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Crash of a Cessna 421C Golden Eagle III in Donzeil: 8 killed

Date & Time: Nov 7, 1996 at 1029 LT
Operator:
Registration:
HB-LRX
Flight Phase:
Survivors:
No
Schedule:
Geneva - Bordeaux
MSN:
421C-0217
YOM:
1976
Location:
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
8
Captain / Total flying hours:
7047
Captain / Total hours on type:
113.00
Aircraft flight hours:
2488
Circumstances:
The twin engine aircraft departed Geneva-Cointrin Airport at 0842LT on a charter flight to Bordeaux-Mérignac, carrying one pilot and seven passengers. At 0903LT, while cruising at an altitude of 20,000 feet, the pilot informed ATC about the failure of the right engine and was cleared to reduce his altitude and to divert to Limoges Airport. The pilot elected to restart the engine below FL100 but was unable to do so. Due to high drag, the aircraft continued to lose height and was unable to reach Limoges Airport. At 1029LT, the aircraft went out of control and crashed in an open field, bursting into flames. The wreckage was found near Donzeil, between Guéret and Aubusson, about 60 km northeast of Limoges. The aircraft was totally destroyed by impact forces and a post crash fire and all eight occupants were killed.
Pilot:
Jean-Claude Kaufmann.
Passengers:
Jacques Faini,
Serge Frochot,
Didier Hostettler,
Étienne Moinat,
Jean-Claude Paccaud,
Michel Rothen,
Jean-François Troger.
Probable cause:
It was determined that the accident was the consequence of an inappropriate management of the flight following jamming of the propeller in an intermediate position after the RH crankshaft rupture. The inappropriate management was due to:
- The pilot's relative lack of experience on this aircraft type,
- His false notions about the aircraft's performance and about the existence of a flight level to maintain level flight with an unfeathered propeller and an heavy aircraft,
- A series of misjudged strategies to attempt to continue the flight then to land at Limoges when the aircraft's altitude no longer made this possible.
The lack of instructions relative to inspections by a reliable method for detection of cracks on crankshafts installed on GTSIO-520 engines was a contributory factor.
Final Report:

Crash of a Transall C-160D in Bordeaux: 6 killed

Date & Time: Jul 2, 1988
Type of aircraft:
Operator:
Registration:
50+80
Flight Type:
Survivors:
Yes
Schedule:
Stuttgart - Bordeaux
MSN:
D117
YOM:
1971
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
On approach to Bordeaux-Mérignac Airport following an uneventful flight from Stuttgart-Echterdingen Airport, one of the engine failed. The aircraft lost height, struck power cables and crashed in a wooded area located in Eysines, few km short of runway 23 threshold. The aircraft was destroyed and all six occupants were killed.
Probable cause:
Engine failure for unknown reasons.

Crash of an Embraer EMB-120RT Brasília in Bordeaux: 16 killed

Date & Time: Dec 21, 1987 at 1510 LT
Type of aircraft:
Operator:
Registration:
F-GEGH
Survivors:
No
Schedule:
Brussels - Bordeaux
MSN:
120-033
YOM:
1986
Flight number:
AF1919
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
13
Pax fatalities:
Other fatalities:
Total fatalities:
16
Captain / Total flying hours:
2394
Captain / Total hours on type:
101.00
Copilot / Total flying hours:
1326
Copilot / Total hours on type:
215
Aircraft flight hours:
2505
Circumstances:
Following an uneventful flight from Brussels, the crew contacted Bordeaux Approach at 15:01 and was vectored for an ILS approach to runway 23. Visibility was poor with low clouds at 100 feet and a runway visual range (RVR) of between 650 and 350 metres. Flight 1919 crossed the KERAG beacon, the initial approach fix (IAF) at an altitude of FL144, at 15:04:40. Cloud base was still around 100 feet so the crew requested to enter a holding pattern to the south of the airport. The weather conditions slightly improved during the next few minutes and Bordeaux Approach reported a cloud base at 160 feet. Flight 1919 had not reached the holding pattern yet and the pilot decided to attempt to rejoin the ILS. At 15:06:38 the flight was cleared direct to the BD beacon and to descend down to 2000 feet. At the BD beacon, the flight was cleared for final approach and instructed to contact Bordeaux Tower. The airplane had overshot the centreline and was slightly right on the glidepath. Bordeaux Tower then instructed the flight to report over the Outer Marker, which was acknowledged by the captain. After crossing the Outer Marker, the airplane was still not properly established on the ILS. The airplane descended below the glideslope with the crew hurriedly deploying flaps and landing gear. The captain did not contact Bordeaux Tower as requested. Instead he took over control of the airplane, attempting to continue the approach. Both crew members had very little time to adapt to their new roles as the airplane was descending below the glide slope. The descent continued until the aircraft struck tree tops and crashed in the Eysines forrest, about 5 km short of runway. The aircraft was totally destroyed and all 16 occupants were killed.
Probable cause:
The accident was the direct result of poorly managed aircraft trajectory.
- The lack of vigilance with respect to altitude, by one pilot and then the other, when they were in a pilot-flying situation (PF, according to the Air Littoral Operations Manual) both when the aircraft descended out of the ILS beam through 2000 feet altitude and when it descended below 220 feet, the decision height.
- Inadequate coordination of tasks between the two pilots who formed the flight crew, neither of which had performed important tasks related to this function, such as monitoring and reporting ILS or altitude deviations, while in a nonpilot-flying situation (PNF, according to the same manual).
Final Report:

Crash of a SNCAC NC.701 Martinet in Bordeaux: 5 killed

Date & Time: Apr 29, 1963
Type of aircraft:
Operator:
Registration:
120
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
120
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
While taking off from Bordeaux-Mérignac Airport, the twin engine aircraft went out of control and crashed. Two passengers were seriously injured while five other occupants were killed.

Crash of a Douglas DC-7C in Bordeaux: 54 killed

Date & Time: Sep 24, 1959 at 2324 LT
Type of aircraft:
Operator:
Registration:
F-BIAP
Flight Phase:
Survivors:
Yes
Schedule:
Paris – Bordeaux – Bamako – Abidjan
MSN:
45366
YOM:
1957
Flight number:
TAI307
Country:
Region:
Crew on board:
9
Crew fatalities:
Pax on board:
56
Pax fatalities:
Other fatalities:
Total fatalities:
54
Captain / Total flying hours:
11704
Captain / Total hours on type:
479.00
Copilot / Total flying hours:
10829
Copilot / Total hours on type:
312
Aircraft flight hours:
5844
Circumstances:
Shortly after a night takeoff from runway 23 at Bordeaux-Mérignac Airport, the aircraft followed a straight-in path but failed to gain sufficient height. After a short course, while at an altitude of about 100 feet, the four engine aircraft struck pine trees, stalled and crashed in flames in a wooded area located 1,050 meters past the runway end. The aircraft was destroyed by impact forces and a post crash fire and all 9 crew members and 45 passengers were killed. Eleven passengers were seriously injured.
Probable cause:
The Board considered that the accident was probably caused by the most unfavorable combination of several of the following factors:
- Failure of one or more engine,
- Wrong maneuver of the undercarriage or flaps,
- Malfunction of the control systems,
- Incident in the cockpit,
- False indication on one or more instruments,
- Wrong indication of the artificial horizon,
- Failure of the anemometer,
- Incorrect altimeter setting,
- Error in the variometer.
The reconstructed flight showed that during the first segment of climbout and during a very short critical phase, a slight increase in speed will produce a considerable decrease in rate of climb or even a slight loss of altitude. In view of the rapid sequence of cockpit operations during this phase, together with the rapid variation in flight parameters, and the lack of precision - even inaccuracy - of readings of certain instruments, and lacking time reference and external visual references, a pilot may follow a line of flight that will bring the aircraft back near the ground if, during this period, optimum climbing speed is not maintained and the altimeter is not carefully watched.
Final Report:

Crash of a Douglas C-47A-50-DL in Bordeaux

Date & Time: Sep 21, 1955
Operator:
Registration:
F-BCYU
Flight Type:
Survivors:
Yes
Schedule:
Pau – Bordeaux
MSN:
10151
YOM:
1943
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
10898
Circumstances:
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.

