Air France

Airbus A320-214

Air France flight AF4236, an Airbus A320-214, encountered turbulence while descending through FL200 towards the destination Ajaccio. Two passengers and three crew members were injured.

Airbus A330

On Sunday 31 May 2009, the Airbus A330-203 registered F-GZCP operated by Air France was programmed to perform scheduled flight AF 447 between Rio de Janeiro-Galeão and Paris Charles de Gaulle. Twelve crew members (3 flight crew, 9 cabin crew) and 216 passengers were on board. The departure was planned for 22 h 00. At around 22 h 10, the crew was cleared to start up engines and leave the stand. Takeoff took place at 22 h 29. The Captain was Pilot Not Flying (PNF); one of the copilots was Pilot Flying (PF). At the start of the Cockpit Voice Recorder (CVR) recording, shortly after midnight, the aeroplane was in cruise at flight level 350. Autopilot 2 and auto-thrust were engaged. Auto fuel transfer in the “trim tank” was carried out during the climb. The flight was calm. At 1 h 35, the aeroplane arrived at INTOL point and the crew left the Recife frequency to change to HF communication with the Atlántico Oceanic control centre. A SELCAL test was successfully carried out, but attempts to establish an ADS-C connection with DAKAR Oceanic failed. Shortly afterwards, the co-pilot modified the scale on his Navigation Display (ND) from 320 NM to 160 NM and noted “…a thing straight ahead”. The Captain confirmed and the crew again discussed the fact that the high temperature meant that they could not climb to flight level 370. At 1 h 45, the aeroplane entered a slightly turbulent zone, just before SALPU point. Note: At about 0 h 30 the crew had received information from the OCC about the presence of a convective zone linked to the inter-tropical convergence zone (ITCZ) between SALPU and TASIL. The crew dimmed the lighting in the cockpit and switched on the lights “to see”. The co-pilot noted that they were “entering the cloud layer” and that it would have been good to be able to climb. A few minutes later, the turbulence increased slightly in strength. Shortly after 1 h 52, the turbulence stopped. The co-pilot again drew the Captain’s attention to the REC MAX value, which had then reached flight level (FL) 375. A short time later, the Captain woke the second co-pilot and said “[…] he’s going to take my place”. At around 2 h 00, after leaving his seat, the Captain attended the briefing between the two co-pilots, during which the PF (seated on the right) said specifically that “well the little bit of turbulence that you just saw we should find the same ahead we’re in the cloud layer unfortunately we can’t climb much for the moment because the temperature is falling more slowly than forecast” and that “the logon with DAKAR failed”. Then the Captain left the cockpit. The aeroplane approached the ORARO point. It was flying at flight level 350 and at Mach 0.82. The pitch attitude was about 2.5 degrees. The weight and balance of the aeroplane were around 205 tonnes and 29%. The two copilots again discussed the temperature and the REC MAX. The turbulence increased slightly. At 2 h 06, the PF called the cabin crew, telling them that “in two minutes we ought to be in an area where it will start moving about a bit more than now you’ll have to watch out there” and he added “I’ll call you when we’re out of it”. At around 2 h 08, the PNF proposed “go to the left a bit […]”. The HDG mode was activated and the selected heading decreased by about 12 degrees in relation to the route. The PNF changed the gain adjustment on his weather radar to maximum, after noticing that it was in calibrated mode. The crew decided to reduce the speed to about Mach 0.8 and engine de-icing was turned on. At 2 h 10 min 05, the autopilot then the auto-thrust disconnected and the PF said “I have the controls”. The aeroplane began to roll to the right and the PF made a nose-up and left input. The stall warning triggered briefly twice in a row. The recorded parameters showed a sharp fall from about 275 kt to 60 kt in the speed displayed on the left primary flight display (PFD), then a few moments later in the speed displayed on the integrated standby instrument system (ISIS). The flight control law reconfigured from normal to alternate. The Flight Directors (FD) were not disconnected by the crew, but the crossbars disappeared. Note: Only the speeds displayed on the left side and on the ISIS are recorded on the FDR; the speed displayed on the right side is not recorded. At 2 h 10 min 16, the PNF said “we’ve lost the speeds ” then “alternate law protections”. The PF made rapid and high amplitude roll control inputs, more or less from stop to stop. He also made a nose-up input that increased the aeroplane’s pitch attitude up to 11° in ten seconds. Between 2 h 10 min 18 and 2 h 10 min 25, the PNF read out the ECAM messages in a disorganized manner. He mentioned the loss of autothrust and the reconfiguration to alternate law. The thrust lock function was deactivated. The PNF called out and turned on the wing anti-icing. The PNF said that the aeroplane was climbing and asked the PF several times to descend. The latter then made several nose-down inputs that resulted in a reduction in the pitch attitude and the vertical speed. The aeroplane was then at about 37,000 ft and continued to climb. At about 2 h 10 min 36, the speed displayed on the left side became valid again and was then 223 kt; the ISIS speed was still erroneous. The aeroplane had lost about 50 kt since the autopilot disconnection and the beginning of the climb. The speed displayed on the left side was incorrect for 29 seconds. At 2 h 10 min 47, the thrust controls were pulled back slightly to 2/3 of the IDLE/CLB notch (85% of N1). Two seconds later, the pitch attitude came back to a little above 6°, the roll was controlled and the angle of attack was slightly less than 5°. The aeroplane’s pitch attitude increased progressively beyond 10 degrees and the plane started to climb. From 2 h 10 min 50, the PNF called the Captain several times. At 2 h 10 min 51, the stall warning triggered again, in a continuous manner. The thrust levers were positioned in the TO/GA detent and the PF made nose-up inputs. The recorded angle of attack, of around 6 degrees at the triggering of the stall warning, continued to increase. The trimmable horizontal stabilizer (THS) began a nose-up movement and moved from 3 to 13 degrees pitch-up in about 1 minute and remained in the latter position until the end of the flight. Around fifteen seconds later, the ADR3 being selected on the right side PFD, the speed on the PF side became valid again at the same time as that displayed on the ISIS. It was then at 185kt and the three displayed airspeeds were consistent. The PF continued to make nose-up inputs. The aeroplane’s altitude reached its maximum of about 38,000 ft; its pitch attitude and angle of attack were 16 degrees. At 2 h 11 min 37, the PNF said “controls to the left”, took over priority without any callout and continued to handle the aeroplane. The PF almost immediately took back priority without any callout and continued piloting. At around 2 h 11 min 42, the Captain re-entered the cockpit. During the following seconds, all of the recorded speeds became invalid and the stall warning stopped, after having sounded continuously for 54 seconds. The altitude was then about 35,000 ft, the angle of attack exceeded 40 degrees and the vertical speed was about -10,000 ft/min. The aeroplane’s pitch attitude did not exceed 15 degrees and the engines’ N1’s were close to 100%. The aeroplane was subject to roll oscillations to the right that sometimes reached 40 degrees. The PF made an input on the side-stick to the left stop and nose-up, which lasted about 30 seconds. At 2 h 12 min 02, the PF said, “I have no more displays”, and the PNF “we have no valid indications”. At that moment, the thrust levers were in the IDLE detent and the engines’ N1’s were at 55%. Around fifteen seconds later, the PF made pitch-down inputs. In the following moments, the angle of attack decreased, the speeds became valid again and the stall warning triggered again. At 2 h 13 min 32, the PF said, “[we’re going to arrive] at level one hundred”. About fifteen seconds later, simultaneous inputs by both pilots on the side-sticks were recorded and the PF said, “go ahead you have the controls”. The angle of attack, when it was valid, always remained above 35 degrees. From 2 h 14 min 17, the Ground Proximity Warning System (GPWS) “sink rate” and then “pull up” warnings sounded. The recordings stopped at 2 h 14 min 28. The last recorded values were a vertical speed of -10,912 ft/min, a ground speed of 107 kt, pitch attitude of 16.2 degrees nose-up, roll angle of 5.3 degrees left and a magnetic heading of 270 degrees. No emergency message was transmitted by the crew. The wreckage was found at a depth of 3,900 metres on 2 April 2011 at about 6.5 NM on the radial 019 from the last position transmitted by the aeroplane. Both CVR and DFDR were found 23 months after the accident, in May 2011 at a depth of 3,900 metres. The final report was published in July 2012.

Airbus A340-300

The Air France Airbus A340-313 aircraft (registration F-GLZQ, serial number 0289) departed Paris, France, at 1153 Coordinated Universal Time (UTC) as Air France Flight 358 on a scheduled flight to Toronto, Ontario, with 297 passengers and 12 crew members on board. Before departure, the flight crew members obtained their arrival weather forecast, which included the possibility of thunderstorms. While approaching Toronto, the flight crew members were advised of weather-related delays. On final approach, they were advised that the crew of an aircraft landing ahead of them had reported poor braking action, and Air France Flight 358’s aircraft weather radar was displaying heavy precipitation encroaching on the runway from the northwest. At about 200 feet above the runway threshold, while on the instrument landing system approach to Runway 24L with autopilot and autothrust disconnected, the aircraft deviated above the glideslope and the groundspeed began to increase. The aircraft crossed the runway threshold about 40 feet above the glideslope. During the flare, the aircraft travelled through an area of heavy rain, and visual contact with the runway environment was significantly reduced. There were numerous lightning strikes occurring, particularly at the far end of the runway. The aircraft touched down about 3800 feet down the runway, reverse thrust was selected about 12.8 seconds after landing, and full reverse was selected 16.4 seconds after touchdown. The aircraft was not able to stop on the 9000-foot runway and departed the far end at a ground speed of about 80 knots. The aircraft stopped in a ravine at 2002 UTC (1602 eastern daylight time) and caught fire. All passengers and crew members were able to evacuate the aircraft before the fire reached the escape routes. A total of 2 crew members and 10 passengers were seriously injured during the crash and the ensuing evacuation.

Aérospatiale-BAC Concorde

On Tuesday 25 July 2000 the Concorde registered F-BTSC, operated by Air France, took off from Paris Charles de Gaulle to undertake charter flight AF4590 to New York with nine crew members (3 FC, 6 CC) and 100 passengers on board. The Captain was Pilot Flying (PF), the First Officer was Pilot Not Flying (PNF). The total weights of the aircraft and of the fuel on board stated by the Flight Engineer (FE) at the time the aircraft started out were 186.9 t and 95 t respectively. The speeds selected by the crew were V1: 150 kt, VR: 198 kt, V2: 220 kt. At 13 h 58 min 27 s, the crew contacted ATC on the Flight data frequency and requested the whole length of runway 26 right for a takeoff at 14 h 30. At 14 h 07 min 22 s, the controller gave start-up clearance and confirmed runway 26 right for takeoff. At 14 h 34 min 38 s, the Ground controller cleared the aircraft to taxi towards the runway 26 right holding point via the Romeo taxiway. At 14 h 40 min 02 s, the Loc Sud controller cleared 4590 to line up. At 14 h 42 min 17 s, he gave it takeoff clearance, and announced a wind from 090° at 8kt. The crew read back the takeoff clearance. The FE stated that the aircraft had used eight hundred kilos of fuel during taxiing. At 14 h 42 min 31 s, the PF commenced takeoff. At 14 h 42 min 54.6 s, the PNF called one hundred knots, then V1 nine seconds later. A few seconds after that, tyre No 2 (right front) on the left main landing gear was destroyed after having run over a piece of metal lost by an aircraft that had taken off five minutes before. The destruction of the tyre in all probability resulted in large pieces of rubber being thrown against the underside of the left wing and the rupture of a part of tank 5. A severe fire broke out under the left wing and around the same time engines 1 and 2 suffered a loss of thrust, severe for engine 2, slight for engine 1. By 14 h 43 min 13 s, as the PF commenced the rotation, the controller informed the crew the presence of flames behind the aircraft. The PNF acknowledged this transmission and the FE announced the failure of engine 2. The recorded parameters show a transient loss of power on engine 1 that was not mentioned by the crew. At around 14 h 43 min 22 s the engine fire alarm sounded and the FE announced "shut down engine 2" then the Captain called for the "engine fire" procedure. A few seconds later, the engine 2 fire handle was pulled and the fire alarm stopped. The PNF drew the PF’s attention to the airspeed, which was 200 kt. At 14 h 43 min 30 s, the PF called for landing gear retraction. The controller confirmed the presence of large flames behind the aircraft. At 14 h 43 min 42 s the engine fire alarm sounded again for around 12 seconds. It sounded for the third time at about 14 h 43 58 s and continued until the end of the flight. At 14 h 43 min 56 s, the PNF commented that the landing gear had not retracted and made several callouts in relation to the airspeed. At 14 h 43 min 59 s, the GPWS alarm sounded several times. The FO informed ATC that they were trying for Le Bourget aerodrome. The recorded parameters then indicate a loss of power on engine 1. A few seconds later, the aircraft crashed onto a hotel at “La Patte d’Oie” in Gonesse at the intersection of the N17 and D902 roads. The aircraft was totally destroyed by impact forces and a post crash fire and all 109 occupants were killed as well as four people working in the hotel. Five other employees were injured. The aircraft was chartered by the German Operator Deilmann to carry German tourists to New York. On board were nine French citizens (all crew members), 96 Germans, two Danish, one American and one Austrian.

Boeing 737-200

Air France Flight 7638, a Boeing 737-228, operated on a domestic flight from Paris-Charles de Gaulle Airport to Biarritz. The co-pilot on the flight was Pilot Flying (PF). While en route, about an hour before arrival, the flight crew listened out the ATIS frequency. The latest report mentioned a visibility of 10 km, a headwind of 15 to 30 kt and rain. When descending towards Biarritz the crew obtained an avoidance heading to bypass a thunderstorm cell. The flight was subsequently cleared for an ILS DME Cat I for runway 27. In the four minutes before landing, the visibility was 1500 metres in a squall, wind 6 kt with gusts to 3 kt, its direction changing from 250° to 290°, with variations up to 330°. The Vref is 129 kt and the Vapp 149 kt. The controller cleared the flight for landing and indicated a wind of 250° at 16 kt, gusts to 30 kt and heavy rain. The first officer disconnected the autopilot and autothrottle at an altitude of approximately 1200 ft, while established on the ILS. As the aircraft descended through 1100 feet, the captain was able to see the runway ahead. On short final, the controller reported a wind of 280° at 15 to 30 kt. The aircraft gradually deviated to the left of the centre line. The captain said: "a little to the left". The aircraft then gradually returned to align with the runway centreline. The PF banked the aircraft to the left as it slightly overshot the runway centreline. The aircraft passed the threshold approximately 4 m to the right of the centreline, parallel to it, with its wings horizontal. The PF started the flare with a slight bank to the left. The thrust reduction occurred a few seconds later. The left main gear touched the runway first at an indicated airspeed of 148 kt, while the aircraft was 12 m to the left of the runway centreline. The aircraft moved 7 m to the left, rolling on the only left main gear for about two seconds. The PF used the control column and the rudder pedals to steer the airplane to the right. The right main gear touched the runway while the left wheels were about 3 m from the edge of the runway. The PF corrected the trajectory using the rudders, without using the full amplitude. The aircraft exited the runway on the left at a speed of 133 kt. The nose gear struck the concrete support of a light and broke. The right gear was damaged and the aircraft rolled approximately 400 m off the runway and came to rest near the runway, 1150 m from the threshold.

Airbus A300

On December 24, prior to departure from Algiers-Houari Boumediene Airport, four members of the Groupe Islamique Armé (GIA) hijacked the aircraft that remained parked there for two days. On December 26, the aircraft was flown to Marseille. After being parked there for few hours, the aircraft was stormed by French Police Forces. Few hand grenades exploded in the main cabin and the cockpit, causing serious damages to the aircraft. All four terrorists and three passengers were killed during the attack. Ten other people were injured.

Airbus A320

A newly delivered Airbus A320, F-GFKC, was destroyed when it impacted trees during a low pass over the runway at Mulhouse-Habsheim Airport, France. A fire broke out, killing three occupants. The Mulhouse Flying Club had requested Air France to perform a fly by at their air show at Mulhouse-Habsheim Airport on June 26, 1988. Air France prepared a low speed pass with the gear down at 100 feet and the another pass at high speed in clean configuration. While Air France had performed more than twenty low passes since 1987, the altitude of 100 feet was not allowed according to regulations. French air safety regulations imposed a minimum VFR overflight height of 170 feet. The fly by was to be performed using an Airbus A320, an aircraft model that was introduced by launching customer Air France in March 1988. F-GFKC was the third A320 in the fleet and had been delivered on June 23. The flight crew scheduled to perform the demonstration flight were two captains: the head of A320 training subdivision (Pilot Flying) and a captain participating in the placing into service of the A320(Pilot Monitoring). On board the flight were four cabin crew members and 130 passengers. The aircraft took off from nearby Basel-Mulhouse Airport at 14:41 and climbed to 1000 feet agl. The crew started the descent three minutes later and Habsheim was in sight at 450 feet agl. The Pilot Monitoring informed the Pilot Flying that the aircraft was reaching 100 feet at 14:45:14. The descent continued to 50 feet 8 seconds later and further to 30-35 feet. Go-around power was added at 14:45:35. The A320 continued and touched trees approximately 60 meters from the end of runway 34R at 14:45:40 with a 14 degree pitch attitude and engines at 83% N1. The plane sank slowly into the forest and a fire broke out.

Boeing 747-200

Air France flight 091 was involved in runway excursion accident at Rio de Janeiro-Galeão International Airport, Brazil. The aircraft, a Boeing 747-200, took off from Paris-Charles de Gaulle Airport, France at 21:30 UTC on a flight to Santiago, Chile with en route stops at Rio de Janeiro and Buenos Aires, Argentina. The flight to Rio de Janeiro took about eleven hours and was uneventful. At 08:34 UTC the aircraft touched down on runway 14, 400 meters from the threshold. After reversers were set, the aircraft deviated from the runway heading and at 2,000 meters from the threshold it veered off the right side of the runway. The aircraft ran over the grass for 765 meters, until passing over a drainage ditch and the load apron concrete step, where the landing gears folded aft with the left wing gear completely separating. On the load apron concrete the aircraft spun around for 275 meters until stopping, after the left outboard wing section struck an illumination stand. For a few seconds engines 2, 3 and 4 kept running at maximum reverse thrust, while engine number one run operated at full forward thrust. After the engines were shut down, the passengers evacuated using three of the aircraft's left hand side escape slides. The fire that started on the area near engines number 2 and 3 was extinguished by the airport fire fighters. It appeared that the n°1 engine throttle cable had broken, making it impossible for the flight crew to control engine power. The engine had accelerated to an unusually high level of (forward) thrust (above takeoff power).

Airbus A300

During the takeoff roll at Sana'a Intl Airport, at a speed of 95 knots, the crew noticed a loud bang followed by vibrations. The captain decided to abandon the takeoff procedure and initiated an emergency braking maneuver. The airplane came to rest on runway with its right wing on fire. All 124 occupants were evacuated safely, nevertheless, two passengers were slightly injured. The aircraft was considered as damaged beyond repair.

Sud-Aviation SE-210 Caravelle

While taxiing at Frankfurt-Main Airport, the pilot-in-command lost control of the airplane that collided with a fence and ground lights marking construction work before coming to rest. The right wing was seriously damaged and a tank was punctured, causing 500 liters of fuel to leak on the ground. All 41 occupants were evacuated safely while the aircraft was damaged beyond repair.

Sud-Aviation SE-210 Caravelle

While parked at Ho Chi Minh-City Airport, the airplane was hijacked by a Vietnamese passenger. All 19 occupants were quickly released and when police forces approached the aircraft, the hijacker set off two grenades that exploded in the cabin. The hijacker was killed and the aircraft was considered as damaged beyond repair.

Boeing 747-100

The crew was completing a 180 turn on runway 27 threshold to prepare for takeoff when the fire alarm sounded in the cockpit panel. The crew stopped the aircraft and ordered all 402 occupants to evacuate the aircraft. Fire spread quickly on the right side of the airplane that was destroyed. All 402 occupants escaped, 10 of them were slightly injured.

Fokker F27 Friendship

The crew was completing a mail flight from Rennes to Clermont-Ferrand with intermediate stops in Nantes and Poitiers on behalf of the French Postal Service (La Poste). On final approach to Nantes-Château Bougon Airport by night, the crew failed to realize his altitude was too low when the airplane struck power cables and crashed in flames in a field located about 12 km from the airport. The aircraft was destroyed and all three crew members were killed.

Boeing 707

Three minutes after takeoff from Maiquetía-Simon Bolivar Airport, while climbing to a height of 3,000 feet by night, the aircraft went out of control, nosed down and plunged into the sea about 5 km offshore. The wreckage sank by a depth of 50 meters and all 62 occupants were killed.

Douglas C-54 Skymaster

During the takeoff roll on runway 26, at an IAS of 61 knots, the pilot-in-command lost control of the airplane that swerved. It veered off runway to the left, hit several obstacles, went down an embankment, broke into several parts and came to rest in flames by the Route Nationale 7. The aircraft was destroyed by impact forces and a post crash fire and all three crew members were injured.

Sud-Aviation SE-210 Caravelle

Following an uneventful flight from Ajaccio, the crew started the descent to Nice-Côte d'Azur Airport when the pilot sent a brief mayday message, saying 'fire on board, request urgent landing'. Few second later, the airplane went into a dive and crashed into the Mediterranean Sea some 40 km off Antibes. Few debris were found on water surface and none of the 95 occupants survived the crash.

Boeing 707

Air France Flight 212 was a scheduled service from Santiago (Chile) to Paris (France) with en route stops at Quito (Ecuador), Caracas (Venezuela), Pointe-à-Pitre (Guadeloupe) and Lisbon (Portugal). The flight was operated by a brand new Boeing 707, named "Château de Lavoûte-Polignac", which had just been delivered to Air France a month and a half before the accident. The aircraft took off from Caracas at 19:27 for an estimated one hour and eight-minute flight to Pointe-à-Pitre on the French Caribbean island of Guadeloupe. The aircraft climbed to a cruising altitude of FL330 and the flight crew contacted the Piarco FIR controller at approximately 19:53 hours. They reported flying at FL330 and estimating over Piarco at 20:00, over the OA reporting point at 20:09 and reaching Pointe-à-Pitre at 20:32. At approximately 20:09 the flight reported over OA and requested authorization to descend in five minutes time. Piarco cleared the flight to the Guadeloupe radio beacon at FL90 and asked it to report when leaving FL330 and when reaching FL150. At 20:14, three minutes sooner than planned, the crew reported leaving FL330. Seven minutes later they reported passing FL150. It was then cleared to contact the Guadeloupe ACC and was advised that an aircraft proceeding from Martinique to Guadeloupe was flying at FL80 and estimating Guadeloupe at 20:44 hours. About 20:24 the flight reached the cleared altitude of FL90. After several unsuccessful attempts the flight established radio contact with Pointe-à-Pitre Tower at 20:29. It was again cleared to FL90, given a QNH of 1016 mb and requested to report at FL90, or runway in sight. Following a different route than normal, the airplane passed a brightly lit town (Basse Terre) on the coast of Guadeloupe. The pilot-in-command probably erroneously believed that it was Pointe-à-Pitre and that he would reach Le Raizet Airport in approximately one minute. At 20:29:35 the crew replied that the aircraft was at FL90 and they estimated they would be over the airport in approximately 1-1,5 minute. Less than one minute later they reported seeing the airport and were cleared for a visual approach to runway 11. The aircraft then descended over mountainous terrain and passed Saint Claude at an altitude of approximately 4,400 ft. Flight 212 was observed to impact on the southern slope of La Découverte, the peak of the La Soufrière Volcano, at an elevation of 1,200 m (3,937 ft).

Douglas DC-3

The crew consisting of pilot students and instructors was completing a local training flight at Coulommiers-Voisins Airport, Seine-et-Marne. After rotation, the airplane encountered difficulties to gain height and struck a truck with one of its wing. The wing was sheared off and then airplane crashed in a field 450 m past the runway end. Five crew members were killed while three others were seriously injured. The aircraft was destroyed. It was reported that one of the engine was voluntarily shut down by the crew prior to takeoff. Among those killed were: Mr. Laurent, student pilot, Mr. Brohan, student pilot, Mr. Mauger, mechanic, Mr. Perusseau, instructor and captain by Transports Aériens Intercontinentaux.

Boeing 707

While descending to Pointe-à-Pitre on a flight from Paris to Santiago de Chile, the crew encountered poor weather conditions at destination, worse than forecast. On approach by night, the four engine aircraft struck the slope of a hill (427 m) located 25 km northwest of Le Raizet Airport. The aircraft crashed in flames in a dense wooded area and was totally destroyed by impact forces and a post crash fire. All 113 occupants were killed. At the time of the accident, the VOR was unserviceable and the approach was possible via an NDB only. Weather conditions were poor with low visibility due to thunderstorm activity in the area. Also, the aircraft was off course by 15 km due to interference on the ADF systems caused by the thunderstorm activity. Crew: Mr. Lesieur, pilot, Mr. Farret, copilot, Mr. Hurlimann, navigator, Mr. Pruvost, mechanic, Mrs. Micoud, stewaradess, Mrs. D’Horne, stewardess, Mrs. Page, stewardess, Mr. Epper, steward, Mr. Gassler, steward, Mr. Cage, steward.

Boeing 707

The Boeing 707 aircraft, named "Chateau de Sully", was on a non-scheduled (charter) international flight from Paris (ORY) to Atlanta (ATL) and Houston via New York (JFK). Ten crew and 122 passengers were on the flight when, after a considerable delay to await the arrival of passengers, it was cleared to take off from runway 08 at Orly Airport at 11:32 UTC. It aligned itself for takeoff and waited 6 seconds, which permitted the setting and checking of takeoff parameters on the four engines. Full thrust was applied, and the aircraft accelerated normally. From testimony and flight recorder data, the takeoff was reconstructed as follows. Between 20 to 40 seconds after the start of the roll, the rate of acceleration was steady at 1.80 m/s2. The aircraft rolled along the runway centre line without showing any tendency to veer to either side. V1, determined as 147 kt IAS, was attained after a ground roll of 1500 m. This was followed by VR, 158 kt IAS. Forty-eight seconds after the beginning of the takeoff run and approximately when passing the 1800 m mark, the aircraft reached the rotation speed (VR), and the pilot-in-command initiated the takeoff manoeuvre by pulling backwards on the control column. According to witnesses, the aircraft made an incomplete rotational movement about 2100 m from the threshold. It remained for 4 to 6 seconds with its nose slightly raised. Then the nose dropped when the brakes were applied. Thick smoke streamed from the wheels. The aircraft was 2600 m from its starting point and had reached a maximum speed of 179 kt IAS. It braked for the last 680 m of the runway with an average deceleration of 1.2 to 1.3 m/s After 250 m of braking the aircraft veered slightly to the left, and 50deg of flap were selected. Then after another 250 m the aircraft listed heavily to starboard. Its path then curved right, which suggests a possible attempt to ground loop. However, the aircraft's speed precluded the success of this manoeuvre, and it left the runway while still on the centre line. It rolled for a while on the grass extension of the runway but, because of the unevenness of the terrain and the high speed of the aircraft (160 kt), the port gear broke off 110 m from the end of the runway and was wrenched away. The aircraft pivoted left, and engines No. 1 and 2 scraped the ground. Fire broke out in the port wing at the level of the landing gear. About 300 m beyond the end of the runway the aircraft crossed the encircling road. The starboard gear collapsed, and No. 2 engine broke loose. It then struck the approach lights, which represented a considerable obstacle. It started to disintegrate when reaching the hollow at the end of the runway extension, which descends at a steep angle towards the Seine. The front part of the fuselage struck a house and garage. The nose of the aircraft broke away, and the rest of the fuselage came to a stop 100 m further on. The site of the accident was 550 m beyond the end of runway 08 on its extended centre line, at an elevation of 89 m. The airplane was completely destroyed by a post crash fire. Two stewardess who seated in the rear were slightly injured while all 130 other occupants were killed. Crew members who were killed: Roland-Paul Hoche, pilot, Jacques-Marcel Pitoiset, copilot, Raymond Gautrand, navigator, Robert-Gaston Barres, mechanic, Marie-Geneviève Barot, stewardess, Robert Mancel, cabin chief, François Gutrupi, steward, Robert Lugon, steward.

Sud-Aviation SE-210 Caravelle

After a normal flight from Orly Airport, Paris, Flight 2005, Paris-Rabat-Casablanca, reported over the Rabat-Sale Airport, where meteorological conditions were unfavorable owing to thick, low fog which reduced horizontal visibility and ceiling. The pilot reported his intention to attempt a break-through over the non directional beacon; the control tower immediately replied that that facility was not in line with the runway, but the message was not acknowledged. The aircraft crashed to the ground at 2109 hours GMT. The aircraft was completely destroyed by impact and the fire which followed. Crew: Mr. Seaume, pilot, Mr. Simeoni, copilot, Mr. Nicora, mechanic, Mrs. Metenier, stewardess, Mr. Duhamel, steward, Mr. Jacomon, steward.

Boeing 707

During the takeoff roll on runway 23, at a speed of 120 knots, the captain noted the aircraft was turning slightly to the left and was unable to counteract. As a result, he decided to abandon the takeoff procedure and attempted an emergency braking maneuver. Unable to stop within the remaining distance, the airplane overran, lost its undercarriage and came to rest in a field located 140 meters the runway end, broken in three. Four crew members and six passengers were seriously injured while 31 other occupants were unhurt. The aircraft was destroyed.

Lockheed L-1649 Starliner

While cruising by night at an altitude of 20,000 feet vertical to the Sahara Desert, the airplane disintegrated in the air and crashed in a desert area located in the east part of Algeria, at the border with Libya. The crew was unable to send any distress call. The debris were scattered on a wide area between Ghadamès (Libya) and Zarzaïtine, Algeria. All 78 occupants were killed in the crash. Crew: Mr. Bouchier, pilot, Mr. Best, copilot, Mr. Baylion, navigator, Mr. Guntz, radio operator, Mr. Gambart de Lignières, mechanic, Mr. Burgaut, mechanic, Mrs. Chiapolino, stewardess, Mr. Eichelberger, steward, Mr. Pasqueron, steward.

Lockheed L-1049 Super Constellation

The aircraft was on its way from Paris-Orly to Abidjan with intermediate stops at Dakar and Monrovia. While approaching Dakar just before sunset, the crew started an approach to runway 01 after declining an ILS approach to runway 30. The approach was abandoned due to low visibility caused by poor weather conditions and the captain decided to follow a holding pattern, waiting for an improvement of the weather conditions. Shortly after 0641LT, the crew started a second attempt to land on runway 01 but after reporting downwind at 0647LT, the airplane disappeared in a rain squall and crashed into the sea some 2,400 meters off the Mamelles lighthouse. The airplane sank by a depth of 40 meters and few debris and dead bodies were found about two hours later. All 63 occupants were killed. Crew: Lucien Boirre, pilot, Jean Roze, copilot, Eugène Schuller, radio operator, Jean-Camille Baty, mechanic, Louis Meleder, mechanic, Geneviève Sabourin, stewardess, François Quiret, steward, Albert-Émile Guepratte, steward.

Douglas C-47 Skytrain (DC-3)

After touchdown at Poitiers-Biard Airport, the aircraft was unable to stop within the remaining distance. It overran, lost its undercarriage and came to rest few yards farther. While both crew members were uninjured, the aircraft was written off.

Lockheed L-749 Constellation

Following an uneventful flight from Munich, the crew started an ILS approach to Vienna-Schwechat runway 30. On final, the captain made a visual circuit when ground contact was apparently lost, causing the airplane to lose height. On short final, the Constellation crash landed in a field 2,2 km short of runway 30 threshold and came to rest. All 34 occupants were rescued and the aircraft was damaged beyond repair.

Caudron C.440 Goéland

The crew was completing a local training flight at Pontoise-Cormeilles-en-Vexin when he encountered an unexpected situation. The pilot attempt an emergency landing in a field and while all three crew members were unhurt, the aircraft was damaged beyond repair.

Douglas C-47 Skytrain (DC-3)

While on a flight from Algiers to Colomb-Béchar, the airplane struck the slope of a mountain located near Molière (today Bordj Bounaama). The aircraft was totally destroyed and all 15 occupants have been killed. Crew: Mr. Yasoni, pilot, Mr. Vincent, radio operator, Mr. Brillant, mechanic.

Douglas C-54 Skymaster

The crew encountered a sand storm while approaching In Salah Airport. On final, in limited visibility, the aircraft was too low and struck a sand dune short of runway. On impact, the undercarriage were sheared off and the airplane belly landed in sand before coming to rest. Both engines number two and three detached. There were no casualties.

Douglas DC-3

The aircraft was dispatched at Poitiers-Biard Airport for training purposes. The crew (five pilots under supervision, one instructor and two passengers) left the airport at 1245LT for local training mission. While approaching the airfield with one engine voluntarily inoperative, the crew encountered difficulties with the undercarriage that failed to lock down in time. The instructor decided to make a go around when the airplane banked right and crashed on a military building housing ammunition. All eight occupants were injured and evacuated while the aircraft was destroyed. No one on ground was injured.

Caudron C.440 Goéland

Crashed in unknown circumstances near Pontoise-Cormeilles-en-Vexin Airport. No casualties.

Lockheed L-1049 Super Constellation

The crew was engaged in a training mission consisting of a half-yearly check. After the pilot completed several manoeuvres at Reims Airport, he returned to Paris-Orly to complete four landings. The ILS approach to runway 26L was correct and completed by night with a ceiling at 60 meters and a horizontal visibility of 1,600 meters, under GCA surveillance. Just before touchdown, the airplane banked left and hit the ground 400 meters past the runway threshold. The airplane then crashed on the left side of the runway, lost its left wing and came to rest in flames about 700 meters past the runway threshold. All six crew members were quickly evacuated while the aircraft was destroyed.

Douglas C-54 Skymaster

Caught fire while parked at Toulouse-Blagnac Airport. There were no injuries but the aircraft was destroyed.

Douglas C-47 Skytrain (DC-3)

Shortly after takeoff from Biskra Airport, while climbing, the left engine failed. The aircraft stalled and crashed less than one km from the airfield and was destroyed upon impact. All 32 occupants have been killed. Crew: Jean-Marie Girardeau-Montaut, pilot, M. Leclerc, copilot, M. Vergnolle, radio operator, M. Lageat, mechanic, M. Ramel, steward.

Vickers Viscount

The crew left Paris-Orly Airport at 0849LT on a training flight to Reims, carrying three pilots, one instructor and one controller from the Vilgenis Instruction center. After takeoff, the crew climbed to 3,000 feet and above the cloud layer, continued under VFR. At 0858LT, the captain requested permission to climb to 5,000 feet when control was lost. The airplane entered a dive and crashed in a field located in Dannemois, about 31 km south of Paris-Orly Airport. The aircraft was destroyed by impact forces and a post crash fire and all five crew members were killed. Crew: Mr. Marchandise, Mr. Brunot, Mr. Colsy, Mr. Heymard, Mr. Nicolai.

Caudron C.440 Goéland

The crew left Pontoise-Cormeilles-en-Vexin Airport for a local training mission. En route, an unexpected situation forced the crew to attempt an emergency landing. The airplane crash landed in a field near the airport and came to rest. All four crew members were unhurt while the airplane was written off.

Douglas C-47 Skytrain (DC-3)

While descending to Lyon-Bron Airport, the crew encountered poor visibility with fog. On final, the airplane was too low and hit telephone lines before crashing in a field located in Saint-Priest, about 2 km short of runway 34. The aircraft was destroyed and all three crew members were killed. Built in 1943, the aircraft has been delivered to Air France on 20 April 1953. Crew: Gilbert Navarri, pilot, Léopold Bat, radio operator, Fernand Rozet, mechanic.

Douglas C-47 Skytrain (DC-3)

The crew was completing a local training flight at Nantes-Château Bougon Airport. In-flight, technical difficulties forced the pilot to attempt an emergency landing. The aircraft crashed on a railroad located near the airport. While all five crew members were rescued, the aircraft was written off.

Douglas C-47 Skytrain (DC-3)

On approach to Bordeaux-Mérignac Airport, the crew encountered poor visibility due to fog. On final, the airplane was too low and hit the ground few hundred yards short of runway. All three crew members were injured while the aircraft was destroyed. Crew: Serge Ponsot, pilot, Yves Rolland, radio operator, Maurice Yrissou, mechanic.

Douglas DC-3

The crew was conducting a local training flight at Beauvais-Tillé Airport. On takeoff from runway 31, the airplane encountered difficulties to gain height, hit power cables and crashed in a field. The aircraft was destroyed and all nine occupants were killed.

Lockheed L-749 Constellation

The crew started the approach to Gander Airport by night and in good weather conditions. Following a stabilized approach, the four engine aircraft landed normally on runway 32. After touchdown, the reverse thrust system were activated when the aircraft veered to the left. Despite several corrections on part of the flying crew such as braking action, movement on the nose wheel steering and power added on both left engines number one and two, the aircraft continued down the runway, overran, lost its undercarriage and came to rest into a ravine. While all 67 occupants were evacuated safely, the aircraft was damaged beyond repair.

Lockheed L-1049 Super Constellation

Air France Flight 075 originated at Orly Field, Paris, August 2, 1954, with a crew consisting of Captain Jean Caboche, Copilot Jean Roussean, Navigator Jacques Geffard., First Flight Engineer Albert Grandvaux, Second Flight Engineer Jean-Baptiste *** Stewardess Francine Dono, First Steward Michael Gallet, and Second Steward Jean Capron. The dispatch office had prepared two flight plans - one for a stop at Gander, Newfoundland, the other with a stop at Shannon, Ireland. Owing to marginal weather at Gander with the forecast indicating no improvement, the captain chose the latter plan. The flight departed Paris at 2024 and arrived Shannon at 2247. Fuel tanks were filled and the pilots ware briefed on weather for the nonstop flight to New York. Flight 075 departed Shannon at 0003 the next morning (August 3), estimating 11 hours 49 minutes an route, with fuel for nearly 14 hours. The gross weight at takeoff, 126,100 pounds, was less than the maximum allowable 133,000, and the load was correctly distributed relative to the canter of gravity of the aircraft. The Atlantic crossing was uneventful. Routine position reports were made en route and the flight periodically received weather reports for points along the route and at the destination. Stronger headwinds than had been anticipated were encountered near the North American continent, resulting in lower ground speed and somewhat higher fuel consumption per mile. The flight had approximately 600 gallons of fuel left at 1230 when it reported over Scotland Intersection (15 statute miles southwest of New York International Airport) and received clearance for an ILS approach. It was then 38 minutes behind its original flight plan estimate made at Shannon and had approximately 100 gallons less fuel than anticipated. During the approach, which was being monitored by New York International Airport radar, the flight encountered unexpected heavy turbulence, heavy rain, and a low ceiling, and the captain discontinued the approach at 1237 (0737 e. s. t.) when near his minimum prescribed altitude of 200 feet. The heavy turbulence made control of the aircraft difficult and when the missed approach was made, the captain found himself left of the localizer and below of glide path. The tower, which was immediately advised of the missed approach, told the flight to turn right to 130 degrees (the missed approach course), proceed to Scotland Intersection, and climb to 2,500 feet. Approximately three minutes after the missed approach and while on the 130-degrees course, the flight requested clearance to Boston. Such clearance was issued nine minutes later, as soon as possible consistent with other traffic. Meanwhile, the flight had reported being low on fuel but when asked if an emergency as being declared replied, "Negative, negative, not yet." At the approximate time clearance to Boston was received the flight engineer advised the captain that they had fuel of one more hour of flight. Thirty-three minutes after being cleared to Boston, the flight, at that time in the vicinity of Providence, Rhode Island, called Providence Tower, declared an emergency, and requested weather information. Providence weather, which was marginal, was furnished and the flight was cleared for an approach. However, the pilots found that their navigation kit did not contain an approach plate for Providence Airport and they advised they were not landing there. The captain then descended through a break in the overcast, circled two or three times, and landed with the gear retracted in a field at Preston City, Connecticut. It came to rest in flames in a garden and was destroyed by a post crash fire. All 37 occupants were evacuated safely. Nevertheless, 12 occupants were injured, among them both pilots.

Lockheed L-749 Constellation

The airplane left Paris-Orly in good weather conditions. However, few minutes later, the crew was informed about few turbulences over the Alps. While cruising by night at an altitude of 9,500 feet, the four engine aircraft hit the slope of Mt Cemet or Mt Cimet (3,020 meters high) located about 8 km northeast of Allos, in the department of Alpes-de-Haute-Provence. The wreckage was found at the altitude of 2,870 meters, about 150 meters below the summit. The aircraft disintegrated on impact and all 42 occupants were killed, among them the French violinist Jacques Thibaud and the French composer René Herbin. Crew: Jacques Tranoy, pilot, Jacques Calmette, copilot, Robert Mathis, radio navigator, M. Fontaine, mechanic, Jean-Marie Christophe, mechanic, Monique Perret, stewardess, Jean Menard, steward, Rémy Lebars, steward, Charles Delhomme, steward.

Lockheed L-749 Constellation

While cruising at an altitude of 17,500 feet between Rhodes Island and Cyprus, the crew noted slight vibrations but was unable to localize them. Four minutes later, a loud bang was noted, an explosion occurred, a brutal depressurization occurred and the aircraft lost 1,000 feet. The captain, who was sleeping, joined immediately his seat, disengaged the automatic pilot system and started an emergency descent with a rate of 300-500 feet per minute. In the mean time, the copilot informed ATC he elected to divert to Nicosia Airport. The crew realized that the engine number three fell off and decided to shut down the engine number four and feathered its propeller. Eventually, the captain decided to ditch the aircraft on a calm sea about two NM off the Fethiye lighthouse. Ten minutes after landing, the empennage broke off and sank. Some passengers swum to the shore and the aircraft eventually sank two hours later. Three crew members were injured, 35 occupants were unhurt and four passengers were killed.

AAC.1 Toucan

Shortly after takeoff from Miandrivazo Airport, the three engine aircraft nosed down and crashed in a field located about 500 meters from the runway. All three crew members and one passenger were killed while 11 others were injured. The aircraft was carrying a load of tobacco to Antananarivo. Crew: Henri Dedieu, pilot, Mr Aubert, radio operator, Mr. Cattelin, mechanic.

AAC.1 Toucan

Crashed in unknown circumstances. There were no casualties.

SNCASE SE.161 Languedoc

During takeoff run, the four engine aircraft skidded and went out of control. It veered off runway, lost its undercarriage and came to rest in a grassy area. All 23 occupants were evacuated safely while the aircraft was damaged beyond repair.

SNCASE SE.161 Languedoc

Forty-five seconds after takeoff from runway 04 at Nice Airport, while in initial climb, the four engine aircraft banked left, overturned and crashed in a huge explosion near the Saint-Augustin station, north of the airfield. The airplane disintegrated on impact and only a female passenger was found alive. Unfortunately, she died from her injuries four days later. Among those killed were both French actresses Michèle Verly and Lise Topart, and also the Welsh politician John Emlyn-Jones. Crew: Mr. Farrugia, pilot, Mr. Fraillon, radio operator, Mr. Cavaille, mechanic, Mr. Biancheri, steward.

AAC.1 Toucan

Crashed in unknown circumstances in the region of Andapa, killing six occupants. Crew: Mr. Duterriez, pilot, Mr. Desriac, radio navigator, Mr. Daumarie, mechanic, Mr. Caruana, steward.

Douglas DC-3

The aircraft took off from Paris-Le Bourget Airport at 0750LT on a flight to test a new type of air scoop. The new scoop was fitted to one engine only to allow comparison tests to be made. Five minutes later, the aircraft reached the altitude of 4,300 feet and four minutes later, at 0759LT, the starboard engine was stopped and the test commenced with a climb on the port engine with cooling gills open. At 0811LT, at an altitude of 6,980 feet, the crew commenced the second phase of the test with the port engine cooling gills in the trail position. Level off was completed at 0822LT at an altitude of 7,900 feet with the cooling gills closed. About an hour later, while flying at a relative low speed, the airplane went out of control and entered a spin, lost its empennage and eventually crashed in a field located in Moisville. The aircraft was destroyed and all five crew members were killed. Crew: René Gallichet, pilot, Louis Pichard, flight engineer, Jacques Légalité, radio navigator, Lucien Goulay, engineer, Paul Martin, engineer.