Country
code

Val-de-Marne

Crash of a Douglas C-54A-15-DC Skymaster in Paris-Orly

Date & Time: May 28, 1969
Type of aircraft:
Operator:
Registration:
F-BFCP
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Paris- Poitiers – Bordeaux – Toulouse – Pau
MSN:
10346
YOM:
1944
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
35777
Circumstances:
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.
Probable cause:
The loss of control was the consequence of an engine malfunction due to an error on part of the flight engineer who placed the main fuel selectors in a 'half-on' position which corresponded with the 'On' position in five of the DC-4 aircraft of the company.

Crash of a Boeing 707-328 in Paris: 130 killed

Date & Time: Jun 3, 1962 at 1234 LT
Type of aircraft:
Operator:
Registration:
F-BHSM
Flight Phase:
Survivors:
Yes
Schedule:
Paris – New York – Atlanta – Houston
MSN:
17920
YOM:
1960
Flight number:
AF007
Country:
Region:
Crew on board:
10
Crew fatalities:
Pax on board:
122
Pax fatalities:
Other fatalities:
Total fatalities:
130
Captain / Total flying hours:
14225
Captain / Total hours on type:
743.00
Copilot / Total flying hours:
15194
Copilot / Total hours on type:
1407
Aircraft flight hours:
4491
Circumstances:
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.
Probable cause:
The accident was due to the concurrence of: 1) a considerable out-of-trim condition producing major loads on the control column at VR and VLOF which may have seemed prohibitive to the pilot-in-command; and 2) a failure of the trim servo motor control system which prevented the pilot-in-command from rectifying the faulty setting of the stabilizer and, consequently, from reducing the reaction at the control column. These factors led the pilot-in-command to discontinue take-off, but it was too late to stop the aircraft on the runway or slow it down sufficiently before the end of the runway.
Final Report:

Crash of a Lockheed L-1049G Super Constellation at Paris-Orly

Date & Time: Dec 6, 1957 at 1900 LT
Operator:
Registration:
F-BHMK
Flight Type:
Survivors:
Yes
Schedule:
Paris - Reims - Paris
MSN:
4670
YOM:
22
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
11960
Captain / Total hours on type:
1078.00
Copilot / Total flying hours:
9044
Copilot / Total hours on type:
385
Aircraft flight hours:
3075
Circumstances:
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.
Probable cause:
The accident was the result of excessive corrective manoeuvres performed at the time of contact with the runway. Icing on the aircraft might have reduced its aerodynamic qualities.
Final Report:

Crash of a SNCASE SE.2010 Armagnac in Paris: 2 killed

Date & Time: Jan 29, 1957 at 2024 LT
Type of aircraft:
Registration:
F-BAVG
Survivors:
Yes
Schedule:
Tunis – Paris
MSN:
06
YOM:
1952
Country:
Region:
Crew on board:
10
Crew fatalities:
Pax on board:
60
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
After a normal flight from Tunis the aircraft arrived at Paris at night and in weather conditions close to the operational minima and made an unsuccessful attempt to land using ILS monitored by GCA. The pilot-in-command then decided to land with GCA guidance. Lacking sufficient visual references to permit landing, the pilot applied full power at low altitude, in the immediate vicinity of the runway end. The aircraft, on a heading divergent from the landing runway, continued to lose altitude and struck the ground (at 1924 hours GMT) in a slightly nose-down position, banking to starboard. The right wing burned after separation from the fuselage and the rest of the aircraft turned over in a half-roll and broke up into four main parts. A crew member and a passenger were killed while 33 occupants were injured and 35 others were unhurt.
Probable cause:
The immediate cause of the accident was as follows: stalling as a result of delayed application of power with a heavy aircraft in final approach configuration and inadequate control of heading, airspeed and altitude after the visual break-through. The following contributing factors are noteworthy:
- Deterioration in weather conditions in the immediate vicinity of the runway threshold,
- Absence of radio altimeter,
- Faulty application of landing tech niques by both ground and flight personnel.
Final Report:

Crash of a Douglas DC-6B in Paris-Orly: 34 killed

Date & Time: Nov 24, 1956 at 0018 LT
Type of aircraft:
Operator:
Registration:
I-LEAD
Flight Phase:
Survivors:
Yes
Schedule:
Rome – Milan – Paris – Shannon – Gander – Boston – New York
MSN:
45075
YOM:
1956
Flight number:
LAI451
Country:
Region:
Crew on board:
10
Crew fatalities:
Pax on board:
25
Pax fatalities:
Other fatalities:
Total fatalities:
34
Captain / Total flying hours:
10000
Circumstances:
After liftoff from runway 26 at Paris-Orly Airport, the four engine aircraft encountered difficulties to gain height, hit successively two houses, stalled and crashed in a huge explosion about 600 meters past the runway end. The aircraft disintegrated on impact and debris were scattered for about 200 meters. A passenger was seriously injured while all 34 other occupants, among them the Italian Director Guido Cantelli, were killed.
Probable cause:
The Commission was unable to find any malfunctioning of the aircraft or its equipment which would make it possible to determine why the aircraft followed the observed flight path. The Commission, therefore, believes that:
- the aircraft's slight loss of altitude soon after take-off was the main cause of the accident. There is no explanation for this loss of altitude,
- although the regulations in force were observed, the presence of unmarked obstructions in the take-off path constituted an aggravating factor,
- the initial and direct cause of the accident remains unknown.
Final Report:

Crash of a Fairchild C-119C-26-FA Flying Boxcar in Choisy-le-Roi: 6 killed

Date & Time: Nov 27, 1953
Operator:
Registration:
51-2621
Flight Type:
Survivors:
No
Schedule:
Dover – Lajes – Paris – Frankfurt
MSN:
10610
YOM:
1951
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
The crew was performing a ferry flight from Dover, Delaware, to Frankfurt-Main Airbase with intermediate stops in Lajes, Azores Islands, and Paris-Orly. On final approach, the airplane went out of control and crashed in flames in Choisy-le-Roi, less than four km from the runway threshold. All six occupants were killed.
Probable cause:
It is believed that the loss of control may have been caused by the loss of the rear clam shell door which detached on final approach and struck the horizontal stabilizer, causing the failure of the empennage and the subsequent crash of the airplane.

Crash of a Douglas VC-47A in Paris-Orly

Date & Time: Feb 4, 1953
Operator:
Registration:
42-93722
Flight Type:
Survivors:
Yes
MSN:
13665
YOM:
1944
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed on landing. There were no casualties.

Crash of a SNCASE SE.161 Languedoc in Bonneuil-sur-Marne: 11 killed

Date & Time: Oct 23, 1952 at 1030 LT
Type of aircraft:
Operator:
Registration:
86/F-RAPC
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Paris - Paris
MSN:
86
YOM:
1949
Country:
Region:
Crew on board:
10
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
11
Circumstances:
The aircraft was involved in a training flight from Paris-Le Bourget to Paris-Orly, carrying ten crew members and one engineer from SNCASE. Shortly after takeoff from Paris-Le Bourget Airport, while in initial climb, the crew encountered technical problems when the flaps were retracted. The four engine aircraft went out of control and crashed in a field located in Bonneuil-sur-Marne, about 8 km northeast of Le Bourget Airfield. The aircraft was destroyed and all 11 occupants were killed.
Crew:
Cdt Danna,
Cpt Humbert,
Lt Dutheil de la Rochère,
Adj Dumont,
Adj Lottiaux,
Adj Verdier,
S/Sgt Mauconduit,
Sgt Dervin,
Sdt Cosson,
Sdt Biava.
Passenger:
Mr. Devos.
Probable cause:
The loss of control occurred when the crew decided to raise the flaps, apparently following an asymmetric issue.

Crash of a Douglas VC-47A in Paris: 3 killed

Date & Time: Sep 20, 1952
Operator:
Registration:
42-23967
Flight Type:
Survivors:
Yes
MSN:
9829
YOM:
1943
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
On final approach to Paris-Orly Airport, the aircraft was too low and hit a telephone pole, passed just over the roofs of several houses and crashed in flames one km short of runway. A crew member was rescued while three others were killed.

Crash of a SNCASO SO.30P-1 Bretagne in Paris

Date & Time: Oct 30, 1951
Type of aircraft:
Operator:
Registration:
F-OAIY
Flight Phase:
Survivors:
Yes
Schedule:
Paris – Algiers
MSN:
12
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
30
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The right main undercarriage leg retracted suddenly while the aircraft was on a take-off run. The right wing struck the ground and slewed the aircraft round in the opposite direction. Fire broke out in the cargo hold but all passengers and crew were safely evacuated. The aircraft and cargo were about 80% destroyed.
Probable cause:
The cause of the sudden retraction of the right leg of the main landing gear could not be determined. However, the assumption that a tire on the right main gear burst during takeoff is not ruled out.
Final Report: