Crash of a Boeing 737-524 in Usinsk

Date & Time: Feb 9, 2020 at 1227 LT
Type of aircraft:
Operator:
Registration:
VQ-BPS
Survivors:
Yes
Schedule:
Moscow - Usinsk
MSN:
28909/2960
YOM:
1997
Flight number:
UT595
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
94
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
17852
Captain / Total hours on type:
7672.00
Copilot / Total flying hours:
6595
Copilot / Total hours on type:
4989
Aircraft flight hours:
57410
Aircraft flight cycles:
29162
Circumstances:
Following an uneventful flight from Moscow-Vnukovo Airport, the crew initiated the descent to Usinsk Airport Runway 13. On short final, the aircraft hit a snow bank (1,1 metre high) located 32 metres short of runway threshold, still on the concrete zone. Upon impact, both main gears were torn off and the airplane belly landed and slid for few hundred metres before coming to rest. All 100 occupants evacuated safely and the aircraft was damaged beyond repair.
Probable cause:
The accident with the Boeing 737-500 VQ-BPS aircraft occurred during the landing as a result of a collision of the aircraft with a snow parapet 1.1 m high at a distance of 32 m to the runway threshold (within the paved section of the runway), which resulted in damage to the main landing gear and their subsequent "folding" in the process of moving along the runway.
The accident was caused by a combination of the following factors:
- the presence of contradictions in the Federal Aviation Rules for flights in the airspace of the Russian Federation, the airline's radio control system and the aircraft operational documentation regarding the need and procedure for introducing temperature corrections to the readings of barometric altimeters at low ambient temperatures;
- Failure by the operator of the Usinsk aerodrome to comply with the FAP-262 requirements for the maintenance of the aerodrome, which resulted in the presence of snow parapets on the paved section of the landing strip;
- the operator of the Usinsk aerodrome did not eliminate the shortcomings in the winter maintenance of the aerodrome, noted based on the results of the inspection by the Rosaviatsia commission on January 22, 2020;
- lack of risk assessment in the airline associated with the execution of approaches in the baro-VNAV mode in the presence of factors that impede such approaches (low ambient temperatures, snow-covered underlying surface, drifting snow (snowstorm), significant changes in the relief in front of the runway end, lack of PAPI-type lights), as well as appropriate recommendations to the crews on the specifics of such approaches, including after the transition to visual flight, and crew training;
- insufficient assessment by the crew during the preparation of the existing threats (hazard factors) and making an insufficiently substantiated decision to perform an RNAV (GNSS) approach (under the control of the autopilot in LNAV/VNAV mode) without introducing a correction for low outside air temperature in altitude overflying waypoints, which led to a flight below the established glide path;
- performing a flight along the "extended glide path" after turning off the autopilot and switching to manual piloting without attempting to enter the set glide path;
- the PIC may have had a visual illusion of a "high glide path" due to a snow-covered underlying surface, a snowstorm and the presence of a ravine directly in front of the runway end in the absence of PAPI type lights, which led to an incorrect assessment of the aircraft's flight altitude after switching to manual piloting, lack of reaction to timely and correct warnings of the co-pilot and exit to the runway end at a height significantly less than the established one.
Final Report:

Crash of a Being 737-86J in Istanbul: 3 killed

Date & Time: Feb 5, 2020 at 1820 LT
Type of aircraft:
Operator:
Registration:
TC-IZK
Survivors:
Yes
Schedule:
Izmir - Istanbul
MSN:
37742
YOM:
2009
Flight number:
PC2193
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
177
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
Following an uneventful flight from Izmir-Adnan Menderes Airport, the crew initiated the approach to Istanbul-Sabiha Gökçen Airport runway 06. Weather conditions were poor with thunderstorm activity, rain, CB's and a wind from 290 gusting to 37 knots. After touchdown on a wet runway, the airplane was unable to stop within the remaining distance. It overran, turned slightly to the left then went down an embankment (25 meters high) and came to rest, broken in three. Three passengers were killed while all 180 other occupants were evacuated to local hospitals. It is understood that the airplane apparently landed 1,500 meters past the runway threshold (runway 06 is 3,000 meters long) with a non negligible tailwind component that must be confirmed.

Crash of a Beechcraft B60 Duke in Big Spring

Date & Time: Jan 29, 2020 at 1710 LT
Type of aircraft:
Operator:
Registration:
N50JR
Flight Type:
Survivors:
Yes
Schedule:
Abilene – Midland
MSN:
P-303
YOM:
1974
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
25000
Captain / Total hours on type:
7.00
Circumstances:
The pilot was conducting a cross-country flight at a cruise altitude of 10,500 ft mean sea level when the left engine lost all power. He secured the engine and elected to continue to his destination. Shortly thereafter, the right engine lost all power. After selecting an airport for a forced landing, he overflew the runway and entered the pattern. The pilot stated that on short final, after extending the landing gear, "the plane quit flying and the airspeed went to nothing." The airplane landed 200 to 300 yards short of the runway threshold, resulting in substantial damage to the wings and fuselage. During a postaccident examination, only tablespoons of fuel were drained from the left tank. Due to the position of the airplane, the right tank could not be drained; however, when power was applied to the airplane, both fuel quantity gauges indicated empty fuel tanks. Neither fuel tank was breached during the accident, and there was no discoloration present on either of the wings or engine nacelles to indicate a fuel leak; therefore, the loss of engine power is consistent with fuel exhaustion.
Probable cause:
A total loss of engine power in both engines due to fuel exhaustion, which resulted in a landing short of the runway.
Final Report:

Crash of a McDonnell Douglas MD-83 in Bandar-e Mahshahr

Date & Time: Jan 27, 2020 at 0736 LT
Type of aircraft:
Operator:
Registration:
EP-CPZ
Survivors:
Yes
Schedule:
Tehran - Bandar-e Mahshahr
MSN:
53464
YOM:
1994
Flight number:
RV6936
Country:
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
136
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
18430
Captain / Total hours on type:
7840.00
Copilot / Total flying hours:
300
Copilot / Total hours on type:
124
Circumstances:
On Jan. 27, 2020, at 03:12 UTC Caspian Airlines (CPN) Flight 6936, an MD83, EP-CPZ took off from Mehrabad International Airport and climbed to FL320 as final cruising level. At about 03:45:37 UTC, the aircraft was flying according to the flight plan route on Airway B417 at an assigned FL320. Due to another traffic departing flight, an A320, IRA356 from Abadan Airport (OIAA) to destination Mashhad International Airport (OIMM), the ACC controller issued direct routing to the flight CPN 6936 position GODMO. At 03:49:34 UTC, CPN6936 requested descent clearance, so the flight was cleared to FL100. At 03:52:30 UTC, the pilot called Mahshahr AFISO and reported position 50 nm inbound GODMO and estimated time over GODMO at 03:59 UTC. At 03:52:51 UTC, Mahshahr AFISO reported necessary information as below: "RWY active is 31; wind is now 280/08kts, CAVOK, temperature +06, DP 04 and QNH 1023, expected VOR approach RWY 31 via GODMO 1E ARRIVAL" At 03:53: 33 UTC, the pilot requested RWY 13 and Mahshahr AFISO performed VOR/DME approach RWY 13, via GODMO 1F arrival. At 03:59:39 UTC, the pilot reported, “we are approaching position GODMO in contact with destination Mahshahr.” At 04:00:41UTC, the pilot reported his position “GODMO” to Mahshahr AFISO. At 04:02:46 UTC, the pilot reported leaving of IAF and received landing clearance for RWY13. Finally, at 04:06:11 UTC, the aircraft landed on RWY 13, passed two-thirds of RWY length and ran off the end of runway13 after landing at Mahshahr Airport at 04:06 UTC, Khuzestan province. The accident flight was being operated on an Instrument Flight Rules (IFR) flight plan in a Visual Meteorological Condition (VMC). The main door of the accident aircraft was opened in emergency condition, but the slide skid did not operate automatically. The cabin floor was just too close to the ground (grass surface) due to the impact of the nose and main landing gears strut which were broken after the runway overrun. The evacuation was performed from the main door, and all 136 passengers and 8 crew members disembarked.
Probable cause:
The Aircraft Accident Investigation Board determines that the probable causes of this accident were the pilots’ failures below, resulting in a runway overrun:
- Poor decision-making for acceptance of the risk of high-speed landing;
- Un-stabilized approach against the normal flight profile;
- Poor CRM in the cockpit; and
- Poor judgment and not accomplishing go-around while performing an unstabilized approach.

Contributing Factors:
- Loading of 5 tons of extra fuel, which increased the landing distance required.
- Decision to make a landing on RWY 13 with tailwind.
- Inability of the copilot (PM) to take control of the aircraft and proper action to execute goaround.
Final Report:

Crash of a Stinson V-77 Reliant in Auburn: 2 killed

Date & Time: Jan 24, 2020 at 0956 LT
Type of aircraft:
Registration:
N50249
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Auburn - Auburn
MSN:
77-458
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
650
Circumstances:
The pilot departed on a local flight with two passengers. Several witnesses reported that they heard the airplane’s engine backfiring and sputtering and subsequently heard the engine quit. The surviving passenger, who was seated in the front right seat, stated that the engine lost power and there was nowhere to land. The airplane subsequently impacted heavily wooded terrain about 1 mile from the departure airport. Postaccident examination of the engine revealed that the No. 7 cylinder intake valve was stuck open. The No. 2 cylinder front spark plug was defective, and the Nos. 2- and 4-cylinders’ ignition wires were frayed, worn, and displayed arcing, which likely led to erratic operation or a lack of ignition in these two cylinders. The culmination of these issues most likely led to the engine running rough, backfiring, and subsequently losing total power. An annual inspection was accomplished on the airframe and engine about 2 months before the
accident. General maintenance practices and the inspection should have identified the anomalies that were found during the postaccident engine examination.
Probable cause:
A total loss of engine power due to a combination of mechanical engine anomalies. Contributing to the accident was inadequate maintenance that failed to identify the engine anomalies.
Final Report:

Crash of a Lockheed C-130BZ Hercules in Goma

Date & Time: Jan 9, 2020
Type of aircraft:
Operator:
Registration:
403
Flight Type:
Survivors:
Yes
Schedule:
Beni - Goma
MSN:
3750
YOM:
1962
Location:
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
59
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The four engine airplane was completing a flight from Beni to Goma, carrying 59 South African troops and eight crew members from the 28th Squadron on behalf of the MONUSCO (Mission de l’Organisation des Nations unies pour la stabilisation en République Démocratique du Congo). The approach and landing were completed in heavy rain falls. After touchdown, the airplane veered off runway to the left and came to rest in a grassy area with the left wing broken in two and the n°1 engine on fire. All 67 occupants escaped uninjured and the fire was quickly contained. However, the aircraft seems to be damaged beyond repair.

Crash of an Antonov AN-12A in Geneina: 18 killed

Date & Time: Jan 2, 2020
Type of aircraft:
Operator:
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Geneina - Khartoum
MSN:
2340606
YOM:
1962
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
11
Pax fatalities:
Other fatalities:
Total fatalities:
18
Circumstances:
Shortly after takeoff from Geneina Airport, the four engine aircraft went out of control and crashed in flames about 5 km from the airport. The aircraft was destroyed by impact forces and a post crash fire and all 18 occupants were killed, among them three children. The aircraft was returning to Khartoum after delivering medical aid.

Crash of a Let L-410UVP-E10 in Kamina

Date & Time: Dec 28, 2019 at 1434 LT
Type of aircraft:
Operator:
Registration:
9S-GDX
Survivors:
Yes
Schedule:
Lubumbashi – Kamina
YOM:
1987
Location:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
16
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After touchdown on a wet earth runway, the airplane went out of control. It veered off runway to the right, struck a shoulder and lost its nose gear before coming to rest. All 18 occupants escaped uninjured while the airplane was substantially damaged.

Crash of a Fokker 100 in Almaty: 12 killed

Date & Time: Dec 27, 2019 at 0721 LT
Type of aircraft:
Operator:
Registration:
UP-F1007
Flight Phase:
Survivors:
Yes
Schedule:
Almaty – Nursultan
MSN:
11496
YOM:
1996
Flight number:
Z92100
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
93
Pax fatalities:
Other fatalities:
Total fatalities:
12
Captain / Total flying hours:
20141
Captain / Total hours on type:
3956.00
Copilot / Total flying hours:
11544
Copilot / Total hours on type:
4144
Aircraft flight hours:
44632
Aircraft flight cycles:
52771
Circumstances:
The Fokker 100 departed Almaty Airport on a regular schedule service (flight Z92100) to Astana-Nursultan Nazarbayev Airport, carrying 93 passengers and a crew of five. During the takeoff roll on runway 05R with flaps at zero, after a course of 36 seconds and at a speed of 148 knots, the crew started the rotation. Immediately after liftoff, the airplane rolled to the right at an angle of 5° then to the left at an angle of 19° without an increase of the indicated airspeed. After reaching the height of 20 feet in a pitch angle of 14°, the airplane started to descend then hit the runway surface with the base of the tail. It landed on its main landing gear and rolled for about 15 seconds with the nose gear still in the air. The airplane took off again at a speed of 138 knots then the crew retracted the landing gear. In a pitch angle of 19°, the airplane lost speed (130 knots), veered to the right, belly landed and slid for about 850 metres, went through a fence and eventually crashed into a house located near the perimeter fence, some 80 metres to the right of the extended center line. 47 occupants were injured, 39 escaped unhurt and 12 others were killed, among them the captain. The aircraft was destroyed. There was not fire.
Probable cause:
The accident was the consequence of an asymmetrical loss of wing lift properties at the stage of takeoff, which resulted in the aircraft crashing down immediately after leaving the runway and rolling to the right on the snowy ground, breaching the airport perimeter fence and colliding with a two-story private building located 9-10 m from the fence. As a result of collision, 11 passengers and one crew member died and 47 passengers received different injuries because of overloading, striking, destruction and crushing of the aircraft structure. The cause of the loss of wing lift properties was most likely the effect of ground icing.
Contributing factors:
- The crew, after analyzing the actual meteorological situation at Almaty airport, may not have drawn sufficient conclusions to better inspect the entire aircraft and especially (tactile method) the leading edge of the wing;
- The Flight Safety Management System (FMS) of Beck Air JSC contains mainly only general provisions and specific actions that were not adapted for implementation, which did not allow timely identification and elimination of existing risks affecting flight safety.
- Collision of the aircraft with a two-storey private structure, which affected the severity of the consequences.
Final Report:

Crash of a Beechcraft A100 King Air in Charallave: 9 killed

Date & Time: Dec 19, 2019
Type of aircraft:
Operator:
Registration:
YV1104
Flight Type:
Survivors:
No
Schedule:
Guasipati – Charallave
MSN:
B-231
YOM:
1977
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
On final approach to Charallave-Óscar Machado Zuloaga Airport in marginal weather conditions, the twin engine airplane crashed in unknown circumstances about 8 km from the runway threshold. The aircraft was destroyed and all nine occupants were killed.