Crash of an Antonov AN-24RV in Donetsk: 5 killed

Date & Time: Feb 13, 2013 at 1809 LT
Type of aircraft:
Operator:
Registration:
UR-WRA
Survivors:
Yes
Schedule:
Odessa - Donetsk
MSN:
3 73 087 09
YOM:
1973
Flight number:
YG8971
Country:
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
44
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
3245
Captain / Total hours on type:
560.00
Copilot / Total flying hours:
175
Aircraft flight hours:
51136
Aircraft flight cycles:
32645
Circumstances:
On final approach to Donetsk-Sergei Prokofiev Airport, during the last segment, the aircraft banked right to a angle of 48°, causing the right wing to struck the ground. The aircraft overturned and crashed in a grassy area to the left of runway 08, coming to rest upside down. Five passengers were killed while all other occupants were injured. The aircraft was destroyed. It was performing a charter flight from Odessa with 44 football fans on their way to a match between Shakhtar Donetsk and Borussia Dortmund. At the time of the accident, the visibility was poor due to the night and foggy conditions. The horizontal visibility was reported to be 250 metres with an RVR of 750 metres for runway 08 and vertical visibility of 200 feet.
Probable cause:
It was planned that an instructor should perform the flight with the crew but he did not show up, so the captain decided to do the flight without him. On final approach to Donetsk, the visibility was limited and the captain was authorized to descent until 1,000 feet on approach where he should establish a visual contact with runway 08 or the approach lights. At this decision height, he continued the approach without any calls to the rest of the crew despite he did not establish any visual contact with the runway. During the last segment, the aircraft banked right due to a too low approach speed of 103 knots, stalled and crashed. The crew failed to monitor the approach speed, and the captain decided to continue the approach despite the visibility was below minimums. At the decision height, he should abandon the approach for a go-around procedure.
Final Report:

Crash of a Piper PA-31-325 Navajo C/R in Tuxtla Gutierrez: 8 killed

Date & Time: Jan 17, 2013 at 1334 LT
Type of aircraft:
Registration:
XB-EZY
Flight Phase:
Survivors:
No
Schedule:
Tuxtla Gutierrez – Puebla
MSN:
31-8212007
YOM:
1982
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
8
Circumstances:
At 1339LT, the crew was cleared for takeoff from runway 32 at Tuxtla Gutierrez-Angel Albino Corzo Airport. During initial climb, after being cleared to climb to 12,500 feet, the crew informed ATC he was returning to the airport. Shortly later, the aircraft lost height and crashed in a field, bursting into flames. The aircraft was totally destroyed and all 8 occupants were killed.
Probable cause:
One of the engine failed after takeoff due to a fuel pump malfunction. The crew elected to return but the aircraft stalled due to an insufficient speed. Poor engine maintenance was considered as a contributing factor as well as the fact that the crew initiated the flight while the aircraft's weight was above the allowable MTOW.
Final Report:

Crash of a Britten-Norman BN-2A-27 off Los Roques: 6 killed

Date & Time: Jan 4, 2013 at 1145 LT
Type of aircraft:
Operator:
Registration:
YV2615
Flight Phase:
Survivors:
No
Schedule:
Los Roques - Caracas
MSN:
20
YOM:
1968
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
The twin engine aircraft departed Los Roques Island Airport Runway 07 at 1132LT on a charter flight to Caracas, carrying four passengers and two pilots. During initial climb, the crew was cleared to climb to 6,500 feet. Seven minutes later, the crew informed ATC he was climbing to 5,000 feet and reported his position some 10 NM from Gran Roque VOR. While cruising at 5,400 feet at a speed of 120 knots, the aircraft entered an uncontrolled descent and crashed in the sea. SAR operations did not find any trace of the aircraft nor the six occupants and all operations were abandoned after one week. The Italian couturier Vittorio Missoni was among the passenger. In June 2013, some debris were localized at a depth of 75 meters and five bodies were found on 17OCT2013. Eventually, the wreckage was recovered on 25NOV2013.

Crash of a Cessna 208B Grand Caravan in Snow Lake: 1 killed

Date & Time: Nov 18, 2012 at 0956 LT
Type of aircraft:
Operator:
Registration:
C-GAGP
Flight Phase:
Survivors:
Yes
Schedule:
Snow Lake - Winnipeg
MSN:
208B-1213
YOM:
2006
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
2865
Captain / Total hours on type:
1020.00
Aircraft flight hours:
1487
Circumstances:
The Gogal Air Services Limited Cessna 208B (registration C-GAGP, serial number 208B1213) departed Runway 21 at Snow Lake en route to Winnipeg, Manitoba, with the pilot and 7 passengers on board. At approximately 0956 Central Standard Time, shortly after take-off, the aircraft descended and struck the terrain in a wooded area approximately 0.9 nautical miles beyond the departure end of the runway. The pilot was fatally injured, and the 7 passengers sustained serious injuries. The aircraft was destroyed by impact forces, and a small fire ensued near the engine. The aircraft’s emergency locater transmitter activated. First responders attended the scene, and the injured passengers were taken to area hospitals. The aircraft’s fuel cells ruptured, and some of the onboard fuel spilled at the site.
Probable cause:
Findings as to causes and contributing factors:
1. The aircraft departed Snow Lake overweight and with an accumulation of ice on the leading edges of its wings and tail from the previous flight. As a result, the aircraft had reduced take-off and climb performance and increased stall speed, and the protection afforded by its stall warning system was impaired.
2. A breakdown in the company’s operational control resulted in the flight not operating in accordance with the Canadian Aviation Regulations and the company operations manual.
3. As a result, shortly after departure, the aircraft stalled at an altitude from which recovery was not possible.
Findings as to risk:
1. If companies operate in instrument meteorological conditions for which they are not authorized, there is an increased risk that accidents may occur.
2. If Transport Canada does not provide the same degree of oversight for repetitive charter operations as it does for a scheduled operator, the risks in the operator’s activities may not be fully evaluated.
3. If passenger briefings are not provided and passengers are not properly seated and restrained, there is an increased risk of injuries to those passengers and the other occupants in the event of an accident.
4. If flights are conducted without ensuring an ice-free airframe, there is a risk of decreased aircraft performance and of loss of control and collision with terrain.
Other findings:
1. On impact, the aircraft’s seats and cabin deformed as designed, and this deformation partially attenuated the impact forces.
Final Report:

Crash of a Fokker 50 in Aweil

Date & Time: Nov 15, 2012 at 1700 LT
Type of aircraft:
Operator:
Registration:
5Y-CAN
Survivors:
Yes
Schedule:
Khartoum - Aweil
MSN:
20175
YOM:
1990
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
53
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After touchdown at Aweil Airport, the left main gear collapsed. The aircraft veered off runway to the left, slid on soft ground for few dozen metres before coming to rest in bushes with its left wing torn off. There was no fire. All 57 occupants evacuated safely, only one passenger suffered minor injuries. The aircraft was damaged beyond repair. The plane was contracted by the International Organization for Migration (IOM) and the Government of South Sudan to airlift South Sudanese refugees back to Aweil.

Crash of a Cessna 525B Citation CJ3 in São Paulo

Date & Time: Nov 11, 2012 at 1721 LT
Type of aircraft:
Operator:
Registration:
PR-MRG
Survivors:
Yes
Schedule:
Florianópolis – São Paulo
MSN:
525B-0187
YOM:
2008
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4048
Captain / Total hours on type:
521.00
Copilot / Total flying hours:
648
Copilot / Total hours on type:
189
Circumstances:
Following an uneventful flight from Florianópolis, the crew started the approach to São Paulo-Congonhas Airport Runway 35R. After touchdown, the airplane was unable to stop within the remaining distance. It overran, went down an embankment and came to rest against a fence, broken in two. The passenger and the copilot were slightly injured and captain was seriously injured. The aircraft was destroyed.
Probable cause:
The following findings were identified:
- The commander was overconfident in himself and the aircraft which led him to lose the critical capacity to discern the risks involved in the procedure that was adopting. Corroborating was the fact that the pilot judged he had much knowledge in this operation and knew exactly how the aircraft responded. It can be inferred there was complacency by the copilot on the actions of the commander, during the approach at high speed, because even feeling uncomfortable, he did not make an incisive interference because he believed in the idea that the commander had done this kind of approach, with high speed, and so knowing what he was doing.
- The pilot failed to identify the location of touch down during landing and not knowing how much runway was remaining, he decided he should not rush, thus demonstrating low situational awareness and lack of awareness, impacting the proper reaction time for the situation (Rush), which was not performed , leading the occurrence in question.
- The crew failed to properly assess the information available like speed and the runway length for the realization of a safe landing, which led to a poor judgment of the situation at hand, making the decision not to adopt the missed approach procedure.
- The distance between the crew, caused unconsciously by the commander's position with excess knowledge in the operation and the aircraft, and the insecurity of the copilot in considering new and inexperienced, resulted in a lack of assertiveness of the copilot to inform, with little emphasis, the commander of his perception of excessive airspeed.
- The crew did not adopt good crew resource management, failing to communicate with assertiveness and share critical information in time prior to landing, allowing the speeding remained present until the touchdown.
- Despite having adequate experience and training, the commander did not use the resources available, such as speed brakes to reduce the aircraft approach speed.
- The variable wind direction and predominantly tail intensity equal to or greater than 10 knots, allowed excessive speed during landing.
- The crew did not adopt good crew resource management, allowing the high speed to remain present until the touchdown.
- The commander thought he would be able to perform the approach and landing with the speed above the expected.
Final Report:

Crash of a Piper PA-31T2 Cheyenne II XL in Curitiba: 4 killed

Date & Time: Nov 6, 2012 at 1725 LT
Type of aircraft:
Operator:
Registration:
PT-MFW
Survivors:
No
Schedule:
Dourados – Curitiba
MSN:
31-8166067
YOM:
1981
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
11088
Captain / Total hours on type:
618.00
Copilot / Total flying hours:
771
Copilot / Total hours on type:
16
Circumstances:
The twin engine aircraft departed Dourados-Francisco de Matos Pereira Airport on an on-demand flight to Curitiba, carrying two passengers, two pilots and a load consisting of valuables. On final approach to Curitiba-Bacacheri Airport, both engines failed simultaneously. The crew attempted an emergency landing when the aircraft crashed in a field and came to rest near trees. A passenger was seriously injured while three other occupants were killed. The following day, the only survivor died from his injuries.
Probable cause:
The following findings were identified:
- Fatigue is likely to have occurred, since there are reports of high workload, capable of affecting the perception, judgment, and decision making of the crew.
- In view of the fact that the captain displayed an attitude of gratefulness toward the company which hired him, working for consecutive hours and many times more than was prescribed for his daily routine, it is possible that such high motivation may have been present in the accident flight, harming his capacity to evaluate the conditions required for a safe flight.
- The crew neither gathered nor properly evaluated the available pieces of information for the correct refueling of the aircraft, something that led to their decision of not refueling the aircraft in SBDO.
- The company crews did not usually keep fuel records, and made approximate calculations based on the fuel remaining from previous flights, whose control parameters were not dependable. Such attitudes reflected a work-group culture that became apparent in this accident.
- The pilots were presumably undergoing a condition of stress on account of the company flight routine, in which they flew every day, with little time dedicated to rest or even holidays. Under such condition, the pilots may have had their cognitive processes affected, weakening their performance in flight.
- The flights had the objective of transporting valuables, causing concern in relation to security issues involving the aircraft on the ground. Thus, it is suspected that decisions made by the pilots may have been affected by this complexity, such as, for example, deciding not to refuel the aircraft on certain locations.
- The way the work was structured in the company was giving rise to overload due to the routine of many flights and few periods of rest or holidays. This situation may have affected the crew’s performance, interfering in the analysis of the conditions necessary for a safe flight.
- The company did not monitor the performance of its pilots for the identification of contingent deviations from standard procedures, such as non-compliance with the MGO.
- Failures in the application of operational norms, as well as in the communication between the crew members, may have occurred on account of inadequate management of tasks by each individual, such as, for example, the use of the checklist and the filling out of control forms relative to fuel consumption contained in the company MGO.
- The crew judged that the amount of fuel existing in the aircraft was sufficient for the flight in question.
- The fact that the fuel gauges were not indicating the correct quantity of fuel had direct influence on the flight outcome, since the planning factors and the pilots’ situational awareness were affected.
- The crew did not analyze appropriately the amount of fuel necessary for the flight leg between SBDO and SBBI. The Mission Order did not establish the minimum amount of fuel necessary for the flight legs, and the crew had to take responsibility for the decision.
- The company was not rigorous with the filling out of aircraft logbooks and cargo manifestos, resulting that it did not have control over the operational procedures performed by the crews, and this may have contributed to the aircraft taking off with an amount of fuel that was insufficient for the flight. Although the MGO had parameters established for calculating the endurance necessary for VFR/IFR flights, the company did not define the fuel necessary in the Mission Orders, transferring the responsibility for the decision to the aircraft captain.
Final Report:

Crash of an Antonov AN-12BP near Khartoum: 15 killed

Date & Time: Oct 7, 2012 at 1200 LT
Type of aircraft:
Operator:
Registration:
ST-ARV
Flight Phase:
Survivors:
Yes
Site:
Schedule:
Khartoum - Al Fashir
MSN:
7 34 53 10
YOM:
1967
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
16
Pax fatalities:
Other fatalities:
Total fatalities:
15
Circumstances:
The four engine aircraft was performing a flight from Khartoum to Al Fashir with 16 passengers and a crew of six on behalf of the Sudanese National Army. Few minutes after he departed Khartoum-Haj Yusuf Airport, the crew informed ATC about an engine failure and was cleared to return. Few seconds later, a second engine failed on the same side and the crew attempted to make an emergency landing. The aircraft crashed in a desert area located about 22 km from Khartoum Airport. The aircraft disintegrated on impact. 13 occupants were killed while nine other were seriously injured. Few days later, two passengers died from their injuries.
Probable cause:
Double engine failure for unknown reasons.

Crash of a De Havilland DHC-2 Beaver in Big River Lake

Date & Time: Aug 25, 2012 at 0800 LT
Type of aircraft:
Operator:
Registration:
N314HA
Survivors:
Yes
Schedule:
Soldotna - Big River Lake
MSN:
868
YOM:
1956
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1500
Captain / Total hours on type:
725.00
Aircraft flight hours:
20174
Circumstances:
The pilot of a float-equipped airplane was landing at a remote lake. The pilot stated that he was on a left base leg turning onto a short final approach when the left float struck the ground. The airplane sustained substantial damage to the wings and fuselage. The pilot indicated there were no preaccident mechanical malfunctions or anomalies that would have precluded normal operation. Accident occurred in Big River Lake, in the Kenai region.
Probable cause:
The pilot’s failure to maintain adequate ground clearance during his landing approach, which resulted in a collision with terrain.
Final Report:

Crash of an Embraer EMB-505 Phenom 300 in Altenrhein

Date & Time: Aug 6, 2012 at 1540 LT
Type of aircraft:
Operator:
Registration:
CN-MBR
Survivors:
Yes
Schedule:
Geneva - Altenrhein
MSN:
505-00025
YOM:
2011
Flight number:
DLI211
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7025
Captain / Total hours on type:
75.00
Copilot / Total flying hours:
5854
Copilot / Total hours on type:
465
Aircraft flight hours:
510
Circumstances:
On 6 August 2012 the Embraer EMB-505 Phenom 300 aircraft, registration CN-MBR, took off at 12:59 UTC from Geneva (LSGG) on a commercial flight to St. Gallen-Altenrhein (LSZR). After the initial call to the aerodrome control centre St. Gallen tower, the crew quickly decided, after an enquiry from the air traffic controller, on a direct approach on the runway 10 instrument landing system (ILS). Shortly thereafter, the landing gear and flaps were extended. The flaps jammed at approximately 10 degrees and the FLAP FAIL warning message was displayed. The crew carried out a go-around shortly before landing. The landing gear subsequently remained extended. The flaps remained jammed for the remainder of the flight. The crew decided immediately on a second ILS approach with jammed flaps, which according to the manufacturer's information required an increased approach speed. During the approach, the crew had difficulty in reducing the airspeed to this increased approach speed. At 13:40 UTC, the aircraft subsequently touched down on the wet runway at an indicated air speed of 136 kt, approximately 290 m after the runway threshold, and could not be brought to a standstill on the remaining length of runway. The aircraft then rolled over the end of runway 10, broke through the aerodrome perimeter fence and overrun the road named Rheinholzweg running perpendicular to the runway centreline, on which a public transport bus was travelling. The aircraft rolled very close behind the bus and came to a standstill in a maize field, approximately 30 m from the end of the runway. The female passenger and the two pilots were not injured in the accident. The aircraft was badly damaged. There was crop damage and damage to the aerodrome perimeter fence.
Probable cause:
The accident is attributable to the fact that the aircraft touched down late and at an excessively high speed on the wet runway after an unstabilized final approach and consequently rolled over the end of the runway.
The following factors contributed to the accident:
- The insufficient teamwork and deficient situation analysis by the crew.
- The flaps remained jammed at approximately 10 degrees, a position that is almost consistent with the flaps 1 position.
- Late initiation of full brake application after landing.
Final Report: