Country
code

São Paulo

Crash of a Piper PA-42-720 Cheyenne III in Sorocaba: 2 killed

Date & Time: Mar 31, 2017 at 1445 LT
Type of aircraft:
Operator:
Registration:
PP-EPB
Flight Type:
Survivors:
No
Schedule:
Manaus - Sorocaba
MSN:
42-8001035
YOM:
1980
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
3382
Captain / Total hours on type:
118.00
Circumstances:
The twin engine aircraft departed Manaus-Aeroclub de Flores Airport on a flight to Barra do Garças, carrying one passenger and one pilot. After takeoff from Manaus, the pilot changed his mind and decided to fly to Sorocaba. On final approach to Sorocaba-Bertram Luiz Leupolz Airport in good weather conditions, the aircraft impacted trees and crashed in a wooded area located about one km short of runway 18. The aircraft was destroyed and both occupants were killed. There was no fire.
Probable cause:
Contributing factors:
- Flight indiscipline – a contributor
The pilot failed to comply with the minimum fuel requirements laid down in the regulations, providing conditions for both engines to stop operating in flight, due to lack of fuel.
- Piloting judgment – a contributor
It was found in this flight an inadequate evaluation for certain parameters related to aircraft operation, particularly with regard to the influence of the chosen flight level on fuel consumption. This misjudgment led to the decision to proceed with the flight to the Aerodrome where it was intended to land, to the detriment of the more conservative option of finding a suitable place for an intermediate landing and a refueling, which led to the depletion of usable fuel in flight.
- Flight planning – a contributor
Inadequate flight preparation work, especially with regard to fuel calculation and cruise level selection, has degraded the safety level and also contributed to the actual accident.
- Decision-making process – undetermined
Difficulties in perceiving, analyzing, choosing alternatives, and acting appropriately due to inadequate judgment, may have resulted in poor assessment of flight parameters (available fuel, distance to destination, verified consumption, etc.), which may have favored the occurrence of lack of fuel failure.
Final Report:

Crash of a BAe 125-800B in São Paulo

Date & Time: Feb 9, 2017 at 2211 LT
Type of aircraft:
Operator:
Registration:
PT-OTC
Survivors:
Yes
Schedule:
Brasília – São Paulo
MSN:
258194
YOM:
1991
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The airplane departed Brasilía-Presidente Juscelino Kubitschek Airport in the evening on a charter flight to São Paulo-Congonhas, carrying two pilots and one passenger, the Senator Aécio Neves da Cunha. During the takeoff roll, a tire on one of the main landing gear failed. The crew continued the flight, informed ATC about his situation and preferred to divert to São Paulo-Guarulhos Airport that offered longer runway for an emergency landing. After touchdown by night, the aircraft deviated to the right then veered off runway. The left main gear collapsed and the aircraft came to rest in a grassy area. All three occupants evacuated safely and the aircraft was damaged beyond repair.

Crash of a Comp Air CA-9 in Campo de Marte: 7 killed

Date & Time: Mar 19, 2016 at 1523 LT
Type of aircraft:
Operator:
Registration:
PR-ZRA
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Campo de Marte – Rio de Janeiro
MSN:
0420109T01
YOM:
2012
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
7
Captain / Total flying hours:
215
Circumstances:
Shortly after takeoff from Campo de Marte Airport runway 30, the single engine airplane entered a right turn without gaining altitude. Less than one minute after liftoff, the aircraft impacted a building located in the Frei Machado Street, some 370 metres from runway 12 threshold. The aircraft was totally destroyed by impact forces and a post crash fire and all seven occupants were killed. One people on the ground was slightly injured. Owned by the Brazilian businessman Roger Agnelli, the aircraft was on its way to Santos Dumont Airport in Rio de Janeiro. Among the victims was Roger Agnelli, his wife Andrea, his both children John and Anna Carolina, the pilot and two other friends. They were enroute to Rio to take part to the wedding of the nephew of Mr. Agnelli.
Probable cause:
Contributing factors
- Pilot judgment - undetermined
The absence of manuals and performance charts to guide the operation and actions based only on empirical knowledge about the aircraft may have taken to an inadequate evaluation of certain parameters related to its operation. In this case, the performance of the aircraft under conditions of weight, altitude and high temperatures may have provided its conduction with reduced margins of safety during takeoff that resulted in the on-screen accident.
- Flight planning - undetermined
The informality present in the field of experimental aviation, associated with the absence of support systems, may have resulted in an inadequacy in the work of flight preparation, particularly with regard to performance degradation in the face of adverse conditions (high weight, altitude and temperature), compromising the quality of the planning carried out, thus contributing to it being carried out a takeoff under marginal conditions.
- Project - undetermined
During the PR-ZRA assembly process, changes were incorporated into the Kit's original design that directly affected the airplane's take-off performance. Since the submission of documentation related to in-flight testing or performance graphics was not required by applicable law, it is possible that the experimental nature of the project has enabled the operation of the aircraft based on
empirical parameters and inadequate to their real capabilities.
- Support systems - undetermined
The absence of a support system, in the form of publications that allowed obtaining equipment performance data in order to carry out proper planning, added risk to operations and may have led to an attempt to take off under unsafe conditions.
Final Report:

Crash of an Embraer EMB-820C Navajo in Santa Isabel

Date & Time: Feb 16, 2016 at 1430 LT
Operator:
Registration:
PT-WZA
Flight Phase:
Survivors:
Yes
Schedule:
Jacarepaguá – Campinas
MSN:
820-020
YOM:
1976
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
En route, the pilot encountered an unexpected situation and attempted an emergency landing. After landing on a road in Santa Isabel, the airplane collided with various obstacles and came to rest. All three occupants evacuated safely and the airplane was damaged beyond repair.

Crash of a Cessna 560XLS Citation Excel in Santos: 7 killed

Date & Time: Aug 13, 2014 at 1003 LT
Operator:
Registration:
PR-AFA
Survivors:
No
Site:
Schedule:
Rio de Janeiro – Santos
MSN:
560-6066
YOM:
2011
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
7
Captain / Total flying hours:
6235
Captain / Total hours on type:
130.00
Copilot / Total flying hours:
5279
Copilot / Total hours on type:
95
Aircraft flight hours:
434
Aircraft flight cycles:
392
Circumstances:
The aircraft took off from Santos Dumont Airport (SBRJ) at 12:21 UTC, on a transport flight bound for Santos Aerodrome (SBST), with two pilots and five passengers on board. During the enroute phase of the flight, the aircraft was under radar coverage of the approach control units of Rio de Janeiro and São Paulo (APP-RJ and APP-SP, respectively), and no abnormalities were observed. Upon being released by APP-SP for descent and approach toward SBST, the aircraft crew, already in radio contact with Santos Aerodrome Flight Information Service (Santos Radio), reported their intention to perform the IFR ECHO 1 RWY 35 NDB approach chart profile. After reporting final approach, the crew informed that they would make a go-around followed by a holding procedure, and call Santos Radio again. According to an observer that was on the ground awaiting the arrival of the aircraft at Santos Air Base (BAST) and to another observer at the Port of Santos, the aircraft was sighted flying over the aerodrome runway at low height, and then making a turn to the left after passing over the departure end of the runway, at which point the observers lost visual contact with the aircraft on account of the weather conditions. Moments later, the aircraft crashed into the ground. All seven occupants were killed.
Probable cause:
The following factors were identified:
- Considering the pronounced angle formed between the trajectory of the aircraft and the terrain, as well as the calculated speed (which by far exceeded the aircraft operating limit) moments before the impact, it is possible to infer that, from the moment the aircraft disappeared in the clouds, it could only have reached such speed and flown that trajectory if it had climbed considerably, to the point of being detected by the radar. Such condition presented by the aircraft may have been the result of an exaggerated application of controls.
- The making of an approach with a profile different from the one prescribed shows lack of adherence to procedures, which, in this case, may have been influenced by the self-confidence of the pilot on his piloting ability, given his prior experiences.
- Despite the lack of pressure on the part of the passengers to force compliance with the agenda, it is a known fact that this type of routine creates in the crew a self-pressure, most of the time unconscious, for accomplishing the flight schedule on account of the commitments undertaken by the candidate in campaign, and, therefore, the specific characteristics of this type of flight pose demands in terms of performance that may have influenced the pilots to operate with reduced safety margins.
- The meteorological conditions were close to the safety minimums for the approach and below the minimums for the circle-to-land procedure prescribed in the ECHO 1 approach. However, such conditions, by themselves, would not represent risk for the operation, if the profile of the ECHO 1 procedure was performed in accordance with the parameters established in the aeronautical publications and the flight parameters defined by the aircraft manufacturer. Upon verifying that the above mentioned parameters were not complied with, one observes that the meteorological conditions became a complicating factor for flying the aircraft, rendering it difficult to be stabilized on the final approach, and a go-around became necessary, as a result.
- In the scenario of the aircraft collision with the ground, there were aspects favorable to the occurrence of spatial disorientation, such as: reduction of the visibility on account of meteorological conditions, stress and workload increase due to the missed approach procedure, maneuvers with a G-load above 1.15G, and a possible loss of situational awareness. The large pitch-down angle, the high speed, and the power developed by the engines at the moment of impact are also evidence compatible with incapacitating disorientation, and point towards a contribution of this factor.
- The integration between the pilots may have been hindered by their little experience working together as one crew, and also by their different training background. In addition, the personal characteristics of the captain, as a more impositive and confident person, in contrast with the more passive posture of the copilot, may also have hampered the crew dynamics in the management of the flight.
- In the seven days preceding the day of the accident, the crew was in conformity with the Law 7183 of 5 April 1984 in relation to both duty time and rest periods. However, the analysis of copilot’s voice, speech, and language indicated compatibility with fatigue and somnolence, something that may have contributed to the degradation of the crew’s performance.
- Their lack of training of missed approach procedures in CE 560XLS+ aircraft may have demanded from the crew a higher cognitive effort in relation to the conditions required for the aircraft model, since they possibly did not have conditioned behaviors for controlling the flight and that could otherwise provide them with more agility with regard to the cockpit actions. Thus, they probably missed the skills, knowledge, and attitudes that would allow them to more adequately perform their activities in that operational context.
- Even though Santos Radio reported, in the first contact with the aircraft, that the aerodrome was operating IFR, the messages transmitted to the aircraft did not include the conditions of ceiling, visibility, and SIGMET information (ICA 100-37). This may have contributed to reducing the crew’s situational awareness, since the last information accessed by them was probably the 11:00 UTC SBST METAR, which reported VMC conditions for operation in the aerodrome. Thus, the pilots may have built a mental model of unreal SBST meteorological conditions more favorable to the operation.
- After coordination of the descent, the PR-AFA aircraft made a left turn and, for an unknown reason, deviated from the W6-airway profile, reporting six positions that were not compatible with the real flight path until the moment it started a final approach. This approach was different from the trajectory of the final approach defined for the ECHO 1 procedure, and was flown with speed parameters different from those recommended by the aircraft manufacturer. These aspects reduced the chances of the aircraft to align with the final approach in a stabilized manner. The fact that the aircraft made a low pass over the runway and then a left turn at low altitude in weather conditions below the minimum established in the circle-to-land procedure instead of performing the profile prescribed in the ECHO 1 approach chart also resulted in risks to the operation, and created conditions which were conducive to spatial disorientation.
- Since the captain had already conducted FMS visual approaches on other occasions, his acquired work-memory may have strengthened his confidence in performing the procedure again, even though in another scenario, on account of the human being tendency to rely on previous successful experiences.
- A poor perception on the part of the pilots relative to the real meteorological conditions on the approach may have compromised their level of situational awareness, thus leading the aircraft to a condition of operation below the safe minimums.
- The TAF/GAMET weather prognostics with validity up to 12:00 UTC, and available to the crew at the time the flight plan was filed at the AIS-RJ, indicated a possibility of degradation of the ceiling and visibility parameters on account of rain associated with mist, encompassing the duration of the aforementioned flight, especially in the area of SBST. The 11:00 UTC satellite image and the SIGMET valid from 10:30 UTC to 13:30 UTC, also showed an active cold front in the Southeast with stratiform cloud layers over SBST and a forecast of convective cells with northeasterly movement at an average speed of 12kt. Despite the availability of such information, the crew may not have made a more accurate analysis showing the swift deterioration of the weather conditions in the period between their takeoff from SBRJ and the approach to SBST, and thus may have failed to plan their conduct of the flight in accordance with the weather conditions forecast by the meteorological services.
- Despite having the C560 qualification required to operate the CE 560XLS+aircraft, the pilots were not checked by the employers as to their previous experience on this kind of equipment, or as to the need of transition training and/or specific formation to fly the PRAFA aircraft. The adoption of a formal process for the recruitment, selection, monitoring and evaluation of the performance of the professionals could have identified their training needs for that type of aircraft.
- Although the RBAC 61 requires pilots to undergo flight instruction and proficiency checks to switch between models of the CE 560XL family, the need of specific training was only clarified on 4 July 2014, with the publication of the ANAC Supplementary Instruction (IS 61-004, Revision A). Until that date, this need could only be determined by means of consultation of the FSB Report, made available only on the FAA website. In this context, the PR-AFA pilots would only be evaluated on the CE 560XLS+ aircraft on the occasion of their type revalidation, which would take place shortly before the expiration date of their C560 qualifications, which were valid until October 2014 (captain), and May 2015 (copilot). The fact that there was a qualification (C560) that was shared for the operation of C560 Citation V, C560 Encore, C560 Encore+, CE 560XL, CE 560XLS, or CE 560XLS + aircraft was not enough to make the DCERTA system refuse flight plans filed by pilots who lacked proper training to operate one of the aforementioned aircraft models. The RBAC 67 contained physical and mental health requirements which were not clear, inducing physicians to resort to other publications for guidance and support of their decisions and judgments relative to the civil aviation personnel. The absence of clear requirements to be adopted as the acceptable minimum for the exercise of the air activity, led the physicians responsible for judging the pilots’ health inspections’ to use their own discretion on the subject, opening gaps that could allow professionals not fully qualified to perform functions in flight below the minimum acceptable safety levels.
- Considering the possibility that the captain accumulated tasks as a result of a possible difficulty of the copilot in assisting him at the beginning of the missed approach procedure, such accumulation may have exceeded his ability to deal with the tasks, leading him to committing piloting errors and/or experiencing spatial disorientation.
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 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:

Crash of a Cessna 525B Citation CJ3 in São Paulo

Date & Time: Nov 11, 2012 at 1721 LT
Type of aircraft:
Operator:
Registration:
PR-MRG
Survivors:
Yes
Schedule:
Florianópolis – São Paulo
MSN:
525B-0187
YOM:
2008
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4048
Captain / Total hours on type:
521.00
Copilot / Total flying hours:
648
Copilot / Total hours on type:
189
Circumstances:
Following an uneventful flight from Florianópolis, the crew started the approach to São Paulo-Congonhas Airport Runway 35R. After touchdown, the airplane was unable to stop within the remaining distance. It overran, went down an embankment and came to rest against a fence, broken in two. The passenger and the copilot were slightly injured and captain was seriously injured. The aircraft was destroyed.
Probable cause:
The following findings were identified:
- The commander was overconfident in himself and the aircraft which led him to lose the critical capacity to discern the risks involved in the procedure that was adopting. Corroborating was the fact that the pilot judged he had much knowledge in this operation and knew exactly how the aircraft responded. It can be inferred there was complacency by the copilot on the actions of the commander, during the approach at high speed, because even feeling uncomfortable, he did not make an incisive interference because he believed in the idea that the commander had done this kind of approach, with high speed, and so knowing what he was doing.
- The pilot failed to identify the location of touch down during landing and not knowing how much runway was remaining, he decided he should not rush, thus demonstrating low situational awareness and lack of awareness, impacting the proper reaction time for the situation (Rush), which was not performed , leading the occurrence in question.
- The crew failed to properly assess the information available like speed and the runway length for the realization of a safe landing, which led to a poor judgment of the situation at hand, making the decision not to adopt the missed approach procedure.
- The distance between the crew, caused unconsciously by the commander's position with excess knowledge in the operation and the aircraft, and the insecurity of the copilot in considering new and inexperienced, resulted in a lack of assertiveness of the copilot to inform, with little emphasis, the commander of his perception of excessive airspeed.
- The crew did not adopt good crew resource management, failing to communicate with assertiveness and share critical information in time prior to landing, allowing the speeding remained present until the touchdown.
- Despite having adequate experience and training, the commander did not use the resources available, such as speed brakes to reduce the aircraft approach speed.
- The variable wind direction and predominantly tail intensity equal to or greater than 10 knots, allowed excessive speed during landing.
- The crew did not adopt good crew resource management, allowing the high speed to remain present until the touchdown.
- The commander thought he would be able to perform the approach and landing with the speed above the expected.
Final Report:

Crash of a McDonnell Douglas MD-11F in Campinas

Date & Time: Oct 13, 2012 at 1852 LT
Type of aircraft:
Operator:
Registration:
N988AR
Flight Type:
Survivors:
Yes
Schedule:
Miami - Campinas
MSN:
48434/476
YOM:
1991
Flight number:
CWC425
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
12900
Copilot / Total flying hours:
5198
Copilot / Total hours on type:
1368
Circumstances:
The airplane took off from Miami International Airport (KMIA), destined for Viracopos Airport (SBKP), with two pilots and a mechanic on board, on a non-regular cargo transport flight. The flight was uneventful up to the moment its landing in SBKP. On the approach for landing on runway 15, the crew performed the IFR ILS Z procedure. The weather conditions were VMC, with the wind coming from 140º at 19kt. When the aircraft was granted clearance to land, the wind strength was 20kt, gusting up to 29kt. The copilot was the Pilot Flying (PF), and the captain was the Pilot Monitoring (PM) at the moment of landing. When the aircraft touched down on the runway after the flare, the left main landing gear collapsed, causing the aircraft to skid on the runway for approximately 800 meters before stopping. There was substantial damage to the left main gear assembly, to the left wing, and left engine. The aircraft stopped within the runway limits. All three crew members were uninjured.
Probable cause:
It was determined that the “the landing gear failed due to overload in the cylinder structure”. The fracture started in the rear section of the cylinder in a connection hole which served as a tension concentration point, and ended in the front part of the cylinder with its breakage into two parts. Following a failure of the right main gear upon landing in Montevideo on 20 October 2009, the right main landing gear was replaced by VARIG Engineering & Maintenance (VEM), but the organization responsible for the research of damage, the specification of the services necessary for the restoration of airworthiness, and the provision of the services that enabled the restoration of the aircraft to an airworthy condition was not identified. The same aircraft parts were subjected to metallurgical analysis at the Boeing Long Beach Materials, Processing and Physics [MP&P] Laboratories, in Huntington Beach, California, USA; and the technical report issued by Boeing highlighted that in one of the points of origin of the failure, the analysis had identified characteristics similar to a pre-crack point, which would have begun earlier, probably due to overload. In the tasks that led to the restoration of the aircraft airworthiness after the accident in Uruguay in 2009 (Hard-Landing), and also in subsequent periodic inspections, the existence of pre-crack traces resulting from a previous overload condition may not have been identified, something that could have resulted in a point of stress concentration.
Final Report:

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

Date & Time: Apr 20, 2012 at 1430 LT
Type of aircraft:
Registration:
PP-WCA
Flight Type:
Survivors:
No
Schedule:
Jundiaí - Jundiaí
MSN:
LJ-1676
YOM:
2002
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The pilot, sole aboard, was completing a local flight from Jundiaí-Comandante Rolim Adolfo Amaro Airport. Shortly after takeoff from runway 36, the pilot reported to ATC that the engine lost power and that he was not able to maintain a safe altitude. He was cleared for an immediate return and completed a circuit. On final approach to runway 18, he lost control of the airplane that crashed 180 metres short of runway and came to rest upside down, bursting into flames. The aircraft was totally destroyed and the pilot was killed.
Probable cause:
The following factors were identified:
- Upon intercepting the final leg for landing, the aircraft crossed the approach axis, and the pilot, in an attempt to make the aircraft join the approach axis again, may have depressed the rudder pedal in an inadequate manner, inadvertently making the aircraft enter a Cross Control Stall.
- The pilot, intentionally, violated a number of aeronautical regulations in force in order to fly an aircraft for which he had no training and was not qualified.
- The short experience of the pilot in the aircraft model hindered the correct identification of the situation and the adoption of the necessary corrective measures.
- The DCERTA’s vulnerability allowed a non-qualified pilot to file a flight notification by making use of the code of a qualified pilot. Thus, the last barrier capable of preventing the accident flight to be initiated was easily thrown down, by making it difficult to implement a more effective supervisory action.
Final Report: