Crash of a Learjet 35A in Campo de Marte: 8 killed

Date & Time: Nov 4, 2007 at 1410 LT
Type of aircraft:
Operator:
Registration:
PT-OVC
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Campo de Marte - Rio de Janeiro
MSN:
35A-399
YOM:
1981
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
8
Captain / Total flying hours:
10049
Captain / Total hours on type:
3749.00
Copilot / Total flying hours:
643
Copilot / Total hours on type:
125
Aircraft flight hours:
10583
Circumstances:
The aircraft was returning to its base in Rio de Janeiro-Santos Dumont following an ambulance flight to Campo de Marte AFB. Shortly after takeoff from runway 30, while climbing to an altitude of 1,400 feet, the aircraft rolled to the right to an angle of 90° then entered an uncontrolled descent and crashed onto several houses located on Bernardino de Sena Street, bursting into flames. Both pilots as well as six people on the ground were killed. Six others people were seriously injured.
Probable cause:
A possible loss of control during initial climb consecutive to a fuel imbalance. The following contributing factors were identified:
- Crew fatigue,
- Non-compliance with published procedures,
- Poor distribution of tasks prior to the flight and during the initial climb,
- Overconfidence on part of the crew,
- Poor flight preparation,
- Loss of situational awareness,
- Incorrect application of controls,
- The crew failed to follow the pre-takeoff checklist.
Final Report:

Crash of a Beechcraft 60 Duke in Silvânia: 2 killed

Date & Time: Sep 17, 2007 at 1340 LT
Type of aircraft:
Operator:
Registration:
PT-OOH
Flight Phase:
Survivors:
No
Schedule:
Montes Claros – Goiânia
MSN:
P-27
YOM:
1969
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
1000
Captain / Total hours on type:
85.00
Circumstances:
The twin engine aircraft departed Montes Claros Airport at 1200LT on a flight to Goiânia, carrying one passenger and one pilot. As he started the descent to Goiânia Airport, the pilot reported the failure of the left engine and requested the permission to proceed with a direct approach to runway 32 despite the runway 14 was in use. Few seconds later, the right engine failed as well. The pilote reduced his altitude and attempted an emergency landing when the aircraft crashed in an open field located near Silvânia, about 50 km east of Goiânia Airport. On impact, the fixing points of the seat belts broke away, causing both occupants to impact the instrument panel. The aircraft was severely damaged and both occupants were killed.
Probable cause:
Failure of both engines in flight due to fuel exhaustion. The following contributing factors were identified:
- Poor judgment on the part of the pilot who considered that the quantity of fuel present in the tanks before departure was sufficient, which was not the case,
- Poor flight planning on part of the pilot who miscalculated the fuel consumption,
- The pilot failed to follow the procedures related to fuel policy.
Final Report:

Crash of an Embraer EMB-110P1 Bandeirante in Curitiba: 2 killed

Date & Time: Aug 22, 2007 at 0035 LT
Operator:
Registration:
PT-SDB
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Curitiba – Jundiaí
MSN:
110-323
YOM:
1980
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
18400
Captain / Total hours on type:
8200.00
Copilot / Total flying hours:
5600
Copilot / Total hours on type:
1600
Circumstances:
After passengers were dropped at Curitiba-Afonso Pena Airport, the crew was returning to his base in Jundiaí. Shortly after takeoff from runway 11 by night and marginal weather conditions, the airplane entered clouds at an altitude of 300 feet and continued to climb. Following a left turn, the aircraft climbed to an altitude of 700 feet then entered a right turn and an uncontrolled descent until it crashed in a field located near the Guatupê Police Academy located 3 km northeast of the airport. The accident occurred two minutes after takeoff. The aircraft was totally destroyed and both pilots were killed. At the time of the accident, the visibility was poor due to the night and a cloud base at 300 feet.
Probable cause:
Loss of control during initial climb in IMC conditions after the crew suffered a spatial disorientation. The following factors were identified:
- Weather conditions were not suitable for the completion of the flight,
- The crew failed to prepare the flight according to published procedures,
- The crew failed to follow the pre-takeoff checklist,
- The copilot did not have adequate training for this type of operation,
- The captain had emotional conditions that compromised flight operations,
- The relationship between both pilots was incompatible,
- The main attitude indicator was out of service since a week and the crew referred to the emergency attitude indicator,
- Because of poor flight preparation and non observation of the pre-takeoff checklist, the captain forgot to switch on the emergency attitude indicator prior to takeoff,
- At the time of the accident, the captain had accumulated 15 hours and 22 minutes of work without rest, which is against the law,
- The captain showed overconfidence and inflexibility which weakened his performances,
- Both pilots disagreed on operations,
- The visibility was poor due to the night and the ceiling at 300 feet above ground,
- The state of complacency of the organization was characterized by a culture adaptable to internal processes, without the adoption of formal rules for the operations division and the acceptance of operating conditions incompatible with security rules and protocols, which allowed the newly hired crew to feel free to act in disagreement with the standards and regulations in force at the time of the accident,
- Performing a sharp turn to the right in IMC conditions associated with a long working day and a lack of rest,
- The level of stress of the captain due to intense fatigue generated by a high workload and an insufficient rest period,
- Poor crew discipline,
- Poor judgment of the situation,
- Poor flight planning,
- Failures in the operator's organizational processes and lack of supervision of flight operations.
Final Report:

Crash of an Airbus A320-233 in São Paulo: 199 killed

Date & Time: Jul 17, 2007 at 1854 LT
Type of aircraft:
Operator:
Registration:
PR-MBK
Survivors:
No
Site:
Schedule:
Porto Alegre – São Paulo
MSN:
789
YOM:
1998
Flight number:
JJ3054
Country:
Crew on board:
6
Crew fatalities:
Pax on board:
181
Pax fatalities:
Other fatalities:
Total fatalities:
199
Captain / Total flying hours:
13654
Captain / Total hours on type:
2236.00
Copilot / Total flying hours:
14760
Copilot / Total hours on type:
237
Aircraft flight hours:
20000
Aircraft flight cycles:
9300
Circumstances:
On 17 July 2007, at 17:19 local time (20:19 UTC), the Airbus aircraft, model A320, registration PR-MBK, operating as flight JJ3054, departed from Porto Alegre (SBPA) destined to Congonhas Airport (SBSP) in São Paulo city, São Paulo State. There were a total of 187 souls on board the aircraft, being six active crew members and 181 passengers, including 2 infants and 5 extra crew members (not on duty). The weather prevailing along the route and at the destination was adverse, and the crew had to make a few deviations. Up to the moment of the landing, the flight occurred within the expected routine. The aircraft was operating with the number 2 engine reverser de-activated, in accordance with the Minimum Equipment List (MEL). According to information provided to the TWR by crews that had landed earlier, the active runway at Congonhas (35L) was wet and slippery. During the landing, at 18:54 local time (21:54 UTC), the crew noticed that the ground spoilers had not deflected, and the aircraft, which was not slowing down as expected, veered to the left, overran the left edge of the runway near the departure end, crossed over the Washington Luís Avenue, and collided with a building in which the cargo express service of the very operator (TAM Express) functioned, and with a fuel service station. All the persons on board perished. The accident also caused 12 fatalities on the ground among the people that were in the TAM Express building. The aircraft was completely destroyed as a result of the impact and of the raging fire, which lasted for several hours. The accident caused severe damage to the convenience shop area of the service station and to some vehicles that were parked there. The TAM Express building sustained structural damages that determined its demolition. The aircraft was completely destroyed.
Probable cause:
Human factors
1.1 Medical aspect
a. Pain - Undetermined
At a certain moment, during the approach, the PIC reported having a mild headache. Although it was not possible to verify which type of headache it was, or even to evaluate its intensity, it is possible that this trouble may have influenced his cognitive and psychomotor capabilities during the final moments of the flight, when the unpredictability of the situation demanded a higher effectiveness of performance. This factor was considered undetermined due to the impossibility of confirming its contribution in factual terms.

1.2 Operational aspect
a. Training - A contributor
The theoretical qualification of their pilots was founded on the exclusive use of computer interactive courses (CBT), which allowed a massive training, but did not ensure the quality of the training received. In addition, the formation of the SIC was restricted to the “Right Seat Certification”, something that proved insufficient for him to deal with the critical situation experienced after the landing. Lastly, there was a perception among the crews interviewed that the training through the years and on account of the high demand resulting from the company’s growth was being abbreviated.

b. Application of the commands - Undetermined
One of the hypotheses considered in this investigation was that the pilot may have attempted to perform a procedure no longer in force at the time of the accident for the landing with a pinned reverser. This procedure consisted in the receding of both levers to the “IDLE” position during the flare at about a 10-foot altitude, and, after touching down, in activating the only reverser available, maintaining the thrust lever of the other engine in the “IDLE” position.
This procedure, though being more efficient from a braking perspective, could induce the crew to making mistakes, as there were several reports of occurrences in which there was a wrong setting of the levers, motivating the manufacturer to establish a new procedure, months before the accident. Thus, there is a high probability that the PIC inadvertently left one of the thrust levers in the “CL” position, placing the other one first in “IDLE” and later in the “REV” position. This factor was considered undetermined due to the impossibility of confirming its contribution in factual terms.

c. Cockpit coordination - A contributor
Independently of the hypothesis considered, the monitoring of the flight at the landing was not appropriate, since the crew did not have perception of what was happening in the moments that preceded the impact. This loss of situational awareness hindered the adoption of an efficient and timely corrective action.

d. Forgetfulness by the pilot - Undetermined
It is possible that the pilot has inadvertently left one of the levers at the “CL” position, while trying to perform a procedure no longer in force for the operation with a pinned reverser. This factor was considered undetermined due to the impossibility of confirming its contribution in factual terms.

e. Flight indiscipline - Undetermined
The procedure prescribed for the operation with a pinned reverser had been modified by the manufacturer and, according to the FDR recordings, the procedure in force was known to the crew and executed by them on the leg that preceded the accident. However, as this procedure imposed an increase of up to 55 meters in the calculations of runway distance required for landing, it is possible that the PIC deliberately tried to perform adoption of a procedure no longer in force would characterize flight indiscipline. This factor was considered undetermined due to the impossibility of confirming its contribution in factual terms.

f. Influence from the environment - Undetermined
The operating conditions of the Congonhas runway, may have affected the crew’s performance from a psychological perspective, considering the state of anxiety that was present in the cockpit.
In addition, the lack of luminosity resulting from the operation at night time, associated with the size and color of the thrust levers may have hindered the verification of a contingent inappropriate positioning of those controls during the landing. This factor was considered undetermined due to the impossibility of confirming, in factual terms, the psychological influence of the runway operating conditions and/or lack of luminosity on the performance of the crew.

g. Judgment of pilotage - Undetermined
In view of all the operation scenario - the 55 meters added on account of the reverser procedure, the 2.4 extra tons of fuel on account of the tankering, the crowded aircraft, the pressure to proceed to Congonhas, the PIC’s physiological condition (headache), a SIC with little experience in the A-320 and in its autothrust system, the wet and slippery runway, the occurrences of the preceding days - there is a high probability that the PIC deliberately tried to perform the procedure no longer in force for the operation with a pinned reverser, in order to increase the braking efficiency, inadvertently leaving the number 2 engine thrust lever in the “CL” position. Considering this hypothesis, the diversion to an alternate airport would be desirable, instead of trying to perform a procedure that was not prescribed. This factor was considered undetermined due to the impossibility of confirming its contribution in factual terms.

h. Management planning - A contributor
At the time of the accident, the operator had a disproportional number of captains in comparison with the number of co-pilots, a fact that obliged the scheduling sector to form crews with 2 captains. Thus, although complying with the minimum requirements of the regulation in force, such a practice may have contributed to the creation of a climate of complacency in the cockpit of the JJ3054. Besides, the long experience of the SIC as a captain was not a guarantee of his competence in the co-pilot function - for which he had done only the “Right Seat Certification” training - and, added to his little experience in that aircraft, it contributed to the loss of situational awareness in the most critical moments of the flight.

i. Flight planning - Undetermined
Thus, considering the hypothesis that the PIC deliberately tried to perform the old procedure for a landing with a pinned reverser to increase the braking efficiency, it is possible that the use of that procedure was not appropriately prepared, something that could have favored the wrong positioning of the levers (according to the hypothesis mentioned above, it is possible that the PIC inadvertently left the nº2 engine thrust lever in the “CL” position.). The lack of a briefing for the descent in the CVR recording hindered the confirmation of a possible intention of applying the old procedure, no longer in force at the time. This factor was considered undetermined due to the impossibility of confirming its contribution in factual terms.

j. Little experience of the pilot - A contributor
Despite his long experience in commercial jets, the SIC possessed only about 200 flight hours in aircraft of the A320 type. Besides, his experience in the function of co-pilot was restricted to the “Right Seat Certification” training, which proved insufficient to deal with the emergency situation.

k. Management oversight - A contributor
The operator allowed the crew to be composed of two captains, with the occupant of the right-hand seat having done only the “Right Seat Certification” training. Besides, the lack of coordination between the several sectors of the company, especially between the sectors of operation and training, determined the lack of an appropriate monitoring of the processes and of the quality of the pilots’ professional formation.

Psychological aspect
a. Anxiety - Undetermined
The CVR recording allows to perceive that the PIC was showing anxiety in relation to the runway conditions for landing, and on two different occasions he asked the SIC to request from the TWR-SP the rain and runway conditions, and on one of them specifically, whether the runway was slippery. It is possible that the state of anxiety present in the PIC may have influenced the performance of the crew to some extent. This factor was considered undetermined due to the impossibility to confirm that this anxiety has effectively influenced the performance of the crew.

b. Perception error - A contributor
Although perceiving that the ground spoilers had not deflected, the pilots were not able to associate the non-deflection with the positioning of the thrust levers. In addition, there is a high probability that the pilots were led to believe that the lack of the expected deceleration after landing was a result of the conditions of operation with a wet runway, the influence of which, from a psychological aspect perspective in the field of individual variables, was perceived along the investigation.

c. Stress - Undetermined
The stress has effect on the cognitive level (diminution of the concentration, diminution of the response speed, degradation of the memory, etc.), emotional level (alteration of the characteristics of personality, weakening of the emotional control, lowering of the self-esteem, etc.), behavioral level (alterations of the sleep pattern, diminution of interests, verbal articulation problems, etc.), and physiological level (sudoresis, tachycardia, sleep pattern alterations, gastric and dermatologic symptoms, etc.). The presence of stress triggering stimuli was perceived, such as the state of anxiety on the part of the pilots, especially regarding the runway conditions, the cephalalgia of the PIC, the issues concerning the operation in Congonhas with a wet runway, the crowded aircraft and the inoperative reverser. However, it was not possible to determine whether those stimuli effectively led any of the two pilots to a high level of stress. This factor was considered undetermined due to the impossibility to confirm its contribution in factual terms.

d. Lack of perception - A contributor
Considering the hypothesis of a failure in the thrust control system, the contingent stimulus generated from the loss of resistance to the movement of the thrust levers may not have been perceived by the pilot(s), according to the CVR recordings. On the other hand, if one considers the hypothesis that the nº 2 engine thrust lever was inadvertently left in the “CL” position, while the pilots were trying to perform a procedure no longer in force, the characteristics of the autothrust system, which keep the levers motionless during the variations of thrust, in addition to the size and color of those control levers, hard to be observed on a night flight, were not sufficiently evident to be perceived by the pilots. This situation was aggravated by the lack of a warning device relative to the conflicting positioning of the thrust levers.

e. Loss of situational awareness - A contributor
Thus, no matter which hypothesis is considered, the loss of the situational awareness emerged as a result of the very lack of perception on the part of the pilots. In this sense, the automation of the aircraft, however complex, was not capable of providing the pilots with sufficiently clear and accurate stimuli, to the point of favoring their understanding of what was happening in the moments just after the landing in Congonhas.

f. Organizational climate - Undetermined
In relation to the crews of the company, the investigation identified the perception that there was a pressure on the part of the management against diversions, on account of the inconvenience they could arise for the passengers and for the company itself. If the pilots of the JJ3054 shared that perception, it is possible that this factor could have some influence on the pilot’s decision to proceed for the landing in Congonhas, in spite of his concern with the runway operating conditions. This factor was considered undetermined due to the impossibility to confirm its contribution in factual terms.

g. Regulation - A contributor
The regulatory organization, although having already considered the availability of the reversers as a requirement for the operation in Congonhas, at least since April 2006, such a requirement was only formalized as a norm in May 2008. The opportune regulation of this requisite would have prevented the aircraft from operating in Congonhas with a wet runway condition.

h. Training - Undetermined
In relation to the training, the investigation identified in the crews a perception that the company seemed to have reduced the contact hours applied to it, although in formal terms those contact hours had remained unaltered. In relation to crew professional formation, the investigation identified a tendency on the part of the company to reduce the number of hours assigned to training, which remained unaltered in formal terms. Moreover, the FDR recordings showed that, during the period in which the aircraft operated with the pinned reverser, 5 different types of landing procedures were performed by the various crews who operated it. This factor was considered undetermined due to the impossibility to confirm, in factual terms, that the crews’ perception of a shortening in the training processes being applied was consistent with reality and/or whether such alleged shortening effectively influenced the performance of the crew, contributing to the accident.

2 Material factors
a. Design - A contributor
It was verified that, for an A320 airplane proceeding to land, it is possible to place one of the thrust levers at the “REV” position and the other at “CL”, and no alerting device will advise the pilots in an efficient way. This situation may put the aircraft in a critical condition and, depending on the time it takes the crew to identify this configuration, and on the runway parameters, a catastrophic situation may occur. In the specific case of this accident, even with the aircraft on the ground (Weight on Wheels - WOW), with the number 1 engine thrust lever at the “REV” position, with the ground spoilers armed, with the autobrake selected, and with application of maximum braking pressure on the pedals, the power control system gave priority to the information that one of the levers was at “CL”, and this lever did not have any safety devices regarding a possible inadvertent setting.
Final Report:

Crash of an ATR42-300 in São Paulo

Date & Time: Jul 16, 2007 at 1242 LT
Type of aircraft:
Operator:
Registration:
PT-MFK
Survivors:
Yes
Schedule:
Araçatuba – Bauru – São Paulo
MSN:
225
YOM:
1991
Flight number:
PTN4763
Country:
Crew on board:
4
Crew fatalities:
Pax on board:
21
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7420
Captain / Total hours on type:
4993.00
Copilot / Total flying hours:
947
Copilot / Total hours on type:
797
Circumstances:
The aircraft departed Araçatuba on a flight to São Paulo with an intermediate stop in Bauru, carrying 21 passengers and a crew of four. After touchdown on wet runway 17R at Congonhas Airport, the crew started the braking procedure when the aircraft deviated to the left and veered off runway. While contacting soft ground, the aircraft collided with a concrete block housing the electrical device supplying the runway light system. On impact, the nose gear was torn off and the aircraft came to rest. All 25 occupants evacuated safely while the aircraft was damaged beyond repair.
Probable cause:
Loss of control upon landing after the aircraft suffered aquaplaning. The following contributing factors were identified:
- A light rain caused the presence of water on the runway, enabling the occurrence of hydroplaning.
- The accumulation of water on the surface of the runway, as a result of inadequate drainage, lack of "grooving", enabled the hydroplaning.
- The pilot applied full pressure on the right pedal, generating a force to the left that contributed to the departure off the runway.
- During hydroplaning, the pilot should not apply pedal to the opposite side to which the aircraft slides; this fact was not covered during the instruction of the pilot.
- In the face of hydroplaning, the pilot applied the right pedal, aggravating the departure of the aircraft to the left.
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 Boeing 737-8EH near Peixoto de Azevedo: 154 killed

Date & Time: Sep 29, 2006 at 1657 LT
Type of aircraft:
Operator:
Registration:
PR-GTD
Flight Phase:
Survivors:
No
Schedule:
Manaus – Brasília – Rio de Janeiro
MSN:
34653
YOM:
2006
Flight number:
GLO1907
Country:
Crew on board:
6
Crew fatalities:
Pax on board:
148
Pax fatalities:
Other fatalities:
Total fatalities:
154
Captain / Total flying hours:
15498
Captain / Total hours on type:
13521.00
Copilot / Total flying hours:
3981
Copilot / Total hours on type:
3081
Aircraft flight hours:
202
Aircraft flight cycles:
162
Circumstances:
The B737-8EH airplane was operating as flight GLO1907, regular passenger transport, under the rules of RBHA 121. It had departed Eduardo Gomes International Airport (SBEG) in Manaus – Amazonas State, at 18:35 UTC, destined to Rio de Janeiro – Rio de Janeiro State (SBGL), carrying 6 crewmembers and 148 passengers. The aircraft was scheduled to make a technical stop at Brasilia International Airport (SBBR), in the Brazilian capital city. The EMB-135BJ Legacy airplane, with 2 crewmembers and 5 passengers onboard, departed from São José dos Campos (SBSJ), São Paulo State, at 17:51 UTC, destined to Manaus (SBEG), from where it would later proceed to Fort Lauderdale (KFLL), Florida, USA. The B737-8EH airplane made its last radio contact with the Amazonic Area Control Center (ACC AZ) at 19:53 UTC, and was instructed to call the Brasilia Area Control Center (ACC BS) at NABOL position, but the contact was not made. At 20:14 UTC, the ACC AZ received a message from Polar Air Cargo 71, in relay for the Legacy airplane, stating that the N600XL was declaring emergency, having difficulties with its flight control system, and that it would proceed for an emergency landing at SBCC (military aerodrome of the Command of Aeronautics (COMAER), known as Campo de Provas Brigadeiro Veloso, in Novo Progresso county, Pará State). After landing, the N600XL crew reported that their airplane had collided in flight with an unknown object. The airplane sustained damages at the left wingtip and left elevator. The wreckage of the B737-8EH was found the next day, 30 September, in a region of thick forest, in the county of Peixoto de Azevedo, Mato Grosso State. All the 154 occupants of the PR-GTD had perished in the accident.
Probable cause:
The following factors were identified:
Human Factor
PR-GTD - Neither active failures were identified in relation to the crew, nor latent failures in relation to the organizational system of the company.
N600XL - Relatively to the crew of the N600XL, the following active failures were identified: lack of an adequate planning of the flight, and insufficient knowledge of the flight plan prepared by the Embraer operator; non-execution of a briefing prior to departure; unintentional change of the transponder setting, failure in prioritizing attention; failure in perceiving that the transponder was not transmitting; delay in recognizing the problem of communication with the air traffic control unit; and non-compliance with the procedures prescribed for communications failure. The low situational awareness of the pilots (airmanship) was a relevant factor for the occurrence of the accident. It began during the phase of preparation for the operation, which was considered by them as 'routine'. The attitude of the pilots about the mission permeated their behavior during the other phases, with the addition of several factors that contributed to aggravate the lowering of the situational awareness:
• The non-elaboration of an adequate planning of the flight, a behavior that was influenced by the habitual procedure of the company, an aspect not favorable for the construction of a mental model to guide the conduction of the flight;
• The haste to depart and the pressure from the passengers, hindering adequate knowledge of the flight plan, and negatively influencing the sequence of actions during the pre-flight and departure phases;
• The crew dynamics, characterized by lack of division of tasks, lack of an adequate monitoring of the flight, and by informality. It was influenced by the lack of knowledge of the weight and balance calculations, and by the predominant little experience of the pilots in that aircraft model; and
• The lack of specific Standard Operational Procedures (SOP’s) set by the company for that aircraft model to be complied with by the pilots.
Within this context, the inadvertent switch-off of the transponder occurred, possibly on account of the pilots’ little experience in the aircraft and its avionics. The transponder switch off was not perceived by the crew, due to the reduction of the situational awareness relative to the alert of the TCAS condition, which did not draw the attention of the pilots. The lack of situational awareness also contributed to the crew’s not realizing that they had a communication problem with the ATC. Although they were maintaining the last flight level authorized by the ACC BS, they spent almost an hour flying at a non-standard flight level for the heading being flown, and did not ask for any confirmation from the ATC. The performance deficiencies shown by the crew have a direct relationship with the organizational decisions and processes adopted by the operator: the inadequate designation of the pilots for the operation; the insufficient training for the conduction of the mission, and the routine procedures relative to the planning of the flight, in which there was not full participation of the crew. Considering the diversity and complexity of the non-conformities observed in the air traffic control domain, they will be presented in topics. It is important to point out that the refusal of the Brasilia ACC controllers involved in the accident to participate in the interviews hindered the precise identification of the individual aspects that contributed to the occurrence of the non-conformities. Some of these aspects were kept in the field of hypotheses.

a) Transmission of an incomplete flight clearance by the assistant controller of the São Paulo Region of Brasilia ACC, and by the Ground controller of DTCEA-SJ. There was a deviation from the procedure, together with an informal procedure pattern concerning the transmission of clearances, originated at Brasilia ACC, and disseminated at DTCEA-SJ, as an outcome of daily practice, in replacement of the model prescribed by the legislation. The reception and transmission of incomplete clearances were erroneously adopted as normal, routine practices, rationally justifiable, within the DTCEA-SJ. The incomplete clearance transmitted to the N600XL crew favored the understanding by the pilots that they had to maintain FL 370 all the way to Manaus.

b) The ATCO of sectors 5 and 6 of Brasilia ACC did not provide the ATCO 1 of sectors 7, 8 and 9 with the necessary information, when coordinating and handing off the N600XL aircraft.
The incomplete information transmitted by the ATCO of sectors 5 and 6 is an indication that he had a low situational awareness concerning the N600XL in his sector. He, possibly, considered that his priority in relation to the mentioned aircraft would be an early transfer to the next sector, as his own sector was showing an increasing volume of traffic at that moment (09 aircraft), although it was below the limits prescribed for grouped sectors.

c) The ATCO 1 of sectors 7, 8 and 9 of ACC BS did not make a radio contact with N600XL to change the aircraft flight level and to switch the frequency from sector 9 to sector 7; did not perceive the N600XL loss of mode C; he assumed that the N600XL was at flight level FL360; did not perform the procedures prescribed for the loss of transponder in RVSM airspace, and for the control position relief, by both omitting information and transmitting incorrect information. The non-transmission of important information to the ATCO 1 of sectors 7, 8 and 9, concerning the N600XL in sector 5, contributed to the diminishing of the situational awareness of that controller in relation to the aircraft and the need to change its level and frequency. The failure of the ATCO 1 of sectors 7, 8 and 9 to act in relation to the change of frequency allowed the aircraft to get out of the coverage of the frequency 125.05 MHz, making it impossible to receive the transmissions. By not contacting the aircraft to change its level at the vertical of Brasilia, the ATCO 1 of sectors 7, 8 and 9 let the N600XL join the UZ6 airway at an incorrect level in relation to the active flight plan. Although the system presented the prescribed indications for the loss of the N600XL transponder, they did not draw the attention of the controller to the need of changing the flight level. The lack of action after the loss of the N600XL Transponder mode C allowed the aircraft to maintain a flight level that was incorrect in relation to the active flight plan. When he passed the information to the ATCO 2 of sectors 7, 8 and 9 that the aircraft was at flight level FL360, the ATCO inserted a false assumption, which became very difficult to be detected, on account of the lack of the Transponder altitude information and the impossibility of communication due to the failure to timely instruct the aircraft to change the frequency. Misjudging that the aircraft was at the flight level planned for the segment (FL360), the ATCO 1 possibly disregarded the risks resulting from the inaccurate 3D radar altitude information. The controller, also, failed to resort to the support of the regional supervisor. His attitude of evaluating the resulting risks in an incorrect manner may have influenced on the lack of information/ transmission of incorrect information, when he was relieved by the ATCO 2 of sectors 7, 8 and 9.

d) The ATCO 2 of sectors 7, 8 and 9 of ACC BS did not perform the procedures prescribed for the loss of transponder and loss of radar contact within RVSM airspace, and for communications failure, and failed to communicate with the assistant controller. By failing to perform the prescribed procedures for the loss of Transponder and radar contact, as well as for communications failure, the ATCO 2 of sectors 7, 8 and 9 allowed the N600XL to maintain the incorrect flight level (FL370) on the UZ6 airway. The lack of communication with the Assistant-Controller allowed a deficient hand-off of the N600XL to the ACC AZ, with incomplete information, by not mentioning the difficulties of the ACC BS in relation to the radar contact and communications. The attitudes and incorrect evaluation of the resulting risks by the controller may have been generated by the wrong assumption that the N600XL was at FL 360. Such attitudes may have influenced his behavior of not resorting to the support of the regional supervisor, and of not advising his assistant-controller to inform the ACC AZ about the conditions of the aircraft.

e) Lack of communication between controllers and supervisors: lack of information and/or transmission of incorrect information by the ATCO of sectors 5 and 6, the ATCO’s 1 and 2, and Assistant-ATCO of sectors 7, 8 and 9, during the execution of the procedures for coordination and handoff of the N600XL between sectors and between Control Centers, and at the control position relief; lack of communication between controllers and supervisors. Deviations from the procedures regarding the prescribed phraseology were observed, in various situations of the air traffic control activity and in the various control units involved in the accident. Such deviations contributed to the lowering of the situational awareness of the controllers responsible for controlling the N600XL flight. The supervisors were not advised by the controllers about the problems experienced in the control of the N600XL, an aspect that generated the making of inadequate decisions, which occurred isolatedly and individually, reflecting a deficient coordination of the team resources.

f) Supervisors of the Brasilia ACC: lack of involvement in the events concerning the control of the N600XL. The lack of involvement of the supervisors allowed the decisions to be made and the actions to be taken in relation to the N600XL in an individual manner, without due monitoring, advisory and guidance prescribed for the air traffic control. Among the duties of the regional supervisors, listed in the Operational Model of the ACC BS, there is the following: “to supervise the provision by the controllers under his/her responsibility of the air traffic services in their respective sectors, and to correct errors, omissions, irregularities or inadequate employment of ATS procedures”. Thus, when the supervisors did not participate in the events, an opportunity was lost, with the participation of more people in the process, to detect the need of efficient actions for the reestablishment of the radar contact and radio contact with the N600XL, in addition to other procedures prescribed. It was not possible to define the aspects that contributed to the non-involvement of the supervisors in the events, as there was a refusal to participate in interviews.

g) The ATCO of the Manaus Sub Center of the ACC AZ showed deviation from the standard procedure during the hand-off of the PR-GTD and the take-over of the N600XL; erroneously confirmed the existence of the N600XL traffic; and did not perform the procedure prescribed for the loss of radar contact. The ATCO did not perceive the control condition of the N600XL as critical, and did not demonstrate discomfort with the situation, thus displaying a low situational awareness. This may have been influenced by the information received from the ACC BS that the aircraft was at flight level FL360, and by not being informed that the aircraft had been without radar contact and radio contact for some time. Again, this allowed the two airplanes to fly in opposite directions, along the same airway and at the same flight level. The personnel shortage at CINDACTA IV hindered the maintenance of a continued training of the controllers, by means of refreshers, TRM trainings and English courses. It was observed that the annual theoretical evaluation (TGE) was not being able to aid in the identification and diagnostic of the controllers’ performance deficiencies, thus failing to assist in the process of determination of the training needs. There were difficulties in re-creating the operational profile of the ATCO’s involved, due to the shortage of records relative to the instruction and technical qualification. Lastly, it is important to point out that the personnel shortage hindered the structuring of the operational work-shifts, as well as the instructional activities, as mentioned earlier. The effects of the personnel shortage were reflected in the quality of the services as they contributed to the degradation of the controllers’ performance and/or to the insufficient technical qualification.

1.2. Physiological Aspect - not a contributor
No factors of physiological origin were evidenced that may have contributed directly or indirectly to the occurrence of the accident.

1.3. Operational Aspect.
a) Training - a contributor
(Participation of the received training process, due to a qualitative or quantitative deficiency, for not providing the trainee with full knowledge and other technical skills required for the
performance of the activity). The FSI refused to receive the visit of the CIAA at the unit of Houston-Texas and brought considerable difficulties for the investigation of the instruction given to the pilots in the simulator. The training provided to the N600XL pilots proved insufficient for the conduction of the repositioning flight from Brazil to the USA. The lack of interaction between the pilots was apparent in the difficulties with the division of tasks and in the coordination of the cockpit duties, with both of them devoting their attention to the calculations of the aircraft weight and balance during the flight. The lack of theoretical knowledge became evident when they showed difficulty operating the aircraft systems, mainly the fuel system, according to the CVR.
These gaps in the received training favored a deviation of the pilots’ attention to other aspects during the flight, in detriment of the aircraft operation. Such distraction allowed the discontinuance of the transponder transmission to go unperceived, resulting in the incorrect maintenance of the FL370 on the UZ6 airway and lack of TCAS collision alert. Upon completion of the training at the FSI, both pilots would be entitled to fly domestic and international flights, under the aegis of the 14 CFR Part 91, without previous interaction as a crew. Since the prescriptions of the regulation mentioned were complied with, it was observed that they were not adequate to meet the minimum required levels for a safe operation of high performance jet aircraft in acceptance and repositioning flights.

b) Air traffic control - a contributor
(Participation of the air traffic service provider, on account of inadequate service provision)
The authorization to maintain flight level FL370 was given to the crew of the N600XL, as the result of a clearance transmitted in an incorrect manner. The vertical navigation conducted by the crew ended up being different from the one prescribed in the flight plan that was filed and activated, on account of the instruction incorrectly transmitted that led the N600XL crew to maintain flight level FL370. The air traffic control units involved, although providing radar surveillance (radar monitoring) service, did not correct the flight level and did not perform the prescribed procedures for altitude verification when they stopped receiving essential information from the Transponder due to the loss of mode C. The controllers assumed that the traffic was at a different flight level, without even being in two-way radio contact with the N600XL for confirmation. They did not make a correct handoff of the traffic between sectors and between FIRs. They maintained RVSM separation when the necessary requirements no longer existed. As a final consequence, they did not provide the proper traffic separation as prescribed in the ICAO Doc. 4444, item 5.2 “Provisions for the Separation of Controlled Traffic”, thus allowing the in-flight collision between the two airplanes. Neither material nor design failures were found in the pieces of equipment of the air traffic infrastructure that might have contributed to the accident. The various contributing non-conformities found by the investigation are presented in the item 1.1 of this report, as they are directly related to the Human Factor.

c) Cockpit coordination - a contributor
(Error resulting from an inadequate utilization of the human resources for the operation of the aircraft, on account of an ineffective distribution and management of the tasks affecting each crew member, failure or confusion in the interpersonal communication or relationship, inobservance of operational rules)
The attention of both pilots of the N600XL focused on solving the question relative to the performance of the aircraft for the operation in Manaus, as they had learned of a NOTAM limiting the length of the runway of that airport. This hindered the routine of monitoring the evolution of the flight, because both pilots got busy with the same subject, creating the environment in which the interruption of the Transponder transmission was not perceived. There was not a good division of the flight management tasks, culminating with a prolonged absence of the PIC from the cockpit, thus overburdening the SIC when he tried to establish contact with the control units. The utilization of the screens by both pilots to show the fuel system, consequently without visualization of the TCAS, contributed to the lack of perception of the inoperative TCAS.

d) Judgment - a contributor
(Error committed by the pilot, resulting of an inadequate assessment of certain aspects of the operation, despite his being qualified for that operation)
The pilots judged that they would be able to conduct the flight even with their little adjustment as a crew and with their little knowledge of the aircraft systems, mainly the fuel system and the calculations of the weight and balance. They believed they could hasten the departure, resulting that they had just a short time to verify the flight plan and other documents, such as the NOTAM informing about the reduction of the runway length available at Manaus airport. On account of that, they judged that they both could concentrate on the calculations of the weight and balance in flight, something that allowed the non-functioning of the Transponder and TCAS to occur unperceived. There was an incorrect evaluation of the situation relative to the attempts to contact the ATC, as more than 43 minutes had elapsed without communication with the ACC BS, and they were late to recognize the need to contact the control center. The PIC left the cockpit and stayed away 16 minutes, not considering the consequences of overburdening the SIC.

e) Planning - a contributor
(Pilot error, resulting of inadequate preparation for the flight, or part of the flight)
The planning of the flight was inadequate. Before the departure, there was not a monitoring of the elaboration of the flight plan that was being prepared by the Embraer employee, not allowing the pilots to have a previous knowledge of the proposed route and flight levels, although, in accordance with the Excelaire Manual of Operations, the PIC had to open and close the flight plan at the nearest FAA FSS or ATC office. There are numerous situations recorded in the CVR showing the lack of an adequate concern of the crew with details of the pre-flight planning. An example was that only in flight did they learn of NOTAM of SBEG containing information about the reduction of the runway length available. This fact, added to the little familiarization of the pilots with the fuel system and with the aircraft weight and balance calculations, favored the deviation of their attention, during the flight, from the aspects relative to the operation of the aircraft, allowing the non functioning of the Transponder and TCAS to go by unperceived.

f) Oversight - a contributor
(participation of third parties, not belonging to the crew, on account of lack of adequate supervision of the planning or execution of the operation, at administrative, technical or operational levels)
The oversight conducted by the operator for the flight proposed was inadequate. The composition of the crew, with two pilots that had never flown together before, to receive, in a foreign country, an airplane in which they had little experience, with air traffic rules different from those with which they were used to operate, favored the lack of a good adjustment between the pilots, along with the already mentioned difficulties of cockpit coordination. Besides, there was not a specific SOP for the receipt of aircraft from the manufacturer, resulting that their decisions were made according to the individual experience of the pilots, who had never received an aircraft in those conditions. The decisions made, as seen in the contributing factors “Judgment” and “Planning” influenced the sequence of events that led to the accident. The monitoring of the instruction provided to the pilots was inadequate, because the operator did not perceive that the acquired knowledge was not sufficient for the conduction of the intended flight. The performance of the N600XL crew had a direct relationship with the decisions and organizational processes adopted by the operator, on account of culture and attitudes of informality. All of this was considered as a chain of errors, without violations on the part of the operator.

g) Little flight experience in the airplane - Undetermined
(Pilot error, resulting from little experience in the aviation activity, in the aircraft, or, specifically, in the circumstances of the operation)
The CVR indicated that, shortly before the moment of silence and the moment at which the Transponder discontinued the transmission, the PIC was looking at the fuel page of the MFD, and solved a doubt about fuel management with the SIC. It is possible that the PIC may have continued to look at other pages of the MFD and, possibly, to pages of the RMU. The little experience of the PIC in this aircraft possibly made him look for information about the fuel consumed on the RMU fuel page, and, when leaving from this page and pushing the pertinent buttons, he unintentionally changed the setting of the Transponder from TA/RA to STANDBY, thus interrupting the altitude information of the mode C; The insufficient adaptation of the crew with this type of aircraft and with the DISPLAYS of the respective avionics may have contributed to the unintentional selection of the STANDBY mode and to the subsequent lack of perception of the Transponder/TCAS status.
Final Report:

Crash of a Rockwell Shrike Commander 500S in Natal

Date & Time: May 5, 2006 at 0710 LT
Operator:
Registration:
PT-IGL
Flight Type:
Survivors:
Yes
Schedule:
Recife - Natal
MSN:
500-3129
YOM:
1972
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3000
Captain / Total hours on type:
500.00
Circumstances:
The twin engine aircraft departed Recife-Guararapes Airport at 0609LT on a flight to Natal, carrying one passenger, one pilot and a load consisting of bags containing bank documents. On approach to Natal-Augusto Severo Airport runway 16L, the left engine failed. Shortly later, at a height of about 600 feet, the right engine failed as well. Aware that he will not be able to reach the airport, the pilot attempted an emergency landing in an open field. On touchdown, the undercarriage collapsed and the aircraft slid for about 200 metres before coming to rest in a muddy field. Both occupants escaped with minor injuries and the aircraft was damaged beyond repair.
Probable cause:
Double engine failure on approach caused by a fuel exhaustion. The following findings were identified:
- Poor flight preparation on part of the pilot,
- Miscalculation of fuel consumption for the flying distance (about an hour),
- The day prior to the accident, tanks were filled with a quantity of 130 liters of fuel, barely 13 liters more than the quantity theoretically necessary for the flight in the conditions existing at the time of the accident,
- No technical anomalies were found on the airplane and its equipment,
- Poor organizational culture within the operator regarding fuel policy,
- Qualitative deficiency in the instruction given to the pilot who had not acquired the basic knowledge for fuel management,
- Failure to observe the actual quantity of fuel in the tanks prior to departure,
- Shortcomings in the operator's organizational processes,
- Inadequate supervision of flight planning activities by the operator who failed to identify any flaws in the fuel management procedures by the pilots.
Final Report:

Crash of a Let L-410UVP-E20 near Rio Bonito: 19 killed

Date & Time: Mar 31, 2006 at 1739 LT
Type of aircraft:
Operator:
Registration:
PT-FSE
Flight Phase:
Survivors:
No
Site:
Schedule:
Macaé – Rio de Janeiro
MSN:
91 25 32
YOM:
1991
Flight number:
TIM6865
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
17
Pax fatalities:
Other fatalities:
Total fatalities:
19
Captain / Total flying hours:
10000
Captain / Total hours on type:
39.00
Copilot / Total flying hours:
5220
Copilot / Total hours on type:
1719
Aircraft flight hours:
2739
Aircraft flight cycles:
3960
Circumstances:
The twin engine aircraft departed Macaé Airport at 1719LT on a flight to Rio de Janeiro-Santos Dumont Airport with 17 passengers and two pilots on board. Few minutes later, the copilot cancelled the IFR flight plan and continued under VFR mode at an altitude of 4,500 feet. Approaching São Pedro da Aldeia, the copilot was cleared to descend to 2,000 feet to avoid poor weather conditions. Later, while approaching Saquarema, the crew initiated a left turn to avoid clouds when shortly later, at an altitude of 1,920 feet, the aircraft struck the Pedra Bonita Peak. The wreckage was found six km southeast of Rio Bonito in a dense wooded area. The aircraft was totally destroyed and all 19 occupants were killed.
Probable cause:
Controlled flight into terrain after the crew decided to continue under VFR mode in IMC conditions. The following contributing factors were identified:
- Overconfidence on part of the captain who was familiar with the area,
- The organizational culture of the company proved to be complacent by not inhibiting the adoption of procedures incompatible with flight safety, such as the low altitude flights made by the instructor captain,
- There was inadequate assessment of the situation by the crew, causing them to fly at a lower altitude than the safe limits under visual conditions unsuitable for visual flight, resulting in the collision of the aircraft with high ground,
- The use of human resources for the operation of the aircraft was unsuitable because of failure to comply with operational standards, leading the crew to perform a passenger flight to the lower altitude limits of safety, under inadequate visual conditions,
- The preparation for the flight proved inadequate because the crew did not have a meteorological analysis of the appropriate level of flight performed, considering that the conditions for the region were overshadowing the Serra do Mar and surrounding areas of low clouds and / or mist, especially on the slopes of the mountain,
- The weather conditions prevailing in the region made visual flight impossible, resulting in the concealment of the elevation at which the aircraft crashed,
- The pilots intentionally not complying with rules of air traffic and civil aviation rules, without grounds, performing flight at low altitude, under conditions of visibility below the limits established for VFR flight, colliding with high grounD,
- The company has not taken appropriate supervisory measures, enabling the existence of a culture of undeveloped flight safety, which prevented advance identification of actions taken by the crew and injured misconception exists in the CRM business, which represented a potential risk to their operations, as well as by the failure of some educational measures provided for in its PPAA (Plan for the Prevention of Aeronautical Accidents).
Final Report:

Crash of a Cessna 525 CJ1 in Alto da Boa Vista: 2 killed

Date & Time: Sep 16, 2005 at 1405 LT
Type of aircraft:
Operator:
Registration:
PT-WLX
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Rio de Janeiro - Jacarepaguá
MSN:
525-0176
YOM:
1997
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total hours on type:
917.00
Copilot / Total hours on type:
2231
Aircraft flight hours:
2231
Circumstances:
The twin engine airplane departed Rio de Janeiro-Santos Dumont at 1402LT on a positioning flight to Jacarepaguá Airport located 23 km southwest from Santos Dumont Airport. After takeoff, the copilot informed ATC he maintained the altitude of 1,500 feet via route Bravo until the coast. Shortly later, while cruising in clouds at an altitude of 1,380 feet, the aircraft struck the slope of Mt Morro da Taquara located in the Tijuca National Park. The wreckage was found near Alto da Boa Vista and both pilots were killed. At the time of the accident, weather conditions were considered as marginal with low ceiling above the mountainous area.
Probable cause:
The accident was the consequence of a controlled flight into terrain after the crew decided to conduct this short flight under VFR mode in IMC conditions. The following contributing factors were identified:
- The visibility was reduced by the presence of a low ceiling over the mountains,
- Poor judgment on part of the crew regarding the existing flight conditions,
- Inadequate assessment of the distance between the aircraft and the ground,
- Continuation of the flight at an unsafe altitude for the area,
- Complacency and indiscipline of the crew,
- Poor flight planning,
- Lack of operational supervision.
Final Report: