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Crash of a Boeing 707-330C in Manaus

Date & Time: Oct 23, 2004 at 0840 LT
Type of aircraft:
Operator:
Registration:
PP-BSE
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Manaus – São Paulo
MSN:
19317
YOM:
1967
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
9487
Captain / Total hours on type:
6600.00
Copilot / Total flying hours:
14180
Copilot / Total hours on type:
3180
Aircraft flight hours:
95933
Circumstances:
Ready for takeoff on runway 10 at Manaus-Eduardo Gomes Airport, the crew released brakes and increased engine power when a loud noise was heard coming from the right side of the aircraft. The captain decided to reject takeoff and applied brakes when the aircraft started to deviate to the right. It veered off runway and came to rest. All three crew members escaped uninjured while the aircraft was considered as damaged beyond repair after the right main gear punctured the wing.
Probable cause:
The right main gear collapsed during takeoff following a structural failure caused by the presence of fatigue cracks that were not detected by the maintenance crew because of poor maintenance. The aircraft already suffered an accident in Guarulhos Airport, causing damages to the right main gear.
Final Report:

Crash of an Embraer EMB-120ER Brasília near Manaus: 33 killed

Date & Time: May 14, 2004 at 1835 LT
Type of aircraft:
Operator:
Registration:
PT-WRO
Survivors:
No
Schedule:
São Paulo de Olivença – Tabatinga – Tefé – Manaus
MSN:
120-070
YOM:
1988
Flight number:
RLE4815
Location:
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
30
Pax fatalities:
Other fatalities:
Total fatalities:
33
Captain / Total flying hours:
19069
Captain / Total hours on type:
5819.00
Copilot / Total flying hours:
11927
Copilot / Total hours on type:
4637
Circumstances:
While descending to Manaus-Eduardo Gomes Airport following an uneventful flight from Tefé, the aircraft was correctly established on the ILS when the crew was instructed by ATC to initiate a go-around and to follow a holding pattern as the priority was given to an ambulance flight. The crew made a left turn heading 060° and continued the descent after passing 2,000 feet when the aircraft struck the ground and crashed about 33 km from the airport. The aircraft disintegrated on impact and all 33 occupants were killed.
Probable cause:
Controlled flight into terrain after the crew continued the descent below 2,000 feet until the aircraft impacted ground. The following contributing factors were identified:
- The crew reported his altitude at 2,000 feet while the real altitude of the airplane was 1,300 feet,
- The crew continued the descent until final impact,
- The crew did not react to the GPWS alarm that sounded four times when the aircraft reached the altitude of 400 feet,
- No corrective action was taken by the crew,
- Lack of crew coordination,
- Poor approach planning that led the aircraft descending to a critical altitude,
- Lack of supervision,
- Operational deficiencies.
Final Report:

Ground accident of an Embraer EMB-120RT Brasília in Manaus

Date & Time: Aug 13, 2002 at 1225 LT
Type of aircraft:
Operator:
Registration:
PT-WGE
Flight Phase:
Survivors:
Yes
Schedule:
Humaitá – Manaus
MSN:
120-004
YOM:
1986
Flight number:
RLE4847
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
22
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
13474
Captain / Total hours on type:
518.00
Copilot / Total flying hours:
4110
Copilot / Total hours on type:
3660
Aircraft flight hours:
26756
Circumstances:
Following an uneventful flight from Humaitá, the crew completed the landing at Manaus-Eduardo Gomes Airport. After taxi, the crew was approaching the apron when he feathered the propellers and applied the brakes as they wanted to stop the aircraft. There was no deceleration despite both crew applied brakes. The copilot suggested to use reverse thrust but this was not possible as the propellers were already feathered. Out of control, the aircraft struck a brick building, damaging the left engine, and the right landing gear fell into a drainage ditch, approximately one meter deep. All 25 occupants evacuated safely while the aircraft was damaged beyond repair.
Probable cause:
The following factors were identified:
- The crew did not have sufficient training to enable the desired assertiveness for the correct use of aircraft resources, which would probably have prevented the accident, since, instead of applying the emergency brake, they applied reverse with the feathered props, contrary to the procedure provided for in the Aircraft Manual.
- The maintenance services were not efficient, as they did not comply with the Aircraft Maintenance Manual in relation to the dimensional adjustment of the Hub Cap Drive Clips' drive clips, and the Service Bulletin incorporated stickers to the outer doors of the main landing gear, as a reminder to the mechanic to check the clearances.
- The copilot failed to apply the reverse pitch on the propellers as they were feathered, and at that moment the emergency brake should be commanded to brake the aircraft.
- The company failed to adequately check the execution of the actions provided for in the Aircraft Maintenance Manual regarding the 'Antiskid' system and to verify the application of all service bulletins issued by the manufacturer.
Final Report:

Crash of an Embraer EMB-110P1 Bandeirante in Envira

Date & Time: Jan 31, 2000 at 1030 LT
Operator:
Registration:
PP-EAM
Flight Type:
Survivors:
Yes
Schedule:
Tefé - Eirunepé
MSN:
110-498
YOM:
1990
Location:
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
17
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4800
Captain / Total hours on type:
4000.00
Copilot / Total flying hours:
2000
Copilot / Total hours on type:
1600
Circumstances:
En route from Tefé to Eirunépé, weather conditions deteriorated and the crew decided to divert to the non controlled Envira Airport. Following a visual approach in heavy rain falls, the aircraft landed 500 metres past the runway threshold. After touchdown, the crew started the braking procedure but the aircraft encountered aquaplaning conditions and was unable to stop within the remaining distance. It overran and came to rest 100 metres further in a ravine. The captain was seriously injured, the copilot suffered minor injuries and all 16 passengers escaped uninjured.
Probable cause:
The aircraft suffered aquaplaning after landing and was unable to stop within the remaining distance. The following contributing factors were identified:
- The operator authorized the crew to divert to an unapproved airport with an aircraft weighing more than the limits specified in the operations manual without performing adequate supervision in the execution of the flight;
- Deviations on part of the crew;
- Lack of Crew Resources Management;
- Lack of crew coordination and communication;
- Lack of crew instruction and training on part of the operator;
- Poor weather conditions with heavy rain falls;
- The runway surface was wet and the aircraft suffered aquaplaning;
- The aircraft was overloaded;
- The landing was completed with a tailwind component;
- The crew failed to perform the approach briefing according to published procedures.
Final Report:

Crash of an Embraer EMB-110P1 Bandeirante near Manacapuru: 12 killed

Date & Time: Jul 29, 1998 at 1300 LT
Registration:
PT-LGN
Flight Phase:
Survivors:
Yes
Schedule:
Manaus – Tefé
MSN:
110-343
YOM:
1982
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
24
Pax fatalities:
Other fatalities:
Total fatalities:
12
Captain / Total flying hours:
15000
Captain / Total hours on type:
8000.00
Copilot / Total flying hours:
2500
Copilot / Total hours on type:
2000
Circumstances:
The EMB-110 Bandeirante operated on a domestic flight from Manaus to Tefé, Brazil. Although the airplane was certificated for a maximum of 19 passengers, there were 25 passengers on board. Also, for financial reasons the crew decided to take more fuel than necessary for this flight. This resulted in the airplane departing with an excess of weight of 852 kg. About 20 minutes into the flight the oil pressure of the no. 2 engine dropped. The crew reduced engine power to 72% and continued to Tefé. When the flight was 185 km from Manaus at FL85 the oil pressure dropped to 40psi and the TGT increased. The copilot shut down the engine and the captain turned the airplane around, back to Manaus. At 13:15 the crew contacted Manaus ACC reporting that they were returning on one engine. The overloaded airplane flying on one engine, began to lose height. During the descent the speed was kept around 105 kts which occasionally caused activated stick shaker. To lose weight, the left overwing exit was opened and luggage of the passengers was jettisoned. The airplane did not make it to Manaus and an emergency landing on the Manacapuru River was made. The Bandeirante landed hard on the water, causing an opening in the fuselage. It sank quickly.
Probable cause:
The following factors were identified:
- It was not possible to examine the debris of the aircraft to determine the contribution of this factor to the failure of the left engine.
- It is possible that the failure to carry out a type B2 inspection and/or to carry out a type A1 inspection by an unqualified person may have contributed to the occurrence of a low oil pressure emergency, due to material deterioration or inadequate services. The impossibility of examining the aircraft could not determine this aspect.
- The owner of the air taxi company participated due to lack of adequate supervision in the planning of operations, at the technical, operational and administrative levels. This deficiency can be characterized, among other things, by the owner of the company that allowed the aircraft to fly with the type B2 inspection expired; by the excessive amount of fuel, when refueling in Manaus; by the unreasonable number of people on board, causing the aircraft to fly with excess weight, and still, by the receipt of pilots' salary to be conditioned to the accomplishment of the fateful flight.
- Errors were made by the aircraft crew due to the improper use of the resources available in the cabin, intended for the operation of the aircraft, due to non-compliance with operational rules.
- There was a mistake made by the crew due to the inadequate preparation for the flight, assuming numerous failures, such as: the non conference, by the pilots, of the cargo and passengers manifest; the lack of the realization of a briefing and still, to accept an aircraft for a flight, being the same with its inspection not carried out.
- An error was made by the crew due to inadequate evaluation of certain aspects of the flight. Such deficiency was evidenced when the first sign of failure of the lubrication system occurred, after twenty minutes of flight, and even so, they decided to proceed with the flight, when the most sensible and safe would be the return, immediately, to Manaus.
- The airline's support staff participated in the planning of weight and balance of the aircraft and the number of passengers on board, providing incorrect information to the aircraft's crew members. In addition, the mechanic who performed the A1 type inspection was not qualified for the function.
- There has been intentional non-compliance by the crew members with the operational rules established by the aircraft manufacturer.
- The Commander did not foresee what was predictable, for lack of caution, thus intentionally increasing the risk margin of the mission.
Final Report:

Crash of a De Havilland C-115 Buffalo at Ponta Pelada AFB

Date & Time: May 15, 1995
Type of aircraft:
Operator:
Registration:
2361
Flight Type:
Survivors:
Yes
Schedule:
Ponta Pelada AFB - Ponta Pelada AFB
MSN:
31
YOM:
1969
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing a local training flight at Ponta Pelada AFB, Manaus. Upon landing, the aircraft went out of control, veered off runway and came to rest few dozen metres further. There were no casualties while the aircraft was damaged beyond repair.

Crash of an Embraer EMB-110EJ Bandeirante in São Gabriel da Cachoeira

Date & Time: May 7, 1994 at 1248 LT
Operator:
Registration:
PT-GJW
Survivors:
Yes
Schedule:
Santa Isabel do Rio Negro – São Gabriel da Cachoeira
MSN:
110-072
YOM:
1976
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
14
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
15000
Captain / Total hours on type:
5180.00
Circumstances:
The crew encountered poor weather conditions on approach to São Gabriel da Cachoeira Airport with low visibility due to fog. On short final, the crew failed to realize his altitude was insufficient when the aircraft collided with trees and crashed few hundred metres short of runway. All 16 occupants were injured, three seriously. The aircraft was destroyed.
Probable cause:
Contributing factors
a. Human Factor
(1). Psychological Aspect
It contributed, since the pilot in command adopted an improvisational attitude through the adoption of unforeseen procedures in the face of the insistence on landing, despite the weather conditions present. A likely channeling of attention to external references may have contributed to the loss of operational performance, leading to the loss of the maintenance condition of the basic flight parameters.
(2). Physiological Aspect
Undetermined since the absence of interference from toxicological factors was not effectively verified.
b. Material Factor
Didn't contribute.
c. Operational Factor
(1). Deficient Instruction
It contributed since there was no periodic simulator training and also no cockpit resource management (CRM) training.
(2). Deficient Supervision
It contributed since there was no adequate monitoring of the circumstances of operation by the Company's operations sector and, also, there were no defined and clear rules and specific operating routines that adequately addressed the various aspects of the operation.
(3). Little Flight or Aircraft Experience
It contributed because of the small experience in the aircraft by the copilot.
(4). Influence of the Environment
It contributed since visibility was limited at the time of the accident.
(5). Deficient Cockpit Coordination
Contributed since there was no briefing to the accomplishment of the descent procedure by instruments, the copilot did not follow the execution of the procedures after the critical point since he concentrated his attention to the search of external references, thus abandoning the monitoring of the flight parameters.
(6). Disabled Infrastructure
Indetermined since the influence of the low accuracy of the NDB on the heading lags occurred in the descent procedure was not perfectly established and no effective test was performed.
(7). Poor Planning
It contributed because there was no briefing in the procedure of descent by instrument and approach lost.
(8). Deficient discipline of Flight
The pilot therefore continued the flight, without visibility, at an altitude below the minimum for this operating condition.
(9). Adverse Weather Conditions
It contributed as the prevailing weather conditions were marginal, with the aerodrome closed for IFR operation.
Final Report:

Crash of a Boeing 707-365C in Manaus

Date & Time: Nov 26, 1992 at 0226 LT
Type of aircraft:
Operator:
Registration:
PT-TCP
Flight Type:
Survivors:
Yes
Schedule:
Manaus - Miami
MSN:
19416
YOM:
1967
Country:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After liftoff from Manaus-Eduardo Gomes Airport runway 28, while in initial climb, the right main gear struck an element of the approach light system. An alarm sounded in the cockpit, informing the crew about landing gear problems. As the crew was unable to raise the landing gear, the captain informed ATC about the situation and was cleared to return for an emergency landing. Upon touchdown on runway 28, the right main gear collapsed. The aircraft slid for few dozen metres then veered off runway and came to rest in a ravine. All five occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
It was reported that the crew adopted a wrong takeoff configuration and that the rate of climb and gradient were too low after takeoff (positive but insufficient vario), causing the aircraft to collide with an equipment of the approach light system.

Crash of a Beechcraft C90A King Air in Manaus: 7 killed

Date & Time: May 30, 1990 at 1500 LT
Type of aircraft:
Operator:
Registration:
N31434
Survivors:
No
Schedule:
Pitinga - Manaus
MSN:
LJ-1186
YOM:
1988
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
The approach to Manaus-Eduardo Gomes was completed in heavy rain falls. On short final, the crew failed to realize his altitude was too low when the aircraft struck an element of the approach light system and crashed 200 meters short of runway, bursting into flames. All seven occupants were killed.

Crash of an Embraer C-95 Bandeirante near Manaus: 1 killed

Date & Time: Jun 16, 1987 at 0745 LT
Type of aircraft:
Operator:
Registration:
2185
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Ponta Pelada – Boa Vista
MSN:
110-114
YOM:
1976
Location:
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
Fifteen minutes after takeoff from Ponta Pelada AFB, en route to Boa Vista, one of the engine lost power. The crew elected to return but as he was unable to maintain a safe altitude, he attempted an emergency landing when the aircraft crashed onto a house. All nine occupants were injured and one people in the house was killed.
Probable cause:
Engine problems for unknown reasons.