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B738, Sochi Russia, 2018
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|On 1 September 2018, a Boeing 737-800, making its second night approach to Sochi beneath a large convective storm with low level windshear reported, floated almost halfway along the wet runway before overrunning it by approximately 400 metres and breaching the perimeter fence before stopping. A small fire did not prevent all occupants from safely evacuating. The Investigation attributed the accident to crew disregard of a number of windshear warnings and a subsequent encounter with horizontal windshear resulting in a late touchdown and noted that the first approach had meant that the crew had been poorly prepared for the second.|
|Actual or Potential
|Fire Smoke and Fumes, Human Factors, Runway Excursion, Weather|
|Type of Flight||Public Transport (Passenger)|
|Origin||Moskow/Vnukovo International Airport|
|Intended Destination||Sochi International|
|Take off Commenced||Yes|
|Location - Airport|
|Tag(s)||Approach not stabilised,|
Unplanned PF Change less than 1000ft agl
|Tag(s)||Post Crash Fire,|
|Tag(s)||Inappropriate crew response - skills deficiency,|
Inappropriate crew response (automatics),
Procedural non compliance,
Ineffective Monitoring - PIC as PF
|Tag(s)||Overrun on Landing,|
Significant Tailwind Component,
Significant Crosswind Component,
Ineffective Use of Retardation Methods,
Runway Condition not as reported
|Tag(s)||Strong Surface Winds,|
Low Level Windshear
|Safety Net Mitigations|
|Malfunction of Relevant Safety Net||No|
|GPWS||Available but ineffective|
|Damage or injury||Yes|
|Causal Factor Group(s)|
On 1 September 2018, a Boeing 737-800 (VQ-BJI) being operated by UTAir on a scheduled domestic passenger flight from Moscow Vnukovo to Sochi as UT579 overran the wet destination runway 06 after touchdown after making a second approach to it in night IMC. The aircraft was substantially damaged but all 172 occupants successfully evacuated the aircraft with just 8 serious and 10 minor injuries to passengers. A fuel fed fire broke out in the left wing but was quickly brought under control. Damage was caused to various aerodrome installations as well as the perimeter fence.
An Investigation was carried out by the Air Accident Investigation Commission of the Interstate Aviation Committee (IAC-MAK). The SSFDR, the SSCVR and the QAR were all recovered undamaged from the aircraft and their data were successfully downloaded and found to cover the whole accident flight.
It was noted that the 51 year-old Captain had a total of 13,995 flying hours of which 6,391 hours, including 5,147 hours in command, had been on type. The 53 year-old First Officer had a total of 12,277 flying hours of which 5,147 hours were on type. The Boeing 737 experience of both pilots had been accumulated on both ‘Classic’ and ‘NG’ variants of the type. The previous aircraft type experience of the Captain had been on the Yak-40 and that of the First Officer on the Let 410 and An-24.
The flight, with the First Officer as PF, was uneventful until it arrived in the Sochi area whereupon ATC approved own navigation to the initial approach fix (IAF) waypoint ‘PITOP’ (see the illustration below) descending to FL070 so as to allow the crew to use the onboard weather radar to avoid the worst of the convective weather which was persisting over the area as forecast. By then, the flight crew were aware from the ATIS that the thunderstorm activity in the area was producing frequent heavy showers around the airport and that there was “moderate wind shear” in the layer between the ground and 660 feet agl. These conditions were in line with a SIGMET transmitted earlier by VOLMET which advised of a stationary thunderstorm with hail and cumulonimbus cloud tops up to FL380 over and around Sochi.
During the descent towards PITOP, the radar controller advised that the visibility had dropped in a heavy squall and that there was 5.8 mm of water on runway 06 which they would be using. Noting that these conditions were outside approach minima, but “fast-changing”, the crew said that they hoped “to find their way between two squalls”. On reaching PITOP, the flight was re-cleared direct to waypoint SS062 to expect an ILS approach to runway 06 (see the illustration below).
An automatic ILS was subsequently flown with the GS intercepted from level flight at 1976 feet QFE. On transfer to TWR, landing clearance was given and soon after this whilst completing the landing checklist and passing 1100 feet, the EGPWS predictive wind shear caution ‘Monitor Radar Display’ was annunciated. On hearing this, the Captain was recorded as saying “what is that about”, to which the First Officer responded with “suppose, about the wind shear” and the Captain said “we will try”. The approach, stabilised when passing 1000 feet, was continued and at 850 feet, with about 2.7 nm to go to the runway 06 threshold, an EGPWS predictive wind shear warning “Go Around Windshear Ahead” was annunciated. The QRH required that in this situation, either a windshear escape manoeuvre or a go around must be flown but the approach was continued with the only recorded verbal response from the Captain being “... the speed is the main issue” to which the First Officer had replied “yes, yes”.
The 627 feet DH was passed and followed by confirmation that both pilots could see the runway and that the First Officer was monitoring the speed. Then, passing 170 feet, an EGPWS ‘Windshear, Windshear, Windshear’ Warning was annunciated indicating an actual windshear encounter and requiring that “the Windshear Escape Manoeuvre be commenced immediately”. No such action immediately followed but when almost immediately the RVRs, which had been previously advised as 3500 metres, 1500 metres and 3500 metres reduced during a heavy shower to the extent that sight of the runway was compromised, the Captain took over as PF and commenced a go around from 50 feet at a distance of 40 metres from the runway threshold, confirming later that this had been because of degraded visibility in heavy rain.
During the go around, climb made as required towards FL100 and with the Captain remaining as PF, CVR data revealed a number of instances language use, procedural error and procedural non-compliance which collectively were considered to evidence both pilots’ now-disrupted psychoemotional state. As the climb continued, ATC advised that there were now no wind gusts above 17 knots and that the RVRs were all at least 2400 metres. The crew decided to make another approach and were cleared to descend from 8500 feet to 2000 feet and again position via waypoint SS062 for another runway 06 ILS approach.
There was evidence of some confusion in configuring the automatics for ILS capture but simultaneous capture of both the LLZ and GS did occur and descent was commenced. On reporting this, TWR gave a landing clearance with a spot wind from 200° at 8 knots - which meant a tailwind component in contrast to the headwind component on the previous approach. Passing 1100 feet, there was another EGPWS ‘Monitor Radar Display’ annunciation and after a further 5 seconds and passing 1050 feet, a EGPWS ‘Go Around, Windshear Ahead’ warning. Neither were discussed and descent on the approach continued. As the aircraft passed the 1000 feet stabilisation gate, it was within the required speed envelope but thereafter it began to fluctuate outside the allowable limits. FDR parameters showed this speed instability could be attributed to wind velocity changes which, with the A/T engaged, had caused it to attempt to maintain the aircraft target speed by commanding large thrust variations - within the range 30% to 90%.
In accordance with the Captain’s prior briefing, the First Officer was calling out speed and height continually, which was assumed to indicate that the Captain wanted to look outside continuously to ensure he had sighted the runway by DH. At about 470 feet with 1½ nm to run, an EGPWS ‘Windshear, Windshear, Windshear’ warning was annunciated indicating an actual windshear encounter and requiring that “the Windshear Escape Manoeuvre be commenced immediately”. As on the first approach, this warning was again ignored. The Captain’s subsequent explanation for this was that “the wrong decision to land was caused by [my] emotional state, I just did not hear the windshear warning, my mind had added it to the flight deck unwanted acoustic overhead”. He added that “it worked so loudly during the first approach and was keeping me off my work, therefore it became an unwanted acoustic overhead instead of a necessary warning system that alarms you".
At 75 feet agl, the Captain disconnected the AP and auto-throttle (A/T) but having overflown the runway threshold at close to 50 feet, the aircraft then floated at a groundspeed which peaked at 178 knots - well over 20 knots above the applicable VREF and did not touch down until 14 seconds after arriving over the runway with 1285 metres of its 2894 metre available length behind the aircraft. Touchdown was immediately followed by automatic spoiler deployment and autobrake at maximum as pre-set but the Captain forgot to select the thrust reversers and was not prompted to do so by the First Officer. The Captain only realised the reversers had not been selected after about 20 seconds by which time there was only 200 metres of runway left so the selection to maximum reverse was only reached after the aircraft had already passed the end and was still at a speed of approximately 75 knots. It was noted that not only did the First Officer not notice the Captain’s failure to select reverse, he had made the call “reversers maximum” immediately after calling “speedbrake up”. However it was concluded that although prompt deployment of the thrust reversers would have reduced the extent of the overrun, it would not have stopped it happening.
The Investigation found no evidence that there was an airworthiness issue with the pre-accident aircraft that could have had any bearing on the accident. However, it was noted that the aircraft braking performance had not corresponded to the braking actions measured and broadcast to inbound aircraft. It was concluded that failure to compensate for the tailwind component on short final and its persistence during the flare had led to the late touchdown. However, compliance with even one of the applicable policies on go-around in the event of the approach becoming unstabilised or an EGPWS windshear warning occurring would have meant the landing attempt would not have been made since the fuel endurance during the second approach had been considerably greater than that required to safely divert.
The Causal Factors of the accident were formally documented as:
- repeated disregarding of the wind shear warnings which when the aircraft then entered horizontal wind shear (changing from head wind to tail wind) at low altitude, was followed by a touchdown which occurred at a distance of 1285 metres past the runway threshold (overrunning the landing zone by 385 metres) due to the increased IAS and tail wind
- landing on the runway when its normative friction coefficient was less than 0.3 that, according to the regulations in force, meant that landings were not allowed.
A total of 7 Contributory Factors were also identified as follows:
- the violation by the flight crew of the AFM and Operator's OM requirements in respect of the actions required in the case of a forecast or actual wind shear warning;
- use of the automatic flight mode (autopilot, autothrottle) in the flight during wind shear conditions which resulted in the aircraft being unstable (excess thrust) when reverting to manual control;
- lack of prevention measures taken by the Operator when the previous cases of poor crew response to wind shear warning were found;
- insufficient crew training in regards to CRM and TEM that did not allow the recognition of mistakes and/or violations in good time;
- the crew members' high psycho-emotional state caused by inconsistency between the actual landing conditions and the training they had received as well as the psychological limit which was determined by the individual psychological constitution of each member;
- insufficient braking both in auto and manual mode during the aircraft rollout caused by the insufficient tyre-to-ground friction aiming to achieve the specified rate of braking. Most probably the insufficient tyre-to-ground friction was caused by the significant amount of water on the runway surface;
- the aerodrome services' noncompliance of Sochi International Aerodrome Manual requirements related to the runway after heavy showers inspection which resulted in the crew provision of wrong normative friction coefficients;
- in respect of the high overrun speed of about 75 knots, the delay in selecting the engines to reverse (this was only done some 16 seconds after the aircraft had landed) which added about 200 metres to the overrun distance.
A total of 7 Other Shortcomings revealed in the Investigation were also identified as follows:
- The normative friction coefficient determined by an airport service and provided to a crew for the operational landing distance calculation in case of wet runway landing does not meet the expected braking efficiency and therefore has to be recalculated by a methodology developed for each aircraft type.
- The responsible aerodrome staff failed to inspect the runway condition after heavy showers as required by provisions of Sochi International Aerodrome Manual, Part 4.5, item 7.1.
- In the Runway Condition log encoded (by ICAO code) entries related to the fraction of runway surface covered by water do not reflect the measured values.
- Taking into consideration the individual natural and climatic characteristics of the area around Sochi airport (all-year thunderstorm activity with significant precipitations mostly in summer time), it is necessary to mention the insufficient activity of the Runway Safety Group in respect of hazard identification and response, for instance prevention of cases of landing on runways when their surface condition does not meet normal requirements.
- An "Alarm" signal was not provided to the meteorologist on duty at the Sochi Aviation Meteorological Centre, no requests for special meteorological observations were issued by the Flight/Shift Supervisor or by the controller of Sochi International Airport Flight Operations Control Centre.
- The Operator was aware of previous cases when crews had delayed beginning a go-around after they had received a wind shear warning on final approach to land which is evidence that the measures taken to improve flight safety improvement were insufficient.
- In violation of the requirements of national document FAP-128 (item 3.117) and recommendations of ICAO Annex 3, Doc 9817 AN/449 Manual on Low-level Wind Shear, when going around after wind shear warnings the crew failed to inform ATC about those warnings which, as they might be the only source of information, are therefore very important from the viewpoint of the provision of flight safety information to other aircraft.
A total of 12 Safety Recommendations were issued at the conclusion of the Investigation as follows:
- that the Civil Aviation Administration (CAA) of the Russian Federation provide airports’ management, airlines' management, flying and maintenance personnel and ATC personnel with the results of the Boeing 737-800 VQ-BJI accident investigation (in order to) pay special attention to the performance of flight operations in accordance with the AFM and airlines' OM requirements.
- that the Civil Aviation Administration (CAA) of the Russian Federation consider whether to implement the new methodology for providing flight crew with information on actual runway surface condition information on the basis of the TALPA (Takeoff and Landing Performance Assessment) developed by the Advisory and Rulemaking Committee (ARC) in the form of the Runway Condition Assessment Matrix (RCAM).
- that the Civil Aviation Administration (CAA) of the Russian Federation given the adverse runway condition after heavy shower precipitation should conduct an evaluation of the conformance of the Sochi aerodrome design documentation to climatic conditions and norms with regard to water drainage, as well as the evaluation of the conformance of the actual runway design to the approved project documentation. This should pay special attention to the runway section between 2230 metres and 2580 metres from the runway 06 threshold.
- that the Civil Aviation Administration (CAA) of the Russian Federation consider whether to develop a list of runways where an overrun might be hazardous for flight safety and to install for these runways a deceleration system such as Engineered Materials Arresting System (EMAS) or similar.
- that the Civil Aviation Administration (CAA) of the Russian Federation consider implementing additional (special) requirements and methodologies to require flying personnel to undergo psychological testing in respect of their adaptiveness / maladaptiveness level using qualitative readings (in addition to the quantitative ones) of the personality profile analysis, and to (thereby) detect risk groups which should be subjected to additional testing using non-verbal methodology and, if necessary, relevant corrective measures.
- that the Certification Authorities consider whether to update the airworthiness standards for large transport category aircraft with conversion tables for each type of aircraft where a braking parameter will be indicated as a function of runway state, the measured friction coefficient and the type of measuring equipment used.
- that UTair, take timely and effective measures within its SMS to provide flight crew with the recorded hazard factors and the measures taken to mitigate the associated risks.
- that Airline Executives update their Safety Management Systems having considered the shortcomings revealed during the course of the investigation, paying special attention to the measures that should be taken for (control) of the hazards that can affect flight safety.
- that Airline Executives identify the aerodromes with adverse navigational conditions for approach and develop recommendations for go-around procedures from the altitudes below DA.
- that Airline Executives provide training for flying personnel on the following items:
- flight operations, including decision making aspects when there is a thunderstorm over the aerodrome area;
- actions required when wind shear warnings are received and procedures for ATC reporting on the wind shear availability;
- actions required when the aircraft has failed to follow the requirements for a stabilised approach after passing a reference height point;
- CRM policy when performing a landing;
- The importance of informing ATC about adverse weather conditions.
- that Airline Executives of civil airport operators, Runway Safety Groups together with the State ATM Corporation, identify hazard factors and develop (corresponding) measures to prevent landings on unprepared runways using accident investigation information issued for flight safety purposes and published on the IAC-MAK website, as well as other relevant documents stored in the Archive of Incident and Accident Investigation Materials (AMRIPP) held by the Federal Air Transport Agency (Rosaviatsia).
- that Airline Executives provide additional training for aerodrome and ATC staff on the following matters:
- the requirements for frequency of airfield condition inspections depending on the weather conditions and seasons;
- the acceptance criteria for runways related to operational elements and the procedures for an airfield condition assessment.
The Investigation was completed on 12 December 2019 and the Final Report in an English language translation was subsequently released.
- Performance Shear
- Runway Excursion
- Stabilised Approach
- Low Level Wind Shear
- Airborne Wind Shear Warning Systems
- Tailwind Operations
- Cumulonimbus (Cb)
- Landing on Contaminated Runways
- Runway Surface Friction
- Runway Surface Condition Reporting
- Deceleration on the Runway
- Engineered Materials Arresting System (EMAS)
- Runway End Safety Area
- Crew Resource Management (CRM)
- Cross-checking Process