Crash of a Beechcraft E90 King Air in Casigua El Cubo: 3 killed

Date & Time: Sep 19, 2014
Type of aircraft:
Operator:
Registration:
YV1537
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Anaco – Santa Bárbara del Zulia
MSN:
LW-309
YOM:
1979
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
En route from Anaco to Santa Bárbara del Zulia, the twin engine aircraft crashed in unknown circumstances by a wooded area located near Casigua El Cubo. The aircraft was destroyed by a post crash fire and all three occupants were killed. It is believed that the aircraft was engaged in an illegal contraband flight.

Crash of a Beechcraft 300LW Super King Air in Nordelta: 2 killed

Date & Time: Sep 14, 2014 at 1515 LT
Operator:
Registration:
LV-WLT
Flight Type:
Survivors:
No
Site:
Schedule:
Lincoln – Buenos Aires
MSN:
FA-221
YOM:
1992
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
14004
Captain / Total hours on type:
2000.00
Aircraft flight hours:
2630
Aircraft flight cycles:
2419
Circumstances:
The twin engine aircraft departed Lincoln-Estancia La Nueva Airport on a private flight to Buenos Aires, carrying one passenger and one pilot. While descending to Buenos Aires-Aeroparque-Jorge Newbury Airport, the pilot was unable to intercept the ILS for runway 13 because of an excessive speed of 260 knots and a too high angle of descent. In such conditions, he could not configure the aircraft for approach and landing (flaps) in accordance with the information in the BE 300 flight manual. He completed a left turn at a speed of 228 knots and descended below the glide before initiating a second turn to the right when control was lost. The aircraft entered a dive and crashed onto two houses located in Nordelta, about 26 km northwest of the airport. The aircraft and two houses were destroyed and both occupants were killed, among them Gustavo Andres Deutsch aged 78 who was the former owner of the defunct airline LAPA.
Probable cause:
The accident resulted from the combination of immediate triggers and failures in the aeronautical system's defenses, including:
- Prevailing weather conditions at the scene of the accident;
- Pilot-in-command experienced difficulties in managing aircraft control and flight path during an instrument approach;
- The probability of overload of work of the pilot in command as a result of the operational demands presented by the situation;
- The execution of the operation by a single pilot (single pilot operation), taking into account the age of the pilot; and
- Deficiencies in pilot-in-command certification denying the value of CE-6 as a defense barrier for the aeronautical system (CE-6 is a Critical Element of ICAO Annex 19 regarding responsibilities in issuing licenses).
Final Report:

Crash of a Piper PA-31-350 Navajo Chieftain in Araracuara: 10 killed

Date & Time: Sep 6, 2014 at 1505 LT
Operator:
Registration:
HK-4755
Flight Phase:
Survivors:
No
Schedule:
Araracuara – Florencia
MSN:
31-7952044
YOM:
1979
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
10
Captain / Total flying hours:
792
Captain / Total hours on type:
523.00
Copilot / Total flying hours:
211
Aircraft flight hours:
14601
Circumstances:
The twin engine aircraft departed Araracuara Airport runway 09 at 1503LT on a charter flight to Florencia, carrying eight passengers and two pilots. During initial climb, the right engine failed. The crew lost control of the airplane that stalled and crashed in a wooded area. The wreckage was found 8,2 km from the airport. The airplane disintegrated on impact and all 10 occupants were killed, among them a Swiss citizen.
Probable cause:
Loss of control during initial climb following the failure of the right engine for undetermined reasons.
The following contributing factors were identified:
- The crew failed to follow the published procedures when the right engine failed,
- The aircraft was likely operated with a total weight above MTOW,
- A poor risk assessment while performing an operation outside of the aircraft's performance limits.
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 an Embraer EMB-110P1 Bandeirante in Foz do Iguaçu

Date & Time: Jul 28, 2014 at 1500 LT
Operator:
Registration:
PT-TAW
Flight Phase:
Survivors:
Yes
Schedule:
Foz do Iguaçu - Curitiba
MSN:
110-258
YOM:
1980
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Shortly after takeoff from Foz do Iguaçu-Cataratas Airport, while climbing, the crew reported technical problems and elected to return. The crew realized he could not make it so he attempted an emergency landing in a corn field. Upon landing, the aircraft lost its undercarriage and slid for few dozen metres before coming to rest. Among the four occupants, one passenger was slightly injured and the aircraft was damaged beyond repair.

Crash of a Britten Norman BN-2A-26 Islander in Monkey Mountain

Date & Time: Jul 6, 2014 at 0950 LT
Type of aircraft:
Registration:
8R-GGY
Survivors:
Yes
Schedule:
Ogle – Omai – Mahdia – Monkey Mountain
MSN:
470
YOM:
1975
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The Authority said the aircraft left the Ogle International Airport earlier in the day and made stops at Omai and Mahdia before heading at Monkey Mountain Airfield with several goods on board. On approach to Monkey Mountain, the plane circled the airstrip several times before landing. Shortly after setting down, it was claimed the aircraft veered off the runway, hit few obstacles and came to rest. While both occupants were uninjured, the aircraft was damaged beyond repair. It appears that weather was poor at the time of the accident with rain and winds and low clouds.
Probable cause:
Guyana Civil Aviation Authority (GCAA) Director General Zulficar Mohamed disclosed that an initial investigation revealed that the Pilot involved in the Monkey Mountain mishap landed short of the runway. As a result, the landing gear of the plane was damaged and from there on, it was difficult to control the 10-seater Islander aircraft. The aircraft subsequently veered off the airstrip causing extensive damage. Mr. Mohamed further stated that the wrecked aircraft is beyond repair, but he was unsure if the operators will attempt to salvage what is left. The aircraft, owned by Domestic Airways, was piloted by Captain Orlando Charles.

Crash of a Cessna 525 CitationJet CJ1 in Aruanã

Date & Time: Jun 13, 2014 at 0747 LT
Type of aircraft:
Operator:
Registration:
PP-PIM
Survivors:
Yes
Schedule:
Goiânia – Aruanã
MSN:
525-0548
YOM:
2005
Location:
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
17000
Captain / Total hours on type:
38.00
Copilot / Total flying hours:
1078
Copilot / Total hours on type:
4
Aircraft flight hours:
3517
Circumstances:
The aircraft departed Goiânia on a flight to Aruanã, carrying two pilots and five passengers who should take part to the funeral of former football player Fernandão who died in an helicopter crash. Following an uneventful flight, the crew completed the landing on runway 24 which is 1,280 metres long. After touchdown, the aircraft was unable to stop within the remaining distance and overran. While contacting soft ground, the nose gear collapsed then the aircraft collided with a concrete fence and came to a halt 150 metres further against a second fence. All seven occupants were injured, the captain seriously. The aircraft was damaged beyond repair.
Probable cause:
The following findings were identified:
- The copilot was not certified in the C525 type aircraft,
- The aircraft was above the maximum landing weight limit, but within the balance limit,
- On 13JUN2014, there was a NOTAM in force, informing the prohibition of jet aircraft operation in SWNH,
- The pilot acted incorrectly on the handle of the auxiliary gear control, thinking that he was applying the emergency brake, making the braking of the aircraft impossible.
- The activation of the incorrect lever for the emergency braking of the aircraft was due to insufficient training received by the pilot for the use of the system in question, thus compromising the proper management of the abnormal condition.
- The emergency brake actuator handle of the aircraft was located outside the pilot's sight field, which, together with the lack of knowledge about the correct lever to be activated for emergency braking, favored the pilot's automatic response in triggering the lever that was most adjusted and visually available on the panel - the emergency landing gear drive lever.
- The instruction that the pilot received to operate the Cessna aircraft, model 525 did not emphasize in the theoretical phase the proper use of the emergency brake, nor contemplated training for the use of this system.
- Despite having a lot of experience in aviation, the pilot was little experienced in the aircraft and still did not know basic functionalities like the use of the emergency brake and the engine shutdown through the evacuation checklist procedure.
Final Report:

Crash of a Beechcraft B200 Super King Air in Bahía Solano

Date & Time: Jun 2, 2014 at 1700 LT
Operator:
Registration:
PNC-0225
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
BB-1644
YOM:
1998
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Shortly after takeoff from Bahía Solano-José Celestino Mutis Airport, while in initial climb, the crew encountered engine problems. The captain attempted an emergency landing in a prairie. The aircraft landed gear up and slid for few dozen metres before coming to rest. While all three occupants escaped with minor injuries, the aircraft was damaged beyond repair.

Crash of an ATR42-500 in Coari

Date & Time: May 30, 2014 at 2055 LT
Type of aircraft:
Operator:
Registration:
PR-TKB
Flight Phase:
Survivors:
Yes
Schedule:
Coari - Manaus
MSN:
610
YOM:
2000
Location:
Country:
Crew on board:
4
Crew fatalities:
Pax on board:
45
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total hours on type:
2601.00
Copilot / Total flying hours:
5898
Copilot / Total hours on type:
548
Circumstances:
During the takeoff roll from Coari-Urucu Airport by night, the aircraft collided with a tapir that struck the right main gear. The crew continued the takeoff procedure and the flight to Manaus. After two hours and burning fuel, the aircraft landed at Manaus-Eduardo Gomes Airport. Upon touchdown, the right main gear collapsed and the aircraft veered to the right and came to rest. All 49 occupants evacuated safely while the aircraft was damaged beyond repair.
Probable cause:
Collision with a tapir during takeoff, causing severe damages to the right main gear.
The following findings were identified:
- The lack of isolation of the operational area allowed the land animal to enter the runway for landings and takeoffs, contributing to the accident.
- The crew did not notice the presence of the land animal on the runway early enough to abort the takeoff without extrapolating the runway limits and avoiding collision.
- The presence of the land animal (Tapirus terrestris) interfered with the operation and led to the collision of the right main landing gear.
Final Report:

Crash of a Beechcraft B200 Super King Air near Carmelo: 5 killed

Date & Time: May 27, 2014 at 1240 LT
Operator:
Registration:
LV-CNT
Survivors:
Yes
Schedule:
San Fernando - Carmelo
MSN:
BB-1367
YOM:
1990
Location:
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
8039
Captain / Total hours on type:
478.00
Aircraft flight hours:
4616
Aircraft flight cycles:
4490
Circumstances:
Owned by Grupo Kowzef (Federico Alejandro Bonomi), the twin engine aircraft departed San Fernando (Buenos Aires) at 1222LT on an executive flight to Carmelo, Uruguay. On approach to Carmelo-Zagarzazú Airport runway 35, the pilot encountered marginal weather conditions and initiated a go-around procedure. Few minutes later, he attempted a second approach under VFR mode. While completing a slight turn to the left in descent, the aircraft impacted the surface of the Río de la Plata and came to rest in shallow water some 10 km southwest of Carmelo Airport. The pilot and four passengers were killed and four other occupants were injured. The aircraft was destroyed.
Probable cause:
The accident was the consequence of a controlled flight into terrain after the pilot suffered a loss of situational awareness due to a poor evaluation of the flight conditions upon arrival. The following contributing factors were identified:
- The pilot failed to return to his departure airport or to divert to the alternate airport due to poor weather conditions at the destination airport,
- The pilot continued the approach under VFR mode in IMC conditions with visibility below minimums,
- Poor evaluation of the flight conditions at destination on part of the pilot due to the combination of psychological and physiological factors.
Final Report: