Crash of a Douglas DC-3-455 in Gao: 3 killed

Date & Time: Jul 24, 1951 at 0545 LT
Type of aircraft:
Operator:
Registration:
OO-CBA
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Brussels – Gao – Léopoldville
MSN:
6327
YOM:
1942
Location:
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
Shortly after takeoff from runway 25, while climbing to a height of 10 meters, the airplane turn sharply to the left and climbed to a height of 30 meters when it turn again to the left. It then lost altitude and hit the ground with its left wing tip, crashing into flames. All three crew members were killed.
Probable cause:
It was determined that the right engine failed shortly after rotation due to hydraulic failure. Meanwhile, hydraulic fluid spurted on the cockpit windshield, temporarily reducing the visibility of the pilots who lost control of the aircraft.

Crash of a Douglas DC-3D in Gramacho: 2 killed

Date & Time: Jun 6, 1951 at 1740 LT
Type of aircraft:
Registration:
PP-NAL
Survivors:
Yes
Schedule:
Vitória – Rio de Janeiro
MSN:
42979
YOM:
1946
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
16
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew started the approach to Santos Dumont Airport in poor weather conditions. While flying at an insufficient height of 180 feet in low visibility, the aircraft hit a hill and crashed in Gramacho, about 20 km north of Santos Dumont Airfield. A pilot and a passenger were killed while 17 other occupants were injured.
Probable cause:
The crew decided to complete the approach under visual flight rules while poor weather conditions necessitated an approach under instruments flight rules. Due to low visibility, the aircraft was approaching at the insufficient height of 180 feet while the minimum descent altitude was fixed at 1,200 feet.

Crash of a Douglas DC-3A-197 in Fort Wayne: 11 killed

Date & Time: Apr 28, 1951 at 1932 LT
Type of aircraft:
Operator:
Registration:
N16088
Survivors:
No
Schedule:
Cleveland – Fort Wayne – South Bend – Chicago
MSN:
1927
YOM:
1937
Flight number:
UA129
Crew on board:
3
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
11
Captain / Total flying hours:
6827
Captain / Total hours on type:
5694.00
Copilot / Total flying hours:
1121
Copilot / Total hours on type:
121
Aircraft flight hours:
43550
Circumstances:
Flight 129 departed Cleveland, Chic, at 1807, April 28, 1951, for Chicago, Illinois, with stops scheduled at Fort Wayne and South Bend, Indiana The crew consisted of Captain E K Swallow, First Officer H R Miller, and Stewardess Beverly Fllis, there were eight passengers on board at the time of departure The aircraft weighed 24,180 pounds, which was within the certificated gross weight limit of 25,320 pounds, and the load was properly distributed A flight plan filed by the crew with ARTC (Air Route Traffic Control) indicated an IFR (instrument flight rule) flight at a cruising altitude of 4,000 feet with South Bend and Toledo, Ohio, designated as the alternate airports The "Trip Weather Analysis" (a form prepared by the crew before departure) indicated that scattered cumulus and thunderstorms were expected south of the course to Fort Wayne Also, that a squall line extending in a north-south direction was moving eastward across Illinois and Indiana at an estimated speed of 35 miles per hour and was expected to be in the vicinity of South bend upon the flight's arrival there. After takeoff, Flight 129 was advised by company radio that it was cleared by ARTC via Green Airway No 3 over Sandusky, Ohio, to the Toledo range, to maintain 3,000 feet and to contact Toledo approach control upon arriving there Flight 129 advised they were going to Fort Wayne and not Toledo Accordingly, ARTC amended the flight's clearance to proceed to Fort Wayne via Green Airway No 3 and Blue Airway No 44 and to maintain 4,000 feet The flight proceeded and a routine company radio report was made when over Sandusky At 1847, the flight reported over Toledo and estimated its arrival Fort Wayne at 1932 At this time, the Fort Wayne 1830 weather sequence report was given the flight which was, "ceiling estimated 25,000 feet, thin Broken clouds, visibility 0 miles, wind southwest 5 miles per hours "Seventeen minutes later at 190', flight 129 called Toledo tower and requested, through APTC permission to cruise at 2,300 feet because of turbulent conditions This was not approved because of other traffic At 1920 the flight reported it was approaching Fort Wayne and was changing to tower frequency The flight reported again when nineteen in less northeast of Bauer Field and was advised at Runway 22 was the runway in use and that the wind was five to ten miles per hour from the southwest At the time this transmission was made there was a moderate amount of station and the flight reported "We are not recanting you very clearly but I think you said, `Straight 11 runway 22' We will call later, closer in ". Because of thunderstorm activity in the area, three other aircraft were requesting instructions to land at approximately the time Flight 129 was making its approach Two of these aircraft landed successfully and the pilot of one, upon request, advisee the tower that the thunderstorm was approximately ten miles west of the airport. At the time the four aircraft were approaching Baer Field, United *** 12 degrees was number four to land in the traffic pattern immediately behind *** World Airlines' Flight 240, a DC-3 aircraft then these latter aircraft were approximately one and two and one-half miles, respectively, from the approach end of Runway 22, the wind at the airport shifted to west-northwest and increased in velocity from 5-10 miles per hour to 40 miles per hour Both flights were advised by the tower of the sudden change of wind direction and increased velocity, and a landing on Runway 27 was suggested, it being more nearly into the wind Upon receiving this message the flights immediately turned to the left to align with this runway. When these aircraft were east of the airport the wind increased to 60-65 miles per hour with gusts to 85 miles per hour and a heavy rainfall began, accompanied by lightning and severe static The flights were quickly advised of the weather change but, due to the sudden decrease in visibility, neither flight was seen again by the tower Flight 129 immediately advised, "United 129 heading east" This was closely followed by a message from TWA's 240, "Pulling out" In order to avoid a possible collision the tower then requested separation altitudes for these aircraft from Chicago ARTC and was advised that Flight 129 was assigned an altitude of 4,000 feet and that Flight 240 was assigned 3,000 feet Both clearances were broadcast from the tower several times without acknowledgment. At 1932 m orange-colored flash was seen to the east-southeast from the tower It was later determined that United's Flight 129 had crashed in a field 2 6 miles east-southeast of the airport TWA's Flight 240 proceeded safely to Toledo. The aircraft disintegrated on impact and all 11 occupants were killed.
Probable cause:
The Board determines that the probable cause of the accident was the severe down draft encountered which caused the aircraft to strike the ground in a near level attitude. The following findings were reported:
- The squall line moved across northern Illinois and northern Indiana considerably faster than was forecast,
- A line of thunderstorms was known to be approaching Fort Wayne However, it was believed that aircraft in the area could effect safe landings prior to the storm's arrival there,
- When the subject flight and another were approaching Runway 27, they were advised of the surface wind's increased velocity to 65 miles per hour with gusts to 85 miles per hour,
- When the approach was abandoned the aircraft encountered the forward edge of the squall line and was subjected to a severe down draft from which recovery could not be made.
Final Report:

Crash of a Douglas DC-3 off Hong Kong: 16 killed

Date & Time: Apr 9, 1951
Type of aircraft:
Operator:
Registration:
HS-SAE
Survivors:
No
Schedule:
Bangkok – Hong Kong
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
11
Pax fatalities:
Other fatalities:
Total fatalities:
16
Circumstances:
While descending to Hong Kong-Kai Tak Airport, the pilot was unable to locate the runway due to poor visibility caused by night and foggy conditions. The pilot decided to divert to Tainan Airport but was unable to land there so returned to Kai Tak. On final approach to runway 31, while descending by night below the 400 feet ceiling, the aircraft hit the water surface and crashed into the sea off the Aguilar Cape, about 11 km south of runway 31 threshold. All 16 occupants were killed and the aircraft was destroyed. It appears that the left wing tip hit the water surface while the pilot was performing a left turn to join the runway 31 approach path.

Crash of a Douglas DC-3A in Sioux City: 16 killed

Date & Time: Mar 2, 1951 at 0912 LT
Type of aircraft:
Operator:
Registration:
N19928
Survivors:
Yes
Schedule:
Kansas City – Omaha – Sioux City – Minneapolis
MSN:
7400
YOM:
1942
Flight number:
MD016
Location:
Crew on board:
4
Crew fatalities:
Pax on board:
21
Pax fatalities:
Other fatalities:
Total fatalities:
16
Captain / Total flying hours:
8585
Captain / Total hours on type:
6971.00
Copilot / Total flying hours:
3695
Copilot / Total hours on type:
1445
Aircraft flight hours:
28202
Circumstances:
Flight 16 departed Kansas City, Missouri, at 0724LT, bound for Omaha, Nebraska, Sioux City, Iowa, and other intermediate stops with final destination as Minneapolis, Minnesota. The crew consisted of Captain James H. Graham, First Officer Philip K. Toler, and Stewardess Marilyn Woodbury. Ernest F. Eilert, a trainee copilot, was riding in the cockpit as the fourth crew member. From Kansas City, the aircraft carried 21 passengers, cargo, and fuel, which resulted in a total gross weight of 25,100 pounds, which was within the certificated unit of 25,200 pounds The load was properly distributed with relation to the center of gravity of the aircraft. Weather conditions over the intended route were instrument with a general overcast lowering from 4,200 feet at Kansas City to about 1,000 feet at Omaha. No difficulty was experienced as the flight proceeded to Omaha at 4,000 feet in accordance with an instrument flight plan. A normal landing was made on Runway 11 about 1,000 feet from its approach end, but near the completion of the landing roll the aircraft ran off the right side of the runway, passing over one of the high intensity runway lights. Captain Graham reported this to one of the ground crew at Omaha, and both the aircraft and light were inspected for damage. None was found and the aircraft was prepared for departure to Sioux City. At 0841 the flight took off for Sioux City on an instrument flight plan with Omaha as the alternate airport. There were 21 passengers, 920 pounds of cargo, and 1,500 pounds of fuel, which resulted in a take-off weight of 24,630 pounds. The take-off was without incident and no difficulty was encountered en route to Sioux City, the flight proceeding at 3,000 feet altitude. At 0904 Flight 16 reported over the Sloan Fan Marker, 11.9 miles south-southeast of the approach end of Runway 35 at the Sioux City Airport. It was immediately cleared by the Sioux City Airport tower for a “straight-in” approach and landing on Runway 35. Weather information was furnished to the flight as precipitation, ceiling 500 feet, sky obscured, visibility one mile in light snow showers, and wind from the east at 14 miles per hour. The medium-intensity lights for Runway 17/35 were turned on and placed at the position of full brilliance. Following receipt of this information, the flight requested permission to land to the southeast on Runway 13 and received clearance to do so. At 0909 the flight reported that it was contact over the southeast corner of the field and was cleared to land. At the same time the aircraft was seen by a ground witness one mile southeast of the airport. Shortly thereafter, it was sighted approximately over the intersection of Runways 4/22 and 17/35 on an east-southeast heading. A left climbing turned to the north was then made and the pilot was advised that he was cleared to land on either Runway 17 or Runway 13. The pilot was also advised by the tower that there would be a 90-degree cross-wind if he elected to land on Runway 17. All transmissions to the flight were acknowledged The aircraft was not further observed, and crashed about 600 feet north and west of the approach end of Runway 17. Fire developed immediately. Three crew members and 13 passengers were killed while nine other occupants were seriously injured. The aircraft was destroyed by fire.
Probable cause:
The Board determines that the probable cause of this accident was a stall during a left turn too close to the ground to effect recovery.
Final Report:

Crash of a Douglas DC-3A in Holguín

Date & Time: Nov 25, 1950
Type of aircraft:
Operator:
Registration:
CU-T7
Survivors:
Yes
MSN:
11646
YOM:
1943
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On touchdown, the aircraft went out of control, veered off runway to the right, hit a wooden perimeter fence, lost its undercarriage and came to rest. There were no casualties but the aircraft was damaged beyond repair. At the time of the accident, the visibility was reduced due to fog.

Crash of a Douglas DC-3C on the Mt Moran: 21 killed

Date & Time: Nov 23, 1950 at 1750 LT
Type of aircraft:
Operator:
Registration:
N74586
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Chico – Billings
MSN:
19711
YOM:
1944
Crew on board:
3
Crew fatalities:
Pax on board:
18
Pax fatalities:
Other fatalities:
Total fatalities:
21
Circumstances:
While cruising by night and in foggy conditions, the aircraft hit the slope of the Mt Moran (12,605 feet high) located in the northwest part of Wyoming, south of the Yellowstone National Park. The aircraft departed Chico, California, at 1515LT, to Billings, Montana, carrying eight children, ten adults and a crew of three. The aircraft hit the mountain at approximately 1750LT. As the aircraft failed to arrive in Billings, SAR operations were conducted. The following day, farmers told the local authorities that fire was spotted in the mountain and that it was not possible to find anything burning at this period of the year except maybe the crashed aircraft. As the accident zone was unreachable, it took time to rescuers to find the wreckage. All 21 occupants have been killed.

Crash of a Douglas DC-3 in Vitória da Conquista

Date & Time: Nov 4, 1950
Type of aircraft:
Operator:
Registration:
PP-IBC
Flight Phase:
Survivors:
Yes
MSN:
4360
YOM:
1942
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll, the left engine suffered vibrations and the captain decided to abandon the takeoff. In a certain confusion, the copilot inadvertently retracted the undercarriage, causing the aircraft to sink on its belly. It skidded for several yards before coming to rest. While the airplane was damaged beyond repair, there were no casualties.
Probable cause:
Vibrations on the left engine during takeoff caused by the failure of a propeller hub. Poor crew coordination and communication, making the copilot to retract the undercarriage while the aircraft was still rolling for takeoff.

Crash of a Douglas DC-3-229 in Utica: 16 killed

Date & Time: Sep 4, 1950 at 1410 LT
Type of aircraft:
Operator:
Registration:
N18936
Flight Phase:
Survivors:
Yes
Schedule:
Ithaca – Syracuse – Utica – Newark
MSN:
2011
YOM:
1937
Flight number:
RBS032
Location:
Crew on board:
3
Crew fatalities:
Pax on board:
20
Pax fatalities:
Other fatalities:
Total fatalities:
16
Captain / Total flying hours:
4431
Captain / Total hours on type:
1900.00
Copilot / Total flying hours:
3600
Copilot / Total hours on type:
2273
Aircraft flight hours:
19023
Circumstances:
Prior to takeoff, the engines were given a pre-flight check, following which the takeoff roll was commended. The flaps were in the "full up" position for the takeoff. The aircraft became airborne in a normal manner approximately 1,500 feet down the runway and climbed to an altitude of approximately 50 feet and leveled off. At this time, the landing gear was retracted and the air speed was estimated to be 105 to 110 miles per hour by qualified observers. Approximately 3,000 feet from the point of take-off parts were observed falling from the left engine and the aircraft made a shallow turn to the left. At this time, the left propeller appeared to be fully feathered. The flight continued in a left turn, slowly losing altitude until it struck a grove of trees 1.5 miles southeast of the airport. The elevation of the terrain at this point was 480 feet which is 256 feet below the elevation of the airport. The tree tops were 80 feet above the ground. First impact with the trees was made on a heading of approximately 60 degrees and as the aircraft descended through the trees, it turned anti-clockwise 180 degrees to the original heading. Following impact with the trees, the fuel tanks ruptured causing a fire which consumed the fuselage. Sixteen of the occupants were fatally injured and seven seriously injured. The survivors escaped either through broken windows on the right side, or the right rear escape hatch.
Probable cause:
The Board determines that the probable cause of the accident was the failure of the left engine shortly after take-off, coupled with increased drag due to loss of left engine cowling and reduced power output of the right engine because the right propeller was in the high pitch position.
Final Report: