Crash of a Dornier DO228-200 in Goma: 29 killed

Date & Time: Nov 24, 2019 at 0910 LT
Type of aircraft:
Operator:
Registration:
9S-GNH
Flight Phase:
Survivors:
No
Site:
Schedule:
Goma - Butembo
MSN:
8030
YOM:
1984
Location:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
17
Pax fatalities:
Other fatalities:
Total fatalities:
29
Circumstances:
The twin engine airplane departed runway 17 at Goma International Airport on a schedule service to Butembo (first service of the day). After takeoff, while in initial climb, the airplane lost height and crashed onto several houses located in the district of Birere, south of the airport, and burst into flames. All 19 occupants were killed as well as 10 people on the ground.

Crash of a Boeing 737-8F2 in Odessa

Date & Time: Nov 21, 2019 at 2055 LT
Type of aircraft:
Operator:
Registration:
TC-JGZ
Survivors:
Yes
Schedule:
Istanbul – Odessa
MSN:
35739/2654
YOM:
2008
Flight number:
TK467
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
136
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6094
Captain / Total hours on type:
5608.00
Copilot / Total flying hours:
252
Copilot / Total hours on type:
175
Aircraft flight hours:
38464
Aircraft flight cycles:
22633
Circumstances:
On November 21, 2019, a regular THY2UT flight en-route Istanbul – Odesa at B737-800 aircraft, nationality and registration mark TC-JGZ of the Turkish Airlines, was performed by the aircraft crew consisting of the Pilot-in-Command (PIC), co-pilot and four flight attendants of the aircraft. In fact, the departure from Istanbul Airport was performed at 17:33. The actual aircraft landing took place at 18:55. According to the flight plan, the alternate aerodromes were Istanbul and Chișinău. There were 136 passengers and 2793 kg of luggage on board the aircraft. The PIC was a Pilot Flying, and the co-pilot was a Pilot Monitoring of the aircraft. The pre-flight briefing of the crew, according to its explanations, was carried out before departure from the Istanbul Airport, after which the PIC took the decision to perform the flight. The climb and level flight were performed in the normal mode. The landing approach was performed to the Runway16 with ILS system at a significant crosswind component of variable directions. At the final stage of approaching with ILS to Runway 16, the ATC controller of the aerodrome control tower (ATC Tower) gave the aircraft crew a clearance for landing. The aircraft crew confirmed the controller’s clearance and continued the landing approach. Subsequently, from a height of about 50 meters, the aircraft performed a go-around due to the aircraft non-stabilization before landing. Following the go-around, the aircraft headed to the holding area to wait for favorable values of wind force and direction. At 18:45, the PIC took the decision to carry out a repeated landing approach, reported of that to the ATC controller, who provided ATS in the Odesa Terminal Maneuvering Area (TMA.) At 18:51, the crew re-contacted the Tower controller and received the clearance to land. At 18:55, after touchdown, during the runway run, the aircraft began to deviate to the left and veered off of the runway to the left onto the cleared and graded area. After 550 m run on the soil, the aircraft returned to the runway with its right main landing gear and nose part (while moving on the soil, the nose landing gear collapsed) and came to rest at the distance of 1612 m from the runway entrance threshold. The crew performed an emergency evacuation of passengers from the aircraft. As a result of the accident, the aircraft suffered a significant damage to the nose part of the fuselage and left engine. None of the passengers or crew members was injured.
Probable cause:
The cause of the accident, i.e. runway excursion, which caused significant damage to the structural elements of the aircraft B-737-800 TC-JGZ of Turkish Airlines, which took place on 21.11.2019 during landing at «Odesa» Aerodrome, was failure to maintain the direction of the aircraft movement during the landing run in the conditions of a strong crosswind of variable directions.
Contributing Factors:
- Use by the crew of the landing approach method using the Touchdown in Crab technique, which is not recommended by FCTM B-737NG document for use on dry runways in the conditions of a strong crosswind;
- Untimely and insufficient actions of the crew to maintain the landing run direction;
- Presence of a significant cross component of the wind;
- Effect of an omnidirectional wind – from cross-headwind to cross-tailwind directions – during the landing run.
Final Report:

Crash of a Saab 2000 in Unalaska: 1 killed

Date & Time: Oct 17, 2019 at 1740 LT
Type of aircraft:
Operator:
Registration:
N686PA
Survivors:
Yes
Schedule:
Anchorage - Unalaska
MSN:
017
YOM:
1995
Flight number:
AS3296
Crew on board:
3
Crew fatalities:
Pax on board:
39
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
14761
Captain / Total hours on type:
131.00
Copilot / Total flying hours:
1447
Copilot / Total hours on type:
138
Aircraft flight hours:
12617
Aircraft flight cycles:
9455
Circumstances:
On October 17, 2019, a Saab SA-2000 airplane, operated by Peninsula Aviation Services Inc. d.b.a. PenAir flight 3296, overran the end of runway 13 at Unalaska Airport (DUT), Unalaska, Alaska. The flight crew executed a go-around during the first approach to runway 13; the airplane then entered the traffic pattern for a second landing attempt on the same runway. Shortly before landing, the flight crew learned that the wind at midfield was from 300° at 24 knots, indicating that a significant tailwind would be present during the landing. Because an airplane requires more runway length to decelerate and stop when a tailwind is present during landing, a landing in the opposite direction (on runway 31) would have favored the wind at the time. However, the flight crew continued with the plan to land on runway 13. Our postaccident calculations showed that, when the airplane touched down on the runway, the tailwind was 15 knots. The captain reported after the accident that the initial braking action after touchdown was normal but that, as the airplane traveled down the runway, the airplane had “zero braking” despite the application of maximum brakes. The airplane subsequently overran the end of the runway and the adjacent 300-ft runway safety area (RSA), which was designed to reduce airplane damage during an overrun, and came to rest beyond the airport property. The airplane was substantially damaged during the runway overrun; as a result, of the 3 crewmembers and 39 passengers aboard, 1 passenger sustained fatal injuries, and 1 passenger sustained serious injuries. Eight passengers sustained minor injuries, most of which occurred during the evacuation. The crewmembers and 29 passengers were not injured.
Probable cause:
The National Transportation Safety Board determines that the probable cause of this accident was the landing gear manufacturer’s incorrect wiring of the wheel speed transducer harnesses on the left main landing gear during overhaul. The incorrect wiring caused the antiskid system not to function as intended, resulting in the failure of the left outboard tire and a significant loss of the airplane’s braking ability, which led to the runway overrun.
Contributing to the accident were
1) Saab’s design of the wheel speed transducer wire harnesses, which did not consider and protect against human error during maintenance;
2) the Federal Aviation Administration’s lack of consideration of the runway safety area dimensions at Unalaska Airport during the authorization process that allowed the Saab 2000 to operate at the airport; and
3) the flight crewmembers’ inappropriate decision, due to their plan continuation bias, to land on a runway with a reported tailwind that exceeded the airplane manufacturer’s limit. The safety margin was further reduced because of PenAir’s failure to correctly apply its company-designated pilot-incommand airport qualification policy, which allowed the accident captain to operate at one of the most challenging airports in PenAir’s route system with limited experience at the airport and in the Saab 2000 airplane.
Final Report:

Crash of a Fokker 50 in Nairobi

Date & Time: Oct 11, 2019 at 0902 LT
Type of aircraft:
Operator:
Registration:
5Y-IZO
Flight Phase:
Survivors:
Yes
Schedule:
Nairobi - Mombasa - Lamu
MSN:
20244
YOM:
1992
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
50
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7492
Captain / Total hours on type:
262.00
Copilot / Total flying hours:
4156
Circumstances:
On October 11, 2019 at about 0902 Kenya daylight time, a Silverstone Air Services Fokker 27 Mark 050 registration 5Y-IZO experienced runway excursion on takeoff runway 14 at Wilson Airport with 55 occupants onboard (5 crew and 50 passengers). The aircraft was performing a scheduled flight from Wilson airport to Mombasa, Lamu and back to Wilson airport. The aircraft was fueled then the passengers boarded the plane before the normal pre take off procedures which were reported as uneventful as collaborated by the information from the FDR. The Right Hand engine receded the Left Hand engine in startup as depicted by the parameters from the recorders. From engine startup, taxi, lineup runway 14, power up and including the initial stages of ground roll were uneventful. At 06.02.50 GMT, while still on ground roll take off, the LH engine ITT began to fluctuate, dropped from 707.8 to 175.8. The RH ITT remained stable. The other parameters of both engines were stable. Subsequent power down ensued at 06.03.01, IAS dropped from 110.2Knots and the aircraft magnetic heading increased gradually to 144 consistent with the deviation of the aircraft to the right of the runway axis when it left the paved surface of the runway, before colliding with the airport perimeter fence, went through an embankment before coming to rest tilted to the right after the starboard wing made contact with a tree. The passengers were deplaned through the two left hand side front and rear exit doors. Immediately the event occurred, ATS Wilson airport issued a crash alert and Wilson Airport Fire Service (AFS) responded without delay, found the passengers already evacuated from the aircraft and applied foam to the sections of the aircraft with leaking fuel. Runway 14/32 was closed and all inbound and departure traffic made use of the remaining runway. Preliminary information retrieved from the Flight Data Recorder Radar regarding the engine ITT seems to correlate with the flight crew statements regarding the observed fluctuations on the LHS engine ITT.

Crash of a Cessna 208B Grand Caravan in Seronera: 2 killed

Date & Time: Sep 23, 2019
Type of aircraft:
Operator:
Registration:
5H-AAM
Flight Phase:
Survivors:
No
Schedule:
Seronera - Grumeti Hills
MSN:
208B-2430
YOM:
2013
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The single engine airplane departed Seronera Airstrip in the early morning on a short flight to Grumeti Hills, about 40 km northwest, according to a statement from the operator. Shortly after takeoff, the airplane went out of control, struck a concrete wall and crashed upside down. The pilot and the sole passenger were killed.

Statement from the operator:
https://www.auricair.com/About-Us/5HAAM_Accident_23Sept2019

Crash of a Cessna 208B Grand Caravan in Manaus

Date & Time: Sep 16, 2019 at 1225 LT
Type of aircraft:
Operator:
Registration:
PT-MHC
Flight Phase:
Survivors:
Yes
Schedule:
Manaus - Maués
MSN:
208B-0543
YOM:
1996
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
22800
Captain / Total hours on type:
14150.00
Copilot / Total flying hours:
947
Copilot / Total hours on type:
791
Circumstances:
The single engine airplane departed Manaus-Eduardo Gomes Airport Runway 29 in heavy rain falls as weather conditions deteriorated shortly prior to takeoff. After liftoff, while in initial climb, the airplane lost altitude and crashed in a dense wooded area located 600 metres past the runway end. The aircraft was destroyed by impact forces and all 10 occupants were injured, among them six seriously. At the time of the accident, weather conditions were poor with heavy rain falls, turbulence and windshear.
Probable cause:
The accident was the consequence of the combination of the following factors:
- Control skills – undetermined.
While facing adverse conditions, the use of controls may have been inappropriate for the situation and may have contributed to the aircraft not being able to maintain a positive climb rate.
- Attitude – undetermined.
Familiarization with the region may have led to an attitude, on the part of the PIC, of minimizing the importance of analyzing adverse weather conditions, to the detriment of compliance with the minimum limits established by the company in its manuals.
- Training – undetermined.
It is possible that, due to possible inadequate training, the SIC did not identify the critical situation that arose shortly after the take-off in time to assist the PIC in maintaining flight control.
- Tasks characteristics – undetermined.
The characteristics present in the type of operation, compliance with schedules without the possibility of delays, due to the runway closing period, may have favored the self imposed pressure on the part of the PIC, leading him to operate with reduced safety margins.
- Adverse meteorological conditions – a contributor.
The conditions at the time of the take-off contributed to the aircraft not being able to maintain the flight with a positive climb rate. The probable occurrence of Windshear determined that the trajectory of the aircraft was modified until its collision with the ground.
- Crew Resource Management – undetermined.
On the part of the SIC, no assertive attitude was perceived in the sense of alerting the PIC that those conditions were not favorable for takeoff. Thus, the crew decided to carry out the take-off despite the company's SOP.
- Organizational culture – undetermined.
The company encouraged compliance with the legs even though, within the planning of flights, there was not an adequate margin of time to absorb any delays. This culture may have influenced the PIC's decision-making, which, despite encountering adverse conditions, chose to take off, since the short time on the ground in the intermediate locations did not allow room for delays.
- Emotional state – undetermined.
The reports indicated that the PIC felt pressured to perform the take-off even in the weather conditions found on the day of this occurrence. Also, according to the interviewees, this pressure would be related to the fulfillment of the flight schedule and the need to keep to the scheduled times. In this way, it is possible that their assessment of the performance of the flight was influenced by the stress resulting from the pressure to complete the flight within the expected time, given the closing time of the runway for works.
- Flight planning – a contributor.
The flight planning was not carried out properly, considering that the planned schedules and routes would end after the closing time of the SBEG runway for works, provided for in the NOTAM. This meant that there was little time to adjust the legs, increasing the workload and stress in the cabin.
- Decision-making process – a contributor.
There was a wrong assessment of the meteorological conditions, which contributed to the decision of performing it in an adverse situation.
- ATS publication– undetermined.
The TWR-EG did not inform, before the take-off, of the changes in the significant weather conditions that were occurring at the terminal, which could have contributed to the PIC's decision-making.
Final Report:

Crash of a Piper PA-31-350 Navajo Chieftain in Popayán: 7 killed

Date & Time: Sep 15, 2019 at 1406 LT
Operator:
Registration:
HK-5229
Flight Phase:
Survivors:
Yes
Site:
Schedule:
Popayán - López de Micay
MSN:
31-7405212
YOM:
1974
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
7
Captain / Total flying hours:
3291
Captain / Total hours on type:
991.00
Copilot / Total flying hours:
300
Copilot / Total hours on type:
55
Aircraft flight hours:
12304
Circumstances:
The twin engine airplane departed Popayán-Guillermo León Valencia Airport runway 26 at 14:06:06. The aircraft encountered difficulties to gain sufficient height. About 20 seconds after liftoff, at a speed of 82 knots, the aircraft rolled to the right then entered an uncontrolled descent and crashed onto two houses located 530 metres past the runway end. Two passengers were seriously injured and seven other occupants were killed.
Probable cause:
A loss of in-flight control of the aircraft due to possible excess weight. The aircraft probably managed to take off due to "ground effect", but, once in the air and out of ground effect, it was not able to obtain the speed that would allow it to safely accomplish the climb.
Contributing Factors:
- Absence of Dispatch procedures of the operator to perform a correct Weight and Balance of the aircraft, and the effective control of the boarded cargo.
- Incorrect calculation of the weight and balance of the aircraft by the crew, by not considering all the cargo that was loaded, causing the aircraft to take off with a possible excess weight.
- Weak operational safety management processes of the operator by not considering the operating characteristics of airfields such as Popayán (high altitude, high ambient temperature) that significantly limit the operation.
Final Report:

Ground fire of an Airbus A330-343 in Beijing

Date & Time: Aug 27, 2019 at 1648 LT
Type of aircraft:
Operator:
Registration:
B-5958
Flight Phase:
Survivors:
Yes
Schedule:
Beijing - Tokyo
MSN:
1587
YOM:
2014
Flight number:
CA183
Country:
Region:
Crew on board:
14
Crew fatalities:
Pax on board:
147
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
19007
Aircraft flight cycles:
4596
Circumstances:
The airplane was parked at gate 530 (Terminal 3) at Beijing Capital and being prepared for flight CA183 to Tokyo-Haneda. 14 crew members were on board as well as 147 passengers when an abnormal sound was heard coming from the L2 door connected to the jetbridge. The cargo smoke alarm came on in the cockpit while smoke spread in the cabin. The pilot declared an emergency and decision was taken to evacuate all 161 occupants and no one was injured while the aircraft was partially destroyed by fire. The origin of the fire is still under investigation.

Crash of a De Havilland DHC-8-202 in Kichwa Tembo

Date & Time: Aug 16, 2019 at 1100 LT
Operator:
Registration:
5Y-SLM
Survivors:
Yes
Schedule:
Nairobi – Kichwa Tembo
MSN:
506
YOM:
1997
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Following an uneventful flight from Nairobi-Wilson Airport, the crew landed on a gravel runway at Kichwa Tembo Airport. After touchdown, the aircraft collided with two wildebeests. Upon impact, the left main gear was torn off and the aircraft veered off runway to the left and came to rest. All occupants evacuated safely and the aircraft was damaged beyond repair. Both wildebeests were killed.
Probable cause:
Loss of control upon landing following a ground collision with two wildebeests.

Crash of an Airbus A321-211 in Moscow

Date & Time: Aug 15, 2019 at 0615 LT
Type of aircraft:
Operator:
Registration:
VQ-BOZ
Flight Phase:
Survivors:
Yes
Schedule:
Moscow - Simferopol
MSN:
2117
YOM:
2003
Flight number:
U6178
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
226
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Shortly after takeoff from Moscow-Zukhovski Airport runway 12, while climbing to an altitude of 750 feet in excellent weather conditions, the airplane collided with a flock of birds (sea gulls). Some of them were ingested by both engines that lost power. It was later reported by the crew that the left engine stopped almost immediately while the right engine lost power and run irregularly. Unable to maintain a positive rate of climb, the captain decided to attempt an emergency landing in a cornfield. The airplane belly landed approximately 3,5 km past the runway end and slid for dozen meters before coming to rest with its both engines partially torn off. All 233 occupants were able to evacuate the cabin and it is reported that 23 people were slightly injured.