Crash of a Douglas C-54A-5-DC Skymaster in Bordeaux: 9 killed

Date & Time: Feb 7, 1953 at 1028 LT
Type of aircraft:
Operator:
Registration:
F-BFGR
Survivors:
Yes
Schedule:
Abidjan – Conakry – Dakar – Casablanca – Bordeaux – Paris
MSN:
10290
YOM:
1944
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
13
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
6878
Captain / Total hours on type:
1877.00
Copilot / Total flying hours:
350
Copilot / Total hours on type:
40
Aircraft flight hours:
11250
Circumstances:
The final approach to Bordeaux-Mérignac was performed in foggy conditions. Due to low visibility, the flying crew did not realize that his altitude was insufficient when the four engine aircraft hit the top of pine trees, stalled and crashed in flames in a wooded area located in Eysines, north of the airfield. The aircraft was destroyed by a post crash fire and nine occupants were killed, six crew members and three passengers.
Probable cause:
It was determined that the causes of the accident, listed in the chronological order of their occurrence, can be analyzed as follow:
- unfortunate initiative by the tower controller and a misjudgment by the pilot-in-command leading to an attempt to land in insufficient visibility,
- use of an attention-grabbing procedure by an excess of means for guiding in plan to the detriment of altitude safety,
- a probable wrong altimeter setting,
- wrong interpretation of the altitude vertical to the outer marker.
The fatigue of the flying crew resulting from an excessive period of duty and the discomfort caused by the presence in the cockpit of two additional crew members under training may have contributed to the occurrence.
Final Report:

Crash of a Douglas C-47A-5-DK near Mimizan

Date & Time: Apr 2, 1952
Operator:
Registration:
LN-NAE
Survivors:
Yes
Schedule:
Madrid – Bordeaux – Norrköping
MSN:
12372
YOM:
1944
Location:
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
22
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft was completing a charter flight from Madrid to Norrköping with an intermediate stop in Bordeaux, carrying a crew of six and 22 members of a Swedish football team. While descending to Bordeaux-Mérignac Airport in poor weather conditions, a technical failure occurred on one engine. The captain realized that it was not possible to reach the airport of Bordeaux so he reduced his altitude and attempted an emergency landing on a beach located three km north of Mimizan. The airplane belly landed on the sand beach, slid for dozen yards and came to rest partially submerged. All 28 occupants were evacuated safely while the aircraft was considered as damaged beyond repair.
Probable cause:
Engine failure.

Crash of a Fairchild C-82A-FA Packet near Le Mont-Dore: 36 killed

Date & Time: Nov 13, 1951 at 1300 LT
Type of aircraft:
Operator:
Registration:
45-57801
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Frankfurt – Bordeaux
MSN:
10171
YOM:
1945
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
32
Pax fatalities:
Other fatalities:
Total fatalities:
36
Circumstances:
After departure from Frankfurt-Main Airport, the crew was informed about strong winds blowing from the northwest up to 30 knots, on the route between Dijon and Bordeaux. The pilot-in-command continued his route in IFR Mode at the altitude of 6,000 feet. While cruising in marginal weather conditions, the aircraft hit the slope of a mountain located near Le Mont-Dore, about 32 km southwest of Clermont-Ferrand. The airplane was destroyed upon impact and all 36 occupants were killed. It was reported that the visibility was estimated over 40 km below the cloud layer that was 6/8 at 1,000 meters. Nevertheless, the aircraft was off course to the south by 100 km at the time of the accident, probably due to strong winds. Also, the crew continued the flight at an altitude of 6,000 feet instead of the initial intended 8,000 feet.

Crash of a Vickers 639 Viking 1 in Bordeaux

Date & Time: May 8, 1951 at 1412 LT
Type of aircraft:
Operator:
Registration:
G-AHPD
Flight Phase:
Survivors:
Yes
Schedule:
Gibraltar – Bordeaux – Bovingdon
MSN:
134
YOM:
1946
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
26
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
At 1610LT, the aircraft took off for Bovingdon, UK, while on a regular schedule flight from Gibraltar. On throttling down to initial climbing speed, at a height of 50 meters the pilot noted that the speed of the port engine was rapidly decreasing. He shut off this engine and feathered the propeller, opening the starboard engine full out. He then became aware that the aircraft could not maintain its safety speed without losing height and decided to make a wheels up landing on an open space south of the aerodrome. The aircraft slid along the ground for about 100 meters, slewed around and came to a standstill. The copilot was injured, however, the remaining four crew members and twenty-six passengers were unharmed.
Probable cause:
The disconnecting of the articulated control rod of the propeller governor due to the lack of a split pin on the governor spindle and to the nut of the ball-joint of the control spindle having been unscrewed by force.
Final Report: