Crash of a Douglas B-26B Invader in Sorn: 2 killed

Date & Time: Aug 13, 1956 at 2225 LT
Type of aircraft:
Operator:
Registration:
8811-B
Flight Type:
Survivors:
No
Schedule:
Keflavik - Prestwick
MSN:
29029
YOM:
1944
Location:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew was completing a flight from the US to France to deliver the aircraft to the French Air Force (Armée de l'Air) via Keflavik and Prestwick. During a night approach, the crew encountered low visibility due to poor weather conditions. While flying at an altitude of 800 feet, the aircraft hit the ground, became briefly airborne and crashed in a huge explosion some 20 km east of Prestwick Airport, near the village of Sorn. The wreckage was found five hours later and both crew members have been killed.
Crew:
Edgar Joseph Flanagan, pilot,
Wayne Archer Taylor, navigator.

Crash of a Convair CV-440-11 Metropolitan in Shannon: 4 killed

Date & Time: Jul 15, 1956 at 0135 LT
Operator:
Registration:
HB-IMD
Flight Type:
Survivors:
No
Schedule:
San Diego – New York – Gander – Shannon – Zurich
MSN:
335
YOM:
1956
Location:
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
The aircraft departed from San Diego, California, at 0407LT on 12 July for Zurich Airport, Switzerland, with two American pilots at the control, on a delivery flight to Swissair. Intermediate stops included New York, Gander and Shannon. Having left New York at 1240 GMT on 14 July 1956, the aircraft landed at Gander at 1659 GMT. After a stop of 57 minutes, it left Gander for Shannon at 1748 GMT carrying the same crew of 4 members. Following an uneventful ocean crossing the aircraft at 0008 hours on 15 July was given initial descent clearance to Shannon and was then cleared into the Shannon Holding Pattern, where four other aircraft were holding. At 0125 hours the aircraft commenced a Ground Controlled Approach to runway 23 and on establishing visual reference to the ground broke off the approach for a left-hand visual circuit to runway 05. During the turn onto final approach to runway 05, the aircraft, while banking steeply was observed to drop. The aircraft was destroyed on impact with the ground at approximately 0135LT and the 4 occupants were killed. There was no fire.
Probable cause:
The probable cause of the accident was an error of judgment by the pilot, resulting in the execution of an abnormally steep turn onto final approach during which the aircraft slipped into the ground.
Possible contributory factors were:
- That for the successful execution of an approach involving a steep turn near the ground on a very dark night, there had been insufficient visual guidance from the terrain,
- Impairment of the pilots' proficiency due to the length of the period on duty.
Final Report:

Crash of a Grumman SA-16A Albatross off Argentia NAS: 6 killed

Date & Time: Mar 12, 1956
Operator:
Registration:
49-069
Flight Phase:
Flight Type:
Survivors:
No
MSN:
G-27
YOM:
1950
Country:
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
The crew was en route to Spain to deliver the aircraft to the Spanish Air Force (Ejército del Aire). Shortly after takeoff from Argentia NAS, while climbing, the seaplane went out of control and crashed into the Placentia Bay, about 1,5 km off shore. All six crew members were killed.

Crash of a De Havilland U-1A Otter in Toronto: 4 killed

Date & Time: Feb 14, 1956 at 1538 LT
Type of aircraft:
Operator:
Registration:
55-3252
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Toronto - Toronto
MSN:
92
YOM:
1956
Country:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
The aircraft just came out from the De Havilland manufacture and has to be delivered to the US Army. With four crew members on board, the aircraft took off from Toronto-Downsview Airport at 1521LT for a local check flight. While cruising in the vicinity of the airfield, the airplane went out of control, entered a dive, disintegrated and eventually crashed near Keele Street. All four crew members were killed.
Probable cause:
It is believed that the loss of control was caused by wake turbulences coming from another aircraft that could not be identified.

Crash of a Consolidated PBY-5A Catalina off Kyleake: 1 killed

Date & Time: Dec 22, 1955
Type of aircraft:
Operator:
Registration:
CF-EPX
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Montreal – Godthab – Keflavik – Prestwick – Karachi
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The crew was completing a flight from Montreal to Karachi, the aircraft being delivered to the Pakistan government. While approaching the Scottish coast, both engines failed. The captain attempted to ditch the aircraft off Kyleake. On touchdown, the seaplane lost its floats, drifted away and eventually sank. Five crew members were rescued while the navigator was killed.
Probable cause:
Double engine failure caused by a fuel exhaustion due to strong headwinds.

Crash of a Noorduyn Norseman near San Antonio de los Cobres: 1 killed

Date & Time: Oct 23, 1955 at 1400 LT
Type of aircraft:
Operator:
Registration:
ZP-CAX
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Mexico City – Antofagasta – Salta – Asunción
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The aircraft was on a delivery flight from Mexico City to Asunción, Paraguay, with intermediate stops at Antofagasta, Chile and Salta, Argentina. At 1245LT the aircraft took off from Antofagasta for Salta. It was to be a VFR flight via Chosque, Chile and San Antonio de los Cobres, Salta Province. The aircraft was seen at 1400 hours flying in a straight line at very low altitude in the direction of San Antonio de los Cobres 40 km east of Olapacato. One witness, believing that the aircraft intended to land, followed it in a jeep only to find its burned wreckage some 20 km away. It had crashed into the side of a hill rising north of Rio Tocomar, approximately 70 metres above the river bed. The height above sea level at this point is approximately 4,500 metres. One eye witness stated that the aircraft crashed in rectilinear horizontal flight into the northern slope of the hill and that the pilot had not taken any avoiding action. The pilot, the sole occupant, was killed, and the aircraft was destroyed by the crash and the fire which followed.
Probable cause:
The accident was attributed to a loss of control over the aircraft due to a possible state of anoxia on the part of the pilot. A contributing factor was inadequate flight preparation, as no account was taken of the need for oxygen- breathing equipment for high altitude flying.
Final Report:

Crash of a Martin PBM-5 Mariner in Trinidad

Date & Time: Jan 20, 1955
Type of aircraft:
Operator:
Registration:
2-P-22
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
11319
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was supposed to deliver the airplane to Argentina. Enroute, an engine caught fire, forcing the pilot to attempt an emergency landing. The aircraft crashed on Tobago Island and was seriously damaged. There were no injuries. It was later transferred to the US for repair but was destroyed by fire and irreparable.
Probable cause:
An engine caught fire in flight.

Crash of a De Havilland DH.89A Dragon Rapide near Jodhpur: 2 killed

Date & Time: Jun 15, 1954
Operator:
Registration:
G-AKLA
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Jodhpur – Hanoi
MSN:
6764
YOM:
1947
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
Few minutes after takeoff from Jodhpur Airport, the twin engine aircraft crashed in unknown circumstances about 60 km east of the city. Both pilots were killed. They were in charge to deliver the airplane in Hanoi.

Crash of a Douglas C-47A-10-DK in Beirut

Date & Time: Jan 24, 1954 at 0856 LT
Operator:
Registration:
F-BEFS
Flight Type:
Survivors:
Yes
Schedule:
Paris – Brindisi – Nicosia – Basra – Hanoi
MSN:
12416
YOM:
1944
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft, belonging to the Compagnie Autrex-Lopez-Loreta-Lebreton, was on a delivery flight from Paris to Hanoi. It departed from Paris on 22 January 1954 at 0650Z and arrived at Brindisi the same day at 1305Z. The following day the aircraft left Brindisi at 0720Z and landed at Nicosia at 1330Z. From Nicosia the aircraft intended to fly to Basra, but a failure in the HF radio equipment caused a change in the schedule, and it was decided to fly to Beirut where specialists and the spare parts necessary for the repair were available. On final approach by night, the aircraft was too low when, at a speed of 105 knots, it struck a mound of earth located 85 feet short of runway 36, damaging the right mains gear. The aircraft subsequently landed on the runway when the undercarriage collapsed. There were no injuries but the airplane was damaged beyond repair.
Probable cause:
The accident was attributed to a pilot error due to lack of knowledge of the terrain. The existence of the mound was only an aggravating circumstance. The failure of the right landing gear may be explained by the excessive landing weight of the aircraft. The main cause of the accident was probably an unduly short landing which, in view of the length of the runway and the perfect condition of the aircraft, was unwarranted and must, therefore, be ascribed mainly to error on the part of the pilot, due largely to his lack of familiarity with the terrain. The pilot had never landed at the Beirut International Airport. The faulty altimeter setting was possibly an additional reason for the defective approach. Also, restricted visibility prevented the pilot from seeing the mound and taking appropriate action to avoid a crash. The presence of the mound at 26.60 meters from the runway entrance was a contributing factor. Since this mound was 78 cm high, the variation in level was 3%.
Final Report:

Crash of a De Havilland DH.104 Dove in Goose Bay: 2 killed

Date & Time: Feb 29, 1952
Type of aircraft:
Operator:
Registration:
N4964N
Flight Type:
Survivors:
No
Schedule:
Narsarsuaq – Goose Bay
MSN:
04332
YOM:
1952
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew was performing a delivery flight from Bluie West One Airfield (Narsarsuaq) to Goose Bay. On final approach, the pilot-in-command encountered difficulties due to poor weather conditions. The twin engine airplane hit the ground short of runway threshold and crashed. Both occupants were killed.