Accident and Serious Incident Reports: LOC
Accident and Serious Incident Reports: LOC
Definition
Reports relating to accidents or serious incidents which involved in flight Loss of Control as a significant causal factor.
The accident and serious incident reports are grouped together below according to causal factors which led to loss of control.
Airframe Structural Failure
On 1 August 2019, an Airbus A320 annunciated an abnormal gear status indication when retraction was attempted after takeoff. Soon afterwards, an aircraft part was observed by an aircraft following the same taxi route as the A320 and recovered. After completing relevant drills, the A320 returned and completed a landing with significant damage to the left main gear which was nevertheless locked down. The runway was vacated and passengers disembarked. The Investigation found that the cause of the problem was the cyclic fatigue of a pin linking the two parts of the left main gear torque link of manufacturing origin.
On 21 January 2019, a Piper PA46-310P en-route north northwest of Guernsey was reported missing and subsequently confirmed to have broken up in flight during an uncontrolled descent. The Investigation found that neither the pilot nor the aircraft involved were able to be used for commercial passenger flight operations but also found that although the direct cause of loss of control was unproven, it was most likely the consequence of carbon monoxide poisoning originating from an exhaust system leak. The safety implications arising from operation of private flights for commercial passenger transport purposes contrary to regulatory requirements were also highlighted.
On 25 March 2018, an ATR 42-500 main landing gear bay door weighing 15 kg detached shortly after a night descent had begun but this was unknown until the flight arrived at Aurillac. The Investigation found that the root cause of the detachment was a loose securing nut which had triggered a sequence of secondary failures within a single flight which culminated in the release of the door. It was concluded that the event highlighted specific and systemic weakness in relevant airworthiness documentation and practice in relation to the lost door and the use of fasteners on this aircraft type generally.
On 27 August 2016, debris from sudden uncontained failure of the left CFM56-7B engine of a Boeing 737-700 climbing through approximately FL 310 west southwest of Pensacola in day VMC penetrated the fuselage barrel and caused a rapid depressurisation. An emergency descent and a diversion to Pensacola followed without further event. The Investigation found that collateral damage had followed low-cycle fatigue cracking of a single fan blade due to a previously unrecognised weakness in the design of this on-condition component which, because it had not been detected during the engine certification process, meant its consequences “could not have been predicted”.
On 12 July 2013 an unoccupied and unpowered Boeing 787-8, remotely parked at London Heathrow after an arrival earlier the same day caught fire. An investigation found that the source of the fire was an uncontained thermal runaway in the lithium-metal battery within an Emergency Locator Transmitter (ELT). Fifteen Safety Recommendations, all but one to the FAA, were made as a result of the Investigation.
Significant Systems or Systems Control Failure
On 14 September 2021 the crew of a Saab S340B being used for type conversion training purposes were unable to cross start the left engine after it had been temporarily shut down to demonstrate single engine handling performance because the right starter-generator failed. A MAYDAY was declared and after prompt electrical load shedding, sufficient battery power remained to complete a successful diversion. The starter-generator failure was suspected to be attributable to its use whilst in service with a previous operator to support multiple starts at intervals which were insufficient to allow the unit to cool.
On 7 June 2021 an Embraer ERJ170 had just commenced its descent towards destination when both primary and secondary pitch trim systems failed resulting in excessive nose-down pitch control forces and an inoperative autopilot. The flight was completed without further event with the Pilot Flying using both hands on the control yoke to control pitch attitude manually. During the landing roll the nosewhweel steering system also failed. The pitch trim failure was attributed to probable jamming of the trim actuator due to water, possibly condensation, freezing within it. The steering system fault was attributed to a completely unrelated sensor failure.
On 23 February 2019, a Raytheon B200 King Air which had recently departed Saanen was passing FL155 for cleared altitude FL240 when a total electrical failure occurred. On subsequently making contact with ATC on a hand-held personal radio, the pilot advised his intention to exit controlled airspace and complete an already commenced visual diversion to Lausanne which was then done. It was found that failure to use the prescribed normal checklists had resulted in an undetected electrical system selection error which had led to the successive discharge of both main batteries when corresponding alerts and warnings also went unnoticed.
On 13 July 2018, a Boeing 737-800 cruising at FL370 at night experienced a sudden rapid depressurisation. An emergency descent to FL 090 followed but the cabin altitude was not manually controlled and after the cabin pressure had risen to that equivalent to 7000 feet below sea level, immediate equalisation of cabin and actual altitudes resulted in a second sudden depressurisation. Diversion to Frankfurt Hahn was completed without further event. The first depressurisation had resulted from a transient and rare pressure controller malfunction but passenger injuries were considered attributable to a complete absence of pressurisation control during the emergency descent.
On 6 August 2021, an Airbus A319 experienced uncommanded loss of both Flight Directors and the Flight Mode Annunciator and disconnection of both autopilot and autothrust in the climb. After levelling at FL350, significant inertial reference position inconsistencies were observed. A precautionary PAN was declared and the flight was completed. Investigation found that the cause was a momentary abnormal vertical shock load transferred to Inertial Reference System equipment through an overextended nose gear shock absorber by a sharp jolt during takeoff caused by a runway patch repair. Sensitivity of the particular inertial reference system installed on the aircraft was noted.
Degraded flight instrument display
On 23 February 2019, a Raytheon B200 King Air which had recently departed Saanen was passing FL155 for cleared altitude FL240 when a total electrical failure occurred. On subsequently making contact with ATC on a hand-held personal radio, the pilot advised his intention to exit controlled airspace and complete an already commenced visual diversion to Lausanne which was then done. It was found that failure to use the prescribed normal checklists had resulted in an undetected electrical system selection error which had led to the successive discharge of both main batteries when corresponding alerts and warnings also went unnoticed.
On 6 February 1996, a Boeing 757-200 took off from Puerto Plata at night despite awareness at the 80 knot check that the Captains altimeter was not working. Thereafter, the crew became confused as to their actual airspeed and lost control before the aircraft hit the sea surface less than five minutes after takeoff. The Investigation found that the Captain’s pitot probe was blocked and that the three pilots on the flight deck had become confused about which airspeed indications were reliable and had then not recovered from an aerodynamic stall which followed the wholly avoidable mismanagement of the aircraft flight path.
On 18 July 2018, an Airbus A330-300 failed to reject its night takeoff from Brisbane despite the absence of any airspeed indication for either pilot. A PAN call was made as a climb to FL110 continued. Once there, preparations for a somewhat challenging return were made and subsequently achieved. The Investigation noted multiple missed opportunities, including non-compliance with several procedural requirements, to detect that all pitot mast covers had remained in place and was extremely concerned that the takeoff had been continued rather than rejected. Flawed aircraft operator ground handling procedures and ineffective oversight of contractors were also deemed contributory.
On 9 June 2021, an Airbus A320 Captain performing a relatively light weight and therefore rapid-acceleration takeoff from London Heathrow recognised as the standard 100 knot call was imminent that he had no speed indication so announced and performed a high speed rejected takeoff. Subsequent maintenance inspection found that the left pitot mast was blocked by the nest of a seasonally active solitary flying insect, noting that the aircraft had previously been parked for 24 hours on a non-terminal stand. Similar events, including another rejected takeoff, then followed and a comprehensive combined Investigation found all were of similar origin.
On 7 February 2018, a Boeing 737-800 experienced an airspeed mismatch during takeoff on a post maintenance positioning flight but having identified the faulty system by reference to the standby instrumentation, the intended flight was completed without further event. After the recorded defect was then signed off as “no fault found” after a failure to follow the applicable fault-finding procedure, the same happened on the next (revenue) flight but with an air turnback made. The Investigation found that the faulty sensor had been fitted at build three years earlier with a contaminated component which had slowly caused sensor malfunction to develop.
