Crash of a Douglas C-54E-5-DO Skymaster off Sandspit: 36 killed

Date & Time: Jan 19, 1952 at 0138 LT
Type of aircraft:
Operator:
Registration:
N45342
Survivors:
Yes
Schedule:
Seoul – Tokyo – Shemya – Elmendorf – McChord
MSN:
27279
YOM:
1944
Flight number:
NW324
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
40
Pax fatalities:
Other fatalities:
Total fatalities:
36
Captain / Total flying hours:
8557
Captain / Total hours on type:
1762.00
Copilot / Total flying hours:
4197
Copilot / Total hours on type:
1698
Aircraft flight hours:
18859
Circumstances:
Flight 324 departed Elmendorf Air Force Base at 2111, January 18, with the same 40 passengers who had enplaned at Haneda Air Force Base, Tokyo. The aircraft had 2,600 gallons of fuel and 100 gallons of oil aboard. Gross weight at takeoff was 68,275 pounds (permissible 71,800), and the load was properly distributed with relation to the center of gravity. The flight climbed to the 10,000-foot assigned altitude and at 2213, shortly after passing Middleton Island, requested permission to descend to 8,000 feet. ARTC cleared the flight to descend and the new cruising altitude was reached at 2222. The trip was uneventful until opposite Sitka, Alaska, when the pilot reported, at 0003 (January 19), that No. 1 propeller had been feathered. In another radio transmission (0029), the pilot ascribed the trouble to a "broken" oil cooler, and advised that the flight was proceeding to Sandspit. In other transmissions, he requested weather forecasts for Annette, Sandspit, and Port Hardy. Following receipt of this information, which revealed that Annette weather was below minimums, he again advised that a precautionary landing would be made at Sandspit, and gave 0128 as the estimated time of arrival. The flight was cleared to that point and proceeded without further incident on three engines. The aircraft touched down at a point about one-third down the runway. After a short roll, power was applied at about the mid-point of the strip and the aircraft took off, barely clearing a low fence and driftwood which was approximately two feet high at the end of the runway. After it failed to reappear at the approach end of the landing strip, the Sandspit radio operator discovered from the shouting of survivors that the flight had crashed in Hecate Strait. The radio operator immediately sent notification messages to place Search and Rescue facilities in operation. The wreckage could not be seen because of limited visibility, In company with a Canadian customs official, he launched his small boat and effected the rescue of the seven survivors standing on and clinging to the right wing tip of the partially submerged aircraft. Following the alerting of Search and Rescue facilities, messages were relayed by Annette Flight Control to two other aircraft in the area. They attempted to light the area with flares and locate the wreckage, but were unsuccessful in their efforts.
Probable cause:
The Board determines that the probable cause of this accident was the high approach to the airstrip and the attempt to again become airborne at insufficient air speed, which resulted in the aircraft settling into the water. The following findings were pointed out:
- The No. 1 engine suffered an oil loss, which necessitated shutting down the engine and feathering the propeller,
- In accordance with company operating procedures, the captain elected to land at Sandspit, British Columbia, the first available airport, rather than continue to destination on three engines,
- The aircraft, following an aborted landing at Sandspit and when last observed by a ground witness, was in a shallow left bank at low altitude,
- The aircraft, at near stalling speed during the attempted climb-out, settled into the water, bounced, and came to rest 26 degrees to the left and approximately 4,500 feet from the end of the runway,
- All or nearly all of the passengers evacuated the aircraft, with no known serious injuries,
- Air and water temperatures were near freezing; drowning and exposure accounted for 36 fatalities,
- No steps were taken to prepare passengers for a crash landing or possible ditching,
- Emergency lighting in the cabin was not utilized, nor were any effective measures taken to remove life rafts at the rear of the cabin,
- Search and Rescue facilities were not alerted until after the accident because three-engine operation over water was considered a potential, not an actual, emergency.
Final Report:

Crash of a Douglas C-54-D-10-DC Skymaster in Oakland: 3 killed

Date & Time: Nov 17, 1951 at 1014 LT
Type of aircraft:
Operator:
Registration:
N79992
Flight Type:
Survivors:
No
Schedule:
Oakland - Oakland
MSN:
10832
YOM:
1945
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
7871
Captain / Total hours on type:
5028.00
Copilot / Total flying hours:
3590
Copilot / Total hours on type:
1900
Aircraft flight hours:
5257
Circumstances:
Overseas National's DC-4 took off from the Oakland Airport at 0820. Captain Marion Harvey Click, company cheek pilot, was in command and aboard were Captains Hammond Garrard and Warren Cecil Gessner who were to receive their six months DC-4 instrument competency cheeks. There were no other persons aboard. The aircraft had been refueled with 1,229 gallons of gasoline and 11 gallons of oil; the total load was within the certificated gross weight and was properly distributed. At 0925, this flight received a clearance from the Oakland tower to make a practice range approach and to remain above 1,500 feet on the final approach to the airport. At 0935, the California Eastern DC-4 3 took off from the Oakland Airport for the purpose of a six-month instrument competency check. Captain Ralph A. Shope, company chief pilot, was in command and occupied the right scat. Captain Winfield B. Kinner, receiving the cheek, was in the left seat. Louis Goldberg, an upholsterer and company mechanic, occupied a cabin seat and was on board only to sew some arm rests. The aircraft had been refueled with 1600 gallons of gasoline, and the total load was within the certificated gross weight and was properly distributed. According to accepted practice, both flights conducted their training cheeks in the "Bay area," with all maneuvers above 3,000 feet. Both aircraft were equipped with hoods, installed on the left side of each cockpit to prevent the pilots being checked from seeing outside. The cheek pilots in the right seats, also perform the duties of safety pilots, maintaining watch for other aircraft. There was also a third pilot on board Overseas who acted as an observer. Shortly before 1013, the approximate time of the accident, both aircraft approached the Oakland low frequency radio range station, which is 0.2 mile northeast from the approach end of Runway 15 of the Oakland Airport. Overseas was on a magnetic heading of approximately 124 degrees inbound on the NW leg of the range; and California was homing on the range on a heading of 75 degrees M 4 Both aircraft were at an altitude of 3,000 feet. Weather conditions were good in the San Francisco Bay area at the time. The U. S. Weather Bureau reported at 1016 (three minutes after the accident); ceiling 25,000 feet, thin broken clouds, visibility seven miles, wind south four mph at Oakland. The sun's bearing at 1015 was 153 degrees .JPG">, and its altitude above the horizon was 28 degrees and 27 minutes. During a short period prior to 1013, both aircraft were observed to converge without any apparent change in direction or altitude. Neither attempted to avoid collision but remained in straight and level flight, and collided approximately over the range station at an altitude of about 3,000 feet. California was at a slightly lower altitude than Overseas, and contact was made between the leading edge of the vertical stabilizer of California and the right side of the fuselage of Overseas just forward of the horizontal stabilizer. Shortly after the collision, Overseas crashed out of control on Doolittle Drive, the highway paralleling the north side of Oakland Airport. Its three pilots were killed at the time of impact with the ground. A number of persons driving on the highway close to the impact site received burns of varying degrees, and several automobiles were destroyed by fire. The top portions of the vertical stabilizer and rudder of California were torn off in the collision. The aircraft was still controllable at an air speed of 160 miles an hour. Immediately following the collision, Captain Shope had Captain Kinner remove the hood. As California was then south of the Oakland Airport at 2,500 feet, Captain Shops requested permission to land on Runway 9R, the longest runway, and to have emergency equipment stand by. However, since all fire equipment was then at the crash scene of Overseas, the flight was directed to the San Francisco Airport, 12 miles away, where an emergency landing was made at 1021.
Probable cause:
The Board determines that the probable cause of this accident was the failure of the Overseas safety pilot and/or his observer to observe and so avoid the other aircraft and the failure of California's safety pilot to carry a qualified observer aboard the aircraft to insure an adequate field of vision. The following findings were pointed out:
- Both flights were for the purpose or giving six-month instrument competency cheeks, with hoods installed on the left side of both cockpits,
- Overseas carried an observer, as required; California did not,
- Both aircraft were making simulated (hooded) instrument approaches to the Oakland range station at the same altitude,
- The aircraft converged at an angle of approximately 49 degrees,
- Overseas was a few feet higher than California,
- No evasive action was taken by either aircraft before collision,
- The collision occurred at an altitude of 3,000 feet approximately over the Oakland range station.
Final Report:

Crash of a Douglas C-54A-10-DC into the Pacific Ocean: 37 killed

Date & Time: Jul 21, 1951 at 2255 LT
Type of aircraft:
Operator:
Registration:
CF-CPC
Flight Phase:
Survivors:
No
Schedule:
Vancouver – Anchorage – Tokyo
MSN:
10327
YOM:
1944
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
31
Pax fatalities:
Other fatalities:
Total fatalities:
37
Circumstances:
The four engine aircraft left Vancouver at 1853LT bound for Tokyo-Haneda with an intermediate stop in Elmendorf AFB in Anchorage. While cruising along the Alaskan shore, vertical to the Cape Spencer, near Elfin Cove, the crew informed ground about his position and gave an estimate about 0000LT vertical to Yakutat. This was the last message as the airplane disappeared few minutes later. As the aircraft failed to arrive in Anchorage, SAR operations were conducted but no trace of the aircraft nor the 37 occupants was found. All operations were eventually suspended on October 31, 1951.
Probable cause:
As no trace of the aircraft was found, the board was unable to determine conclusively the cause of the accident. At the time of the accident, weather conditions were poor with rain falls, icing conditions and a visibility of 500 feet.
Final Report:

Crash of a Douglas C-54A-DO Skymaster in Antananarivo

Date & Time: Jul 18, 1951
Type of aircraft:
Operator:
Registration:
F-BDRI
Flight Phase:
Survivors:
Yes
Schedule:
Antananarivo - Paris
MSN:
3079
YOM:
1943
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances shortly after takeoff from Antananarivo-Arivonimamo Airport. There were no casualties but the aircraft was written off.

Crash of a Douglas C-54B-10-DO Skymaster in Bangkok

Date & Time: Jul 13, 1951
Type of aircraft:
Operator:
Registration:
HS-POA
Flight Phase:
Survivors:
Yes
Schedule:
Bangkok – Hong Kong
MSN:
18368
YOM:
1944
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll, the pilot in command pulled on control column but the aircraft failed to rotate. He decided to abandon the takeoff procedure and started an emergency landing. Unable to stop within the remaining distance, the four engine aircraft christened 'Bangkok' overran and came to rest in flames. All occupants were evacuated safely while the airplane was destroyed by fire.
Probable cause:
It was determined that the total weight of the aircraft was well above the MTOW admissible in the actual circumstances.

Crash of a Douglas R5D-3 in Busan: 5 killed

Date & Time: May 30, 1951
Type of aircraft:
Operator:
Registration:
56513
Flight Type:
Survivors:
No
Site:
MSN:
10739
YOM:
1945
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
On final approach to Busan AFB, the four engine aircraft hit the slope of a mountain and was destroyed upon impact. All five crew members were killed.

Crash of a Douglas C-54D-10-DC Skymaster in Fort Wainwright AFB: 8 killed

Date & Time: Apr 10, 1951
Type of aircraft:
Operator:
Registration:
42-72734
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Fort Wainwright - Fort Wainwright
MSN:
10839
YOM:
1945
Crew on board:
8
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
8
Circumstances:
The four engine aircraft and its crew were involved in a local training mission consisting of towing a glider. Just after liftoff, while in initial climb, the glider towing rope wound itself around the elevator, causing the aircraft to crash. All eight crew members were killed.

Crash of a Douglas C-54B-1-DC Skymaster in Keflavik

Date & Time: Mar 30, 1951
Type of aircraft:
Operator:
Registration:
N74644
Flight Type:
Survivors:
Yes
MSN:
10540
YOM:
1945
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After touchdown at Keflavik Airport, the four engine aircraft veered to the right of the runway, hit frozen snow banks and came to rest in flames. All six crew members were evacuated safely while the aircraft was destroyed.

Crash of a Douglas C-54D-1-DC Skymaster off Lajes: 14 killed

Date & Time: Jan 31, 1951 at 2303 LT
Type of aircraft:
Operator:
Registration:
6603
Flight Type:
Survivors:
No
Schedule:
Lisbon – Lajes
MSN:
10597
YOM:
1945
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
11
Pax fatalities:
Other fatalities:
Total fatalities:
14
Circumstances:
On a night approach to Lajes AFB, the four engine aircraft crashed into the sea few km offshore. All 14 occupants were killed.

Crash of a Douglas C-54D-1-DC Skymaster in Daegu: 4 killed

Date & Time: Jan 16, 1951
Type of aircraft:
Operator:
Registration:
42-72495
Flight Phase:
Flight Type:
Survivors:
No
MSN:
10600
YOM:
1945
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
Shortly after takeoff from runway 31 at Daegu Airport, while in initial climb, the four engine aircraft hit the slope of a mountain facing the airport and located 4,5 km northwest of the airfield. The aircraft was destroyed upon impact and all four crew members were killed. For unknown reason, the airplane was unable to gain sufficient height after rotation.