Crash of a Douglas DC-3 in Tampico: 3 killed

Date & Time: Aug 31, 1952
Type of aircraft:
Registration:
XA-GER
Flight Phase:
Survivors:
Yes
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
20
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
Just after liftoff, the airplane hit successively a truck and few houses before crashing into flames. Three people on the ground were killed while all 23 occupants survived. It is believed that the crew decided to takeoff from an unsuitable terrain for such aircraft type.

Crash of a Douglas DC-3D into the Malacca Strait: 17 killed

Date & Time: May 9, 1952
Type of aircraft:
Operator:
Registration:
PK-DPA
Flight Phase:
Survivors:
No
Schedule:
Medan – Ipoh – Kuala Lumpur – Jakarta
MSN:
42954
YOM:
1946
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
14
Pax fatalities:
Other fatalities:
Total fatalities:
17
Circumstances:
While approaching Ipoh on a flight from Medan, the crew encountered poor weather conditions when control was lost. The aircraft crashed into the Malacca Strait, few km off shore, killing all 17 occupants.

Crash of a Douglas DC-3 near San Felipe: 12 killed

Date & Time: Mar 29, 1952
Type of aircraft:
Operator:
Registration:
YV-C-AZU
Survivors:
No
Schedule:
Caracas – San Felipe
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
12
Circumstances:
While approaching San Felipe from the east in a limited visibility, the airplane hit the slope of the Cerro Grande located about 30 km from the San Felipe Airport. All 12 occupants were killed.

Crash of a Douglas DC-3-393 in Uberlândia: 9 killed

Date & Time: Feb 28, 1952
Type of aircraft:
Operator:
Registration:
PP-PCN
Survivors:
Yes
Schedule:
Goiânia – Uberlândia – Rio de Janeiro
MSN:
3284
YOM:
1941
Flight number:
PB389
Country:
Crew on board:
4
Crew fatalities:
Pax on board:
27
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
On final approach to Uberlândia Airport, the airplane was too low and hit trees with its left wing, stalled and crashed. Six passengers and three crew members were killed while 22 other occupants were injured. The aircraft was destroyed.
Probable cause:
The pilot-in-command decided to continue the approach below the minimum descent altitude, neglecting the published procedures.

Crash of a Douglas DC-3A in Denver: 3 killed

Date & Time: Dec 4, 1951 at 0725 LT
Type of aircraft:
Operator:
Registration:
N17109
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Denver - Denver
MSN:
4999
YOM:
1942
Flight number:
UA016
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
5793
Captain / Total hours on type:
2404.00
Copilot / Total flying hours:
1250
Copilot / Total hours on type:
100
Aircraft flight hours:
15041
Circumstances:
United Air Lines operates a Flight Training Center at Denver, Colorado, to train applicants for first officer positions with the company. The crew of United Trainer 16 consisted of Senior First Officer Jordan D. Kocher, who had been designated by United Air Lines as captain and instructor, and Trainee First Officers Laurence G. Wilson and Wayne C. Moen. The flight departed Stapleton Airfield at 0655LT. The 0628 weather conditions, upon which the crew had been briefed, were ceiling measured 15,000 feet, visibility 25 miles, and wind northwest 14 knots Ceiling and visibility were unlimited at the time of the accident, with the wind northwest 16 knots. No radio contacts were made by United Trainer 16 after reporting departure time. It was cleared for a training flight of four hours’ duration within a 25-mile radius of Denver Captain Kocher occupied the left pilot’s seat at takeoff. Upon departure, the aircraft load, in addition to the crew, was 820 gallons of gasoline, full oil tanks, and 650 pounds of sand ballast tied down in the rear baggage pit. The load was properly distributed with relation to the aircraft’s center of gravity, and the 22,910-pound gross weight at takeoff was within allowable limits. Witnesses reported that at between 0720 and 0725 the aircraft was seen to stall, enter a spin, and strike the ground in a diving attitude before recovery was effected.
Probable cause:
The Board finds that the probable cause of this accident was an inadvertent spin at an altitude too low for recovery. The following findings were pointed out:
- The load was properly distributed within approved center of gravity limits and the aircraft was lightly loaded, carrying only the crew in addition to the fuel, oil and ballast,
- No malfunctioning of the aircraft or its components was reported prior to the accident, and no evidence of malfunctioning or failure was indicated by examination of the wreckage,
- The aircraft stalled at an altitude of approximately 8,200 feet MSL (about 3,200 feet above the ground), entered a spin, and crashed before recovery could be effected,
- Power was being developed by both engines upon impact.
Final Report:

Crash of a Douglas DC-3D in Moisville: 5 killed

Date & Time: Aug 11, 1951 at 0925 LT
Type of aircraft:
Operator:
Registration:
F-BAXB
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Paris - Paris
MSN:
42971
YOM:
1946
Location:
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
5302
Aircraft flight hours:
5750
Circumstances:
The aircraft took off from Paris-Le Bourget Airport at 0750LT on a flight to test a new type of air scoop. The new scoop was fitted to one engine only to allow comparison tests to be made. Five minutes later, the aircraft reached the altitude of 4,300 feet and four minutes later, at 0759LT, the starboard engine was stopped and the test commenced with a climb on the port engine with cooling gills open. At 0811LT, at an altitude of 6,980 feet, the crew commenced the second phase of the test with the port engine cooling gills in the trail position. Level off was completed at 0822LT at an altitude of 7,900 feet with the cooling gills closed. About an hour later, while flying at a relative low speed, the airplane went out of control and entered a spin, lost its empennage and eventually crashed in a field located in Moisville. The aircraft was destroyed and all five crew members were killed.
Crew:
René Gallichet, pilot,
Louis Pichard, flight engineer,
Jacques Légalité, radio navigator,
Lucien Goulay, engineer,
Paul Martin, engineer.
Probable cause:
Study of the flight conditions and circumstances of the accident to the aircraft revealed no mechanical defect which might have been the initial cause of the accident. The cause would appear to have been an abnormal flight maneuver made when the crew experienced difficulty in resuming normal flight on two engines. Overspeed, reduction of pitch or difficulty in re-starting the engine may have created a dangerous situation and caused the aircraft to stall in dissymmetrical flight, thus subjecting the airframe to stresses accompanied by buffeting which was either alternating or exceeded the design limits of the structure and caused the tail-plane to break off.
Final Report:

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.