Crash of a Douglas C-47B-5-DK in Hassi Messaoud

Date & Time: May 22, 1963
Operator:
Registration:
F-OAVR
Survivors:
Yes
MSN:
14520/25965
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 at Hassi Messaoud Airport. There were no casualties but the aircraft was written off.

Crash of a Douglas C-47 in the Sandia Mountains: 9 killed

Date & Time: Apr 26, 1963
Operator:
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Andrews - March
Crew on board:
4
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
The crew was performing a secret mission from Andrews AFB to March AFB. While overflying New Mexico, he encountered severe icing conditions. A wing fell off and the aircraft crashed in the Sandia Mountain Range located northeast of Albuquerque. All nine occupants were killed and the aircraft was destroyed. All USAF C-47's were grounded following this accident, until the struts had been replaced.
Probable cause:
Investigations revealed that a wing's guy broke in flight, probably when the airplane was flying in an area subject to severe icing.

Crash of a Douglas C-47A-80-DL off Fuerteventura: 7 killed

Date & Time: Apr 21, 1963 at 0311 LT
Operator:
Registration:
T.3-44
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Las Palmas – Los Llanos
MSN:
19750
YOM:
1944
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
The crew departed Las Palmas-Gando Airport at 0227LT on a flight to the airbase of Los Llanos in Albacete. While approaching the island of Fuerteventura, the twin engine aircraft crashed into the sea some 44 minutes after takeoff. SAR operations were conducted but eventually suspended few days later as no trace of the aircraft nor the seven crew members was found.
Probable cause:
Due to lack of evidence, it was not possible to determine the cause of the accident.

Crash of a Douglas C-47B-35-DK near Sora: 8 killed

Date & Time: Mar 30, 1963 at 1837 LT
Operator:
Registration:
I-TAVI
Flight Phase:
Survivors:
No
Site:
Schedule:
Pescara – Rome
MSN:
16477/33225
YOM:
1945
Flight number:
IH703
Location:
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
8
Captain / Total flying hours:
10731
Captain / Total hours on type:
2296.00
Copilot / Total flying hours:
832
Copilot / Total hours on type:
832
Aircraft flight hours:
13941
Circumstances:
Flight IH703 was a scheduled domestic flight from Pescara Airport to Rome-Ciampino. The aircraft which had departed Rome at 1526 hours GMT, took off from Pescara with the same crew at 1736 hours on an IFR plan and climbed to flight level 100, its cruising altitude. At 1739 hours the pilot requested radar guidance from the Pescara defence radar "FIONDA", which is not normally available for flight information service to civil aircraft. The first part of the flight was intentionally carried out south of the direct route to avoid heavy cloud formations. At 1750 hours the Pescara defence radar picked up the flight in the Ortona area and at approximately 1803 hours it passed to the flight "QDM Ciampino 265°, distance 80 NM". At 1805 hours the pilot reported this position to the Rome ACC/FIC. After having directed the flight around some cumulonimbus the Pescara defence radar lost the aircraft at 1812 hours. At 1816 hours the pilot enquired whether the aircraft had been picked up by the Rome surveillance radar. Two minutes later he reported to Rome ACC/FIC that he was crossing the eastern edge of airway A 14 and requested a clearance to Rome NDB "LJ". At 1822 hours he reported having Rome in sight and requested authorization to descend from flight level 100. - Two minutes later, upon confirmation that Rome was in sight, the flight was cleared to proceed to Rome NDB and to descend to 6 000 ft. At 1828 hours the pilot reconfirmed that he had Rome in sight and requested clearance to descend further. The flight was then given instruction to contact Ciampino tower, but was unable to establish communication either on the tower frequency or on 120.1 or 124.1 MC/S and therefore came back on the Rome ACC/FIC frequency. At 1830 hours the pilot reported that he was unable to tune on Rome NDB and had to keep out of the clouds since his radio compass was not working properly. At that time the Rome 2 defence radar which had first picked up the flight around 1802 hours, lost its trace in the Arpino area. Around 1832 hours, on a request from Rome ACC/FIC, the pilot reported that he was in the vicinity of Mount Cavo, of which he could see the antennae. One minute later the flight lost visual contact with the ground and, since the pilot believed that his radio compass was out of order, he requested clearance to proceed on Ostia VOR. At 1835 hours he was cleared to Ostia VOR at 6 000 ft, but reported that his VOR was not giving reliable information and that he would fly on a heading of 270° and break over the sea. This was the last message of the aircraft. The aircraft was subsequently found on a very steep slope on the southeast side of Mount Serra Alta at an elevation of 1,630 m. All eight occupants were killed.
Crew:
Ernesto Roggero , pilot,
Erminio Carlo Bonfanti, copilot,
Luigi Politta, steward.
Passengers:
Leonbruno Angeloni,
Marco Di Michele,
Marvin Walter Gelber,
Nicolò Marcello,
Guido Mancini.
Probable cause:
It was determined that the probable cause of the accident was:
- Significant errors by the pilot in estimating his own position with consequent presumed identification of lights in the Rome area and of the Mount Cavo antennae, which led him to:
- Misjudge the effectiveness of the aircraft radio and navigational equipment,
- Request clearance to descend to 6 000 ft and subsequently below the specified level in order to maintain at all costs visual contact with the ground, with the result that he crashed into the mountain because of inability to achieve the desired visual contact.
- Particularly adverse weather conditions over the last segment of the route flown at night,
- Failure to report to the various ATC units the departures from the flight route indicated in the PLN submitted prior to departure and in the subsequent PLN transmitted by the pilot after departure,
- Added to the above, the unfortunate concurrence of a series of facts and circumstances that all played against the pilot.
Final Report:

Crash of a Douglas R4D-8 in Millington

Date & Time: Mar 15, 1963 at 2040 LT
Operator:
Registration:
17158
Flight Type:
Survivors:
Yes
Schedule:
Saint Louis – Millington
MSN:
43368
YOM:
1944
Crew on board:
3
Crew fatalities:
Pax on board:
30
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The approach to Millington was completed by night and in poor weather conditions. On final, the pilot declared an emergency as an engine failed. As the aircraft was not properly aligned with the runway, the crew elected to make a go around. A second attempt to land was completed in thunderstorm activity when the airplane stalled, hit a pecan tree and crashed in Hill Street, just near some houses. On ground, it lost its right wing and came to rest in flames. All 33 occupants evacuated safely while the aircraft was destroyed by fire.
Probable cause:
Engine failure on final.

Crash of a Douglas C-47A-DL at RAF Bentwaters

Date & Time: Mar 4, 1963
Operator:
Registration:
43-30655
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Bentwaters - Bentwaters
MSN:
13806
YOM:
1944
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew (three engineers) were engaged in a series of ground tests. While rolling at high speed on a taxiway, control was lost. The airplane veered off taxiway to the left and eventually collided with trees. The airplane was damaged beyond repair while all three occupants were uninjured.
Probable cause:
It was determined that the crew failed to prepare the mission properly and forgot to remove the rudder lock prior to start the tests manoeuvres.

Crash of a Douglas C-47B-30-DK on Mt Boca: 27 killed

Date & Time: Mar 2, 1963 at 1005 LT
Operator:
Registration:
PI-C489
Flight Phase:
Survivors:
No
Site:
Schedule:
Zamboanga – Cotabato – Davao
MSN:
16115/32863
YOM:
1945
Flight number:
PR984
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
24
Pax fatalities:
Other fatalities:
Total fatalities:
27
Captain / Total flying hours:
10320
Captain / Total hours on type:
6500.00
Copilot / Total flying hours:
870
Circumstances:
Flight 984 was on a scheduled domestic flight from Zamboanga to Davao, with an intermediate stop at Cotabato. It departed Cotabato at 0940 hours, with a crew of three and twenty-four passengers, estimating Davao at 1025 hours. At 1002 hours the flight reported to the Company radio station at Cotabato that it was halfway to Davao, at Flight level 60, descending. Later on, it contacted the Company radio station at Davao and requested the Davao weather. After having received weather information the flight advised that its arrival would be delayed on account of bad weather. No aircraft difficulty was reported and this was the last message from the flight. When the aircraft failed to arrive, 30 minutes after its ETA a search was started. The aircraft was subsequently found on Mt. Boca, approximately 50 miles SE of Davao Airport, where it had crashed at an altitude of 3 000 ft around 1130 hours. All 27 occupants were killed.
Probable cause:
The probable cause of the accident was due to navigational error, en-route and during let-down. Contributory factors were the limited visibility and the crosswind, all existing on the final phase of the flight.
Final Report:

Crash of a Douglas C-47A-80-DL in Ankara: 52 killed

Date & Time: Feb 1, 1963 at 1513 LT
Operator:
Registration:
CBK-28
Flight Type:
Survivors:
No
Site:
Schedule:
Ankara - Ankara
MSN:
19668
YOM:
1944
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
52
Captain / Total hours on type:
1452.00
Copilot / Total hours on type:
36
Aircraft flight hours:
2340
Circumstances:
Middle East Airlines flight 265, a Vickers Viscount registered OD-ADE, was descending for Ankara-Esenboğa Airport, Turkey and had been cleared for an approach to runway 03. Last radio contact was at 13:09 hours GMT when the flight reported being over the Ankara NDB at 8000 feet, descending for 6500 feet. The crew would contact Ankara again over the NDB when inbound. Earlier in the day, at 11:22 GMT, a Douglas C-47 transport plane of the Turkish Air Force (CBK-28) had taken off from Ankara's Etimesgut Air Base for an instrument training flight in the southeast region of the Gölbasi beacon. The duration of the flight was planned for 1 hour 30 minutes . In this type of flight the student pilot is normally seated in the left-hand seat, an orange plexiglass panel is placed in front of him on the left half of the windshield, and he wears dark blue glasses. The instructor is in the right-hand seat and is able to maintain a lookout. The training manoeuvres had been completed, and the aircraft was returning to Etimesgut flying under visual flight rules by the time MEA flight 265 was descending for Esenboğa Airport. The Viscount, cruising on a heading of 283°, collided with the C-47 which was flying on a heading of 243° towards Etimesgut. The lower right-hand-side of the Viscount's nose and the starboard wing struck the C-47 from behind at a 40° angle in the door area on its port side. Propeller no. 3 also struck the C-47's left horizontal stabilizer, cutting it off. The blade ends broke off and remained with the tail unit of the C-47 near the base of the left horizontal stabilizer. The blade of propeller no. 4 cut the underside of the tip of the right horizontal stabilizer. Both aircraft flew together for a very short time then separated. The tail unit of the C-47 having been cut off, the C-47 fell vertically immediately thereafter. Prior to being cut off, the left horizontal stabilizer of the C-47 damaged the starboard side skin covering of the Viscount in the vicinity of the passenger cabin windows. This piece of skin covering broke off, and some of the passengers fell out through this hole. The Viscount flew a very short while following the separation of the two aircraft, then nosed down and fell. Both aircraft crashed into a residential area of Ankara, killing 87 people on the ground. 50 others were seriously injured.
Probable cause:
The Viscount aircraft had an IFR flight plan but was cruising under VFR conditions when it hit, with the lower side of the nose and with its starboard wing, the C-47 aircraft of the Turkish Air Force between the door on the port side of the fuselage and the tail group at an angle of forty degrees from the left rear and at an angle of approximately five to ten degrees upward. It cut off, with its starboard inner (No.3) propeller, the port side horizontal stabilizer of the C-47 aircraft. The pilots of the Viscount aircraft did not see the C-47 aircraft cruising below 7000 feet on their right-hand side forward, and the Viscount, having a higher speed, caught up with the C-47 from the left rear. At the last moment the Viscount pilots saw the C-47 and tried to avoid the collision by pulling up, but they did not succeed. The following findings were reported:
- The Viscount pilot made an estimation error of two minutes on the distance between Gölbasi and the Ankara NDB,
- His radiocommunications did not conform to the standard international conversation procedures,
- The C-47 was returning to Etimesgut Airport under visual flight rules (VFR) following an instrument training flight,
- These training flights are scheduled to be carried out below 7 000 ft with the trainee-pilot behind blind flight panels and the instructor-pilot sitting so as to be able to see outside thoroughly, The flights normally last for 1 hour- and 30 minutes, however, the instructor is authorized to extend this period if he deems it necessary,
- The C-47 was subjected to an impact from the port side rear at an angle of 40° and from the bottom to the top upwards at an angle of approximately 5 to 10°. The Viscount's flaps were set at 32° down, and the gear was down and locked. The aircraft collided over the City of Ankara at an altitude less than 7 000 feet.
Final Report:

Crash of a Douglas C-47A-15-DL Skytrain at Ellsworth Station

Date & Time: Dec 10, 1962
Operator:
Registration:
TA-33
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
9254
YOM:
1943
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Equipped with a JATO system, the aircraft caught fire during takeoff and crashed. No casualties.