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Accident and Serious Incident Reports: RE

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Category: Runway Excursion Runway Excursion
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Definition

Reports relating to accidents which include Runway Excursion as an outcome.

The reports are organised in two sections. In the first section, reports are organised according to the sub-categories Overrun on Take Off, Overrun on Landing, and Veer Off. In the second section, events are organised according to the tagging system currently employed on Runway Excursion events in our database.

Events by Sub-Category

Overrun on Take Off

Overrun on Take Off.jpg

  • A343, Bogota Colombia, 2017 (On 11 March 2017, contrary to crew expectations based on their pre-flight takeoff performance calculation, an Airbus 340-300 taking off from the 3,800 metre-long at Bogata only became airborne just before the end of the runway. The Investigation found that the immediate reason for this was the inadequate rate of rotation achieved by the Training Captain performing the takeoff. However, it was also found that the operator’s average A340-300 rotation rate was less than would be achieved using handling recommendations which themselves would not achieve the expected performance produced by the Airbus takeoff performance software that reflected type certification findings.)
  • B738, Oslo Gardermoen Norway, 2005 (On a 23 October, 2005 a Boeing 737-800 operated by Pegasus Airlines, during night time, commenced a take-off roll on a parallel taxiway at Oslo Airport Gardermoen. The aircraft was observed by ATC and stop instruction was issued resulting in moderate speed rejected take-off (RTO).)
  • B738, Paris CDG France, 2008 (On 16 August 2008, an AMC Airlines’ Boeing 737-800 inadvertently began a night take off from an intersection on runway 27L at Paris CDG which left insufficient take off distance available before the end of the temporarily restricted runway length. It collided with and damaged obstructions related to construction works in progress on the closed section of the runway but sustained only minor damage and completed the intended flight to Luxor. The context for the flight crew error was identified as inadequate support from the Operator and inadequate airport risk assessment for operations with a reduced runway length.)
  • B738, Manchester UK, 2003 (On 16 July 2003, a Boeing 737-800, being operated by Excel Airlines on a passenger flight from Manchester to Kos began take off on Runway 06L without the flight crew being aware of work in progress at far end of the runway. The take off calculations, based on the full runway length resulted in the aircraft passing within 56 ft of a 14 ft high vehicle just after take off.)
  • LJ60, Columbia SC USA, 2008 (On September 19 2008, a Learjet 60 departing Columbia SC USA on a non scheduled passenger overran after attempting a rejected take off from above V1 and then hit obstructions which led to its destruction by fire and the death or serious injury of all six occupants. The subsequent investigation found that the tyre failure which led to the rejected take off decision had been due to under inflation and had damaged a sensor which caused the thrust reversers to return to their stowed position after deployment with the unintended forward thrust contributing to the severity of the overrun.)

Overrun on Landing

Overrun on Landing.jpg

  • CRJ1, Southampton UK, 2007 (On 17 January 2007, a Bombardier CRJ 100 being operated by French airline Brit Air on a scheduled night passenger flight from Paris CDG to Southampton could not be directionally controlled after touchdown on a dry surface in normal visibility and almost calm winds and departed the side of the runway during the landing roll. There were no injuries to any of the 36 occupants and there was no damage to the aircraft.)
  • B738, Sochi Russia, 2018 (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.)
  • DH8D, Yangon Myanmar, 2019 (On 8 May 2019, a Bombardier DHC8-400 making its second approach to Yangon during a thunderstorm touched down over halfway along the runway after an unstabilised approach but then briefly became airborne again before descending very rapidly and sustaining extreme structural damage on impact before sliding off the end of the runway. The Investigation found that prior to the final rapid descent and impact, the Captain had placed the power levers into the beta range, an explicitly prohibited action unless an aircraft is on the ground. No cause for the accident other than the actions of the crew was identified.)
  • A310, Irkutsk Russia, 2006 (On 8 July 2006, S7 Airlines A310 overran the runway on landing at Irkutsk at high speed and was destroyed after the Captain mismanaged the thrust levers whilst attempting to apply reverse only on one engine because the flight was being conducted with one reverser inoperative. The Investigation noted that the aircraft had been despatched on the accident flight with the left engine thrust reverser de-activated as permitted under the MEL but also that the previous two flights had been carried out with a deactivated right engine thrust reverser.)
  • C402, Virgin Gorda British Virgin Islands, 2017 (On 11 February 2017, a Cessna 402 failed to stop on the runway when landing at Virgin Gorda and was extensively damaged. The Investigation noted that the landing distance required was very close to that available with no safety margin so that although touchdown was normal, when the brakes failed to function properly, there was no possibility of safely rejecting the landing or stopping normally on the runway. Debris in the brake fluid was identified as causing brake system failure. The context was considered as the Operator’s inadequate maintenance practices and a likely similar deficiency in operational procedures and processes.)

Veer Off

Directional Control.jpg On landing...

  • GL5T, Fox Harbour NS Canada, 2007 (On 11 November 2007, a Bombardier BD-700 (Global 5000) operated by Canadian charter company Jetport touched down short of the runway at destination Fox Harbour in normal daylight visibility and then directional control was lost and the aircraft exited the side of the runway ending up having rotated 120° clockwise about its fore-aft axis and came to rest approximately 300metres from the threshold and approximately 50 meters from the runway edge. As a result, the co pilot and one of the passengers suffered serious injuries and the other eight occupants suffered minor injuries. The aircraft sustained major structural damage.)
  • SF34, Marsh Harbour Bahamas, 2013 (On 13 June 2013, a rushed and unstable visual approach to Marsh Harbour by a Saab 340B was followed by a mishandled landing and a runway excursion. The Investigation concluded that the way the aircraft had been operated had been contrary to expectations in almost every respect. This had set the scene for the continuation of a visual approach to an attempted landing in circumstances where there had been multiple indications that there was no option but to break off the approach, including a total loss of forward visibility in very heavy rain as the runway neared.)
  • SW4, New Plymouth New Zealand, 2009 (A visual approach by a Swearingen SA227 at New Plymouth was rushed and unstable with the distraction of a minor propeller speed malfunction and with un-actioned GPWS warnings caused by excessive sink and terrain closure rates. After a hard touchdown close to the beginning of the runway, directional control was lost and the aircraft left the runway to the side before continuing parallel to it for the rest of the landing roll.)
  • AT75, Port Vila Vanuatu, 2018 (On 28 July 2018, a right engine compressor stall on an ATR72-500 bound for Port Vila followed by smoke in the passenger cabin led to a MAYDAY declaration and shutdown of the malfunctioning engine. The subsequent single engine landing at destination ended in a veer-off and collision with two unoccupied parked aircraft. The Investigation noted the disorganised manner in which abnormal/emergency and normal checklists had been actioned and found that the ‘Before Landing’ Checklist had not been run which resulted in the rudder limiter being left in high speed mode making single engine directional control on the ground effectively impossible.)
  • SF34, Izumo Japan, 2007 (On 10 December, 2007 a SAAB 340B being operated by Japan Air Commuter on a scheduled passenger flight left the runway at Izumo Airport during the daylight landing roll in normal visibility and continued further while veering to the right before coming to a stop on the airport apron.)

Directional Control.jpg On take off..

  • DH8A, Rouyn-Noranda QC Canada, 2019 (On 23 January 2019, a Bombardier DHC8-100 failed to complete its intended night takeoff from Rouyn-Noranda after it had not been commenced on or correctly aligned parallel to the (obscured) centreline and the steadily increasing deviation had not been recognised until a runway excursion was imminent. The Investigation attributed this to the failure of the crew to pay sufficient attention to the external perspective provided by the clearly-visible runway edge lighting whilst also noting the Captain’s likely underestimation of the consequences of a significant flight deck authority gradient and a failure to fully follow relevant applicable operating procedures.)
  • B738, Sydney Australia, 2007 (On 14 July 2007, a Boeing 737-800 being operated by New Zealand airline Polynesian Blue on a scheduled passenger service from Sydney to Christchurch New Zealand commenced take off on Runway 16R with asymmetric thrust set and veered off the side of the runway reaching the intersecting runway 07 before rejected take off action initiated by the flight crew took effect and the aircraft came to a stop.)
  • SF34, Stornoway UK, 2015 (On 2 January 2015, the commander of a Saab 340 suddenly lost directional control during a within-limits crosswind take off and the aircraft left the runway onto grass at approximately 80 knots. No call to reject the take off was made and no action was taken to shut down the engines until the aircraft had come to a stop in the soft ground with a collapsed nose gear and substantial damage to the propellers and lower forward fuselage. The Investigation concluded that the most likely explanation for the excursion was the absence of any rudder input as the aircraft accelerated.)
  • A320, Harstad/Narvik Norway 2004 (On 25 November 2004, a MyTravel Airways Airbus A320 departed the side of the runway at Harstad, Norway at a low speed after loss of directional control when thrust was applied for a night take off on a runway with below normal surface friction characteristics. It was found that the crew had failed to follow an SOP designed to ensure that any accumulated fan ice was shed prior to take off and also failed to apply take off thrust as prescribed, thus delaying their appreciation of the uneven thrust produced.)
  • B738, Nuremburg Germany, 2010 (On 8 January 2010, an Air Berlin Boeing 737-800 attempted to commence a rolling take off at Nuremburg on a runway pre-advised as having only ‘medium’ braking action. Whilst attempting to position the aircraft on the runway centreline, directional control was lost and the aircraft exited the paved surface onto soft ground at low speed before the flight crew were able to stop it. The event was attributed to the inappropriately high taxi speed onto the runway and subsequent attempt to conduct a rolling take off. Relevant Company standard operating procedures were found to be deficient.)

Events by A&I Tag

Excessive Airspeed

  • SW4, Sanikiluaq Nunavut Canada, 2012 (On 22 December 2012, the crew of a Swearingen SA227 attempting a landing, following an unstabilised non-precision approach at Sanikiluaq at night with questionable alternate availability in marginal weather conditions, ignored GPWS PULL UP Warnings, then failed in their attempt to transition into a low go around and the aircraft crashed into terrain beyond the runway. One occupant – an unrestrained infant – was killed and the aircraft was destroyed. The Investigation faulted crew performance, the operator and the regulator and reiterated that lap-held infants were vulnerable in crash impacts.)
  • A333, Hong Kong China, 2010 (On 13 April 2010, a Cathay Pacific Airbus A330-300 en route from Surabaya to Hong Kong experienced difficulty in controlling engine thrust. As these problems worsened, one engine became unusable and a PAN and then a MAYDAY were declared prior to a successful landing at destination with excessive speed after control of thrust from the remaining engine became impossible. Emergency evacuation followed after reports of a landing gear fire. Salt water contamination of the hydrant fuel system at Surabaya after alterations during airport construction work was found to have led to the appearance of a polymer contaminant in uplifted fuel.)
  • AT72, Shannon Ireland, 2011 (On 17 July 2011, an Aer Arann ATR 72-200 made a bounced daylight landing at Shannon in gusty crosswind conditions aggravated by the known effects of a nearby large building. The nose landing gear struck the runway at 2.3g and collapsed with subsequent loss of directional control and departure from the runway. The aircraft was rendered a hull loss but there was no injury to the 25 occupants. The accident was attributed to an excessive approach speed and inadequate control of aircraft pitch during landing. Crew inexperience and incorrect power handling technique whilst landing were also found to have contributed.)
  • B738, Georgetown Guyana, 2011 (On 30 July 2011, a Boeing 737-800 overran the wet landing runway at Georgetown after a night non-precision approach, exited the airport perimeter and descended down an earth embankment. There were no fatalities but the aircraft sustained substantial damage and was subsequently declared a hull loss. The Investigation attributed the overrun to a touchdown almost two thirds of the way down the runway and failure to utilise the aircraft’s full deceleration capability. Loss of situational awareness and indecision as to the advisability of a go-around after a late touchdown became inevitable was also cited as contributory to the outcome.)
  • GLF4, Teterboro NJ USA, 2010 (On 1 October 2010, a Gulfstream G-IV being operated by General Aviation Flying Service as ‘Meridian Air Charter’ on a corporate flight from Toronto International to Teterboro made a deep landing on 1833m-long runway 06 at destination in normal day visibility and overran the end of the runway at a speed of 40 to 50 knots before coming to a stop 30m into a 122m long EMAS installation.)

RTO decision after V1

  • B742, Brussels Belgium, 2008 (On 25 May 2008 a Kalitta Air B747-200F, which was departing Brussels on a cargo flight to Bahrain, overran Runway 20 at Brussels Airport, Belgium during a rejected take-off. The aircraft came to a stop 300m beyond the end of runway 20 and broke into three parts. The crew of four and one passenger safely evacuated from the aircraft and suffered only minor injuries.)
  • FA20, Durham Tees Valley UK, 2012 (On 9 August 2012, a serviceable Cobham Leasing Fan Jet Falcon overran the 2291 metre long runway at Durham Tees Valley after beginning rejecting take off from above V1 because of a suspected bird strike. The crew believed there was a possibility of airframe damage from a single medium sized bird sighted ahead which might have been hit by the main landing gear. It was found that the overrun distance had been increased by low friction on the stopway and noted that the regulatory exemption issued for operation without FDR and CVR was no longer appropriate.)
  • MD83, Ypsilanti MI USA, 2017 (On 8 March 2017, a Boeing MD83 departing Ypsilanti could not be rotated and the takeoff had to be rejected from above V1. The high speed overrun which followed substantially damaged the aircraft but evacuation was successful. The Investigation found that the right elevator had been locked in a trailing-edge-down position as a result of damage caused to the aircraft by high winds whilst it was parked unoccupied for two days prior to the takeoff. It was noted that on an aircraft with control tab initiated elevator movement, this condition was undetectable during prevailing pre flight system inspection or checks.)
  • D328, Isle of Man, 2005 (On 28 November 2005, a Dornier 328 departing from Isle of Man was unable to rotate at the speed calculated as applicable but the crew were able to complete a successful rejected take off. The Investigation found that the crew had failed to use the increased tale off speeds which were required for the aircraft type involved after the aircraft had been de/anti iced prior to taxiing for takeoff.)
  • DH8B, Nuuk Greenland, 2019 (On 30 May 2019, a DHC8-200 departing from Nuuk could not be rotated at the calculated speed even using full aft back pressure and the takeoff was rejected with the aircraft coming to a stop with 50 metres of the 950 metre long dry runway remaining. The initial Investigation focus was on a potential airworthiness cause associated with the flight control system but it was eventually found that the actual weights of both passengers and cabin baggage exceeded standard weight assumptions with the excess also resulting in the aircraft centre of gravity being outside the range certified for safe flight.)

High Speed RTO (V above 80 but no above V1)

Unable to rotate at VR

  • B763, Copenhagen Denmark, 1999 (On 24 August 1999, a Boeing 767-300 being operated by SAS on a scheduled passenger flight from Copenhagen to Tokyo was unable to get airborne from the take off roll on Runway 22R in normal daylight visibility and made a rejected take off from high speed. The aircraft was taxied clear of the runway and after a precautionary attendance of the RFFS because of overheated brakes, the passengers were disembarked and transported to the terminal. There was minor damage to the aircraft landing gear and rear fuselage.)
  • MD83, Are/Ostersund Sweden, 2007 (On 9 September 2007, an MD83 being operated by Austrian Company MAP Jet, which was over the permitted weight for the runway and conditions, made a night take off from Are/Ostersund airport, Sweden, very near the end of the runway and collided with the approach lights for the opposite runway before climbing away.)
  • B733, Birmingham UK, 2009 (On 6 February 2009, the crew of a Boeing 737-300 departing Birmingham successfully rejected take off from well above V1 when it became clear to the First Officer as handling pilot, that it was impossible to rotate. The Investigation found that cause of the rotation difficulty was that the crew had failed to set the stabiliser trim to the appropriate position for take off after delaying this action beyond the normal point in pre flight preparations because ground de icing was in progress and not subsequently noticing.)
  • B773, Lagos Nigeria, 2010 (On 11 Jan 2010, an Air France Boeing 777-300ER successfully rejected a night take off from Lagos from significantly above V1 when control column pressure at rotation was perceived as abnormal. The root and secondary causes of the incident were found to be the failure of the Captain to arm the A/T during flight deck preparation and his inappropriate response to this on the take off roll. It was considered that his performance may have being an indirect consequence of his decision to take a 40 minute period of in-seat rest during the 90 minute transit stop at Lagos.)
  • D328, Isle of Man, 2005 (On 28 November 2005, a Dornier 328 departing from Isle of Man was unable to rotate at the speed calculated as applicable but the crew were able to complete a successful rejected take off. The Investigation found that the crew had failed to use the increased tale off speeds which were required for the aircraft type involved after the aircraft had been de/anti iced prior to taxiing for takeoff.)

Collision Avoidance Action

  • E135, George South Africa, 2009 (On 7 December 2009, an South African Airlink Embraer 135 overran the recently refurbished wet landing runway at George after braking was ineffective and exited the aerodrome perimeter to end up on a public road. There was no fire and all occupants were able to evacuate the aircraft. The subsequent investigation attributed the overrun principally to inadequate wet runway friction following the surface maintenance activities and noted various significant non-compliances with ICAO Annex 14.)
  • B733, Aqaba Jordan, 2017 (On 17 September 2017, a Boeing 737-300 requested and was approved for a visual approach to Aqaba which involved a significant tailwind component and, after approaching at excessive speed, it touched down late and overran the 3000 metre runway onto sandy ground. The Investigation found that despite EGPWS Alerts relating to both the high rate of descent and late configuration, the Captain had instructed the First Officer to continue what was clearly an unstabilised approach and when touchdown had still not occurred with around 1000 metres of runway left, the Captain took over but was unable to prevent an overrun.)
  • B733 / DH8D, Fort McMurray Canada, 2014 (On 4 August 2014, a Boeing 737-300 making a day visual approach at Fort McMurray after receiving an ILS/DME clearance lined up on a recently-constructed parallel taxiway and its crew were only alerted to their error shortly before touchdown by the crew of a DHC8-400 which was taxiing along the same taxiway in the opposite direction. This resulted in a go around being commenced from 46 feet agl. The Investigation noted that both pilots had been looking out during the final stages of the approach and had ignored important SOPs including that for a mandatory go around from an unstable approach.)

Parallel Approach Operations

Late Touchdown

  • A310, Khartoum Sudan, 2008 (On 10 June 2008, a Sudan Airways Airbus A310 made a late night touchdown at Khartoum and the actions of the experienced crew were subsequently unable to stop the aircraft, which was in service with one thrust reverser inoperative and locked out, on the wet runway. The aircraft stopped essentially intact some 215 metres beyond the runway end after overrunning on smooth ground but a fuel-fed fire then took hold which impeded evacuation and eventually destroyed the aircraft.)
  • B190, Blue River BC Canada, 2012 (On 17 March 2012, the Captain of a Beech 1900C operating a revenue passenger flight lost control of the aircraft during landing on the 18metre wide runway at destination after an unstabilised day visual approach and the aircraft veered off it into deep snow. The Investigation found that the Operator had not specified any stable approach criteria and was not required to do so. It was also noted that VFR minima had been violated and, noting a fatal accident at the same aerodrome five months previously, concluded that the Operators risk assessment and risk management processes were systemically deficient.)
  • E170, Cleveland OH USA, 2007 (On 18 February 2007, while landing at Cleveland Hopkins International Airport, USA, an Embraer ERJ170 overran the snow contaminated runway. The crew failed to execute a go-around at the minimum decision altitude (MDA) of the localizer approach when adequate visual reference was not available.)
  • B738, Pardubice Czech Republic, 2013 (On 25 August 2013, the type-experienced crew of a Boeing 737-800 operating with one thrust reverser locked out made a late touchdown with a significant but allowable tail wind component present and overran the end of the runway at Pardubice onto grass at 51 knots. No damage was caused to the aircraft and no emergency evacuation was performed. The Investigation concluded that the aircraft had been configured so that even for a touchdown within the TDZ, there would have been insufficient landing distance available. The flight crew were found not to have followed a number of applicable operating procedures.)
  • E190, Kupang Indonesia, 2015 (On 21 December 2015, an Embraer 195 crew continued a significantly unstable approach which included prolonged repetition of 'High Speed' and a series of EGPWS Alerts which were both ignored and which culminated in a high speed late touchdown which ended in a 200 metre overrun. The Investigation attributed the event to poor flight management and noted the systemic lack of any effective oversight of pilot operating standards compounded in the investigated event by the effects of a steep flight deck authority gradient and the failure to detect anomalies in the normal operating behaviour of both the pilots involved.)

Significant Tailwind Component

  • B738, Limoges France, 2008 (On 21 March 2008, a Boeing 737-800 being operated by Ryanair on a scheduled passenger flight from Charleroi, Belgium to Limoges carried out a daylight approach at destination followed by a landing in normal ground visibility but during heavy rain and with a strong crosswind which ended with a 50 metre overrun into mud. None of the 181 occupants were injured but both engines were damaged by ingestion of debris.)
  • B737, Chicago Midway USA, 2005 (On 8 December 2005, a delay in deploying the thrust reversers after a Boeing 737-700 touchdown at night on the slippery surface of the 1176 metre-long runway at Chicago Midway with a significant tailwind component led to it running off the end, subsequently departing the airport perimeter and hitting a car before coming to a stop. The Investigation concluded that pilots’ lack of familiarity with the autobrake system on the new 737 variant had distracted them from promptly deploying the reversers and that inadequate pilot training provision and the ATC failure to provide adequate braking action information had contributed.)
  • CRJ7, Kanpur India, 2011 (On 20 July 2011, an Alliance Air CRJ 700 touched down over half way along the 9000 ft long runway at Kanpur after a stable ILS approach but with an unexpected limiting tailwind component and failed to stop before the end of the paved surface. Although an emergency evacuation was not necessary and there were no injuries, the aircraft was slightly damaged by impact with an obstruction. The subsequent investigation attributed the event to the commanders continued attempt at a landing when a late touchdown became increasingly likely.)
  • B738, Kingston Jamaica, 2009 (On 22 December 2009, the flight crew of an American Airlines’ Boeing 737-800 made a long landing at Kingston at night in heavy rain and with a significant tailwind component and their aircraft overran the end of the runway at speed and was destroyed beyond repair. There was no post-crash fire and no fatalities, but serious injuries were sustained by 14 of the 154 occupants. The accident was attributed almost entirely to various actions and inactions of the crew. Damage to the aircraft after the overrun was exacerbated by the absence of a RESA.)
  • IL76, St John's Newfoundland Canada, 2012 (On 13 August 2012, an Ilyushin IL76 freighter overran landing runway 11 at St John's at 40 knots. The Investigation established that although a stabilised approach had been flown, the aircraft had been allowed to float in the presence of a significant tail wind component and had not finally touched down until half way along the 2590 metre long runway. It was also found that reverse thrust had then not been fully utilised and that cross connection of the brake lines had meant that the anti skid pressure release system worked in reverse sense, thus reducing braking effectiveness.)

Significant Crosswind Component

  • B738, Limoges France, 2008 (On 21 March 2008, a Boeing 737-800 being operated by Ryanair on a scheduled passenger flight from Charleroi, Belgium to Limoges carried out a daylight approach at destination followed by a landing in normal ground visibility but during heavy rain and with a strong crosswind which ended with a 50 metre overrun into mud. None of the 181 occupants were injured but both engines were damaged by ingestion of debris.)
  • JS41, Rhodes Greece, 2015 (On 2 February 2015, a Jetstream 41 made a hard and extremely fast touchdown at Rhodes and the left main gear leg collapsed almost immediately. The crew were able to prevent the consequent veer left from leading to a lateral runway excursion. The Investigation found that the approach had been significantly unstable throughout with touchdown at around 50 knots above what it should have been and that a whole range of relevant procedures had been violated by the management pilot who had flown the approach in wind shear conditions in which approaches to Rhodes were explicitly not recommended.)
  • D328, Sumburgh Shetland Islands UK, 2017 (On 26 January 2017, an EASA Test Pilot carrying out certification test flying to extend the Dornier 328's maximum demonstrated crosswind was unable to retain control during an intended full stop landing on runway 09 at Sumburgh and it departed the side of the runway onto soft ground and stopped abruptly. The Investigation noted the Test Pilot's total type experience was the three circuits immediately prior to the excursion and attributed it to inappropriate flight control inputs and power lever movements. Intervention on the power levers by the aircraft commander had not been enough to prevent the excursion.)
  • B738, East Midlands UK, 2020 (On 9 February 2020, a Boeing 737-800 rejected its takeoff from East Midlands from a speed above V1 after encountering windshear in limiting weather conditions and was brought to a stop with 600 metres of runway remaining. The Investigation found that the Captain had assigned the takeoff to his First Officer but had taken control after deciding that a rejected takeoff was appropriate even though unequivocal QRH guidance that high speed rejected takeoffs should not be made due to windshear existed. Boeing analysis found that successful outcomes during takeoff windshear events have historically been more likely when takeoff is continued.)
  • F50, Isle of Man, 2009 (On 15 January 2009 a VLM Fokker 50 left the side of the runway at the Isle of Man during the daylight landing roll. It was concluded that directional control had been lost on the wet runway because the crew had attempted rudder steering whilst also applying reverse pitch, an action which was contrary to SOPSs.)

Thrust Reversers not fitted

  • B462, Stord Norway, 2006 (On 10 October 2006, a BAE Systems 146-200 being operated by Danish airline Atlantic Airways on a passenger flight from Sola to Stord overran the end of runway 33 at destination at a slow speed in normal visibility at dawn (but just prior to the accepted definition of daylight) before plunging down a steep slope sustaining severe damage and catching fire immediately it had come to rest. The rapid spread of the fire and difficulties in evacuation resulted in the death of four of the 16 occupants and serious injury to six others. The aircraft was completely destroyed.)
  • E135, George South Africa, 2009 (On 7 December 2009, an South African Airlink Embraer 135 overran the recently refurbished wet landing runway at George after braking was ineffective and exited the aerodrome perimeter to end up on a public road. There was no fire and all occupants were able to evacuate the aircraft. The subsequent investigation attributed the overrun principally to inadequate wet runway friction following the surface maintenance activities and noted various significant non-compliances with ICAO Annex 14.)
  • E145, Hannover Germany, 2005 (On 14 August 2005, a British Airways Regional Embraer 145 overran Runway 27L at Hannover by 160 metes after flying a stable approach in daylight but then making a soft and late touchdown on a water covered runway. Dynamic aquaplaning began and this was followed by reverted rubber aquaplaning towards the end of the paved surface when the emergency brake was applied. The aircraft suffered only minor damage and only one of the 49 occupants was slightly injured.)

Landing Performance Assessment

  • B738, Pardubice Czech Republic, 2013 (On 25 August 2013, the type-experienced crew of a Boeing 737-800 operating with one thrust reverser locked out made a late touchdown with a significant but allowable tail wind component present and overran the end of the runway at Pardubice onto grass at 51 knots. No damage was caused to the aircraft and no emergency evacuation was performed. The Investigation concluded that the aircraft had been configured so that even for a touchdown within the TDZ, there would have been insufficient landing distance available. The flight crew were found not to have followed a number of applicable operating procedures.)
  • B738, Christchurch New Zealand, 2015 (On 11 May 2015, a Boeing 737-800 crew making a night landing at Christchurch had to react quickly when braking action deteriorated and only just succeeded in preventing an overrun. The Investigation found that a damp rather than wet runway had been assumed despite recent rain and that the aircraft operator had recently changed their procedures so that a damp runway should be considered as dry rather than wet for runway performance purposes. The questionable determination of the crew that the runway was likely to be damp, not wet, was attributed to a relatively high workload prior to final approach.)
  • CRJ2, Traverse City MI USA, 2007 (On 12 April 2007, a Bombardier CRJ-600 being operated by Pinnacle Airlines on a scheduled night passenger flight from Minneapolis-St. Paul to Traverse City overran the end of the slippery landing runway by 90 metres in normal visibility. There were no injuries to any of the 52 occupants but the aircraft sustained substantial, but repairable, damage, primarily at the forward lower fuselage.)
  • E190, Kupang Indonesia, 2015 (On 21 December 2015, an Embraer 195 crew continued a significantly unstable approach which included prolonged repetition of 'High Speed' and a series of EGPWS Alerts which were both ignored and which culminated in a high speed late touchdown which ended in a 200 metre overrun. The Investigation attributed the event to poor flight management and noted the systemic lack of any effective oversight of pilot operating standards compounded in the investigated event by the effects of a steep flight deck authority gradient and the failure to detect anomalies in the normal operating behaviour of both the pilots involved.)
  • C550, Southampton UK, 1993 (On 26 May 1993, a Cessna Citation II being operated by a UK Air Taxi Company on a positioning flight from Oxford to Southampton to collect passengers with just the flight crew on board overran the ‘very wet’ landing runway at the destination in normal daylight visibility and ended up on an adjacent motorway where it collided with traffic, caught fire and was destroyed. The aircraft occupants and three people in cars received minor injuries.)

Off side of Runway

  • B738, Nuremburg Germany, 2010 (On 8 January 2010, an Air Berlin Boeing 737-800 attempted to commence a rolling take off at Nuremburg on a runway pre-advised as having only ‘medium’ braking action. Whilst attempting to position the aircraft on the runway centreline, directional control was lost and the aircraft exited the paved surface onto soft ground at low speed before the flight crew were able to stop it. The event was attributed to the inappropriately high taxi speed onto the runway and subsequent attempt to conduct a rolling take off. Relevant Company standard operating procedures were found to be deficient.)
  • D328, Norwich UK, 2012 (On 22 March 2012, a Scot Airways Dornier 328 left the side of the runway shortly after touchdown following an unstable visual sequel to a non precision approach at Norwich and then carried out a go around without further event. The aircraft was undamaged by the excursion but a runway edge light was broken. The subsequent Investigation noted the gross violation of Operator SOPs in respect of the way the initial approach had been conducted, the absence of necessary crew procedures following a serious incident and the absence of any OFDM programme.)
  • DHC6, Tiree UK, 2017 (On 7 March 2017, a DHC-6-300 left the side of the runway after touchdown in what the crew believed was a crosswind component within the Operator's crosswind limit. The Investigation concluded that the temporary loss of control of the aircraft was consistent with the occurrence with a sudden gust of wind above the applicable crosswind limits and noted the reliance of the crew on 'spot' winds provided by TWR during the final stages of the approach.)
  • C25A, Bern Switzerland, 2018 (On 2 March 2018, a Cessna 525A touched down at Bern aligned with the left hand edge of the runway and then left it completely before re-entering it after a little over 300 metres and completing the landing roll without further event. Damage to the aircraft and six runway edge and taxi lights was subsequently found. The Investigation noted that the crew stated that they had retained full visual contact with the runway during final approach and that the recorded braking action was good. It was not possible to establish why neither pilot had been aware of the misalignment.)
  • A320, Tehran Mehrabad Iran, 2016 (On 13 August 2016, an Airbus A320 departed the side of the runway at low speed during takeoff from Tehran Mehrabad and became immobilised in soft ground. The Investigation found that the Captain had not ensured that both engines were simultaneously stabilised before completing the setting of takeoff thrust and that his subsequent response to the resulting directional control difficulties had been inappropriate and decision to reject the takeoff too late to prevent the excursion. Poor CRM on the flight deck was identified as including but not limited to the First Officer’s early call to reject the takeoff being ignored.)

Taxiway Take Off/Landing

  • A343, Hong Kong China, 2010 (On 27 November 2010, a Finnair Airbus A340-300 unintentionally attempted a night take off from Hong Kong in good visibility from the taxiway parallel to the runway for which take off clearance had been given. ATC observed the error and instructed the crew to abandon the take off, which they then did. The Investigation attributed the crew error partly to distraction. It was considered that the crew had become distracted and that supporting procedures and process at the Operator were inadequate.)
  • A320, Oslo Norway, 2010 (On 25 February 2010, an Aeroflot Airbus A320-200 unintentionally made a daylight take off from Oslo in good visibility from the taxiway parallel to the runway for which take off clearance had been given. Because of the available distance and the absence of obstructions, the take off was otherwise uneventful. The Investigation identified contributory factors attributable to the airline, the airport and the ANSP.)
  • B738, Oslo Gardermoen Norway, 2005 (On a 23 October, 2005 a Boeing 737-800 operated by Pegasus Airlines, during night time, commenced a take-off roll on a parallel taxiway at Oslo Airport Gardermoen. The aircraft was observed by ATC and stop instruction was issued resulting in moderate speed rejected take-off (RTO).)
  • B734, Palembang Indonesia, 2008 (On 2 October 2008, a Boeing 737-400 being used for flight crew command upgrade line training unintentionally landed off a non precision approach at Palembang in daylight on a taxiway parallel to the landing runway. Neither pilot realised their error until the aircraft was already on the ground when they saw a barrier ahead and were able to brake hard to stop only 700 metres from touchdown. It was found that the taxiway involved had served as a temporary runway five years earlier and that previously obliterated markings from that use had become visible.)
  • B763, Singapore, 2015 (On 12 July 2015, a Japanese-operated Boeing 767-300 deviated from its acknowledged clearance and lit-centreline taxi routing and began take-off from a parallel taxiway in good night visibility, crossing a lit red stop bar in the process. When ATC observed this, the aircraft was instructed to stop which was achieved without further event. A subsequent take-off was uneventful. The crew did not report the event to their airline or their State authorities because the Captain "determined that this case did not need to be reported" and these organisations only became aware when subsequently contacted by the Investigating Agency.)

Runway Length Temporarily Reduced

  • A343, Rio de Janeiro Galeão Brazil, 2011 (On 8 December 2011, an Airbus A340-300 did not become airborne until it had passed the end of the takeoff runway at Rio de Janeiro Galeão, which was reduced in length due to maintenance. The crew were unaware of this fact nor the consequent approach lighting, ILS antennae and aircraft damage, and completed their intercontinental flight. The Investigation found that the crew had failed to use the full available runway length despite relevant ATIS and NOTAM information and that even using rated thrust from where they began their takeoff, they would not have become airborne before the end of the runway.)
  • A320, Surat India, 2017 (On 4 October 2017, an Airbus A320 slightly overran the end of runway 22 at Surat during an early morning daylight landing. A temporarily displaced landing threshold meant the runway length was only 1,905 metres rather than the 2,905 metre full length. The aircraft remained on a paved surface and was undamaged. Its crew did not report the excursion which was only discovered when broken runway lighting was subsequently discovered. The Investigation found that the non-precision approach made was unstable and that a prolonged float in the subsequent flare meant that only 600 metres of runway remained ahead at touchdown.)
  • B738, Paris CDG France, 2008 (On 16 August 2008, an AMC Airlines’ Boeing 737-800 inadvertently began a night take off from an intersection on runway 27L at Paris CDG which left insufficient take off distance available before the end of the temporarily restricted runway length. It collided with and damaged obstructions related to construction works in progress on the closed section of the runway but sustained only minor damage and completed the intended flight to Luxor. The context for the flight crew error was identified as inadequate support from the Operator and inadequate airport risk assessment for operations with a reduced runway length.)
  • GLEX, Montréal St Hubert Canada, 2017 (On 15 May 2017, a Bombardier Global Express crew failed to land on the restricted runway width available at Montréal St Hubert where there was a long-term construction project which had required reductions in both width and length of the main runway. The Investigation found that relevant NOTAM information including a requirement to pre-notify intended arrival had been ignored and that during arrival the crew had failed to respond to a range of cues that their landing would not be on the normally-available runway. Deficiencies in the arrangements made for continued use of part of the runway were also identified.)
  • B738, Manchester UK, 2003 (On 16 July 2003, a Boeing 737-800, being operated by Excel Airlines on a passenger flight from Manchester to Kos began take off on Runway 06L without the flight crew being aware of work in progress at far end of the runway. The take off calculations, based on the full runway length resulted in the aircraft passing within 56 ft of a 14 ft high vehicle just after take off.)

Intentional Premature Rotation

  • B773, London Heathrow UK, 2016 (On 30 August 2016, a Boeing 777-300 crew began takeoff from London Heathrow at an intersection one third of the way along the runway using the reduced thrust calculated for a full-length take off instead of the rated thrust calculated for the intersection takeoff. As a result, the aircraft was only just airborne as it crossed the airport boundary and an adjacent public road. The Investigation attributed the data input error to crew failure to respond appropriately on finding that they had provisionally computed performance data based on different assumptions and concluded that the relevant Operator procedures were insufficiently robust.)
  • MD88, Groningen Netherlands, 2003 (On 17 June 2003, a crew of a Boeing MD-88, belonging to Onur Air, executed a high speed rejected take-off at a late stage which resulted in overrun of the runway and serious damage to the aircraft.)
  • B763, Manchester UK, 2008 (On 13 December 2008, a Thomsonfly Boeing 767-300 departing from Manchester for Montego Bay Jamaica was considered to be accelerating at an abnormally slow rate during the take off roll on Runway 23L. The aircraft commander, who was the pilot not flying, consequently delayed the V1 call by about 10 - 15 because he thought the aircraft might be heavier than had been calculated. During the rotation the TAILSKID message illuminated momentarily, indicating that the aircraft had suffered a tail strike during the takeoff. The commander applied full power and shortly afterwards the stick shaker activated briefly. The aircraft continued to climb away and accelerate before the flaps were retracted and the after-takeoff check list completed. The appropriate drills in the Quick Reference Handbook (QRH) were subsequently actioned, fuel was dumped and the aircraft returned to Manchester for an overweight landing without further incident.)

Incorrect Aircraft Configuration

  • GLF4, Le Castellet France, 2012 (On 13 July 2012, a Gulfstream G-IV left the side of the runway at high speed during the landing roll at Le Castellet following a positioning flight after ineffective deceleration after the flight crew had forgotten to arm the ground spoilers. The Investigation found that pilot response to this situation had been followed by a loss of directional control, collision with obstructions and rapid onset of an intense fire. Contributory factors identified included poor procedural compliance by the pilots, their lack of training on a relevant new QRH procedure which Gulfstream had ineffectively communicated and ineffective FAA oversight of the operation.)
  • B733, Aqaba Jordan, 2017 (On 17 September 2017, a Boeing 737-300 requested and was approved for a visual approach to Aqaba which involved a significant tailwind component and, after approaching at excessive speed, it touched down late and overran the 3000 metre runway onto sandy ground. The Investigation found that despite EGPWS Alerts relating to both the high rate of descent and late configuration, the Captain had instructed the First Officer to continue what was clearly an unstabilised approach and when touchdown had still not occurred with around 1000 metres of runway left, the Captain took over but was unable to prevent an overrun.)
  • A320, Basel-Mulhouse-Freiburg France, 2014 (On 6 October 2014, an A320 crew requested, accepted and commenced an intersection takeoff at Basel using reduced thrust performance data based on the originally anticipated full length takeoff which would have given 65% more TODA. Recognition of the error and application of TOGA allowed the aircraft to get airborne just before the runway end but the Investigation found that a rejected take off from high speed would have resulted in an overrun and noted that despite changes to crew procedures after a similar event involving the same operator a year earlier, the relevant procedures were still conducive to error.)
  • SF34, Marsh Harbour Bahamas, 2013 (On 13 June 2013, a rushed and unstable visual approach to Marsh Harbour by a Saab 340B was followed by a mishandled landing and a runway excursion. The Investigation concluded that the way the aircraft had been operated had been contrary to expectations in almost every respect. This had set the scene for the continuation of a visual approach to an attempted landing in circumstances where there had been multiple indications that there was no option but to break off the approach, including a total loss of forward visibility in very heavy rain as the runway neared.)
  • AT75, Port Vila Vanuatu, 2018 (On 28 July 2018, a right engine compressor stall on an ATR72-500 bound for Port Vila followed by smoke in the passenger cabin led to a MAYDAY declaration and shutdown of the malfunctioning engine. The subsequent single engine landing at destination ended in a veer-off and collision with two unoccupied parked aircraft. The Investigation noted the disorganised manner in which abnormal/emergency and normal checklists had been actioned and found that the ‘Before Landing’ Checklist had not been run which resulted in the rudder limiter being left in high speed mode making single engine directional control on the ground effectively impossible.)

Reduced Thrust Take Off

  • B748, Tokyo Narita Japan, 2017 (On 15 July 2017, a Boeing 747-8F close to its maximum takeoff weight only became airborne just before the end of the 2,500 metre-long north runway at Narita after the reduced thrust applicable to the much longer south runway was used for the takeoff. The aircraft cleared the upwind runway threshold by only 16 feet. The Investigation found that the Captain and the First Officer had both failed to follow elements of the applicable takeoff performance change procedures after the departure runway anticipated during pre-start flight preparations prior to ATC clearance delivery had changed.)
  • B738, Belfast International UK, 2017 (On 21 July 2017, a Boeing 737-800 taking off from Belfast was only airborne near the runway end of the runway and then only climbed at a very shallow angle until additional thrust was eventually added. The Investigation found that the thrust set had been based on an incorrectly input surface temperature of -52°C, the expected top of climb temperature, instead of the actual surface temperature. Although inadequate acceleration had been detected before V1, the crew did not intervene. It was noted that neither the installed FMC software nor the EFBs in use were conducive to detection of the data input error.)
  • B737, Southend UK, 2010 (On 21 Nov 2010, a Boeing 737-700 being operated by Arik Air on a non revenue positioning flight from Southend to Lagos with only the two pilots on board carried out a successful take off in daylight and normal ground visibility from runway 06 but became airborne only just before the end of the runway.)
  • A321, Glasgow UK, 2019 (On 24 November 2019, as an Airbus A321 taking off from the 2665 metre-long runway 05 at Glasgow approached the calculated V1 with the flex thrust they had set, the aircraft was not accelerating as expected and they applied TOGA thrust. This resulted in the aircraft becoming airborne with less than 400 metres of runway remaining. The Investigation confirmed what the crew had subsequently discovered for themselves - that they had both made an identical error in their independent EFB performance calculations which the subsequent standard procedures and checks had not detected. The operator is reviewing its related checking procedures.)
  • A332, Montego Bay Jamaica, 2008 (On 28 October 2008, an Airbus A330-200 could not be rotated for liftoff whist making a night takeoff from Montego Bay until the Captain had increased the reduced thrust set to TOGA, after which the aircraft became airborne prior to the end of the runway and climbed away normally. The Investigation found that the takeoff performance data used had been calculated for the flight by Company Despatch and the fact that it had been based on a takeoff weight which was 90 tonnes below the actual take off weight had not been noticed by any of the flight crew.)

Fixed Obstructions in Runway Strip

  • DH8D, Hubli India, 2015 (On 8 March 2015, directional control of a Bombardier DHC 8-400 which had just completed a normal approach and landing was lost and the aircraft departed the side of the runway following the collapse of both the left main and nose landing gear assemblies. The Investigation found that after being allowed to drift to the side of the runway without corrective action, the previously airworthy aircraft had hit a non-frangible edge light and the left main gear and then the nose landing gear had collapsed with a complete loss of directional control. The aircraft had then exited the side of the runway sustaining further damage.)
  • E55P, Blackbushe UK, 2015 (On 31 July 2015 a Saudi-operated Embraer Phenom on a private flight continued an unstabilised day visual approach to Blackbushe in benign weather conditions. The aircraft touched down with excess speed with almost 70% of the available landing distance behind the aircraft. It overran and was destroyed by impact damage and fire and all occupants died. The Investigation concluded that the combination of factors which created a very high workload for the pilot "may have saturated his mental capacity, impeding his ability to handle new information and adapt his mental model" leading to his continuation of a highly unstable approach.)
  • B738, Manila Philippines, 2018 (On 16 August 2018, a Boeing 737-800 made a stabilised approach to Manila during a thunderstorm with intermittent heavy rain but the crew lost adequate visual reference as they arrived over the runway. After a drift sideways across the 60 metre-wide landing runway, a veer off occurred and was immediately followed by a damaging collision with obstructions not compliant with prevailing airport safety standards. The Investigation found that the Captain had ignored go around calls from the First Officer and determined that the corresponding aircraft operator procedures were inadequate as well as faulting significant omissions in the Captain’s approach brief.)
  • A30B, Bratislava Slovakia, 2012 (On 16 November 2012, an Air Contractors Airbus A300 departed the left the side of the landing runway at Bratislava after an abnormal response to directional control inputs. Investigation found that incorrect and undetected re-assembly of the nose gear torque links had led to the excursion and that absence of clear instructions in maintenance manuals, since rectified, had facilitated this. It was also considered that the absence of any regulation requiring equipment in the vicinity of the runway to be designed to minimise potential damage to aircraft departing the paved surface had contributed to the damage caused by the accident.)

Ineffective Use of Retardation Methods

  • B739, Kathmandu Nepal, 2018 (On 19 April 2018, a Boeing 737-900 made a high speed rejected takeoff at Kathmandu in response to a configuration warning and overran the runway without serious consequences. The Investigation found that when a false Takeoff Configuration Warning caused by an out of adjustment switch had been annunciated just after V1, the Captain had decided to reject the takeoff because of concerns about the local terrain and locally adverse weather. It was noted that the aircraft operator did not provide criteria for rejecting takeoff up to or above the 80 knot crosscheck but that the Boeing reference QRH did so.)
  • B737, New York La Guardia USA, 2016 (On 27 October 2016, a Boeing 737-700 crew made a late touchdown on the runway at La Guardia and did not then stop before reaching the end of the runway and entered - and exited the side of - the EMAS before stopping. The Investigation concluded that the overrun was the consequence of a failure to go around when this was clearly necessary after a mishandled touchdown and that the Captain's lack of command authority and a lack of appropriate crew training provided by the Operator to support flight crew decision making had contributed to the failure to go around.)
  • A320, São Paulo Congonhas Brazil, 2007 (On 17 July 2007, the commander of a TAM Airlines Airbus A320 being operated with one thrust reverser locked out was unable to stop the aircraft leaving the landing runway at Congonhas at speed and it hit buildings and was destroyed by the impact and fire which followed killing all on board and others on the ground. The investigation attributed the accident to pilot failure to realise that the thrust lever of the engine with the locked out reverser was above idle, which by design then prevented both the deployment of ground spoilers and the activation of the pre-selected autobrake.)
  • DH8D, Hubli India, 2015 (On 8 March 2015, directional control of a Bombardier DHC 8-400 which had just completed a normal approach and landing was lost and the aircraft departed the side of the runway following the collapse of both the left main and nose landing gear assemblies. The Investigation found that after being allowed to drift to the side of the runway without corrective action, the previously airworthy aircraft had hit a non-frangible edge light and the left main gear and then the nose landing gear had collapsed with a complete loss of directional control. The aircraft had then exited the side of the runway sustaining further damage.)
  • B737, Chicago Midway USA, 2005 (On 8 December 2005, a delay in deploying the thrust reversers after a Boeing 737-700 touchdown at night on the slippery surface of the 1176 metre-long runway at Chicago Midway with a significant tailwind component led to it running off the end, subsequently departing the airport perimeter and hitting a car before coming to a stop. The Investigation concluded that pilots’ lack of familiarity with the autobrake system on the new 737 variant had distracted them from promptly deploying the reversers and that inadequate pilot training provision and the ATC failure to provide adequate braking action information had contributed.)

Continued Take Off

  • A343, Bogota Colombia, 2017 (On 11 March 2017, contrary to crew expectations based on their pre-flight takeoff performance calculation, an Airbus 340-300 taking off from the 3,800 metre-long at Bogata only became airborne just before the end of the runway. The Investigation found that the immediate reason for this was the inadequate rate of rotation achieved by the Training Captain performing the takeoff. However, it was also found that the operator’s average A340-300 rotation rate was less than would be achieved using handling recommendations which themselves would not achieve the expected performance produced by the Airbus takeoff performance software that reflected type certification findings.)
  • B734, Aberdeen UK, 2005 (Significant damage was caused to the tailplane and elevator of a Boeing 737-400 after the pavement beneath them broke up when take off thrust was applied for a standing start from the full length of the runway at Aberdeen. Although in this case neither outcome applied, the Investigation noted that control difficulties consequent upon such damage could lead to an overrun following a high speed rejected takeoff or to compromised flight path control airborne. Safety Recommendations on appropriate regulatory guidance for marking and construction of blast pads and on aircraft performance, rolling take offs and lead-on line marking were made.)
  • DHC6, Jomson Nepal, 2013 (On 16 May 2013, a DHC6-300 on a domestic passenger flight made a tailwind touchdown at excessive speed in the opposite direction of the of 740 metre-long runway to the notified direction in use and, after departing the runway to one side during deceleration, re-entered the runway and attempted to take off. This failed and the aircraft breached the perimeter fence and fell into a river. The Investigation identified inappropriate actions of the aircraft commander in respect of both the initial landing and his response to the subsequent runway excursion and also cited the absence of effective CRM.)
  • FA50 / Vehicle, Moscow Vnukovo Russia, 2014 (On 20 October 2014 a Dassault Falcon 50 taking off at night from Moscow Vnukovo collided with a snow plough which had entered the same runway without clearance shortly after rotation. Control was lost and all occupants died when it was destroyed by impact forces and post crash fire. The uninjured snow plough driver was subsequently discovered to be under the influence of alcohol. The Investigation found that the A-SMGCS effective for over a year prior to the collision had not been properly configured nor had controllers been adequately trained on its use, especially its conflict alerting functions.)
  • A320, Basel-Mulhouse-Freiburg France, 2014 (On 6 October 2014, an A320 crew requested, accepted and commenced an intersection takeoff at Basel using reduced thrust performance data based on the originally anticipated full length takeoff which would have given 65% more TODA. Recognition of the error and application of TOGA allowed the aircraft to get airborne just before the runway end but the Investigation found that a rejected take off from high speed would have resulted in an overrun and noted that despite changes to crew procedures after a similar event involving the same operator a year earlier, the relevant procedures were still conducive to error.)

Continued Landing Roll

  • B738, Pardubice Czech Republic, 2013 (On 25 August 2013, the type-experienced crew of a Boeing 737-800 operating with one thrust reverser locked out made a late touchdown with a significant but allowable tail wind component present and overran the end of the runway at Pardubice onto grass at 51 knots. No damage was caused to the aircraft and no emergency evacuation was performed. The Investigation concluded that the aircraft had been configured so that even for a touchdown within the TDZ, there would have been insufficient landing distance available. The flight crew were found not to have followed a number of applicable operating procedures.)
  • B738, Georgetown Guyana, 2011 (On 30 July 2011, a Boeing 737-800 overran the wet landing runway at Georgetown after a night non-precision approach, exited the airport perimeter and descended down an earth embankment. There were no fatalities but the aircraft sustained substantial damage and was subsequently declared a hull loss. The Investigation attributed the overrun to a touchdown almost two thirds of the way down the runway and failure to utilise the aircraft’s full deceleration capability. Loss of situational awareness and indecision as to the advisability of a go-around after a late touchdown became inevitable was also cited as contributory to the outcome.)
  • B738, Mangalore India, 2012 (On 14 August 2012, a Boeing 737-800 crew continued a previously stable ILS Cat 1 approach below the prescribed MDA without having acquired the prescribed visual reference. The aircraft was then damaged by a high rate of descent at the initial touchdown in the undershoot in fog. The occurrence was not reported by either the crew or the attending licensed engineer who discovered consequent damage to the aircraft. Dense fog had prevented ATC visual awareness. The Investigation attributed the undershoot to violation of minima and to both pilots looking out for visual reference leaving the flight instruments unmonitored.)
  • AT72, Copenhagen Denmark, 2013 (On 14 January 2013, selection of the power levers to ground idle after an ATR 72-200 touchdown at Copenhagen produced only one of the two expected low pitch indications. As the First Officer called 'one low pitch' in accordance with SOP, the Captain selected both engines into reverse. He was unable to prevent the resultant veer off the runway. After travelling approximately 350 metres on grass alongside the runway as groundspeed reduced, the runway was regained. A propeller control fault which would have prevented low pitch transition on the right engine was recorded but could not subsequently be replicated.)
  • E55P, Blackbushe UK, 2015 (On 31 July 2015 a Saudi-operated Embraer Phenom on a private flight continued an unstabilised day visual approach to Blackbushe in benign weather conditions. The aircraft touched down with excess speed with almost 70% of the available landing distance behind the aircraft. It overran and was destroyed by impact damage and fire and all occupants died. The Investigation concluded that the combination of factors which created a very high workload for the pilot "may have saturated his mental capacity, impeding his ability to handle new information and adapt his mental model" leading to his continuation of a highly unstable approach.)

Excessive Exit to Taxiway Speed

  • JS32, Torsby Sweden, 2014 (On 31 January 2014, an Estonian-operated BAE Jetstream 32 being used under wet lease to fulfil a government-funded Swedish domestic air service requirement landed long at night and overran the end of the runway. The Investigation concluded that an unstabilised approach had been followed by a late touchdown at excessive speed and that the systemic context for the occurrence had been a complete failure of the aircraft operator to address operational safety at anything like the level appropriate to a commercial operation. Failure of the responsible State Safety Regulator to detect and act on this situation was also noted.)

Frozen Deposits on Runway

  • B763, Halifax NS Canada, 2019 (On 4 March 2019, a Boeing 767-300 crew lost directional control of their aircraft as speed reduced following their touchdown at Halifax and were unable to prevent it being rotated 180° on the icy surface before coming to a stop facing the runway landing threshold. The Investigation found that the management of the runway safety risk by the airport authority had been systemically inadequate and that the communication of what was known by ATC about the runway surface condition had been incomplete. A number of subsequent corrective actions taken by the airport authority were noted.)
  • CRJX, Madrid Spain, 2015 (On 1 February 2015, a Bombardier CRJ 1000 departed from Pamplona with slush likely to have been in excess of the regulatory maximum depth on the runway. On landing at Madrid, the normal operation of the brake units was compromised by ice and one tyre burst damaging surrounding components and leaving debris on the runway, and the other tyre was slow to spin up and sustained a serious flat spot. The Investigation concluded that the Pamplona apron, taxiway and runway had not been properly cleared of frozen deposits and that the flight crew had not followed procedures appropriate for the prevailing conditions.)

Excessive Water Depth

  • B738, Mumbai India, 2018 (On 10 July 2018, a Boeing 737-800 marginally overran the wet landing runway at Mumbai after the no 1 engine thrust reverser failed to deploy when full reverse was selected after a late touchdown following a stabilised ILS approach. The Investigation found that the overrun was the result of touchdown with almost 40% of the runway behind the aircraft followed by the failure of normal thrust reverser deployment when attempted due to a failed actuator in one of the reversers. The prevailing moderate rain and the likelihood that dynamic aquaplaning had occurred were identified as contributory.)
  • A320, Sylt Germany, 2017 (On 30 September 2017, an Airbus A320 touched down late after an ILS approach to runway 32 at Sylt with a significant tailwind component being reported and failed to stop before overrunning the end of the runway and subsequently stopped on grass 80 metres beyond it. The Investigation noted that the calculated required landing distance was close to the landing distance available, the actual approach speed was 20 knots above the calculated one and that the aircraft had floated in the flare above a wet runway. It was concluded that the runway excursion was attributable to non-performance of a go-around.)

Intentional Veer Off Runway

  • C402, Virgin Gorda British Virgin Islands, 2017 (On 11 February 2017, a Cessna 402 failed to stop on the runway when landing at Virgin Gorda and was extensively damaged. The Investigation noted that the landing distance required was very close to that available with no safety margin so that although touchdown was normal, when the brakes failed to function properly, there was no possibility of safely rejecting the landing or stopping normally on the runway. Debris in the brake fluid was identified as causing brake system failure. The context was considered as the Operator’s inadequate maintenance practices and a likely similar deficiency in operational procedures and processes.)
  • AN72, Sao Tome, Sao Tome & Principe, 2017 (On 29 July 2017, an Antonov AN-74 crew sighted several previously unseen large “eagles” rising from the long grass next to the runway as they accelerated for takeoff at Sao Tome and, concerned about the risk of ingestion, made a high speed rejected takeoff but were unable to stop on the runway and entered a deep ravine just beyond it which destroyed the aircraft. The Investigation found that the reject had been unnecessarily delayed until above V1, that the crew forgot to deploy the spoilers which would have significantly increased the stopping distance and that relevant crew training was inadequate.)

Misaligned take off

  • E120, Amsterdam Netherlands, 2016 (On 18 January 2016, an Embraer 120 crew made a night takeoff from Amsterdam Runway 24 unaware that the aircraft was aligned with the right side runway edge lights. After completion of an uneventful flight, holes in the right side fuselage and damage to the right side propeller blades, the latter including wire embedded in a blade leading edge, were found. The Investigation concluded that poor visual cues guiding aircraft onto the runway at the intersection concerned were conducive to pilot error and noted that despite ATS awareness of intersection takeoff risks, no corresponding risk mitigation had been undertaken.)
  • DH8A, Rouyn-Noranda QC Canada, 2019 (On 23 January 2019, a Bombardier DHC8-100 failed to complete its intended night takeoff from Rouyn-Noranda after it had not been commenced on or correctly aligned parallel to the (obscured) centreline and the steadily increasing deviation had not been recognised until a runway excursion was imminent. The Investigation attributed this to the failure of the crew to pay sufficient attention to the external perspective provided by the clearly-visible runway edge lighting whilst also noting the Captain’s likely underestimation of the consequences of a significant flight deck authority gradient and a failure to fully follow relevant applicable operating procedures.)
  • AT72, Karup Denmark, 2016 (On 25 January 2016, an ATR 72-200 crew departing from and very familiar with Karup aligned their aircraft with the runway edge lights instead of the lit runway centreline and began take-off, only realising their error when they collided with part of the arrester wire installation at the side of the runway after which the take-off was rejected. The Investigation attributed the error primarily to the failure of the pilots to give sufficient priority to ensuring adequate positional awareness and given the familiarity of both pilots with the aerodrome noted that complacency had probably been a contributor factor.)
  • AT72, Cologne-Bonn Germany, 2020 (On 27 April 2020, an ATR 72-200 freighter crew attempted a night takeoff in good visibility aligned with the edge of runway 06 and did not begin rejecting it until within 20 knots of the applicable V1 despite hearing persistent regular noises which they did not recognise as edge light impacts and so completed the rejection on the same alignment. The Investigation noted both pilots’ familiarity with the airport and their regular work together and attributed their error to their low attention level and a minor distraction during the turnround after backtracking.)

Runway Condition not as reported

  • B738, Sochi Russia, 2018 (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.)
  • B763, Halifax NS Canada, 2019 (On 4 March 2019, a Boeing 767-300 crew lost directional control of their aircraft as speed reduced following their touchdown at Halifax and were unable to prevent it being rotated 180° on the icy surface before coming to a stop facing the runway landing threshold. The Investigation found that the management of the runway safety risk by the airport authority had been systemically inadequate and that the communication of what was known by ATC about the runway surface condition had been incomplete. A number of subsequent corrective actions taken by the airport authority were noted.)
  • CRJ9, Turku Finland, 2017 (On 25 October 2017, a Bombardier CRJ-900 crew lost directional control after touchdown at Turku in the presence of a tailwind component on a contaminated runway at night whilst heavy snow was falling. After entering a skid the aircraft completed a 180° turn before finally stopping 160 metres from the end of the 2500 metre-long runway. The Investigation found that skidding began immediately after touchdown with the aircraft significantly above the aquaplaning threshold and that the crew did not follow the thrust reverser reset procedure after premature deployment or use brake applications and aileron inputs appropriate to the challenging conditions.)

Related Articles

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