Crash of a Boeing 707-345C in Paris: 123 killed

Date & Time: Jul 11, 1973 at 1403 LT
Type of aircraft:
Operator:
Registration:
PP-VJZ
Survivors:
Yes
Schedule:
São Paulo – Rio de Janeiro – Paris
MSN:
19841
YOM:
1968
Flight number:
RG820
Country:
Region:
Crew on board:
17
Crew fatalities:
Pax on board:
117
Pax fatalities:
Other fatalities:
Total fatalities:
123
Captain / Total flying hours:
17959
Captain / Total hours on type:
4642.00
Copilot / Total flying hours:
12613
Copilot / Total hours on type:
5055
Aircraft flight hours:
21470
Aircraft flight cycles:
5677
Circumstances:
The airplane departed Rio de Janeiro-Galeão Airport at 0303LT on flight RG820 to Paris-Orly Airport. The en route part of the flight was uneventful. At 13:57 the aircraft had descended to FL80 and contacted Orly approach, who told the crew to maintain FL80 and head to the OLS VOR which would take the aircraft to the downwind leg of runway 26. At 13:58:20 the flight crew contacted Orly approach and reported a "problem with fire on board". An emergency descent was requested. At 13:59 clearance was given to descend to 3000 feet for a runway 07 landing, making a straight-in approach possible. While the situation on board was getting worse (smoke entering the cockpit and passengers becoming asphyxiated), a clearance to descend to 2000 feet was given at 14:01:10. The flight crew put on oxygen masks as smoke was making it impossible to read the instruments. At 14:03 the pilot decided to make an emergency landing 5 km short of the runway with gear down and flaps at 80°. The Boeing approached with considerable nose-up attitude, in a slight left bank. The aircraft truncated some small trees and made a heavy landing on a field. Both main gears collapsed and the engines were torn off in the subsequent skid. The fuselage however, remained intact. Ten occupants (all crew members) evacuated the aircraft. By the time the firemen arrived (6-7 minutes later) the fire had burned through the roof and there was no sign of life. Of the four unconscious occupants the firemen could evacuate, only one survived.
Probable cause:
A fire which appears to have started in the washbasin unit of the aft right toilet. It was detected because smoke had entered the adjacent left toilet. The fire may have been started by an electrical fault or by the carelessness of a passenger. The difficulty in locating the fire made the actions of cabin personnel ineffective. The flight crew did not have the facilities to intervene usefully from the cockpit against the spread of the fire and the invasion of smoke. The lack of visibility in the cockpit prompted the crew to decided on a forced landing. At the time of touch-down the fire was confined to the area of the aft toilets. The occupants of the passenger cabin were poisoned, to varying degrees by carbon monoxide and other combustion products.
Final Report:

Crash of an Airspeed AS.57 Ambassador 2 in London-Gatwick

Date & Time: Jul 26, 1969
Type of aircraft:
Operator:
Registration:
G-ALZR
Flight Type:
Survivors:
Yes
Schedule:
Paris - London
MSN:
5214
YOM:
1952
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On touchdown at Gatwick Airport, the nose gear collapsed. The airplane slid for dozen yards before coming to rest. All eight occupants were evacuated safely while the aircraft was damaged beyond repair.
Probable cause:
Nose gear collapsed on landing.

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 Douglas C-47B-20-DK in Jersey: 26 killed

Date & Time: Apr 14, 1965 at 1806 LT
Operator:
Registration:
G-ANTB
Survivors:
Yes
Schedule:
Paris – Jersey
MSN:
15762/27207
YOM:
1945
Flight number:
BR1030X
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
23
Pax fatalities:
Other fatalities:
Total fatalities:
26
Captain / Total flying hours:
4750
Captain / Total hours on type:
1227.00
Copilot / Total flying hours:
1188
Copilot / Total hours on type:
730
Aircraft flight hours:
18544
Circumstances:
Flight 1030X was an extra scheduled international flight from Paris (Orly), France, to Jersey, Channel Islands. It took off from Orly at 1626 hours GMT. At 1706 hours, when about 100 miles from Jersey, the pilot made his first radio contact with Jersey zone concerning the Jersey weather. At 1742 hours he informed Jersey zone that he was descending to 1 500 ft and estimated Jersey at 1755 hours. He was then given the 1720 hours Jersey weather report, which included visibility 80 m, RVR 200 m and 818 cloud at the surface, after which the aircraft was cleared to Jersey Approach Control. In response to the approach controller's question as to his intentions concerning diversion, the pilot replied: "We'll come down the ILS and then overshoot and go to Dinard." The controller then cleared the aircraft to 1 000 ft and passed the QFE as 1 007 mb. The aircraft arrived at the Jersey beacon at 1753 hours and began an approach to runway 27, during which the guidance provided from the ILS was supplemented by distance information provided by the controller from the indications of the Decca 424 radar. The approach, the subsequent overshoot and the climb to 1 000 ft appear to have been without incident, following which the pilot informed the controller of his intention to make another approach and requested radar guidance back to the ILS outer marker. After directing the aircraft into position for a second approach to runway 27, the controller advised the pilot to take up his own headings on the ILS and informed him at 1803 hours that the aircraft was 5 miles from touchdown. Just after being given a distance of 4 miles, the pilot reported passing the outer marker and also that he was established, thus indicating that guidance was being received from the ILS and being used for the approach. Subsequent distance information was given by the controller at 1.5 mile, which was not acknowledged by the pilot, and again at 1 mile (at 1806:13 hours). Both these transmissions were clipped and are recorded as "... and a half miles now" and "... mile from touchdown". The latter transmission provoked an immediate "how many?" from the pilot, to which the controller replied by giving "three quarters of a mile now and left of the centre line." The pilot acknowledged this at 1806:24* hours with "TB" (the final two letters of the aircraft's registration). This was the last communication received from the aircraft. According to the air hostess, (the sole survivor), the flight was uneventful up to the time of the accident. She did not have any feeling of descending at any time. There was a bump which she attributed to the starboard undercarriage wheels having hit something; this was followed by a momentary roll to the right and a much greater roll back to the left. Subsequently, it was established that the aircraft had hit with its starboard wing the outermost approach light pole, which was 3 000 ft from the runway threshold, at a height 58 ft above runway level. After climbing slightly,'it rolled to an inverted attitude, at which time the starboard wing folded rearwards and separated as the aircraft dived to the ground, still inverted. It crashed at about 1806:27 hours. The stewardess survived while all 26 other occupants were killed.
Probable cause:
The aircraft struck the approach lighting when it was flown below the safe approach path during an approach to land in conditions of very low cloud and poor visibility, the pilot having disregarded the approach ban applied by his operations manual.
Final Report:

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 Vickers 701 Viscount in Dannemois: 5 killed

Date & Time: Dec 12, 1956 at 0900 LT
Type of aircraft:
Operator:
Registration:
F-BGNK
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Paris – Reims
MSN:
8
YOM:
1953
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
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.
Probable cause:
The cause of the loss of control could bot be determined with certainty.

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 Douglas C-47D in Deftinge

Date & Time: May 28, 1955 at 1315 LT
Operator:
Registration:
43-48479
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Paris – Copenhagen
MSN:
14295/25740
YOM:
1944
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The airplane departed Paris-Orly on a flight to Copenhagen-Kastrup. While overflying Belgium, the crew encountered technical issues with an engine. The captain ordered his crew to bail out, and sole on board, he elected to make an emergency landing when the airplane hit trees, lost its tail and crashed in a field. The pilot was uninjured while the aircraft was damaged beyond repair. All four other crew members were uninjured as well.
Probable cause:
Engine failure.