Crash of a Douglas C-54A-10-DC Skymaster near Missoula: 12 killed

Date & Time: Oct 28, 1960 at 1139 LT
Type of aircraft:
Operator:
Registration:
N48762
Survivors:
No
Site:
Schedule:
Portland – Yakima – Spokane – Missoula
MSN:
10320
YOM:
1944
Flight number:
NW104
Crew on board:
4
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
12
Captain / Total flying hours:
11620
Captain / Total hours on type:
8070.00
Copilot / Total flying hours:
3221
Copilot / Total hours on type:
446
Aircraft flight hours:
36842
Circumstances:
On October 28, 1960, at 1139 m. s. t., a Douglas C-54A-DC, N 48762, operated by Northwest Airlines, Inc., as Flight 104, crashed and burned approximately 13 nautical miles northwest of the Missoula, Montana Airport. The captain, first officer, two hostesses and all eight passengers died in the crash. The flight took off from Spokane, Washington, on an instrument flight plan. En route radio reports were routine and indicated the flight was on schedule, and in no difficulty. The aircraft was observed from the ground flying on course toward Missoula in and along the Clark Fork Valley within six nautical miles west of the scene of the crash. The engines were running and the aircraft was descending as if on an approach to a landing. As the aircraft descended deeper into the valley, flight visibility became restricted by light snow showers, and the tops of the mountains surrounding the valley were obscured by the overcast. The aircraft entered a steep left banking turn and the nose was raised in an apparent attempt to turn and climb out through an intersecting valley; however, the aircraft continued to sink toward the ground, rolled to the left and crashed inverted. The Board believes the accident was caused by the failure of the pilot to continue in accordance with his IFR flight plan by attempting a VFR approach during instrument weather conditions.
Probable cause:
The probable cause of this accident was the failure of the pilot to continue in accordance with his IFR flight plan by attempting a VFR approach during instrument weather conditions.
Final Report:

Crash of a Douglas R5D-3 into the Pacific Ocean: 29 killed

Date & Time: Sep 22, 1960 at 1410 LT
Type of aircraft:
Operator:
Registration:
56541
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Atsugi - Subic Bay
MSN:
22191
YOM:
1945
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
23
Pax fatalities:
Other fatalities:
Total fatalities:
29
Circumstances:
En route from Atsugi to Subic Bay (Cubi Point NAS, Philippines), the crew informed ATC that engine number three caught fire and elected to divert to Naha Airport, Okinawa. Few minutes after 1400LT, the captain informed ATC about his position and maintained the altitude of 6,500 feet with 339° heading and requested maritime assistance in case of ditching. This was the last message. Shortly later, the four engine aircraft crashed into the Pacific Ocean some 290 km southeast from Okinawa Island. No trace of the 29 occupants was found but only 350 kilos of debris floating on water.
Probable cause:
Fire of the engine number three in flight for unknown reason.

Crash of a Douglas R5D-3 in Kénitra

Date & Time: Aug 23, 1960
Type of aircraft:
Operator:
Registration:
56518
Flight Type:
Survivors:
Yes
MSN:
10744
YOM:
1945
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances at Kenitra Airport. The airplane was destroyed by a post crash fire and the occupant's fate remains unclear.

Crash of a Douglas C-54A-DO Skymaster in Bunia: 35 killed

Date & Time: Apr 22, 1960 at 0755 LT
Type of aircraft:
Operator:
Registration:
OO-SBL
Survivors:
No
Schedule:
Brussels – Rome – Cairo – Bunia – Stanleyville – Elisabethville
MSN:
3099
YOM:
1943
Location:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
28
Pax fatalities:
Other fatalities:
Total fatalities:
35
Circumstances:
Following an uneventful flight from Cairo, the crew started the descent to Bunia in marginal weather conditions. In limited visibility due to low clouds, the pilot-in-command continued the approach at an insufficient altitude when the four engine aircraft struck the slope of the Bogoro Peak located about 8 km short of runway. The wreckage was found 60 meters below the summit and all 35 occupants have been killed.
Probable cause:
The accident occurred because the pilot, the captain, carried out a descent while the height of cloud base (ceiling) was below the minimum required by the Administration and the Operator.

Crash of a Douglas C-54A-15-DC Skymaster in Saint-Cléophas-de-Brandon: 5 killed

Date & Time: Nov 4, 1959 at 2307 LT
Type of aircraft:
Operator:
Registration:
CF-ILI
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Montreal – Hall Beach
MSN:
10360
YOM:
1944
Flight number:
WH1658
Country:
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Aircraft flight hours:
30357
Circumstances:
Flight 1658 took off from Montreal-Dorval runway 10 at 2244LT on a cargo flight to Hall Beach, NWT. Following takeoff the aircraft continued runway heading and climbed to 6,000 feet. Course was then changed and the aircraft climbed to the assigned altitude of 9,000 feet, reaching this altitude at 2259LT. Some 3 and a half minutes later the crew reported that they were in an emergency descent because of a no. 2 engine fire. Last radio contact was at 2307LT when the crew reported that the plane had lost its left wing and "was in a spin and going straight in". The DC-4 broke up in midair, causing wreckage to cover a 1,25 x 0,75 mile area. All five crew members were killed.
Probable cause:
A fire of undetermined origin started in no.2 engine nacelle during the climb and developed to the stage where fire extinguishing equipment was inadequate to extinguish it. The following are considered to be primary contributing factors:
- The deteriorated condition of the exhaust collector ring,
- The probable deteriorated condition of the flexible wire braid hose assemblies,
- The probable use of high power during the climb,
- The possible failure of the fire detection and warning system to inform the pilot of the existence of a fire before it had penetrated the firewall and ignited the fuel feed system and oil tank to the rear of no.2 engine. During the rapid letdown, stresses were imposed on the weekened left wing by manoeuvre and/or gusts which were sufficient to sever the left wing spar. No subsequent action by the pilot could have brought the aircraft safely to the ground; neither was it possible to determine what effect a less rapid letdown would have had.

Crash of a Douglas C-54 Skymaster in Jacksonville

Date & Time: Oct 15, 1959 at 2105 LT
Type of aircraft:
Operator:
Registration:
N4000A
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Jacksonville-Charleston-Cherry Point
MSN:
36063
YOM:
1955
Crew on board:
2
Crew fatalities:
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
12166
Captain / Total hours on type:
7303.00
Copilot / Total flying hours:
9024
Copilot / Total hours on type:
255
Aircraft flight hours:
19269

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

Date & Time: Sep 25, 1959 at 1405 LT
Type of aircraft:
Operator:
Registration:
HZ-AAF
Flight Phase:
Survivors:
Yes
Schedule:
Jeddah – Riyadh
MSN:
7474
YOM:
1944
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
67
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The Saudia DC-4 plane took off from Jeddah for a flight to Riyadh. Immediately following lift-off, the aircraft climbed at an abnormal high rate. The flight crew were not able to push the control column forward, so full forward trim and a power reduction were used to avert a stall. The aircraft stalled however and descended at almost a 90° angle. Power was reapplied and the controls were pulled back, effecting a recovery at a very low altitude. The DC-4 then began to climb again, approaching another stall. This time the stall was averted by reducing power and a left turn. A return to the runway was impossible so a forced belly landing was carried out near the airport. The airplane was damaged beyond repair while all 72 occupants were evacuated safely.
Probable cause:
The flight mechanic failed to place the gust lock in the fully secured position to unlock the controls prior to takeoff, and the spring holding the fairing on the tail skid was incorrectly attached to the elevator control lock mechanism. The spring tension caused the elevator gust lock to lock the elevator from down travel when the gust lock was not in the fully secured control unlock position. A contributing factor was that neither the captain nor the flight mechanic checked visually or manually to see that the gust lock was in the secured position to unlock the control prior to takeoff.

Crash of a Douglas C-54B-1-DC Skymaster on Great Sitkin Island: 16 killed

Date & Time: Sep 24, 1959 at 1720 LT
Type of aircraft:
Operator:
Registration:
N63396
Survivors:
No
Site:
Schedule:
Anchorage – Cold Bay – Adak – Shemya
MSN:
10486
YOM:
1944
Flight number:
RV003
Crew on board:
5
Crew fatalities:
Pax on board:
11
Pax fatalities:
Other fatalities:
Total fatalities:
16
Captain / Total flying hours:
12853
Captain / Total hours on type:
1278.00
Copilot / Total flying hours:
3949
Copilot / Total hours on type:
883
Aircraft flight hours:
33390
Circumstances:
Flight 3 was a scheduled flight between Anchorage and Shemya, with intermediate stops at Cold Bay and Adak, Alaska. A routine takeoff was made at Cold Bay, and all en route radio reporting points were made to the company within two or three minutes of their estimated times. At 1650LT, the flight reported that it was 100 miles northeast of Adak, at 4,500 feet, on top and in the clear. Flight 3 then estimated it would be over the Adak low frequency range at 1725LT. The flight was cleared to the Adak low frequency range, to maintain VFR on top, and to call Adak approach control when 30 miles out for landing instructions. At 1715LT, the flight advised the company it was canceling its IFR flight plan and was proceeding VFR. Two minutes later Flight 3 attempted to communicate with Adak approach control. Upon hearing this message, approach control called the flight but was unsuccessful. It was later determined that the aircraft had crashed into the northeast side of the Great Sitkin volcano (1,740 meters high) located on the Great Sitkin Island, about 25 miles northeast of Adak Airport. The aircraft was destroyed and all 16 occupants have been killed.
Probable cause:
The Board determines that the probable cause of this accident was the captain's failure to maintain flight in accordance with visual flight rules during a descent over hazardous terrain.
Final Report:

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

Date & Time: Sep 8, 1958
Type of aircraft:
Operator:
Registration:
VT-DIA
Survivors:
Yes
MSN:
3094
YOM:
1943
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
27
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
En route to Madras, the primary hydraulic system failed. The crew failed to identify the failure properly and after touchdown at Madras Airport, the brake systems were partially inoperative. Unable to stop within the remaining distance, the airplane overran, struck obstacles, lost its undercarriage and came to a halt. All 31 occupants were evacuated safely while the aircraft was considered as damaged beyond repair.
Probable cause:
Failure of the primary hydraulic system in flight due a wrong installed gasket.

Crash of a Douglas C-54A-1-DO Skymaster in In Salah

Date & Time: Apr 30, 1958
Type of aircraft:
Operator:
Registration:
F-BELK
Survivors:
Yes
Schedule:
Algiers – In-Salah – Tamanrasset
MSN:
7451
YOM:
1943
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew encountered a sand storm while approaching In Salah Airport. On final, in limited visibility, the aircraft was too low and struck a sand dune short of runway. On impact, the undercarriage were sheared off and the airplane belly landed in sand before coming to rest. Both engines number two and three detached. There were no casualties.