Crash of a Sud-Est Aviation SE-210 Caravelle VI-N in Marseille

Date & Time: Aug 2, 1969 at 1436 LT
Operator:
Registration:
I-DABF
Survivors:
Yes
Schedule:
Rome – Marseille
MSN:
179
YOM:
1965
Flight number:
AZ342
Country:
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
37
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5000
Captain / Total hours on type:
4193.00
Copilot / Total flying hours:
4100
Copilot / Total hours on type:
1500
Aircraft flight hours:
11848
Circumstances:
Following an uneventful flight from Rome-Fiumicino, the crew started the approach to runway 32 at Marseille-Marignane Airport and calculated the approach speed to be 120 knots. Following a wrong approach configuration and several errors, the crew continued the approach at a speed of 183 knots, causing the aircraft to land too far down the runway, nose gear first. Upon touchdown, the captain released the tailchute that burst immediately due to high speed. Unable to stop within the remaining distance, the airplane overran and eventually crashed in the Etang de Berre. The wreckage sank by a depth of four meter and all 44 occupants were quickly rescued, four of them were injured.
Photo via https://www.azfleet.info/
Probable cause:
The committee believes that the accident resulted initially from an incorrect procedure for the approach, bringing the plane in contact with the runway at abnormally high speed (more than 60 knots over the normal speed calculated and known by the pilot). This situation was further aggravated by the release of the parachute at an excessive speed and due to an inappropriate use of the emergency brake.
Final Report:

Crash of a Fokker F27 Friendship 600 in Reggio de Calabre: 1 killed

Date & Time: May 25, 1969 at 0952 LT
Type of aircraft:
Operator:
Registration:
I-ATIT
Survivors:
Yes
Schedule:
Rome - Reggio de Calabre
MSN:
10363
YOM:
1968
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
31
Pax fatalities:
Other fatalities:
Total fatalities:
1
Aircraft flight hours:
3087
Aircraft flight cycles:
3829
Circumstances:
On final approach to Reggio de Calabre Airport, the pilot-in-command failed to realize his altitude was insufficient when the right main gear struck a concrete wall located along the Agata River canal. The approach was continued when upon touchdown, the right main gear collapsed. Out of control, the airplane crash landed, lost its tail and came to rest on runway 15. A passenger was killed while nine others were seriously injured.
Probable cause:
Wrong approach configuration on part of the flying crew who let the aircraft descending below the glide. Poor flight supervision on part of the instructor who was seating on the jumpseat.

Crash of a Douglas DC-8-43 in Milan: 13 killed

Date & Time: Aug 2, 1968 at 1406 LT
Type of aircraft:
Operator:
Registration:
I-DIWF
Survivors:
Yes
Site:
Schedule:
Rome - Milan - Montreal
MSN:
45630
YOM:
1962
Flight number:
AZ660
Country:
Region:
Crew on board:
10
Crew fatalities:
Pax on board:
85
Pax fatalities:
Other fatalities:
Total fatalities:
13
Circumstances:
Flight AZ660 to Montreal, Canada departed Rome-Fiumicino Airport, Italy at 13:15. An intermediate stop was planned at Milan-Malpensa Airport. The airplane climbed in VMC to the en route altitude of FL220. The en route part of the flight was uneventful. While descending to the south of the airport, preparing for an approach to runway 35, the aircraft entered IMC with heavy turbulence due to the presence of a thunderstorm in the area. About 13:59 the flight was cleared from 9,000 feet down to 4,000 feet for a straight-in approach. Three minutes later the pilot advised that he would make a 360° turn over the beacon as the aircraft was at 6,000 feet. On completion of the turn, at an altitude of 1,500 feet, the flight continued on runway heading and descending. At 14:06 the flight crew became unsure of their position and almost immediately the airplane struck a wooded hillside 11,5 km north of Milan runway 35. 13 passengers were killed while 22 others were injured. 60 people were uninjured. The aircraft was destroyed by impact forces and a post crash fire.
Probable cause:
Insufficient checking of flight times during the final portion of the approach; Positioning for final approach by means of a non standard procedure; Delayed detection of the VOR radial or wrong selection of such radial; Broken view of terrain north of the airport similar to that south of the airport.

Crash of a Douglas DC-8-33 in Monrovia: 56 killed

Date & Time: Mar 5, 1967 at 0256 LT
Type of aircraft:
Operator:
Registration:
PP-PEA
Survivors:
Yes
Schedule:
Beirut – Rome – Monrovia – Rio de Janeiro
MSN:
45253/5
YOM:
1959
Flight number:
RG837
Country:
Region:
Crew on board:
19
Crew fatalities:
Pax on board:
71
Pax fatalities:
Other fatalities:
Total fatalities:
56
Captain / Total flying hours:
17718
Captain / Total hours on type:
1787.00
Copilot / Total flying hours:
15911
Copilot / Total hours on type:
408
Aircraft flight hours:
16775
Circumstances:
VARIG Flight RG837 departed Rome-Fiumicino Airport, Italy, at 21:08 hours GMT on a flight to Monrovia, Liberia. The flight was uneventful until the crew reported at FL45, five miles from the Roberts VOR. ATC then cleared the flight to descend further down to 3000 feet on the VOR and reported a QNH of 1009 mb. The QNH was read back correctly, but the crew did not mention the descent clearance. The pilot-in-command continued to the VOR at FL45 (4500 feet). After sighting the aerodrome runway lights from vertically overhead, the pilot informed the co-pilot that despite the fact that he had the runway completely in sight he would make an IFR/VOR procedure. A VOR/Locator instrument let-down was commenced from 4500 feet over the VOR at an indicated airspeed of 210 slowing to 170 kt, descending at a rate of between 500 to 700 feet per minute until the aircraft arrived at a point inbound over the coastline at 1800 feet on a heading of 047- degrees with the gear down and 35-deg flaps for landing on runway 04. At this point the co-pilot reported: "Runway in sight a little to the left". During the approach from the coast to the airport, the pilot did not make any use of the DME. After the procedure turn, the aircraft was on the correct VOR radial and a smooth approach was carried out during which the aircraft was flown manually. After the procedure turn, the co-pilot called each 100 feet of altitude and the speed and he checked the indication of the vertical speed indicators. At an altitude of about 1000 feet, flaps were put in the full down position and shortly thereafter, at an altitude of 700-800 feet, the aircraft entered some stratus and, further down, fog patches. When entering the stratus layer, the captain told the co-pilot that it was no longer necessary to report altitude and speed and was instructed to look outside and to report as soon as he could see the runway. Over the FR locator beacon, the altitude was about 800 feet, whereas his correct altitude should have been 520 feet. He then increased his rate of descent to between 1200-1500 ft/min, by reduction of power and by pitching the nose of the aircraft down. About 15 seconds after passing FR the co-pilot reported runway in sight, saying also that the visibility was poor and that they were too low. Descent was continued until the DC-8 impacted the ground 6023 feet from the threshold of runway 04, 180 feet to the right of the runway extended centre line with the aircraft coming to rest after a ground slide of approximately 850 feet. The aircraft caught fire and was totally destroyed. A crew members, 50 passengers and five people on a house were killed.
Probable cause:
The failure of the pilot-in-command to arrest in time the fast descent at a low altitude upon which he had erroneously decided, instead of executing a missed approach when he found himself too high over the locator beacon. The following findings were reported:
- The captain did not make use of the available navigational aids by disregarding the indications of his distance measuring equipment during final approach,
- At an altitude below 1 000 ft, the aircraft entered a stratus layer, which at that time completely obscured the runway,
- At the FR, positioned 1.7 NM before the runway threshold, the pilot-in-command saw that his altitude was 800 ft, whereas the correct altitude should have been 520 ft. Contrary to company instructions, he increased his rate of descent to between 1 200-1 500 ft/min by reducing engine power and pitching the nose of the aircraft down, with the intention to arrest his descent at about 500 ft,
- The attempt to level off was insufficient and/or too late, with the result that the aircraft touched the ground some 6 000 ft before the runway threshold when his glide path angle must have been 4.50 or more,
- During impact and the subsequent ground slide of about 850 it, the aircraft broke,up and caught fire,
- Those crew members who escaped relatively unhurt, once outside, might have directed more effort in further evacuation,
- The fire crew acted promptly, but its limited force and the necessary elapse time to reach the scene of the accident prevented them from saving people who might not yet have died.
Final Report:

Crash of a Boeing 707-331 in Rome: 49 killed

Date & Time: Nov 23, 1964 at 1409 LT
Type of aircraft:
Operator:
Registration:
N769TW
Flight Phase:
Survivors:
Yes
Schedule:
Kansas City – Chicago – New York – Paris – Milan – Rome – Athens – Cairo
MSN:
17685/123
YOM:
1960
Flight number:
TW800
Country:
Region:
Crew on board:
11
Crew fatalities:
Pax on board:
62
Pax fatalities:
Other fatalities:
Total fatalities:
49
Captain / Total flying hours:
17408
Captain / Total hours on type:
2617.00
Copilot / Total flying hours:
17419
Copilot / Total hours on type:
1269
Circumstances:
Flight 800 was a scheduled international flight from Rome, Italy to Athens, Greece. It departed the parking area at 1300 hours GMT with the copilot at the controls and the take-off run on runway 25 started at 1307 hours. The aircraft bad reached a speed above 80 kt when the pilot-in-command noticed that the No. 4 engine pressure ratio gauge was reading 1 (zero thrust) and, immediately thereafter, the amber light indicating thrust reversal of No. 2 engine came on. Since the speed was still below V1 for the weights and runway conditions, he decided to abort take-off and took over the controls to carry out the required manoeuvre. The tower was advised of this decision when the aircraft had reached a point 800 to 900 m after the threshold. The aircraft started to decelerate but at a much slower rate than expected, and at the same time veered strongly to the right with the result that the right landing gear was grazing the runway edge. Reverse thrust on the two right engines was reduced in an attempt to bring the aircraft back to the centre Line. The aircraft continued travelling beyond the declared runway limit and struck with No. 4 engine a pavement roller which was being used for maintenance work on taxiway 16/34 in an authorized area. After travelling a further 260 m, the aircraft came to a stop with fire on board. After a series of explosions, it was engulfed in flames and completely destroyed. The accident occurred at 1309 hours GMT. Five crew members and 44 passengers were killed, 24 others occupants were injured, some of them seriously.
Probable cause:
Damage to the reverse thrust system of No. 2 engine, not discernible by means of cockpit instruments, and consisting in the disconnection of a duct with resulting lack of pressure in the pneumatic clamshell door actuating mechanism. This malfunction allowed the development of considerable forward thrust by No. 2 engine even though the four levers were in the 'reverse' position. Rupture of fuel feed tube to No. 4 engine by impact with a power roller, and resulting ignition of spilled fuel. Failure of surge tank drainage because of a blocked valve, forcing the fuel out through the vent scoop and permitting access of fire to the wing. Presence of fuel-air vapor, formed in the tanks in explosive proportions, which caused the explosions when ignited.
Final Report:

Crash of a Vickers 785D Viscount on Mt Somma: 45 killed

Date & Time: Mar 28, 1964 at 2239 LT
Type of aircraft:
Operator:
Registration:
I-LAKE
Survivors:
No
Site:
Schedule:
Milan - Rome - Naples
MSN:
328
YOM:
1957
Flight number:
AZ045
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
40
Pax fatalities:
Other fatalities:
Total fatalities:
45
Circumstances:
Alitalia Flight 045 departed Rome (FCO) at 21:10 GMT and climbed to a cruising altitude of FL70. At 21:32 the crew were cleared to descend to 5,000 feet and further down to 4,000 feet on its way to Naples (NAP). Last radio contact with the flight was at 21:37 when leaving the LD NDB for a direct visual approach. A wide turn on downwind leg caused the aircraft to enter a area of heavy showers. At 2139 the aircraft flew into Monte Somma, at an altitude of 610 m (2000 feet) on a 90° heading with a 20° left bank. Mt Somma is part of the Mt Vesuvius Mountain Range.
Probable cause:
The accident was the consequence of the following factors:
- Delayed interruption of, or failure to interrupt, visual approach in the absence of minimum visibility conditions required for the type of manoeuvre involved;
- Abnormally wide initiation of down wind leg which brought the aircraft considerably south of the circuit for visual descent to the airport and along an unsafe path in relation to the terrain in the area;
- Inaccurate estimate of position of aircraft as a result of which the left turn manoeuvre was initiated too late for completion of the required manoeuvre.

Crash of a Vickers 739B Viscount off Elba Island: 23 killed

Date & Time: Sep 29, 1960 at 1215 LT
Type of aircraft:
Operator:
Registration:
SU-AKW
Flight Phase:
Survivors:
No
Schedule:
Geneva – Rome – Athens – Cairo
MSN:
427
YOM:
21
Flight number:
MS738
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
17
Pax fatalities:
Other fatalities:
Total fatalities:
23
Aircraft flight hours:
1230
Aircraft flight cycles:
535
Circumstances:
The four engine aircraft departed Geneva-Cointrin Airport at 1105LT bound for Rome-Fiumicino Airport. While cruising on airway A3 at an altitude of 21,000 feet, the crew requested permission to ATC to modify his route due to the presence of a low pressure area. Permission was granted and the crew modified his route when contact was lost. The airplane entered a dive and crashed into the Ligurian Sea, about 27 km north of Elbe Island. SAR operations were conducted but no trace of the airplane nor the 23 occupants was found. On October 3, tourists on their sailing ship found a wheel floating on water and the Italian Authorities confirmed it was part of the Egyptian airplane. Unfortunately, only few pieces were recovered.
Probable cause:
Due to lack of evidences, the exact cause of the accident could not be determined with certainty. However, it is believed that the loss of control was the result of severe turbulences encountered in a thunderstorm area which caused the failure of certain components of the aircraft and a eventual structural failure.

Crash of a Consolidated PB4Y-2 Privateer off Rome: 7 killed

Date & Time: Mar 7, 1951 at 1325 LT
Operator:
Registration:
59884
Flight Type:
Survivors:
Yes
Schedule:
Udine - Rome
MSN:
59884
YOM:
1943
Country:
Region:
Crew on board:
12
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
The aircraft left Udine-Campoformido Airport at 1220LT on a one hour flight to Rome-Ciampino. While approaching the capital city from the sea, the airplane apparently suffered a loss of power and crashed into the sea off Fiumicino. Five crew members were rescued while seven others were killed. The aircraft broke in two while contacting water and sank. It is reported from another source that the accident occurred shortly after takeoff from Athens-Hellenikon Airport.

Crash of a Savoia-Marchetti SM.95B in Civitavecchia: 14 killed

Date & Time: Jan 17, 1951 at 1440 LT
Type of aircraft:
Operator:
Registration:
I-DALO
Survivors:
Yes
Schedule:
Paris – Rome
MSN:
10
YOM:
1948
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
12
Pax fatalities:
Other fatalities:
Total fatalities:
14
Circumstances:
The four engine aircraft christened 'Ugolino Vivaldi' left Paris-Le Bourget Airport at 1016LT Bound for Rome-Ciampino. At 1436LT, the crew informed ground about his position at an altitude of 6,500 feet north of Civitavecchia. While descending to Ciampino, the crew encountered poor weather conditions with thunderstorm activity and turbulence. The aircraft was hit by lightning, dove into the ground and crashed near a railway road located 8 km north of Civitavecchia, about 75 km north of Ciampino Airport. A crew member and two passengers were seriously injured while 14 other occupants were killed.
Probable cause:
The probable cause of the accident was fire in flight, due to lightning striking the wing frame of the aircraft and igniting a mixture of air and petrol fumes in one of the wing panels or fuel tanks.
Final Report:

Crash of a Douglas C-54A-5-DO Skymaster in Ponte Galeria

Date & Time: Jan 13, 1948 at 1340 LT
Type of aircraft:
Operator:
Registration:
LV-AFG
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Rome - Rome
MSN:
7479
YOM:
1944
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft was carrying a passenger and six crew members on a test flight in Rome-Fiumicino Airport. While flying in the vicinity of the airfield, an engine caught fire and the captain elected to make an emergency landing. The aircraft belly landed in a field located in Ponte Galeria, east of the airport, and came to rest in flames. All seven occupants were unhurt while the aircraft was destroyed by fire.
Probable cause:
Engine fire.