Crash of a Douglas C-47-DL off Andros Town

Date & Time: Apr 6, 1965 at 1934 LT
Operator:
Registration:
N150A
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
6178
YOM:
1942
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
En route from Haiti to Florida and while cruising along the Andros Island, the crew encountered engine problems and was forced to ditch the aircraft off Andros Town. The airplane came to rest in shallow waters and all seven occupants were evacuated safely.
Probable cause:
Forced landing off airport on water following engine failure/flameout on both engines.
Final Report:

Crash of a Douglas C-47A-1-DK in Saint Pierre

Date & Time: Apr 3, 1965
Operator:
Registration:
CF-FAJ
Survivors:
Yes
MSN:
12099
YOM:
1943
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances while landing at Saint-Pierre Airport. There were no casualties.

Crash of a Douglas C-47-DL in Warrnambool

Date & Time: Apr 2, 1965 at 0817 LT
Operator:
Registration:
VH-ANJ
Flight Phase:
Survivors:
Yes
Schedule:
Warrnambool – Melbourne
MSN:
9105
YOM:
1943
Flight number:
WX001
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
20
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6181
Captain / Total hours on type:
1738.00
Copilot / Total flying hours:
1770
Copilot / Total hours on type:
1561
Circumstances:
Flight No. 1 was a scheduled domestic flight from Hamilton to Melbourne via Warrnambool, Victoria, and the aircraft landed at Warrnambool at 2159 hours GMT after an uneventful flight. After a stay on the ground of 17 minutes, during which time there were load changes, the aircraft taxied for take-off on runway 31. The pre-take-off checks did not indicate any abnormality and the aircraft proceeded to take off. After becoming airborne, but prior to undercarriage retraction, a loss of engine power occurred and the pilot- in-command deduced that the port engine had failed. He feathered the port engine and then became aware that the starboard engine was delivering only partial power, which was insufficient to sustain the aircraft in flight. A suitable area was selected immediately and a landing with wheels and flaps retracted was made in grassy paddocks on level terrain, but the aircraft passed through three fences before coming to rest. All occupants survived while the aircraft was written off.
Probable cause:
The cause of the accident was that the pilot-in-command, on becoming aware of a loss of engine power, took action to feather the propeller after adopting procedures which failed to ensure correct identification of the defective engine.
Final Report:

Crash of a Douglas C-47B-1-DK in Hadibu

Date & Time: Mar 26, 1965 at 0815 LT
Operator:
Registration:
VR-AAA
Survivors:
Yes
Schedule:
Sanaa – Hadibu
MSN:
14141/25586
YOM:
1944
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
14
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After landing at Hadibu Airport (Socotra Island), the airplane encountered difficulties to decelerate properly. As the end of the runway was approaching, the captain decided to veer off runway and completed a quit sharp turn to the left when the right main gear collapsed. Out of control, the airplane skidded and came to rest. All 17 occupants were evacuated safely while the airplane was damaged beyond repair.
Probable cause:
It was determined that the pilot-in-command was no sufficiently familiarized with the airport characteristics and failed to take into consideration the wind component, landing with a tailwind, which was considered as a contributing factor. It was also reported that the ground equipment was not adapted and that the information transmitted to the crew regarding the wind component was improper, which was also considered as a contributing factor.

Crash of a Douglas C-47A-1-DK near Lowari Pass: 22 killed

Date & Time: Mar 26, 1965
Operator:
Registration:
AP-AAH
Flight Phase:
Survivors:
Yes
Site:
Schedule:
Peshawar – Chitral
MSN:
12089
YOM:
1943
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
22
Pax fatalities:
Other fatalities:
Total fatalities:
22
Circumstances:
While cruising in marginal weather conditions at an altitude of 9,000 feet, the airplane struck a mountain located near the Lowari Pass. Four passengers were seriously injured while 22 other occupants were killed.

Crash of a Douglas C-47 at Clark AFB: 5 killed

Date & Time: Mar 25, 1965
Operator:
Flight Type:
Survivors:
No
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
On final approach to Clark AFB, the twin engine airplane collided with a USAF Rockwell T-39A Sabreliner registered 62-4458. The jet was carrying a crew of two who was completing a local training flight. Both airplane crash 1,5 km east of the airfield and all seven occupants on both aircraft were killed.

Crash of a Douglas C-47-Dl near San Vincente de Caguán: 29 killed

Date & Time: Mar 22, 1965 at 1455 LT
Operator:
Registration:
HK-109
Flight Phase:
Survivors:
No
Site:
Schedule:
Bogotá – Bucaramanga
MSN:
4753
YOM:
1942
Flight number:
AV676
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
26
Pax fatalities:
Other fatalities:
Total fatalities:
29
Captain / Total flying hours:
6201
Captain / Total hours on type:
268.00
Copilot / Total flying hours:
4941
Copilot / Total hours on type:
4941
Aircraft flight hours:
32455
Circumstances:
Flight 676 was a scheduled domestic flight from Eldorado Airport, Bogotá to Bucaramanga. It departed Bogotá at 1358 hours, local time. At 1450 hours it reported over Cimitarra at 9 000 ft in VMC, estimating Bucaramanga at 1510 hours. This was the last communication from the flight. When information of arrival was not received at the airport of destination, a state of alert was declared at 1522 hours and an emergency was subsequently declared at 1540 hours. The wreckage of the aircraft was located on 24 March at an altitude of approximately 7 200 ft on the peak known as Pan de Azucar, 35 NM from Bucaramanga on a magnetic bearing of 45'. The accident occurred at approximately 1455 hours. All 29 occupants have been killed.
Probable cause:
The pilot-in-command continued to fly VFR in unfavourable meteorological conditions which necessitated operation by instrument flight rules.
Final Report:

Crash of a Douglas C-47A-1-DK into the Trinity Bay: 2 killed

Date & Time: Mar 18, 1965 at 1810 LT
Operator:
Registration:
N4997E
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Miami – Gander – Santa Maria – Manila
MSN:
12191
YOM:
1943
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
30000
Captain / Total hours on type:
6000.00
Circumstances:
The aircraft has to be delivered to Air Manila in the Philippines and the crew departed Miami for Manila with intermediate stops in Gander and Santa Maria, Azores Islands. While cruising over Newfoundland, the crew was able to send a brief mayday message when the airplane went out of control and crashed into the Trinity Bay. The aircraft was lost and both pilots were killed.
Probable cause:
Loss of control following an emergency of an undetermined nature.
Final Report:

Crash of a Douglas C-47A-1-DK in Lourdes-de-Blanc-Sablon

Date & Time: Mar 16, 1965 at 1730 LT
Operator:
Registration:
CF-PQG
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
12055
YOM:
1943
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
11000
Captain / Total hours on type:
6500.00
Copilot / Total flying hours:
2400
Copilot / Total hours on type:
1000
Circumstances:
During the takeoff roll, the visibility decreased because of the glare of the landing lights on the falling snow. The aircraft deviated 10° or 15° to the left without the crew being aware that this deviation had occurred and, after rolling for about 750 ft, it left the north side of the runway. The attempt to take off was continued. However, adequate speed could not be obtained. After a series of impacts, the aircraft came to rest about 3,150 feet from the start of takeoff and about 700 feet short of the base of a sharply rising hill. All 9 occupants were uninjured while the aircraft was damaged beyond repair. It was operated on behalf of the Département des Transports et des Communications du Québec.
Probable cause:
Loss of directional control during takeoff at night from an unlighted aerodrome.
Final Report: