Crash of an Antonov AN-26 at Hmeimim AFB: 39 killed

Date & Time: Mar 6, 2018 at 1451 LT
Type of aircraft:
Operator:
Registration:
RF-92955
Flight Type:
Survivors:
No
Schedule:
Kuweires – Hmeimim
MSN:
101 07
YOM:
1980
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
33
Pax fatalities:
Other fatalities:
Total fatalities:
39
Circumstances:
The airplane departed Kuweires-Rasin El Aboud Airbase on a flight to Hmeimim AFB, carrying 33 passengers and a crew of six. On final approach, the aircraft went out of control and crashed about 500 metres short of runway, bursting into flames. There were no survivors among the 39 occupants. The airplane was registered RF-92955 (52 red). It is believed that the loss of control that occurred on short final was the result of low level windshear.

Crash of a Boeing 737-322 in Lubumbashi

Date & Time: Mar 4, 2018 at 1201 LT
Type of aircraft:
Operator:
Registration:
9S-ASG
Flight Type:
Survivors:
Yes
Schedule:
Kinshasa – Lubumbashi
MSN:
24378/1704
YOM:
1989
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
18700
Captain / Total hours on type:
1100.00
Copilot / Total flying hours:
7400
Copilot / Total hours on type:
710
Aircraft flight hours:
61721
Aircraft flight cycles:
36555
Circumstances:
The airplane departed Kinshasa-N'Djili Airport on a cargo flight to Lubumbashi, carrying five crew members and one passenger. Following an uneventful flight, the crew was cleared to descend and to land at Lubumbashi-Luano Airport. After landing on runway 07, the crew started the braking procedure. At a speed of 80 knots, the aircraft deviated to the left. It veered off runway and while contacting soft ground, the nose gear collapsed. The airplane came to rest in a grassy area along the left shoulder of the runway after a course of about 200 metres. All six occupants evacuated safely and the aircraft was damaged beyond repair.
Probable cause:
The following factors were identified:
- Reduction of simulator training hours for economic reasons for someone who has never performed the duties of controlling an aircraft on the ground.
- The runway shoulders at Lubumbashi (Luano) do not have the same characteristics with regard to strength (see Annex 14 and Document 9157 Part 3).
In conclusion, the actions taken on the rudder before it became ineffective must have been the cause of the aircraft's deviation from the runway centreline and the loss of control of the aircraft (LOC-G).
Final Report:

Crash of an Airbus A320-214 in Tallinn

Date & Time: Feb 28, 2018 at 1711 LT
Type of aircraft:
Operator:
Registration:
ES-SAN
Flight Type:
Survivors:
Yes
Schedule:
Tallinn - Tallinn
MSN:
1213
YOM:
2000
Flight number:
MYX9001
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
228
Captain / Total hours on type:
0.00
Copilot / Total flying hours:
24046
Copilot / Total hours on type:
40
Aircraft flight hours:
44997
Aircraft flight cycles:
21839
Circumstances:
On 28th February 2018 at 10:021, the Smartlynx Airlines Estonia Airbus A320-214 registered ES-SAN took off from Tallinn airport Estonia to perform training flights with 2 crew members (captain and safety pilot), 4 students and 1 ECAA inspector on board. Following several successful ILS approaches and touch-and-go cycles, at 15:04, after a successful touch down with the runway, the aircraft did not respond as expected to sidestick inputs when reaching rotation speed. After a brief lift-off, the aircraft lost altitude and hit the ground close to the end of the runway. In the impact, the aircraft engines impacted the runway and the landing gear doors were damaged. After the initial impact, the aircraft climbed to 1590 ft from ground level and pitched down again. The pilots were able to stabilize the flight path by using manual pitch trim and engine thrust and make a U-turn back towards the runway. The crew declared an emergency and the aircraft was cleared for an emergency landing. During the approach, the aircraft lost power in both engines. The aircraft landed 150 m before the threshold of runway at 15:11. On landing, aircraft tires burst, and the aircraft veered off the runway and finally came to a stop 15 m left to the runway. The safety pilot and one of the students suffered minor impact trauma in this accident. The aircraft landing gear doors, landing gears, both engine nacelles, engines and aircraft fuselage suffered severe damage in this accident resulting in aircraft hull loss.
Probable cause:
Causal factors:
This accident results from the combination of the following factors:
• The intermittent THSA override mechanism malfunction allowing to cause the loss of pitch control by both ELACs. The repetitive triggering of the ELAC PITCH faults was caused by the non or late activations of the PTA micro-switches, which were due to the OVM piston insufficient stroke. The insufficient OVM stroke was caused by the THSA OVM clutch unit non-standard friction. The oil in the THSA OVM casing appeared to be with a higher viscosity than defined in the CMM. The higher viscosity might have reduced the friction of the OVM clutch unit, causing the THSA OVM nonstandard friction.
• SEC design flaw allowing for a single event, the left landing gear temporary dedecompression, to cause the loss of pitch control by both SECs. The absence of ground spoilers arming for landing in the context of touch and go's training may have contributed to the temporary decompression of the left main landing gear.
• The training instructor`s decision for continuation of the flight despite repetitive ELAC PITCH FAULT ECAM caution messages. The lack of clear framework of operational rules for training flights, especially concerning the application of the MEL, and the specific nature of operations that caused pressure to complete the training program may have impacted the crew decision-making process.

Contributory factors
• Smartlynx Estonia ATO TM does not clearly define the need for arming spoilers when performing touch-and-go training (ATO procedures not in accordance with Airbus SOP). The fact that there is no clear reference in the Smartlynx Estonia ATO TM Touch-And-Go air exercise section to additional procedures that should be used, in combination with lack of understanding of the importance for arming the spoilers during this type of flights contributed to TRI making a decision to disarm the spoilers during touch and go training enabling landing gear bounce on touch down.
• At the time of the event Airbus QRH did not define the maximum allowed number of resets for the flight control computers.
• At the time of the event Airbus FCTM did not require to consider MEL on touch-and-go and stop-and-go training.
• The oil in the THS OVM casing was with higher viscosity than defined in the CMM. The higher viscosity might have reduced the friction of the OVM clutch unit.
• The aircraft maintenance documentation does not require any test of the OVM during aircraft regular maintenance checks.
• Smartlynx Estonia ATO OM does not clearly specify the role in the cockpit for the Safety Pilot. The lack of task sharing during the event caused the ECAM warnings to be left unnoticed and unannounced for a long period.
• The crew not resetting the ELAC 1. The fact that ELAC 1 PITCH FAULT was left unreset lead to the degradation of the redundancy of the system. Considering the remoteness of the loss control of both elevators, there is no specific crew training for MECHANICAL BACKUP in pitch during approach, landing and take-off. This condition of the aircraft occurred for the crew in a sudden manner on rotation and during training flight, where the experienced TRI is not in PF role and cannot get immediate feedback of the aircraft behaviour and condition. Despite these difficult conditions the crew managed to stabilize and land the aircraft with no major damage to the persons on board. The crew performance factors that contributed to the safe landing of the aircraft are the following:
• The TRI followed the golden rule of airmanship (fly, navigate, communicate), by stabilizing the aircraft pitch by using the trim wheel and by keeping the aircraft engine power as long as possible;
• The Safety Pilot started to play a role in the cockpit by assisting the TRI and student by informing them about the status of the aircraft and later on taking the role of the PM.
Final Report:

Crash of a Quest Kodiak 100 off Georgetown: 2 killed

Date & Time: Feb 27, 2018 at 1925 LT
Type of aircraft:
Registration:
N969TB
Flight Type:
Survivors:
No
Schedule:
Welaka - Welaka
MSN:
100-0173
YOM:
2016
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
3400
Aircraft flight hours:
68
Circumstances:
The private pilot and pilot-rated passenger were returning to the airport in night visual meteorological conditions with a cloud ceiling about 1,500 ft above ground level. Radar data indicated that the airplane overflew the airport and completed a 360° descending right turn and overflew the airport again before entering an approximate 180° left climbing turn toward and over an unlighted area within a denselywooded national forest. The airplane continued the left turn and entered a descent to impact in a river about 1 mile from the airport. All major components of the airplane were recovered from the river except the outboard section of the left wing and the left aileron. An examination of the airframe and engine revealed no mechanical malfunctions or failures that would have precluded normal operation. Because each of the two pilots onboard would have been capable of safely landing the airplane, it is unlikely that an acute event from either occupant's heart disease contributed to the accident. The night conditions, which included overcast clouds that would have obscured the nearly full moon, and the pilots' maneuvering for landing over an area devoid of cultural lighting provided conditions conducive to the development of spatial disorientation. It is likely that the pilots experienced a "black hole" illusion while maneuvering to align with the runway for landing, which resulted in an uncontrolled descent and impact with water.
Probable cause:
The pilots' spatial disorientation while maneuvering for landing in night conditions over unlighted terrain, which resulted in an uncontrolled descent and impact with water.
Final Report:

Crash of a Socata TBM-700 in Evanston: 2 killed

Date & Time: Feb 18, 2018 at 1505 LT
Type of aircraft:
Registration:
N700VX
Flight Type:
Survivors:
No
Schedule:
Tulsa – Evanston
MSN:
118
YOM:
1997
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
4154
Captain / Total hours on type:
100.00
Aircraft flight hours:
3966
Circumstances:
The commercial pilot was conducting an instrument approach following a 3.5-hour cross-country instrument flight rules (IFR) flight in a single-engine turboprop airplane. About 1.6 miles from the runway threshold, the airplane began a climb consistent with the published missed approach procedure; however, rather than completing the slight left climbing turn toward the designated holding point, the airplane continued in an approximate 270° left turn, during which the airplane's altitude varied, before entering a descending right turn and impacting terrain. Tree and ground impact signatures were consistent with a 60° nose-low attitude at the time of impact. No distress calls were received or recorded from the accident flight. A postimpact fire consumed a majority of the cockpit and fuselage. Weather information for the time of the accident revealed that the pilot was operating in IFR to low IFR conditions with gusting surface winds, light to heavy snow, mist, cloud ceilings between 700 and 1,400 ft above ground level with clouds extending through 18,500 ft, and the potential for low-level wind shear and clear air turbulence. The area of the accident site was under AIRMETs for IFR conditions, mountain obscuration, moderate icing below 20,000 ft, and moderate turbulence below 18,000 ft. In addition, a winter storm warning was issued about 6 hours before the flight departed. Although the pilot received a weather briefing about 17 hours before the accident, there was no indication that he obtained updated weather information before departure or during the accident flight. Examination of the airframe and engine did not reveal any preimpact anomalies that would have precluded normal operation; however, the extent of the fire damage precluded examination of the avionics system. The airplane was equipped with standby flight instruments. An acquaintance of the pilot reported that the pilot had experienced an avionics malfunction several months before the accident during which the airplane's flight display went blank while flying an instrument approach. During that occurrence, the pilot used ForeFlight on his iPad to maneuver back to the northeast and fly the approach again using his own navigation. During the accident flight, the airplane appeared to go missed approach, but rather than fly the published missed approach procedure, the airplane also turned left towards to northeast. However, it could not be determined if the pilot's actions were an attempt to fly the approach using his own navigation or if he was experiencing spatial disorientation. The restricted visibility and turbulence present at the time of the accident provided conditions conducive to the development of spatial disorientation. Additionally, the airplane's turning flight track and steep descent profile are consistent with the known effects of spatial disorientation.
Probable cause:
The pilot's loss of control due to spatial disorientation.
Final Report:

Crash of a Gulfstream G200 in Abuja

Date & Time: Jan 29, 2018 at 1520 LT
Type of aircraft:
Operator:
Registration:
5N-BTF
Survivors:
Yes
Schedule:
Lagos - Abuja
MSN:
180
YOM:
2007
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5300
Captain / Total hours on type:
280.00
Copilot / Total flying hours:
5700
Copilot / Total hours on type:
93
Aircraft flight hours:
1421
Aircraft flight cycles:
921
Circumstances:
On 25th January 2018 at 14:28 h, a Gulfstream 200 (G200) aircraft with nationality and registration marks 5N-BTF operated by Nestoil Plc, departed Murtala Mohammed International Airport, Lagos (DNMM) as a charter flight to Nnamdi Azikiwe International Airport, Abuja (DNAA) on an Instrument Flight Rules (IFR) flight plan. Onboard were four passengers and three flight crew members. The Pilot in command (PIC) was the Pilot Monitoring (PM) and the Co-pilot was the Pilot Flying (PF). The departure, cruise and approach to Nnamdi Azikiwe International Airport were normal. At 14:45 h, 5N-BTF contacted Abuja radar and was subsequently cleared for Radar vectors ILS approach Runway 22. Abuja Airport Automatic Terminal Information Service (ATIS) Papa for time 14:20 h was monitored as follows; “Main landing runway 22, wind 110/07 kt, Visibility 3,500 m in Haze, No Significant Clouds, Temperature/Dew point 33/- 01°C, QNH 1010 hPa, Trend No Significant Change, End of Information Papa”. At 15:17 h, 5N-BTF reported 4 NM on Instrument approach (ILS) and was requested to report 2 NM because there was a preceding aircraft (Gulfstream 5) on landing roll. Thereafter, 5N-BTF was cleared to land runway 22 with reported wind of 070°/07 kt. At 15:18 h, the aircraft touched down slightly left of the runway centre line. According to the PF, in the process of controlling the aircraft to the centre line, the aircraft skidded left and right and eventually went partly off the runway to the right where it came to a stop. In his report, the PM stated that on touchdown, he noticed the aircraft oscillating left and right as brakes were applied. The oscillation continued to increase and [the aircraft] eventually went off the runway to the right where the aircraft came to a stop, partially on the runway. During the post-crash inspection, the investigation determined that the skid marks on the runway indicated that the aircraft steered in an S-pattern continuously with increasing amplitude, down the runway. On the last right turn, the aircraft exited the right shoulderof the runway, the right main wheel went into the grass and on the final left turn, the right main landing gear strut detached from its main attachment point after which the aircraft finally came to a complete stop on a magnetic heading of 160°. The ATC immediately notified the Aircraft Rescue and Fire Fighting Services (ARFFS), Approach Radar Control, and other relevant agencies about the occurrence. All persons on board disembarked with no injuries. Instrument Meteorological Conditions (IMC) prevailed at the time of the occurrence. The serious incident occcurred in daylight.
Probable cause:
Causal Factor:
The use of improper directional control techniques to maintain the aircraft on the runway.
Contributory Factor:
Improper coordination in taking over control of the aircraft by the PM which was inconsistent with Nestoil SOP.
Final Report:

Crash of a Boeing 737-82R in Trabzon

Date & Time: Jan 13, 2018 at 2325 LT
Type of aircraft:
Operator:
Registration:
TC-CPF
Survivors:
Yes
Schedule:
Ankara – Trabzon
MSN:
40879/4267
YOM:
2012
Flight number:
PC8622
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
162
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The airplane departed Ankara-Esenboğa Airport at 2233LT bound for Trabzon. Following an uneventful flight, the crew started the approach by night to runway 11 and the landing was completed in heavy rain falls at 2325LT. After touchdown at a speed of 143 knots, the airplane rolled for about 2,400 metres then veered off runway to the left, went through a grassy area then down a steep slope. It lost its right engine and came to rest few metres above the sea. All 168 occupants evacuated safely. The right engine was sheared off and fell into the sea. According to first report, it is believed something went wrong with the right engine after touchdown (unintentional forward thrust and asymmetrical thrust).

Crash of a Cessna 525A CitationJet CJ2 in Michigan City

Date & Time: Dec 27, 2017 at 0650 LT
Type of aircraft:
Operator:
Registration:
N525KT
Flight Type:
Survivors:
Yes
Schedule:
DuPage - Michigan City
MSN:
525A-0058
YOM:
2002
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3200
Captain / Total hours on type:
300.00
Copilot / Total flying hours:
2020
Copilot / Total hours on type:
81
Aircraft flight hours:
2681
Circumstances:
The pilot reported that, during the approach following a positioning flight, he saw that the runway had a light dusting of snow on it and that the airplane touched down on speed in the first 1,000 ft of the 4,100- ft-long runway. The copilot, who was the pilot flying, applied heavy braking, but there appeared to be no braking effectiveness, and the airplane did not slow down as expected. The pilot added that, when the airplane reached about two-thirds of the way down the runway, he knew that it was going to overrun the runway due to the loss of only half of its airspeed. He thought that if he aborted the landing, there was a small chance the airplane could become airborne within the remaining runway. The copilot added engine power to abort the landing, and the nose landing gear lifted off, but insufficient runway was remaining to take off. The copilot reduced the engine power to idle, and the airplane overran the runway and went through the airport fence and a guardrail, across a highway, and into a field. Postaccident examination revealed no flat spots or evidence of skidding on the landing gear tires. The flaps were found in the “ground flaps” position, which is not allowed for takeoff. No evidence of any pre-accident mechanical malfunctions or failures were found with the airplane that would have precluded normal operation. Based on an airplane weight of 11,000 lbs, the airplane’s stopping distance would have been about 4,400
ft. The flight crew’s improper decision to land on a snow-covered runway that was too short to accommodate the landing in such conditions led to a runway overrun and impact with obstacles.
Probable cause:
The flight crew's improper decision to land on a snow-covered runway that had insufficient runway distance for the airplane to land with the contamination, which resulted in a runway overrun and impact with obstacles.
Final Report:

Crash of a Cessna 510 Citation Mustang in Sieberatsreute: 3 killed

Date & Time: Dec 14, 2017 at 1814 LT
Operator:
Registration:
OE-FWD
Survivors:
No
Schedule:
Egelsbach – Friedrichshafen
MSN:
510-0049
YOM:
2007
Flight number:
STC228B
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
2816
Captain / Total hours on type:
2000.00
Copilot / Total flying hours:
800
Copilot / Total hours on type:
140
Aircraft flight hours:
3606
Circumstances:
The airplane departed Egelsbach Airport at 1743LT on a charter flight to Friedrichshafen, carrying one passenger and two pilots. Following an uneventful flight at FL210, the crew contacted Zurich ARTCC and was cleared to start the descent and later told to expect a runway 24 ILS approach to Friedrichshafen-Bodensee Airport. After passing 4,000 feet on descent, at a speed of 240 knots, the crew was completing a last turn in clouds when the airplane entered a rapid and uncontrolled descent until it crashed in a wooded area located in Sieberatsreute, some 15 km short of runway 24. The airplane disintegrated on impact and all three occupants were killed.
Probable cause:
The aircraft accident was caused by a sudden loss of control of the aircraft in clouds while turning in for the approach to Friedrichshafen at night. Probably the frontal weather with light to moderate turbulence, snowfall and icing contributed to this. The absence of information about the events on board the aircraft meant that it was not possible to determine the causes of the loss of control.
Final Report:

Crash of a Beechcraft C90 King Air in Lake Harney: 3 killed

Date & Time: Dec 8, 2017 at 1115 LT
Type of aircraft:
Operator:
Registration:
N19LW
Flight Type:
Survivors:
No
Schedule:
Sanford - Sanford
MSN:
LJ-991
YOM:
1981
Flight number:
CONN900
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
243
Captain / Total hours on type:
0.00
Copilot / Total flying hours:
4800
Copilot / Total hours on type:
357
Aircraft flight hours:
10571
Circumstances:
The flight instructor, commercial pilot receiving instruction, and commercial pilot-rated passenger were conducting an instructional flight in the multi-engine airplane during instrument meteorological conditions. After performing a practice instrument approach, the flight was cleared for a second approach; however, the landing runway changed, and the controller vectored the airplane for an approach to the new runway. The pilot was instructed to turn to a southwesterly heading and maintain 1,600 ft until established on the localizer. Radar information revealed that the airplane turned to a southwesterly heading on a course to intercept the localizer and remained at 1,600 ft for about 1 minute 39 seconds before beginning a descending right turn to 1,400 ft. The descent continued to 1,100 ft; at which time the air traffic control controller issued a low altitude alert. Over the following 10 seconds, the airplane continued to descend at a rate in excess of 4,800 ft per minute (fpm). The controller issued a second low altitude alert to the crew with instructions to climb to 1,600 ft immediately. The pilot responded about 5 seconds later, "yeah I am sir, I am, I am." The airplane then climbed 1,400 ft over 13 seconds, resulting in a climb rate in excess of 6,700 fpm, followed by a descent to 1,400 ft over 5 seconds, resulting in a 1,500-fpm descent before radar contact was lost in the vicinity of the accident site. Radar data following the initial instrument approach indicated that the airplane was flying a relatively smooth and consistent flightpath with altitude and heading changes that were indicative of autopilot use until the final turn to intercept the localizer course. Maneuvering the airplane in restricted visibility placed the pilot in conditions conducive to the development of spatial disorientation. The accident circumstances, including altitude and course deviations and the subsequent high-energy impact, are consistent with the known effects of spatial disorientation. Additionally, examination of the airframe, engines, and propellers revealed no evidence of any preexisting anomalies that would have precludednormal operation. Therefore, it is likely that the pilot receiving instruction was experiencing the effects of spatial disorientation when the accident occurred. Toxicology testing of the flight instructor identified significant amounts of oxycodone as well as its active metabolite, oxymorphone, in liver tissue; oxycodone was also found in muscle. Oxycodone is an opioid pain medication available by prescription that may impair mental and/or physical ability required for the performance of potentially hazardous tasks. The flight instructor's tissue levels of oxycodone suggest that his blood level at the time of the accident was high enough to have had psychoactive effects, and his failure to recognize and mitigate the pilot's spatial disorientation and impending loss of control further suggest that the flight instructor was impaired by the effects of oxycodone. Toxicology testing of all three pilots identified ethanol in body tissues; however, given the varying amounts and distribution, it is likely that the identified ethanol was from postmortem production rather than ingestion.
Probable cause:
The pilot's loss of airplane control due to spatial disorientation during an instrument approach in instrument meteorological conditions, and the flight instructor's delayed remedial action. Contributing to the accident was the flight instructor's impairment from the use of prescription pain medication.
Final Report: