were killed.
Probable cause:
Loss of control after the crew encountered adverse weather conditions with low level windshear. The following contributing factors were identified:
- Although the operations were carried out in accordance with the regulations in force, the pilots regularly exceeded the flight times and this type of prospecting mission is extremely tiring insofar as it is systematically operated at low altitude without the aid of the autopilot system in a high outside temperature environment, leading to greater than normal physical wear of the pilots,
- Poor flight preparation regarding the probable evolution of the weather conditions,
- The accident occurred in low visibility as the crew was presumably trying to return to his base,
- The accident occurred outside of the intended flight area,
- The flight, which was scheduled to take three hours, was started with an aircraft whose tanks were full (seven hours autonomy), unnecessarily increasing its weight,
- Poor flight planning,
- Non-compliance with standard operator procedures on part of the crew who positioned the flaps in an inappropriate angle to fly over obstacles,
- In the days preceding the accident, two incidents occurred at Paramirim Airport involving the captain, and neither of these two events had been reported to the management of the operator, indicating the absence of an effective control of operations,
- The supervision of crew schedules was poor,
- The operator wanted this type of flight to be carried out in the morning in order to avoid atmospheric turbulence specific to the region, but the crew decided to take off in the afternoon when the conditions were not favorable.
Final Report:

Crash of an Embraer EMB-820C Navajo in Jequié: 2 killed

Date & Time: Jan 11, 2001
Operator:
Registration:
PT-EFA
Flight Type:
Survivors:
No
Schedule:
Ilhéus – Jequié
MSN:
820-025
YOM:
1976
Location:
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
15536
Captain / Total hours on type:
10179.00
Copilot / Total flying hours:
650
Circumstances:
On approach to Jequié Airport, the crew encountered poor weather conditions. While descending too low in the Vale de Pedra, the aircraft struck the ground and crashed few km from the airport. The captain was killed and the copilot was seriously injured. He died few hours later.
Probable cause:
The crew continued the descent under VFR mode in IMC conditions and descended too low to maintain a visual contact with the ground until the aircraft impacted terrain. The following contributing factors were identified:
- Poor crew coordination,
- Lack of visibility,
- The crew failed to follow the published procedures.
Final Report:

Ground fire of an ATR42-320 in Mucuri

Date & Time: Mar 16, 1999 at 1818 LT
Type of aircraft:
Operator:
Registration:
PT-MFI
Survivors:
Yes
Schedule:
São Paulo – Mucuri
MSN:
302
YOM:
1992
Country:
Crew on board:
4
Crew fatalities:
Pax on board:
10
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
10500
Captain / Total hours on type:
3550.00
Copilot / Total flying hours:
6500
Copilot / Total hours on type:
799
Circumstances:
On approach to Mucuri-Itabatã Airport runway 05, the right engine caught fire. The crew followed the checklist, continued the approach and completed a safe landing. After touchdown, the aircraft slightly deviated to the right and came to rest, bursting into flames. All 14 occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
It is believed that the engine fire was the consequence of the failure of a fuel burner.
Final Report:

Crash of an Embraer EMB-820C Navajo in Guanambi: 3 killed

Date & Time: May 20, 1998 at 1442 LT
Operator:
Registration:
PT-ENP
Flight Type:
Survivors:
No
Schedule:
Salvador - Guanambi
MSN:
820-075
YOM:
1978
Location:
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
9850
Captain / Total hours on type:
4940.00
Copilot / Total flying hours:
867
Copilot / Total hours on type:
218
Circumstances:
The twin engine aircraft was completing a cargo flight from Salvador to Guanambi, carrying one passenger, two pilots and a load consisting of briefcases containing valuables. On final approach to Guanambi Airport, following a 1 hour and 42 minutes of flight, both engines lost power. The crew lost control of the airplane that crashed few hundred metres short of runway. All three occupants were killed.
Probable cause:
The following findings were identified:
- Failure of the left engine on final approach,
- Possible over-correction on part of the pilot-in-command, causing a loss of control after a full rudder compensation,
- The aircraft was in a flaps and landing gear down configuration and it is believed that the copilot failed to assist the pilot during an emergency situation,
- The distance between the aircraft and the ground was insufficient to expect recovery,
- The crew used the auxiliary fuel tanks during all flight without paying attention to the potential danger of such procedure,
- Lack of crew support and crew training on part of the operator,
- Lack of crew resources management.
Final Report: