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 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 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 Learjet 55C Longhorn in Rio de Janeiro

Date & Time: Aug 12, 2010 at 0926 LT
Type of aircraft:
Operator:
Registration:
PT-LXO
Flight Type:
Survivors:
Yes
Schedule:
Rio de Janeiro - Rio de Janeiro
MSN:
55C-135
YOM:
1988
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
17000
Captain / Total hours on type:
500.00
Copilot / Total flying hours:
2800
Copilot / Total hours on type:
49
Circumstances:
The aircraft departed Rio de Janeiro-Santos Dumont Airport on a positioning flight to Rio de Janeiro-Galeão-Antonio Carlos Jobim Airport with three crew members on board. Two minutes after takeoff, while in initial climb, the electrical system of the aircraft suffered a voltage power loss. Several instruments lost their functionality such as TCAS, altimeters and airspeed indicator. In good weather conditions, the captain decided to return to Santos Dumont Airport but did not declare any emergency. After being cleared to descend to 3,000 feet, the crew lost all radio communications. On final approach to runway 02R, most of the instruments failed but the crew continued the approach. The aircraft passed over the runway threshold with an excessive speed of 25 knots and after touchdown, the crew started the braking procedure but the spoilers and the reversers could not be activated. Unable to stop within the remaining distance, the aircraft overran and came to rest in the Guanabara Bay. All three crew members escaped uninjured while the aircraft was damaged repair.
Probable cause:
An error in the assembly was detected in the left generator, which interfered with the D+ terminal signal sent to the voltage regulator. Due to a voltage drop, some of the instruments lost their functionality. The following contributing factors were identified:
- The crew did not follow the emergency procedures;
- The crew decided to return to land at Santos Dumont Airport without considering that the runway length was less than the length required for an emergency landing;
- The speed of the aircraft while passing over the runway threshold was 25 knots above the reference speed;
- The pilots were unable to engage the spoilers or the thrust reversers;
- Wrong attitude from the captain;
- Overconfidence of the crew;
- Emotional load due to an emergency situation;
- Poor assessment of the situation due to high stress associated with decreased situational awareness;
- Poor crew coordination;
- Lack of crew resource management;
- Poor judgment;
- Lack of procedures on the part of the operator.
Final Report:

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 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:

Crash of a Mitsubishi MU-300 Diamond 1A in Santos

Date & Time: Mar 23, 2003 at 1025 LT
Type of aircraft:
Registration:
PT-LNN
Survivors:
Yes
Schedule:
Rio de Janeiro – Santos
MSN:
0048
YOM:
1982
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
12500
Captain / Total hours on type:
35.00
Copilot / Total flying hours:
4500
Copilot / Total hours on type:
19
Circumstances:
The aircraft departed Rio de Janeiro-Santos Dumont Airport on a flight to Santos, carrying one passenger and two pilots. Following an approach via the local NDB, the crew started the descent to Santos Airport but was forced to initiate a go-around procedure because he was not properly aligned. A second attempt to land was started to runway 35 with a tailwind component. Following an unstabilized approach, the aircraft landed 450 metres past the runway threshold (runway 35 is 1,390 metres long). Unable to stop within the remaining distance, the aircraft overran and came to rest in the Bertioga Canal. All three occupants evacuated safely while the aircraft was damaged beyond repair.
Probable cause:
Wrong approach configuration on part of the crew who continued the descent while the aircraft was unstable and moreover with a tailwind component. The aircraft landed at an excessive speed about 450 metres past the runway threshold, reducing the landing distance available. The tailwind component and the crew inexperience was contributing factors.
Final Report:

Crash of a Piper PA-31T Cheyenne II in São Francisco do Sul: 3 killed

Date & Time: Oct 30, 1998 at 2036 LT
Type of aircraft:
Operator:
Registration:
PT-WHI
Survivors:
No
Schedule:
Rio de Janeiro – Joinville
MSN:
31-7920077
YOM:
1979
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
2420
Captain / Total hours on type:
603.00
Circumstances:
Following an uneventful flight from Rio de Janeiro-Santos Dumont Airport, the pilot started the descent to Joinville Airport by night and marginal weather conditions. He was informed about the visibility at destination being 2 km with ceiling at 650 feet. At 2032LT, he initiated the approach and reported to ATC that if it was raining, he would divert to Curitiba. Four minutes later, on final approach, the twin engine aircraft struck trees and crashed about 15 km southeast of runway 33 threshold. The aircraft was destroyed by impact forces and a post crash fire and all three occupants were killed.
Probable cause:
The following findings were identified:
- There was the participation of psychological variables at individual level, related to the profile of the pilot, such as excessive self-confidence in assuming that he always reached his destination, the knowledge of the region and probably the self-induced pressures by the situation in the cabin, combined with the prevailing meteorological condition, as well as the fact that he made a mistake with the procedure he was performing, demonstrating the adoption of an inadequate decision, excessive motivation for landing and lack of attention to the correct procedure.
- It was not possible to perform an effective analysis on the parts and instruments of the aircraft, in view of their degree of destruction, thus the contribution of this factor to the accident could not be determined.
- Weather conditions at destination were fickle and deteriorated during the execution of the descent procedure of the aircraft, contributing to the accident.
- The pilot failed to comply with the planned descent profile in use.
- Despite being aware of the meteorological conditions at destination, the pilot did not adequately plan the accomplishment of the procedure of descent by instruments, coming to throw out of the established profile, suggesting that he did not undertake the briefing of descent.
- The performance of the procedure outside the foreseen profile and in instrument flight conditions, determine the participation of this aspect in the occurrence.
Final Report:

Crash of a Cessna 500 Citation I in Rio de Janeiro

Date & Time: Jul 3, 1997 at 1000 LT
Type of aircraft:
Operator:
Registration:
PT-ILJ
Flight Phase:
Survivors:
Yes
Schedule:
Rio de Janeiro – São José dos Campos
MSN:
500-0057
YOM:
1973
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll at Rio de Janeiro-Santos Dumont Airport, the captain realized that all conditions were not met for a safe takeoff and decided to abort. Unable to stop within the remaining distance, the aircraft overran and came to rest in the Guanabara Bay. All five occupants escaped with minor injuries and the aircraft was damaged beyond repair.