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On 16 January 2013, an Augusta 109E helicopter positioning by day on an implied (due to adverse weather conditions) SVFR clearance collided with a crane attached to a tall building under construction. It and associated debris fell to street level and the pilot and a pedestrian were killed and several others on the ground injured. It was concluded that the pilot had not seen the crane or seen it too late to avoid whilst flying by visual reference in conditions which had become increasingly challenging. The Investigation recommended improvements in the regulatory context in which the accident had occurred.  +
On 20 April 2010, the left wing of an Antonov Design Bureau An124-100 which was taxiing in to park after a night landing at Zaragoza under marshalling guidance was in collision with two successive lighting towers on the apron. Both towers and the left wingtip of the aircraft were damaged. The subsequent investigation attributed the collision to allocation of an unsuitable stand and lack of appropriate guidance markings.  +
On 5 June 2014, an AW139 about to depart from its Ottawa home base on a positioning flight exceeded its clearance limit and began to hover taxi towards the main runway as an A300 was about to touch down on it. The TWR controller immediately instructed the helicopter to stop which it did, just clear of the runway. The A300 reached taxi speed just prior to the intersection. The Investigation attributed the error to a combination of distraction and expectancy and noted that the AW139 pilot had not checked actual or imminent runway occupancy prior to passing his clearance limit.  +
On 3 July 2010, an AW139 helicopter was climbing through 350 feet over Victoria Harbour Hong Kong just after takeoff when the tail rotor detached. A transition to autorotation was accomplished and a controlled ditching followed. All occupants were rescued but some sustained minor injuries. The failure was attributed entirely to manufacturing defects but no corrective manufacturer or regulatory action was taken until two similar accidents had occurred in Qatar (non-fatal) and Brazil (fatal) the following year and two interim Safety Recommendations were issued from this Investigation after which a comprehensive review of the manufacturing process led to numerous changes.  +
On 10 August 2014, one of the engines of an Antonov 140-100 departing Tehran Mehrabad ran down after V1 and prior to rotation. The takeoff was continued but the crew were unable to keep control and the aircraft stalled and crashed into terrain near the airport. The Investigation found that a faulty engine control unit had temporarily malfunctioned and that having taken off with an inappropriate flap setting, the crew had attempted an initial climb with a heavy aircraft without the failed engine propeller initially being feathered, with the gear remaining down and with the airspeed below V2.  +
On 27 October 2018, a single pilot Augusta Westland AW169 lifted off from within the Leicester City Football Club Stadium, but after a failure of the tail rotor control system, a loss of yaw control occurred a few hundred feet above ground. The helicopter began to descend with a high rotation rate and soon afterward impacted the ground and almost immediately caught fire, which prevented those onboard surviving. An Investigation is being conducted by the UK AAIB.  +
On 5 April 1996 a significant loss of separation occurred when a B744, taking off from runway 27R at London Heathrow came into conflict to the west of Heathrow Airport with an A306 which had carried out a missed approach from the parallel runway 27L. Both aircraft were following ATC instructions. Both aircraft received and correctly followed TCAS RAs, the B744 to descend and the A306 to adjust vertical speed, which were received at the same time as corrective ATC clearances.  +
On 10 January 2011, an Air Atlanta Icelandic Airbus A300-600 on a scheduled cargo flight made a bounced touchdown at East Midlands and then attempted a go around involving retraction of the thrust reversers after selection out and before they had fully deployed. This prevented one engine from spooling up and, after a tail strike during rotation, the single engine go around was conducted with considerable difficulty at a climb rate only acceptable because of a lack of terrain challenges along the climb out track.  +
On 30 July 1997, an Airbus A300-600 being operated by Emirates Airline was departing on a scheduled passenger flight from Paris Charles de Gaulle in daylight when, as the aircraft was accelerating at 40 kts during the take off roll, it pitched up and its tail touched the ground violently. The crew abandoned the takeoff and returned to the parking area. The tail of the aircraft was damaged due to the impact with the runway when the plane pitched up.  +
On 16 January 2010, an Iran Air Airbus A300-600 veered off the left side of the runway after a left engine failure at low speed whilst taking off at Stockholm. The directional control difficulty was attributed partly to the lack of differential braking but also disclosed wider issues about directional control following sudden asymmetry at low speeds. The Investigation concluded that deficiencies in the type certification process had contributed to the loss of directional control. It was concluded that the engine malfunction was due to the initiation of an engine stall by damage caused by debris from a deficient repair.  +
On 17 May 2015, an Airbus A300-600 crew descended their aircraft below the correct vertical profile on a visual daytime approach at Yerevan and then landed on a closed section of the runway near the displaced runway threshold. The Investigation found that the crew had failed to review relevant AIS information prior to departing from Tehran and had not been expecting anything but a normal approach and landing. The performance of the Dispatcher in respect of briefing and the First Officer in respect of failure to adequately monitor the Captain's flawed conduct of the approach was highlighted.  +
On 14 August 2013, a UPS Airbus A300-600 crashed short of the runway at Birmingham Alabama on a night IMC non-precision approach after the crew failed to go around at 1000ft aal when unstabilised and then continued descent below MDA until terrain impact. The Investigation attributed the accident to the individually poor performance of both pilots, to performance deficiencies previously-exhibited in recurrent training by the Captain and to the First Officer's failure to call in fatigued and unfit to fly after mis-managing her off duty time. A Video was produced by NTSB to further highlight human factors aspects.  +
On 12 January 2011, an Airbus A300-600 being operated by Monarch Airlines on a passenger flight from London Gatwick to Chania, Greece experienced activations of the stall protection system after an unintended configuration change shortly after take off but following recovery, the flight continued as intended without further event. There were no abrupt manoeuvres and no injuries to the 347 occupants.  +
On 26 April 1994, the crew of an Airbus A300-600 lost control of their aircraft on final approach to Nagoya and the aircraft crashed within the airport perimeter. The Investigation found that an inadvertent mode selection error had triggered control difficulties which had been ultimately founded on an apparent lack understanding by both pilots of the full nature of the interaction between the systems controlling thrust and pitch on the aircraft type which were not typical of most other contemporary types. It was also concluded that the Captain's delay in taking control from the First Officer had exacerbated the situation.  +
On 12 November 2001, an Airbus A300-600 encountered mild wake turbulence as it climbed after departing New York JFK to which the First Officer responded with a series of unnecessary and excessive control inputs involving cyclic full-deflection rudder pedal inputs. Within less than 7 seconds, these caused detachment of the vertical stabiliser from the aircraft resulting in loss of control and ground impact with a post crash fire. The Investigation concluded that elements of the company pilot training process and the design of the A300-600 rudder system had contributed to this excessive use of the rudder and its consequences.  +
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.  +
On 27 June 2000 an Airbus A300-600 being operated by American Airlines on a scheduled passenger service from London Heathrow to New York JFK was being flown manually in the day VMC climb and approaching FL220 when a loud bang was heard and there was a simultaneous abrupt disturbance to the flight path. The event appeared to the flight crew to have been a disturbance in yaw with no obvious concurrent lateral motion. Although following the disturbance, the aircraft appeared to behave normally, the aircraft commander decided to return to London Heathrow rather than commence a transatlantic flight following what was suspected to have been an un-commanded flight control input. An uneventful return was made followed by an overweight landing 50 minutes after take off.  +
On 21 February 2001, a level bust 10 nm north of Oslo Airport by a climbing PIA A310 led to loss of separation with an SAS B736 in which response to a TCAS RA by the A310 not being in accordance with its likely activation (descend). The B736 received and correctly actioned a Climb RA.  +
On 16 May 2018, an Airbus A310 and a Cessna 421 being positioned for ILS approaches to adjacent parallel runways at Montréal by different controllers lost separation. One controller incorrectly believed that he had transferred control of the Cessna to the other when the shift supervisor re-opened a sector which had been temporarily combined with his. The Investigation attributed the conflict to multiple deviations from standard procedures, memory lapses relating to controller information exchange of information and a loss of full situational awareness compounded by the shift supervisor also acting as an instructor whilst being distracted by his other duties.  +
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.  +
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.  +
On 2 March 2013, the crew of an Airbus A310 mishandled a night tailwind touchdown at Ponta Delgada after a stabilised ILS approach had been flown and, after an initial bounce, the pitch was increased significantly and the main landing gear was fully compressed during the subsequent touchdown resulting in a tail strike and substantial related structural damage. The mishandling was attributed to deviation from the recommended 'light bounce' recovery technique. The absence of an instrument approach to the reciprocal (into wind) direction of the runway was noted and a recommendation that an RNAV procedure be made available was made.  +
On 12 July 2000, a Hapag Lloyd Airbus A310 was unable to retract the landing gear normally after take off from Chania for Hannover. The flight was continued towards the intended destination but the selection of an en route diversion due to higher fuel burn was misjudged and useable fuel was completely exhausted just prior to an intended landing at Vienna. The aeroplane sustained significant damage as it touched down unpowered inside the aerodrome perimeter but there were no injuries to the occupants and only minor injuries to a small number of them during the subsequent emergency evacuation.  +
On 6 March 2005, an Airbus A310-300 being operated by Canadian airline Air Transat on a passenger charter flight from Varadero Cuba to Quebec City was in the cruise in daylight VMC at FL350 seventeen minutes after departure and overhead the Florida Keys when the flight crew heard a loud bang and felt some vibration. The aircraft entered a Dutch roll which was eventually controlled in manual flight after a height excursion. During descent for a possible en route diversion, the intensity of the Dutch Roll lessened and then stopped and the crew decided to return to Varadero. It was found during landing there that rudder control inputs were not effective and after taxi in and shutdown at the designated parking position, it was discovered that the aircraft rudder was missing. One of the cabin crew sustained a minor back injury during the event but no others from the 271 occupants were injured.  +
On 30 January 2000, an Airbus 310 took off from Abidjan (Ivory Coast) at night bound for Lagos, Nigeria then Nairobi, Kenya. Thirty-three seconds after take-off, the airplane crashed into the Atlantic Ocean, 1.5 nautical miles south of the runway at Abidjan Airport. 169 persons died and 10 were injured in the accident.  +
On 24 November 2006, an A310 descended significantly below cleared altitude during a radar vectored approach positioning, as a result of the flight crew's failure to set the QNH, which was unusually low.  +
On 29 June 2009, an Airbus A310-300 making a dark-night visual circling approach to Moroni crashed into the sea and was destroyed. The Investigation found that the final impact had occurred with the aircraft stalled and in the absence of appropriate prior recovery actions and that this had been immediately preceded by two separate GWPS 'PULL UP' events. It was concluded that the attempted circling procedure had been highly unstable with the crew's inappropriate actions and inactions probably attributable to their becoming progressively overwhelmed by successive warnings and alerts caused by their poor management of the aircraft's flight path.  +
On 24 September 1994, lack of understanding of automatic flight control modes, by the crew of an Airbus A-310, led to a full stall. The aircraft was recovered and subsequently landed without further event at Paris Orly.  +
On 5 March 2008, an Air Transat A310-300 was unintentionally mishandled by the flight crew during and shortly after departure from Quebec and effective control of the aircraft was temporarily lost. Whilst it was concluded that the origin of the initial difficulties in control were a result of confusion which began on the take off roll and led to a take off at excessive speed followed by subsequent mismanagement and overload, the inappropriate steep descent that followed was attributed to the effect of somatogravic illusion in respect of aircraft attitude control in conjunction with a singular focus on airspeed.  +
On 8 June 2009, an Airbus A318-100 being operated by Air France on a scheduled passenger flight from Belgrade, Serbia to Paris CDG in day VMC came into conflict with a Boeing 737-800 being operated by Ryanair on a scheduled passenger flight from Nottingham East Midlands UK to Bergamo Italy. The conflict was resolved mainly by TCAS RA response and there were no injuries to any occupants during the avoidance manoeuvres carried out by both aircraft.  +
On 25 May 2010 an Air France Airbus A318 making an automatic landing off an ILS Cat 2 approach at Nantes experienced interference with the ILS LOC signal caused by a Boeing 737-800 which was departing from the same runway but early disconnection of the AP removed any risk of un-correctable directional control problems during the landing roll. Both aircraft were operating in accordance with their ATC clearances. Investigation attributed the conflict to the decision of TWR not to instruct the A318 to go around and because of diminished situational awareness.  +
On 6 December 2007 an Airbus A318 being operated by Air France on a scheduled passenger flight from Lyon to Amsterdam carried out missed approach from runway 18C at destination and lost separation in night VMC against a Boeing 737-900 being operated by KLM on a scheduled passenger flight from Amsterdam to London Heathrow which had just departed from runway 24. The conflict was resolved by correct responses to the respective coordinated TCAS RAs after which the A318 passed close behind the 737. There were no abrupt manoeuvres and none of the 104 and 195 occupants respectively on board were injured.  +
On 5 July 2012, an Airbus A319 entered its departure runway at Naha without clearance ahead of an A320 already cleared to land on the same runway. The A320 was sent around. The Investigation concluded that the A319 crew - three pilots including one with sole responsibility for radio communications and a commander supervising a trainee Captain occupying the left seat - had misunderstood their clearance and their incorrect readback had not been detected by the TWR controller. It was concluded that the controller's non-use of a headset had contributed to failure to detect the incorrect readback.  +
On 25 November 2014, the crew of an Airbus A320 taking off from Paris CDG and in the vicinity of V1 saw an A319 crossing the runway ahead of them and determined that the safest conflict resolution was to continue the takeoff. The A320 subsequently overflew the A319 as it passed an estimated 100 feet agl. The Investigation concluded that use of inappropriate phraseology by the TWR controller when issuing an instruction to the A319 crew had led to a breach of the intended clearance limit. It was also noted that an automated conflict alert had activated too late to intervene.  +
On 6 August 2011 an Easyjet Airbus A319 on which First Officer Line Training was in progress exceeded its cleared level during the climb after a different level to that correctly read back was set on the FMS. As a result, it came into conflict with an Alitalia A321 and this was resolved by responses to coordinated TCAS RAs. STCA alerts did not enable ATC resolution of the conflict and it was concluded that a lack of ATC capability to receive Mode S EHS DAPs - since rectified - was a contributory factor to the outcome.  +
On 27 June 2016, an Airbus A319 narrowly avoided a mid-air collision with an AS532 Cougar helicopter whose single transponder had failed earlier whilst conducting a local pre-delivery test flight whilst both were positioning visually as cleared to land at Marseille and after the helicopter had also temporarily disappeared from primary radar. Neither aircraft crew had detected the other prior to their tracks crossing at a similar altitude. The Investigation attributed the conflict to an inappropriate ATC response to the temporary loss of radar contact with the helicopter aggravated by inaccurate position reports and non-compliance with the aerodrome circuit altitude by the helicopter crew.  +
On 7 September 2012, the crew of an Air France Airbus A319 failed to follow their arrival clearance at destination and turned directly towards the ILS FAF and thereby into conflict with a Boeing 737-500 on an ILS approach. When instructed to turn left (and clear of the ILS) by the controller, the crew replied that they were "following standard arrival" which was not the case. As the separation between the two aircraft reduced, the controller repeated the instruction to the A319 to turn left and this was acknowledged. Minimum lateral separation was 1.7nm, sufficient to activate STCA.  +
On 23 November 2002, an A319, landing on Rwy16 at Zurich Switzerland, narrowly missed collision with a B737-600 cleared for take off on an intersecting runway.  +
On 26 May 2013, an A319 in Swiss Class 'C' airspace received a TCAS 'Level Off' RA against a 737 above after being inadvertently given an incorrect climb clearance by ATC. The opposing higher-altitude 737 began a coordinated RA climb from level flight and this triggered a second conflict with another 737 also in the cruise 1000 feet above which resulted in coordinated TCAS RAs for both these aircraft. Correct response to all RAs resulted in resolution of both conflicts after prescribed minimum separations had been breached to as low as 1.5nm when 675 feet apart vertically.  +
On 10 January 2008, an Air Canada Airbus A319 en route over the north western USA encountered unexpected sudden wake vortex turbulence from an in trail Boeing 747-400 nearly 11nm ahead to which the pilots who then responded with potentially hazardous flight control inputs which led to reversion to Alternate Control Law and aggravated the external /disturbance to the aircraft trajectory with roll up to 55° and an unintended descent of 1400 feet which with cabin service in progress and sea belt signs off led to cabin service carts hitting the cabin ceiling and several passenger injuries, some serious.  +
On 10 June 2011 an ATC error put a German Wings A319 and a Hahn Air Raytheon 390 on conflicting tracks over Switzerland and a co-ordinated TCAS RA followed. The aircraft subsequently passed in very close proximity without either sighting the other after the Hahn Air crew, contrary to Company procedures, followed an ATC descent clearance issued during their TCAS ‘Climb’ RA rather than continuing to fly the RA. The Investigation could find no explanation for this action by the experienced crew - both Hahn Air management pilots. The recorded CPA was 0.6 nm horizontally at 50 feet vertically.  +
On 5 February 2011, an Airbus A319-100 being operated by Air Berlin on a passenger flight departing Stockholm inadvertently proceeded beyond the given clearance limit for runway 19R and although it subsequently stopped before runway entry had occurred, it was by then closer to high speed departing traffic than it should have been. There was no abrupt stop and none of the 103 occupants were injured.  +
On 26 June 2017, an Airbus A319 which had just taken off from Stuttgart came into conflict in Class ‘D’ airspace with a VFR light aircraft crossing its track and when, at 1,200 feet agl, the TCAS RA to descend which resulted was followed, an EGPWS Mode 3 Alert was generated. Clear of Conflict was annunciated after 10 seconds and climb resumed. The Investigation concluded that the light aircraft pilot had failed to follow the clearance which had been accepted and had caused the flight path conflict which was resolved by the response of the A319 to the TCAS RA.  +
On 6 January 2011 an Easyjet Airbus A319 experienced the sudden onset of thick "smoke" in the cabin as the aircraft cleared the runway after landing. The aircraft was stopped and an evacuation was carried out during which one of the 52 occupants received a minor injury. The subsequent investigation attributed the occurrence to the continued use of reverse idle thrust after clearing the runway onto a little used taxiway where the quantity of de-ice fluid residue was much greater than on the runway.  +
On 8 August 2011 an Air France Airbus A319 crew failed to correctly identify the runway on which they were cleared to land off a visual approach at Casablanca and instead landed on the parallel runway. ATC, who had already cleared another aircraft to cross the same runway, did not notice until this other aircraft crew, who had noticed the apparently abnormal position of the approaching aircraft and remained clear of the runway as a precaution, advised what had happened. Investigation was hindered by the stated perception of the Air France PIC that the occurrence was not a Serious Incident.  +
On 21 September 2012, an SAS A319 which had just landed normally under the control of an experienced pilot left the paved surface when attempting to make a turn off the RET at a taxi speed greater than appropriate. The pilot was familiar with the airport layout and the misjudgement was attributed in part to the fact that the pilot involved had recently converted to their first Airbus type after a long period operating the DC9/MD80/90 series which had a different pilot eye height and was fitted with steel rather than the more modern carbon brakes.  +
On 3 August 2018, smoke appeared and began to intensify in the passenger cabin but not the flight deck of an Airbus A319 taxiing for departure at Helsinki. Cabin crew notified the Captain who stopped the aircraft and sanctioned an emergency evacuation. This then commenced whilst the engines were still running and inadequate instructions to passengers resulted in a completely disorderly evacuation. The Investigation attributed this to inadequate crew procedures which only envisaged an evacuation ordered by the Captain for reasons they were directly aware of and not a situation where the evacuation need was only obvious in the cabin.  +
On 19 June 2016, an Airbus A320 failed to follow the clearly-specified and ground-marked self-positioning exit from a regularly used gate at Ibiza and its right wing tip collided with the airbridge, damaging both it and the aircraft. The Investigation found that the crew had attempted the necessary left turn using the Operator’s ‘One Engine Taxi Departure’ procedure using the left engine but then failed to follow the marked taxi guideline by a significant margin. It was noted that there had been no other such difficulties with the same departure in the previous four years it had been in use.  +
On 30 January 2006 the Captain of an Airbus A319 inadvertently lined up and commenced a night rolling take off from Las Vegas on the runway shoulder instead of the runway centreline despite the existence of an illuminated lead on line to the centre of the runway from the taxiway access used. The aircraft was realigned at speed and the take off was completed. ATC were not advised and broken edge light debris presented a potential hazard to other aircraft until eventually found. The Investigation found that other similar events on the same runway had not been reported at all.  +
On 12 February 2007, an Airbus A319-100 being operated by British Airways on a scheduled passenger flight into London Heathrow made unintended contact in normal daylight visibility with the stationary airbridge at the arrival gate. This followed an emergency stop made after seeing hand signals from ground staff whilst following SEGS indications which appeared to suggest that there was a further 5 metres to run to the correct parking position. There was no damage to the aircraft, only minimal damage to the airbridge and there were no injuries to the aircraft occupants or any other person  +