Uncommanded AP disconnect
On 5 April 2019, a Boeing 737-500 crew declared an emergency shortly after departing Madrid Barajas after problems maintaining normal lateral, vertical or airspeed control of their aircraft in IMC. After two failed attempts at ILS approaches in unexceptional weather conditions, the flight was successfully landed at a nearby military airbase. The Investigation found that a malfunction which probably prevented use of the Captain’s autopilot found before departure was not documented until after the flight but could not find a technical explanation for inability to control the aircraft manually given that dispatch without either autopilot working is permitted.
On 4 March 2016, the flight crew of an ATR72-500 decided to depart from Manchester without prior ground de/anti icing treatment judging it unnecessary despite the presence of frozen deposits on the airframe and from rotation onwards found that manual forward control column input beyond trim capability was necessary to maintain controlled flight. The aircraft was subsequently diverted. The Investigation found that the problem had been attributable to ice contamination on the upper surface of the horizontal tailplane. It was considered that the awareness of both pilots of the risk of airframe icing had been inadequate.
On 27 February 2012, the crew of an Airbus A330 en route at night and crossing the East African coast at FL360 encountered sudden violent turbulence as they flew into a convective cell not seen on their weather radar and briefly lost control as their aircraft climbed 2000 feet with resultant minor injuries to two occupants. The Investigation concluded that the isolated and rapidly developing cell had not been detected because of crew failure to make proper use of their weather radar, but noted that activation of flight envelope protection and subsequent crew action to recover control had been appropriate.
On 20 July 2011, the flight crew of a Swiss European Avro RJ-100 on a positioning flight from Nuremburg to Zurich responded inappropriately to an unexpected ‘bank angle’ alert in IMC. Near loss of control followed during which a PAN was eventually declared. The situation was resolved by a belated actioning of the QRH checklist applicable to the failure symptoms experienced. The subsequent investigation attributed the event to inappropriate crew response to a failure of a single IRU and poor manual flying skill whilst the situation was resolved.
On 24 May 2013 the fan cowl doors on both engines of an Airbus A319 detached as it took off from London Heathrow. Their un-latched status after a routine maintenance input had gone undetected. Extensive structural and system damage resulted and a fire which could not be extinguished until the aircraft was back on the ground began in one engine. Many previously-recorded cases of fan cowl door loss were noted but none involving such significant collateral damage. Safety Recommendations were made on aircraft type certification in general, A320-family aircraft modification, maintenance fatigue risk management and aircrew procedures and training.
AP Status Awareness
On 23 February 2019, a Boeing 767-300 transitioned suddenly from a normal descent towards Houston into a steep dive and high speed terrain impact followed. The Investigation found that after neither pilot had noticed the First Officer’s inadvertent selection of go around mode during automated flight, the First Officer had then very quickly responded with an increasingly severe manual pitch-down, possibly influenced by a somatogravic illusion. He was found to have had a series of short air carrier employments terminating after failure to complete training, had deliberately and repeatedly sought to conceal this history and lacked sufficient aptitude and competency.
On 20 July 2011, the flight crew of a Swiss European Avro RJ-100 on a positioning flight from Nuremburg to Zurich responded inappropriately to an unexpected ‘bank angle’ alert in IMC. Near loss of control followed during which a PAN was eventually declared. The situation was resolved by a belated actioning of the QRH checklist applicable to the failure symptoms experienced. The subsequent investigation attributed the event to inappropriate crew response to a failure of a single IRU and poor manual flying skill whilst the situation was resolved.
On 20 October 2013, a Boeing 757-200 Co-Pilot believed his aircraft was at risk of stalling when he saw a sudden low airspeed indication on his display during a night descent and reacted by increasing thrust and making abrupt pitch-down inputs. Other airspeed indications remained unaffected. The Captain took control and recovery to normal flight followed. The excursion involved a significant Vmo exceedance, damage to and consequent failure of one of the hydraulic systems and passengers and cabin crew injuries. The false airspeed reading was attributed by the Investigation to transient Ice Crystal Icing affecting one of the pitot probes.
On 17 November 2013, the crew of a Boeing 737-500 failed to establish on the ILS at Kazan after not following the promulgated intermediate approach track due to late awareness of LNAV map shift. A go around was eventually initiated from the unstabilised approach but the crew appeared not to recognise that the autopilot used to fly the approach would automatically disconnect. Non-control followed by inappropriate control led to a high speed descent into terrain less than a minute after go around commencement. The Investigation found that the pilots had not received appropriate training for all-engine go arounds or upset recovery.
On 1 October 2014, an Embraer 190 made a very hard landing at Amsterdam after the flight crew failed to recognise that the aircraft had not been configured correctly for the intended automatic landing off the Cat 1 ILS approach being flown. They were slow to respond when no automatic flare occurred. The Investigation was unable to fully review why the configuration error had occurred or why it had not been subsequently detected but the recent type conversion of both the pilots involved was noted.
Non-normal FBW flight control status
On 14 September 2010, the crew of a Sichuan Airlines Airbus A319 continued an ILS approach into Wuxi despite awareness of adverse convective weather conditions at the airport. Their inattention to automation management then led to a low energy warning and the inappropriate response to this led to the activation of flight envelope protection quickly followed by a stall warning. Inappropriate response to this was followed by loss of control and a full stall and high rate of descent from which recovery was finally achieved less than 900 feet agl.
On 28 February 2018, an Airbus A320 would not rotate for a touch-and-go takeoff and flightpath control remained temporarily problematic and the aircraft briefly settled back onto the runway with the gear in transit damaging both engines. A very steep climb was then followed by an equally steep descent to 600 feet agl with an EGPWS ‘PULL UP’ activation before recovery. Pitch control was regained using manual stabiliser trim but after both engines stopped during a MAYDAY turnback, an undershoot touchdown followed. The root cause of loss of primary pitch control was determined as unapproved oil in the stabiliser actuator.
On 12 September 2015, an Airbus A320 autopilot and autothrust dropped out as it climbed out of Perth and multiple ECAM system messages were presented with intermittent differences in displayed airspeeds. During the subsequent turn back in Alternate Law, a stall warning was disregarded with no actual consequence. The Investigation attributed the problems to intermittently blocked pitot tubes but could not establish how this had occurred. It was also found that the priority for ECAM message display during the flight had been inappropriate and that the key procedure contained misleading information. These ECAM issues were subsequently addressed by the aircraft manufacturer.
On 5 May 2019, a Sukhoi RRJ-95B making a manually-flown return to Moscow Sheremetyevo after a lightning strike caused a major electrical systems failure soon after departure made a mismanaged landing which featured a sequence of three hard bounces of increasing severity. The third of these occurred with the landing gear already collapsed and structural damage and a consequential fuel-fed fire followed as the aircraft veered off the runway at speed. The subsequent evacuation was only partly successful and 41 of the 73 occupants died and 3 sustained serious injury. An Interim Report has been published.
On 21 November 2013, an A330 rejected its take off from Brisbane after an airspeed indication failure. Following maintenance intervention, a similar airspeed indication fault on the subsequent departure was reported to have been detected after V1. Once airborne, reversion to Alternate Law occurred and slat retraction failed. After an air turnback, it was discovered that the cause of both events was blockage of the No. 1 Pitot Head by a mud-dauber wasp nest which was created during the initial two hour turnround at Brisbane. Investigation of a 2014 event to a Boeing 737 at Brisbane with exactly the same causation was noted.
Loss of Engine Power
On 14 September 2021 the crew of a Saab S340B being used for type conversion training purposes were unable to cross start the left engine after it had been temporarily shut down to demonstrate single engine handling performance because the right starter-generator failed. A MAYDAY was declared and after prompt electrical load shedding, sufficient battery power remained to complete a successful diversion. The starter-generator failure was suspected to be attributable to its use whilst in service with a previous operator to support multiple starts at intervals which were insufficient to allow the unit to cool.
On 1 November 2021, a deHavilland DHC6-300 crew en-route to Fort Simpson realised that they had insufficient fuel on board to reach their intended destination and therefore decided to attempt a diversion to the nearest available airport at Fort Providence. As fuel available dwindled, one engine was shut down but after an inadvertent fuel tank selection, the initially intended diversion was no longer possible and a forced landing in a bog was successfully accomplished. The Training Captain involved had developed a habit of performing checklists silently and from memory after gaining all his professional pilot experience at the same operator.
On 3 January 2019, a Boeing 737-500 en-route to Port Harcourt experienced signs of intermittent distress to an engine which subsequently failed during final approach there. After a mismanaged initial response before and after a go around, the failed engine was eventually shut down. After a delay of about 20 minutes, an attempted second approach was discontinued when it could not be stabilised. A third approach was then successfully completed. The engine was damaged beyond economic repair and the Investigation found that the operator had been aware of the intermittent malfunction of both engines over several months but ignored it.
On 19 November 2020, the police operator of a DJI Matrice M210 UA lost control of it over Poole when it drifted beyond Visual Line Of Sight (VLOS) and communication ceased. It was subsequently damaged when colliding with a house in autoland mode. The Investigation found that a partial power failure had followed battery disconnection with its consequences not adequately communicated to the pilot. It faulted both the applicable UA User Manual content and the absence of sufficient UA status and detected wind information to the pilot. A failure to properly define VLOS was identified but not considered directly causal.
On 3 November 2020, a Boeing 767-300 departing Madrid had an explosive main gear tyre deflation just after passing V1 and tyre debris ingested by the adjacent engine led to its failure. After completing the take off on one engine and burning off excess fuel, the aircraft landed back four hours later without further event. The Investigation found that the cause of the deflation was a piece of unidentified debris of a size unlikely to be detected by normal visual runway inspection methods. It also found that there was scope for improvement in related airport and ATC emergency response procedures.
Crew Incapacitation
On 29 October 2019, an Airbus A321 was descending towards its destination, Kaohsiung, when the First Officer suddenly lost consciousness without warning. The Captain declared a MAYDAY and with cabin crew assistance, he was secured clear of the flight controls and given oxygen which appeared beneficial. He was then removed to the passenger cabin where a doctor recommended continuing oxygen treatment. On arrival, he had fully regained consciousness. Medical examination and tests both on arrival and subsequently were unable to identify a cause although a context of cumulative fatigue was considered likely after three consecutive nights of inadequate sleep.
On 27 September 2017, a Boeing 777-200LRF Captain left the flight deck to retrieve their crew meal about 40 minutes after departing Abu Dhabi but whilst doing so he collapsed unconscious in the galley and despite assistance subsequently died. A MAYDAY was declared and a diversion to Kuwait successfully completed by the remaining pilot. The Investigation determined that the cause of death was cardiopulmonary system collapse due to a stenosis in the coronary artery. It was noted that the Captain’s medical condition had been partially concealed from detection because of his unapproved use of potentially significant self-medication.
On 21 January 2019, a Piper PA46-310P en-route north northwest of Guernsey was reported missing and subsequently confirmed to have broken up in flight during an uncontrolled descent. The Investigation found that neither the pilot nor the aircraft involved were able to be used for commercial passenger flight operations but also found that although the direct cause of loss of control was unproven, it was most likely the consequence of carbon monoxide poisoning originating from an exhaust system leak. The safety implications arising from operation of private flights for commercial passenger transport purposes contrary to regulatory requirements were also highlighted.
On 15 August 2016, the cognitive condition of an Airbus A320 Captain deteriorated en-route to Riga and he assigned all flight tasks to the First Officer. When his condition deteriorated further, an off duty company First Officer travelling as a passenger was invited to occupy the flight deck supernumerary crew seat to assist. Once descent had commenced, the Captain and assisting First Officer swapped seats and the flight was thereafter completed without any further significant event. The Investigation concluded that the Captain’s serious physical and mental exhaustion had been the result of the combined effect of chronic fatigue and stress.
On 15 August 2018, a Boeing 737-300SF crew concerned about a small residual pressure in a bleed air system isolated after a fault occurred en-route then sought and were given non-standard further troubleshooting guidance by company maintenance which, when followed, led directly and indirectly to additional problems including successive incapacitation of both pilots and a MAYDAY diversion. The Investigation found that the aircraft concerned was carrying a number of relevant individually minor undetected defects which meant the initial crew response was not completely effective and prompted a request for in-flight assistance which was unnecessary and led to the further outcomes.
Flight Management Error
On 8 February 2021, an Embraer 500 Phenom 100 (9H-FAM) crew lost control of their aircraft shortly before the intended touchdown when it stalled due to airframe ice contamination. The resulting runway impact collapsed the nose and main gear, the latter causing fuel leak and resultant fire as the aircraft slid along the runway before veering off it. The Investigation found that flight in icing conditions during the approach had not been accompanied by the prescribed use of the airframe de-icing system and that such non compliance appeared to be routine and its dangers unappreciated.
On 23 January 2020, a Bombardier CRJ700 making a HUD-supported manual Cat 3a ILS approach to Lyon Saint-Exupéry in freezing fog conditions deviated from the required flight path localiser and reached a minimum of 265 feet agl before a go around was initiated without initially being flown in accordance with standard procedures. The Captain involved was relatively new to type and had not previously flown such an approach in actual low visibility conditions. The Investigation was not able to determine exactly what contributed to the approach and initial go around being misflown but identified a number of possible contributors.
On 31 July 2021, a Boeing 737-800 descending through an area of convective activity which was subject to a current SIGMET encountered some anticipated moderate turbulence whilst visually deviating around storm cells without reducing speed. When it appeared possible that the maximum speed may be exceeded because of turbulence, the autopilot was disconnected and a severe pitch up and then down immediately followed resulting in serious injuries to two of the four cabin crew and a passenger. This disconnection was contrary to the aircraft operator’s procedures and to the explicit training received by the pilot involved who was in command.
On 1 November 2021, a deHavilland DHC6-300 crew en-route to Fort Simpson realised that they had insufficient fuel on board to reach their intended destination and therefore decided to attempt a diversion to the nearest available airport at Fort Providence. As fuel available dwindled, one engine was shut down but after an inadvertent fuel tank selection, the initially intended diversion was no longer possible and a forced landing in a bog was successfully accomplished. The Training Captain involved had developed a habit of performing checklists silently and from memory after gaining all his professional pilot experience at the same operator.
On 23 February 2019, a Raytheon B200 King Air which had recently departed Saanen was passing FL155 for cleared altitude FL240 when a total electrical failure occurred. On subsequently making contact with ATC on a hand-held personal radio, the pilot advised his intention to exit controlled airspace and complete an already commenced visual diversion to Lausanne which was then done. It was found that failure to use the prescribed normal checklists had resulted in an undetected electrical system selection error which had led to the successive discharge of both main batteries when corresponding alerts and warnings also went unnoticed.
Flight Control Error
On 27 January 2020, an MD83 made an unstabilised tailwind non-precision approach to Mahshahr with a consistently excessive rate of descent and corresponding EGPWS Warnings followed by a very late nose-gear-first touchdown. It then overran the runway end, continued through the airport perimeter fence and crossed over a ditch before coming to a stop partly blocking a busy main road. The aircraft sustained substantial damage and was subsequently declared a hull loss but all occupants completed an emergency evacuation uninjured. The accident was attributed entirely to the actions of the Captain which included disregarding multiple standard operating procedures.
On 23 January 2020, a Bombardier CRJ700 making a HUD-supported manual Cat 3a ILS approach to Lyon Saint-Exupéry in freezing fog conditions deviated from the required flight path localiser and reached a minimum of 265 feet agl before a go around was initiated without initially being flown in accordance with standard procedures. The Captain involved was relatively new to type and had not previously flown such an approach in actual low visibility conditions. The Investigation was not able to determine exactly what contributed to the approach and initial go around being misflown but identified a number of possible contributors.
On 31 July 2021, a Boeing 737-800 descending through an area of convective activity which was subject to a current SIGMET encountered some anticipated moderate turbulence whilst visually deviating around storm cells without reducing speed. When it appeared possible that the maximum speed may be exceeded because of turbulence, the autopilot was disconnected and a severe pitch up and then down immediately followed resulting in serious injuries to two of the four cabin crew and a passenger. This disconnection was contrary to the aircraft operator’s procedures and to the explicit training received by the pilot involved who was in command.
On 23 October 2020, a Bombardier DHC8-400 was mishandled during the final stages of landing in slightly turbulent conditions when the Captain responded to a momentary increase in the rate of descent in the flare by increasing the pitch attitude instead of adding power which resulted in a tailstrike as the maximum pitch attitude without this happening was exceeded and structural damage resulted. The pilot involved had very considerable flying experience on other types but relatively little on the accident type and although the First Officer had more type experience he was less than half the age of the Captain.
On 29 November 2017, a Boeing 737-900 on an ILS approach at Atlanta became unstable after the autothrottle and autopilot were both disconnected and was erroneously aligned with an occupied taxiway parallel to the intended landing runway. A go-around was not commenced until the aircraft was 50 feet above the ground after which it passed low over another aircraft on the taxiway. The Investigation found that the Captain had not called for a go around until well below the Decision Altitude and had then failed to promptly take control when the First Officer was slow to begin climbing the aircraft.
Environmental Factors
On 27 January 2020, an MD83 made an unstabilised tailwind non-precision approach to Mahshahr with a consistently excessive rate of descent and corresponding EGPWS Warnings followed by a very late nose-gear-first touchdown. It then overran the runway end, continued through the airport perimeter fence and crossed over a ditch before coming to a stop partly blocking a busy main road. The aircraft sustained substantial damage and was subsequently declared a hull loss but all occupants completed an emergency evacuation uninjured. The accident was attributed entirely to the actions of the Captain which included disregarding multiple standard operating procedures.
On 8 February 2021, an Embraer 500 Phenom 100 (9H-FAM) crew lost control of their aircraft shortly before the intended touchdown when it stalled due to airframe ice contamination. The resulting runway impact collapsed the nose and main gear, the latter causing fuel leak and resultant fire as the aircraft slid along the runway before veering off it. The Investigation found that flight in icing conditions during the approach had not been accompanied by the prescribed use of the airframe de-icing system and that such non compliance appeared to be routine and its dangers unappreciated.
On 7 June 2021 an Embraer ERJ170 had just commenced its descent towards destination when both primary and secondary pitch trim systems failed resulting in excessive nose-down pitch control forces and an inoperative autopilot. The flight was completed without further event with the Pilot Flying using both hands on the control yoke to control pitch attitude manually. During the landing roll the nosewhweel steering system also failed. The pitch trim failure was attributed to probable jamming of the trim actuator due to water, possibly condensation, freezing within it. The steering system fault was attributed to a completely unrelated sensor failure.
On 25 July 2021, a Boeing 737-800 which had previously been manoeuvring visually around storm cells over the Alps during the initial descent into Nice turned back on track believing the avoidance action was complete but was then unable to avoid penetrating a further cell during which severe turbulence caused a serious injury to one of the cabin crew and a lesser injury to another. Multiple aircraft in the area had been simultaneously requesting track deviations at the time with ATC displays not showing weather returns. In the absence of plans to introduce this, a corresponding safety recommendation was made.
On 11 September 2021, a Boeing 737-800 was instructed to discontinue an ILS approach to runway 34 at Aberdeen, climb to 3000 feet and turn left onto a westerly heading. With the Autopilot disconnected it approached the cleared altitude but before reaching it rapidly descended to just over 1500 feet above terrain before climbing away, the whole event occurring in IMC. The episode was attributed to crew overload in manual flight consequent upon the combination of the heading instructions, flap configuration changes and a complete absence of pitch trim. Both pilots’ pandemic-related lack of the usual operational recency was noted.
Bird or Animal Strike
On 28 September 2012, control of a Sita Air Dornier 228 being flown by an experienced pilot was lost at approximately 100 feet aal after take off from Kathmandu in benign daylight weather conditions and the aircraft stalled without obvious attempt at recovery before impacting the ground where a fire broke out. All occupants were killed and the aircraft was destroyed. The comprehensive investigation found that insufficient engine thrust was being delivered to sustain flight but, having eliminated engine bird ingestion and aircraft loading issues, was unable to establish any environmental, airworthiness or loading issue which might have caused this.
On 19 January 2013, a Rolls Royce Trent 700-powered Virgin Atlantic Airbus A330-300 hit some medium sized birds shortly after take off from Orlando, sustaining airframe impact damage and ingesting one bird into each engine. Damage was subsequently found to both engines although only one indicated sufficient malfunction - a complete loss of oil pressure - for an in-flight shutdown to be required. After declaration of a MAYDAY, the return to land overweight was completed uneventfully. The investigation identified an issue with the response of the oil pressure detection and display system to high engine vibration events and recommended modification.
On 3 August 2006, a Qantas Boeing 767-300 encountered a large flock of birds during rotation and sustained multiple strikes on many parts of the aircraft. Left engine vibration immediately increased but as reducing thrust also reduced the vibration, it was decided following consultation with maintenance to continue to the planned destination, Sydney.
On 21 June 2017, an Airbus A320 number 2 engine began vibrating during the takeoff roll at Delhi after a bird strike. After continuing the takeoff, the Captain subsequently shut down the serviceable engine and set the malfunctioning one to TO/GA and it was several minutes before the error was recognised. After an attempted number 1 engine restart failed because an incorrect procedure was followed, a second attempt succeeded. By this time inattention to airspeed loss had led to ALPHA floor protection activation. Eventual recovery was followed by a return to land with the malfunctioning engine at flight idle.
On 10 November 2008, a Boeing 737-800 about to land at Rome Ciampino Airport flew through a large and dense flock of starlings, which appeared from below the aircraft. After the crew had made an unsuccessful attempt to go around, they lost control due to malfunction of both engines when full thrust was applied and a very hard impact half way along the runway caused substantial damage to the aircraft. The Investigation concluded that the Captain s decision to attempt a go around after the encounter was inappropriate and that bird risk management measures at the airport had been inadequate.
Aircraft Loading
On 27 January 2020, an MD83 made an unstabilised tailwind non-precision approach to Mahshahr with a consistently excessive rate of descent and corresponding EGPWS Warnings followed by a very late nose-gear-first touchdown. It then overran the runway end, continued through the airport perimeter fence and crossed over a ditch before coming to a stop partly blocking a busy main road. The aircraft sustained substantial damage and was subsequently declared a hull loss but all occupants completed an emergency evacuation uninjured. The accident was attributed entirely to the actions of the Captain which included disregarding multiple standard operating procedures.
On 21 July 2020, a Boeing 737-800 flight crew identified significant discrepancies when comparing their Operational Flight Plan weights and passengers by category with those on the Loadsheet presented. After examining them and concluding that the differences were plausible based on past experience, the loadsheet figures were used for takeoff performance purposes with no adverse consequences detected. It was found that a system-wide IT upgrade issue had led to the generation of incorrect loadsheets and that ineffective communication and an initially ineffective response within the operator had delayed effective risk resolution although without any known flight safety-related consequences.
On 17 December 2017, it was discovered after completion of an Airbus A330-300 passenger flight from Sydney to Bejing that freight loading had not been correctly documented on the load and trim sheet presented to and accepted by the Captain and as a result, the aircraft had exceeded its certified MTOW on departure. The Investigation found that the overload finding had not been promptly reported or its safety significance appreciated, that the error had its origin in related verbal communications during loading and noted that the aircraft operator had since made a series of improvements to its freight loading procedures.
On 4 August 2018, a Junkers Ju-52 making a low level sightseeing flight through the Swiss Alps crashed killing all 20 occupants after control was lost when it stalled after encountering unexceptional windshear. The Investigation found that the pilots had created the conditions which led to the stall and then been unable to recover from it and concluded that the accident was a direct consequence of their risky behaviour. It found that such behaviour was common at the operator, that the operator was being managed without any regard to operational risk and that safety regulatory oversight had been systemically deficient.
On 29 April 2013, a Boeing 747-400 freighter departed controlled flight and impacted terrain shortly after taking off from Bagram and was destroyed by the impact and post crash fire and all occupants were killed. The Investigation found that a sudden and significant load shift had occurred soon after take off which damaged hydraulic systems Nos. 1 and 2 and the horizontal stabilizer drive mechanism components as well as moving the centre of gravity aft and out of the allowable flight envelope. The Load shift was attributed to the ineffective securing techniques employed.
Malicious Interference
On 8 January 2020, a Boeing 737-800 was destroyed by a ground to air missile when climbing through approximately 4800 feet aal three minutes after takeoff from Tehran for Kiev and its 176 occupants were killed. The Investigation is continuing but it has been confirmed that severe damage and an airborne fire followed the detonation of a proximity missile after a military targeting error, with subsequent ground impact. It is also confirmed that the flight was following its ATC clearance and that a sequence of four separate errors led to two missiles being fired at the aircraft.
Temporary Control Loss
On 25 July 2021, a Boeing 737-800 which had previously been manoeuvring visually around storm cells over the Alps during the initial descent into Nice turned back on track believing the avoidance action was complete but was then unable to avoid penetrating a further cell during which severe turbulence caused a serious injury to one of the cabin crew and a lesser injury to another. Multiple aircraft in the area had been simultaneously requesting track deviations at the time with ATC displays not showing weather returns. In the absence of plans to introduce this, a corresponding safety recommendation was made.
On 11 September 2021, a Boeing 737-800 was instructed to discontinue an ILS approach to runway 34 at Aberdeen, climb to 3000 feet and turn left onto a westerly heading. With the Autopilot disconnected it approached the cleared altitude but before reaching it rapidly descended to just over 1500 feet above terrain before climbing away, the whole event occurring in IMC. The episode was attributed to crew overload in manual flight consequent upon the combination of the heading instructions, flap configuration changes and a complete absence of pitch trim. Both pilots’ pandemic-related lack of the usual operational recency was noted.
On 20 December 2019, an Airbus A318 making a tailwind ILS approach to Toulon-Hyères with the autopilot engaged and expecting to intercept the glideslope from above had not done so when reaching the pre-selected altitude and after levelling off, it then rapidly entered a steep climb as it captured the glideslope false upper lobe and the automated stall protection system was activated. Not fully following the recovery procedure caused a second stall protection activation before a sustained recovery was achieved. The Investigation noted Captain's relative inexperience in that rank and a First Officer's inexperience on type.
On 26 July 2017, a Hawker Beechcraft 850 left wing sustained extensive damage when it contacted the runway at Mykonos during a 2.7g touchdown after an unstabilised approach in benign weather conditions had been continued. The Investigation found that the aircraft was airworthy prior to a temporary loss of control at touchdown which occurred after stick pusher activation due to the airspeed being more than 20 knots below the applicable reference speed and only three knots above the applicable stall speed. The monitoring of the First Officer’s approach by the Captain was minimal and late with few alert calls given.
On 24 July 2019, whilst a Sikorsky S92A was commencing a second missed approach at the intended destination platform, visual contact was acquired and it was decided that an immediate visual approach could be made. However control was then temporarily lost and the aircraft almost hit the sea surface before recovery involving engine overtorque and diversion back to Halifax. The Investigation concluded that the crew had failed to safely control the aircraft energy state in a degraded visual environment allowing it to enter a vortex ring condition. As context, operator procedures, Flight Manual content and regulatory requirements were all faulted.
Extreme Bank
On 25 July 2021, a Boeing 737-800 which had previously been manoeuvring visually around storm cells over the Alps during the initial descent into Nice turned back on track believing the avoidance action was complete but was then unable to avoid penetrating a further cell during which severe turbulence caused a serious injury to one of the cabin crew and a lesser injury to another. Multiple aircraft in the area had been simultaneously requesting track deviations at the time with ATC displays not showing weather returns. In the absence of plans to introduce this, a corresponding safety recommendation was made.
On 6 February 1996, a Boeing 757-200 took off from Puerto Plata at night despite awareness at the 80 knot check that the Captains altimeter was not working. Thereafter, the crew became confused as to their actual airspeed and lost control before the aircraft hit the sea surface less than five minutes after takeoff. The Investigation found that the Captain’s pitot probe was blocked and that the three pilots on the flight deck had become confused about which airspeed indications were reliable and had then not recovered from an aerodynamic stall which followed the wholly avoidable mismanagement of the aircraft flight path.
On 23 January 2020, a Cessna S550 departed George to conduct a calibration flight under VFR with three persons on board and was about to begin a DME arc at 4,000 feet QNH when control was lost after entering IMC. Recovery from a significant descent which followed was not achieved before the aircraft hit mountainous terrain 1,800 feet below and was destroyed killing all occupants. The Investigation considered that the transition into IMC had probably occurred without preparation and that the inability of the crew to perform a prompt recovery reflected unfavourably on the conduct of the aircraft operator.
On 21 January 2019, a Piper PA46-310P en-route north northwest of Guernsey was reported missing and subsequently confirmed to have broken up in flight during an uncontrolled descent. The Investigation found that neither the pilot nor the aircraft involved were able to be used for commercial passenger flight operations but also found that although the direct cause of loss of control was unproven, it was most likely the consequence of carbon monoxide poisoning originating from an exhaust system leak. The safety implications arising from operation of private flights for commercial passenger transport purposes contrary to regulatory requirements were also highlighted.
On 30 August 2018, a Boeing 747-400F making a crosswind landing at Hong Kong which was well within limits veered and rolled abnormally immediately after touchdown and runway impact damaged the two right side engines. The Investigation found that the flight was an experienced Captain’s line check handling sector and concluded that a succession of inappropriate control inputs made at and immediately after touchdown which caused the damage may have been a consequence of the Check Captain’s indication just before touchdown that he was expecting a landing using an alternative technique to the one he was familiar with.
Extreme Pitch
On 6 February 1996, a Boeing 757-200 took off from Puerto Plata at night despite awareness at the 80 knot check that the Captains altimeter was not working. Thereafter, the crew became confused as to their actual airspeed and lost control before the aircraft hit the sea surface less than five minutes after takeoff. The Investigation found that the Captain’s pitot probe was blocked and that the three pilots on the flight deck had become confused about which airspeed indications were reliable and had then not recovered from an aerodynamic stall which followed the wholly avoidable mismanagement of the aircraft flight path.
On 20 December 2019, an Airbus A318 making a tailwind ILS approach to Toulon-Hyères with the autopilot engaged and expecting to intercept the glideslope from above had not done so when reaching the pre-selected altitude and after levelling off, it then rapidly entered a steep climb as it captured the glideslope false upper lobe and the automated stall protection system was activated. Not fully following the recovery procedure caused a second stall protection activation before a sustained recovery was achieved. The Investigation noted Captain's relative inexperience in that rank and a First Officer's inexperience on type.
On 23 January 2020, a Cessna S550 departed George to conduct a calibration flight under VFR with three persons on board and was about to begin a DME arc at 4,000 feet QNH when control was lost after entering IMC. Recovery from a significant descent which followed was not achieved before the aircraft hit mountainous terrain 1,800 feet below and was destroyed killing all occupants. The Investigation considered that the transition into IMC had probably occurred without preparation and that the inability of the crew to perform a prompt recovery reflected unfavourably on the conduct of the aircraft operator.
On 21 January 2019, a Piper PA46-310P en-route north northwest of Guernsey was reported missing and subsequently confirmed to have broken up in flight during an uncontrolled descent. The Investigation found that neither the pilot nor the aircraft involved were able to be used for commercial passenger flight operations but also found that although the direct cause of loss of control was unproven, it was most likely the consequence of carbon monoxide poisoning originating from an exhaust system leak. The safety implications arising from operation of private flights for commercial passenger transport purposes contrary to regulatory requirements were also highlighted.
On 25 November 2019, an Airbus A330-300 being used for type conversion line training was involved in a landing tailstrike at Yangon during the trainee senior Captain’s first line training flight in benign daylight conditions. The Investigation noted that the optional tailstrike prevention system was not installed on the aircraft involved and found that the operator’s standard calls for excessive pitch during landing had not been made, that the trainee had misinterpreted the Training Captain’s pitch attitude guidance during the landing and that the Training Captain was only used to having to take over control when working with junior pilots.
Last Minute Collision Avoidance
On 14 February 2012 a Latvian-operated Saab 340 acknowledged an ATC clearance to make a procedural ILS approach to Mariehamn and then completely disregarded the clearance by setting course direct to the aerodrome. Subsequently, having lost situational awareness, repeated GPWS PULL UP warnings at night in VMC were ignored as control of the aircraft was lost with a recovery only achieved an estimated 2 seconds before ground impact would have occurred and then followed by more ignored PULL UP Warnings due to continued proximity to terrain before the runway was sighted and a landing achieved.
On 15 December 2014, the Captain of a Saab 2000 lost control of his serviceable aircraft after a lightning strike when he attempted to control the aircraft manually without first disconnecting the autopilot and despite the annunciation of a series of related alerts. The aircraft descended from 4,000 feet to 1,100 feet at up to 9,500 fpm and 80 knots above Vmo. A fortuitous transient data transmission fault caused autopilot disconnection making it possible to respond to EGPWS 'SINK RATE' and 'PULL UP' Warnings. The Investigation concluded that limitations on autopilot disconnection by pilot override were contrary to the type certification of most other transport aircraft.
On 3 January 3 2004, a Boeing 737-300 being operated by Flash Airlines on a passenger charter flight from Sharm el-Sheikh Egypt to Cairo for a refuelling stop en route to Paris CDG crashed into the sea 2½ minutes after a night take off into VMC and was destroyed and all 148 occupants killed. The Investigation was unable to establish a Probable Cause but found evidence of AP status confusion and the possibility of distraction leading to insufficient attention being paid to flight path control.
Hard landing
On 27 January 2020, an MD83 made an unstabilised tailwind non-precision approach to Mahshahr with a consistently excessive rate of descent and corresponding EGPWS Warnings followed by a very late nose-gear-first touchdown. It then overran the runway end, continued through the airport perimeter fence and crossed over a ditch before coming to a stop partly blocking a busy main road. The aircraft sustained substantial damage and was subsequently declared a hull loss but all occupants completed an emergency evacuation uninjured. The accident was attributed entirely to the actions of the Captain which included disregarding multiple standard operating procedures.
On 8 February 2021, an Embraer 500 Phenom 100 (9H-FAM) crew lost control of their aircraft shortly before the intended touchdown when it stalled due to airframe ice contamination. The resulting runway impact collapsed the nose and main gear, the latter causing fuel leak and resultant fire as the aircraft slid along the runway before veering off it. The Investigation found that flight in icing conditions during the approach had not been accompanied by the prescribed use of the airframe de-icing system and that such non compliance appeared to be routine and its dangers unappreciated.
On 23 October 2020, a Bombardier DHC8-400 was mishandled during the final stages of landing in slightly turbulent conditions when the Captain responded to a momentary increase in the rate of descent in the flare by increasing the pitch attitude instead of adding power which resulted in a tailstrike as the maximum pitch attitude without this happening was exceeded and structural damage resulted. The pilot involved had very considerable flying experience on other types but relatively little on the accident type and although the First Officer had more type experience he was less than half the age of the Captain.
On 25 December 2016, a type-experienced ATR72-600 Captain bounced the aircraft twice nose gear first whilst attempting a night landing at Semarang and during a third bounce on the right main gear only, it collapsed. The aircraft drifted right and after two further bounces began to decelerate and came to a stop. The Investigation found that after a normally-flown approach, the aircraft had not been flared and effective recovery action had not followed the bounce. It was concluded that the Captain had been subject to a visual illusion which had distorted his perception of height above the runway.
On 19 January 2021, a Boeing 737-400SF on an ILS approach to Exeter became unstabilised below 500 feet but despite multiple EGPWS ‘SINK RATE’ Alerts, a go-around was not initiated. The subsequent touchdown recorded 3.8g and caused such extensive damage that the aircraft was declared a hull loss. The Investigation found that the First Officer, who had more hours flying experience than the 15,000 hour Captain, had failed to adequately control the flight path below 500 feet and noted that whilst the Captain had commented on the excessive rate of descent, he had not called for a go around.
Take off Trim Setting
On 2 April 2012, the crew of an ATR72-200 which had just taken off from Tyumen lost control of their aircraft when it stalled after the flaps were retracted and did not recover before it crashed and caught fire killing or seriously injuring all occupants. The Investigation found that the Captain knew that frozen deposits had accumulated on the airframe but appeared to have been unaware of the danger of not having the airframe de-iced. It was also found that the crew had not recognised the stall when it occurred and had overpowered the stick pusher and pitched up.
On 25 January 2010, a Boeing 737-800 being operated by Ethiopian Airlines on a scheduled passenger flight from Beirut to Addis Ababa in night IMC disappeared from ATC radar soon after departure from Runway 21 and was subsequently found to have impacted the sea in an unintentional out of control condition some five miles south west of the airport less than five minutes after getting airborne Impact resulted in the destruction of the aircraft and the death of all 90 occupants.
On 18 January 2007 an ATR 42-300 freighter developed a control difficulty just after a night take off from Stansted UK, which led the flight crew to declare an emergency and undertake an immediate return to land. The landing was uneventful but the approach flown was unstable, with EGPWS warnings, and the origin of the handling difficulty was considered to be, in part, due to inappropriate control inputs by one of the pilots.
Incorrect Thrust Computed
On 27 January 2020, an MD83 made an unstabilised tailwind non-precision approach to Mahshahr with a consistently excessive rate of descent and corresponding EGPWS Warnings followed by a very late nose-gear-first touchdown. It then overran the runway end, continued through the airport perimeter fence and crossed over a ditch before coming to a stop partly blocking a busy main road. The aircraft sustained substantial damage and was subsequently declared a hull loss but all occupants completed an emergency evacuation uninjured. The accident was attributed entirely to the actions of the Captain which included disregarding multiple standard operating procedures.
On 26 February 2020, an Airbus A330-300 tailstrike occurred during rotation for takeoff from Zurich and was not detected by the crew who completed the planned 7½ hour flight to Nairobi before learning that the aircraft was not airworthy as a result. The Investigation concluded that the tailstrike had been the direct result of the crew’s use of inappropriate inputs to their takeoff performance calculation on the variable headwind encountered during the takeoff and noted a very similar event had previously occurred to the same aircraft type operated by an airline within the same overall ownership.
On 14 April 2012, a Titan Airways Boeing 737-300 attempted to take off from Chambery with incorrect reference speeds taken from the EFB used for performance calculations. As a consequence, the pressure hull was damaged by a tail strike during take off, although not sufficiently to affect cabin pressure during the subsequent flight. The Investigation concluded that the accident raised regulatory issues in respect of the general design and use of EFB computers to calculate performance data.
On 27 October 2017, an Embraer E195-200 missed approach was attempted in response to a predictive windshear alert on short final at Salzburg without ensuring sufficient engine thrust was set and when a stall warning followed, the correct recovery procedure was not initiated until over a minute had elapsed. Thereafter, following two holds, an approach and landing was completed without further event. The operator did not report the event in a timely or complete manner and it was therefore not possible to identify it as a Serious Incident requiring an independent investigation until almost three months after it had occurred.
On 29 March 2018, an augmented Boeing 787-9 crew completed an uneventful takeoff from Tel Aviv on a type conversion line check flight for one of the First Officers in the crew. After getting airborne, the crew found that all performance calculations including that for takeoff had been made on the basis of a Zero Fuel Weight which was 40 tonnes below the actual figure of 169 tonnes. The Investigation found that it was highly probable that automatic reduction in commanded pitch-up when rotation was attempted at too low a speed had prevented an accident during or soon after liftoff.
Unintended transitory terrain contact
On 2 January 2022, an Airbus A350-1000 floated during the landing flare at London Heathrow and when a go-around was commenced, a tail strike accompanied main landing gear runway contact. A subsequent further approach during which the Captain took over as handling pilot was completed uneventfully. The Investigation attributed the tailstrike to a full pitch up input made simultaneously with the selection of maximum thrust when very close to the runway surface, noting that although the initial touchdown had been just beyond the touchdown zone, 2,760 metres of runway remained ahead when the go around decision was made.
On 10 September 2017, the First Officer of a Gulfstream G550 making an offset non-precision approach to Paris Le Bourget failed to make a correct visual transition and after both crew were initially slow to recognise the error, an unsuccessful attempt at a low-level corrective realignment followed. This had not been completed when the auto throttle set the thrust to idle at 50 feet whilst a turn was being made over the runway ahead of the displaced threshold and one wing was in collision with runway edge lighting. The landing attempt was rejected and the Captain took over the go-around.
On 26 February 2020, an Airbus A330-300 tailstrike occurred during rotation for takeoff from Zurich and was not detected by the crew who completed the planned 7½ hour flight to Nairobi before learning that the aircraft was not airworthy as a result. The Investigation concluded that the tailstrike had been the direct result of the crew’s use of inappropriate inputs to their takeoff performance calculation on the variable headwind encountered during the takeoff and noted a very similar event had previously occurred to the same aircraft type operated by an airline within the same overall ownership.
On 14 March 2017, control of a Sikorsky S92A positioning in very poor visibility at 200 feet over the sea in accordance with an obstacle-marked FMS ground track in order to refuel at a coastally-located helipad was lost after it collided with late-sighted terrain ahead before crashing into the sea killing all on board. The Investigation attributed the accident to the lack of crew terrain awareness but found a context of inadequate safety management at the operator, the comprehensively ineffective regulatory oversight of the operation and confusion as to responsibility for State oversight of its contract with the operator.
On 9 February 2020, the tail strike prevention system on a Boeing 787-9 was annunciated during takeoff from London Heathrow in gusting crosswind conditions. Permission to hold at 6000 feet to conduct the response procedure was given and since this procedure did not permit pressurisation, an overweight return to land followed. The Investigation found that although the tail strike protection system had returned the pitch rate to the correct one after an exceedence just before commencing rotation, lateral control inputs then resulted in a decrease in lift resulting in the tail contact angle being reached whilst still on the runway.
Collision Damage
On 15 January 2021, the pilot of a DJI Inspire 2 UAV being operated on a contracted aerial work task under a conditional permit lost control of it and, after it exitied the approved operating area, the UAV collided with the window of a hotel guest room causing consequential minor injuries to the occupant. The Investigation found that the loss of control was attributable to “strong magnetic interference” almost immediately after takeoff which caused the compass to feed unreliable data to the Internal Management Unit which destabilised its accelerometer and led to the loss of directional control which resulted in the collision.
On 16 June 2021, a Boeing 737-400 was taxiing for departure at night after push back from stand when the ground crew who completed the push back arrived back at their base in the tug and realised that the tow bar they had used was not attached to it. The aircraft was prevented from taking off and it was then found that it had taxied over the unseen towbar and sustained damage to both nose gear tyres such that replacement was necessary. The Investigation concluded neither ground crew had checked that the area immediately ahead of the aircraft was clear.
On 30 August 2018, a Boeing 747-400F making a crosswind landing at Hong Kong which was well within limits veered and rolled abnormally immediately after touchdown and runway impact damaged the two right side engines. The Investigation found that the flight was an experienced Captain’s line check handling sector and concluded that a succession of inappropriate control inputs made at and immediately after touchdown which caused the damage may have been a consequence of the Check Captain’s indication just before touchdown that he was expecting a landing using an alternative technique to the one he was familiar with.
On 14 July 2019, after control of a DJI-Inspire 2 UA was lost, it descended into people on the ground under power causing multiple minor injuries. The Investigation found that “professional drone pilots” were operating the UA in gross breach of the approval obtained, had deleted all recorded controller evidence of the accident flight and that their account of the loss of control was not compatible with the evidence recovered from the UA. It also noted that the risk of injury to third parties was increased by the absence of protection around the propellers which was not a regulatory requirement.
On 6 July 2013, an Asiana Boeing 777-200 descended below the visual glidepath on short finals at San Francisco after the pilots failed to notice that their actions had reduced thrust to idle. Upon late recognition that the aircraft was too low and slow, they were unable to recover before the aircraft hit the sea wall and the tail detached. Control was lost and the fuselage eventually hit the ground. A few occupants were ejected at impact but most managed to evacuate subsequently and before fire took hold. The Probable Cause of the accident was determined to be the mismanagement of the aircraft by the pilots.
Incorrect Aircraft Configuration
On 15 August 2015, an Airbus A321 on approach to Charlotte commenced a go around but following a temporary loss of control as it did so then struck approach and runway lighting and the undershoot area sustaining a tail strike before climbing away. The Investigation noted that the 2.1g impact caused substantial structural damage to the aircraft and attributed the loss of control to a small microburst and the crew’s failure to follow appropriate and recommended risk mitigations despite clear evidence of risk given by the aircraft when it went around and available visually.
On 16 January 2018, a McDonnell Douglas MD-82 attempting to land at Tarbes was subject to gross mishandling by the crew and the approach became unstable. A subsequent low level go-around attempt was then made without setting sufficient thrust which resulted in sustained and close proximity to terrain at an airspeed close to stall entry before the required thrust was eventually applied. The Investigation was hindered by non-reporting of the event but was able to conclude that multiple pilot errors in a context of poor crew coordination during the approach had caused confusion when the go around was initiated.
On 23 February 2019, a Boeing 767-300 transitioned suddenly from a normal descent towards Houston into a steep dive and high speed terrain impact followed. The Investigation found that after neither pilot had noticed the First Officer’s inadvertent selection of go around mode during automated flight, the First Officer had then very quickly responded with an increasingly severe manual pitch-down, possibly influenced by a somatogravic illusion. He was found to have had a series of short air carrier employments terminating after failure to complete training, had deliberately and repeatedly sought to conceal this history and lacked sufficient aptitude and competency.
On 26 August 2019, an Airbus A320 attempted two autopilot-engaged non-precision approaches at Birmingham in good weather before a third one was successful. Both were commenced late and continued when unstable prior to eventual go-arounds, for one of which the aircraft was mis-configured causing an ‘Alpha Floor’ protection activation. A third non-precision approach was then completed without further event. The Investigation noted an almost identical event involving the same operator four months later, observing that all three discontinued approaches appeared to have originated in confusion arising from a slight difference between the procedures of the aircraft operator and AIP plates.
On 10 January 2011, a Europe Airpost Boeing 737-300 taking off from Montpelier after repainting had just rotated for take off when the leading edge slats extended from the Intermediate position to the Fully Extended position and the left stick shaker was activated as a consequence of the reduced stalling angle of attack. Initial climb was sustained and soon afterwards, the slats returned to their previous position and the stick shaker activation stopped. The unexpected configuration change was attributed to paint contamination of the left angle of attack sensor, the context for which was inadequate task guidance.
Aerodynamic Stall
On 8 February 2021, an Embraer 500 Phenom 100 (9H-FAM) crew lost control of their aircraft shortly before the intended touchdown when it stalled due to airframe ice contamination. The resulting runway impact collapsed the nose and main gear, the latter causing fuel leak and resultant fire as the aircraft slid along the runway before veering off it. The Investigation found that flight in icing conditions during the approach had not been accompanied by the prescribed use of the airframe de-icing system and that such non compliance appeared to be routine and its dangers unappreciated.
On 15 January 2023, an ATR 72-500 positioning visually for an approach to Pokhara was observed to suddenly depart normal flight and impact terrain a few seconds later. All 72 occupants were killed and the aircraft destroyed by impact. A Preliminary Report published by the Accident Investigation Commission has indicated that a stall warning and subsequent loss of control was preceded by an apparently unintentional and subsequently undetected selection of both propellers to feather in response to a call for Flaps 30. The Training Captain in command was supervising the Captain flying during familiarisation training for the new Pokhara airport.
On 6 February 1996, a Boeing 757-200 took off from Puerto Plata at night despite awareness at the 80 knot check that the Captains altimeter was not working. Thereafter, the crew became confused as to their actual airspeed and lost control before the aircraft hit the sea surface less than five minutes after takeoff. The Investigation found that the Captain’s pitot probe was blocked and that the three pilots on the flight deck had become confused about which airspeed indications were reliable and had then not recovered from an aerodynamic stall which followed the wholly avoidable mismanagement of the aircraft flight path.
On 7 December 2016, the crew of an ATR 42-500 lost control after airworthiness-related complications followed shutdown of the left engine whilst in the cruise and high speed terrain impact followed. The Investigation concluded that three pre-existing faults with the left engine and its propeller control mechanism had led to a loss of power which had necessitated its shutdown but that these faults had then caused much higher left side drag than would normally result from an engine shutdown and made it progressively more difficult to maintain control. Recovery from a first loss of control was followed by another without recovery.
On 31 December 2017, a de Havilland DHC2 floatplane being manoeuvred at low level over Jerusalem Bay shortly after takeoff was observed to enter a steeply banked turn from which it appeared to depart controlled flight and impact the water surface below almost vertically. The Investigation concluded that the aircraft had stalled despite the exemplary proficiency record of the pilot and that in the absence of any other plausible explanation found that the loss of control was likely to have been the effect of an elevated exposure to carbon monoxide found during post mortem toxicology testing.
Minimum Fuel Call
On 2 March 2018, a Cessna 441 conducting a single-pilot scheduled passenger flight to Broome suffered successive failures of both engines due to fuel exhaustion and a MAYDAY was declared. Unable to reach the destination or any other aerodrome by the time this occurred, an uneventful landing was made on the area’s main highway. The Investigation found that the fuel quantity was over-reading due to water in the fuel tanks, that cross-checking of fuel used versus indicated fuel in tanks was not done and that when the possibility of fuel exhaustion was first indicated, an available diversion was not made.
On 10 October 2016, an Airbus 319 was cleared to divert to its first alternate after failing to land off its Cat II ILS approach at Porto and obliged to land at its second alternate with less than final reserve fuel after the first alternate declined acceptance due to lack of parking capacity. The Investigation concluded that adjacent ATC Unit coordination in respect of multiple diversions was inadequate and also found that the crew had failed to adequately appraise ATC of their fuel status. It also noted that the unsuccessful approach at the intended destination had violated approach ban visibility conditions.
Flight Envelope Protection Activated
On 19 August 2017, an Airbus A340-300 encountered significant unforecast windshear on rotation for a maximum weight rated-thrust night takeoff from Bogotá and was unable to begin its climb for a further 800 metres during which angle of attack flight envelope protection was briefly activated. The Investigation noted the absence of a windshear detection system and any data on the prevalence of windshear at the airport as well as the failure of ATC to relay in English reports of conditions from departing aircraft received in Spanish. The aircraft operator subsequently elected to restrict maximum permitted takeoff weights from the airport.
On 27 November 2017, an Embraer EMB 550 crew ignored a pre-takeoff indication of an inoperative airframe ice protection system despite taxiing out and taking off in icing conditions. The flight proceeded normally until approach to Paris Le Bourget when the Captain was unable to flare for touchdown at the normal speed and a 4g runway impact which caused a main gear leg to pierce the wing followed. The Investigation found that the crew had failed to follow relevant normal and abnormal operating procedures and did not understand how flight envelope protection worked or why it had activated on approach.
On 24 March 2012, an Air France Airbus A319 Captain continued descent towards destination Tunis at high speed with the landing runway in sight well beyond the point where a stabilised approach was possible. With 5nm to go, airspeed was over 100 KIAS above the applicable VApp and the aircraft was descending at over 4000fpm with flaps zero. EGPWS activations for Sink Rate, PULL UP and Too Low Terrain apparently went unnoticed but at 400 feet agl, ATC granted a crew request for a 360° turn. The subsequent approach/landing was without further event. Investigation attributed the event to “sloppy CRM”.
On 3 April 2012, the crew of an Air France Airbus A320 came close to loosing control of their aircraft after accepting, inadequately preparing for and comprehensively mismanaging it during an RNAV VISUAL approach at Tel Aviv and during the subsequent attempt at a missed approach. The Investigation identified significant issues with crew understanding of automation - especially in respect of both the use of FMS modes and operations with the AP off but the A/T on - and highlighted the inadequate provision by the aircraft operator of both procedures and pilot training for this type of approach.
On 27 February 2012, the crew of an Airbus A330 en route at night and crossing the East African coast at FL360 encountered sudden violent turbulence as they flew into a convective cell not seen on their weather radar and briefly lost control as their aircraft climbed 2000 feet with resultant minor injuries to two occupants. The Investigation concluded that the isolated and rapidly developing cell had not been detected because of crew failure to make proper use of their weather radar, but noted that activation of flight envelope protection and subsequent crew action to recover control had been appropriate.
Related Articles
For all accident reports held on SKYbrary, see the main section on Accident Reports.
Further Reading
- Aircraft Loss of Control: Causal Factors and Mitigation Challenges, by S. R. Jacobson (NASA)
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