Crash of a Douglas DC-6B in Minneapolis

Date & Time: Aug 28, 1958 at 0329 LT
Type of aircraft:
Operator:
Registration:
N575
Flight Phase:
Survivors:
Yes
Schedule:
Washington DC – Pittsburgh – Cleveland – Detroit – Milwaukee – Minneapolis – Portland – Seattle
MSN:
45200
YOM:
1957
Flight number:
NW537
Crew on board:
4
Crew fatalities:
Pax on board:
58
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
12376
Captain / Total hours on type:
572.00
Copilot / Total flying hours:
9089
Copilot / Total hours on type:
148
Aircraft flight hours:
4471
Circumstances:
At approximately 0329LT, the airplane crashed on takeoff from Wold-Chamberlain Field, Minneapolis, Minnesota. A number of the 62 persons (including 2 infants) aboard suffered serious injuries but there were no fatalities. Fire, which broke out a short time after all occupants were evacuated, consumed the aircraft. The aircraft took off normally and climbed to a height of about 100 feet. It then gradually nosed over and entered a descent which continued until it struck the ground. Sky conditions were clear; however, the prevailing visibility was about three miles in fog, and in localized areas around the airport it was reduced to lens than a mile by patches of denser fog. Takeoff was made on runway 22 and the climbout was a from a lighted, built-up section toward an open, unlighted area. The Board believes that the pilot while trying to remain contact in reduced visibility allowed the nose of the aircraft to drop when flaps were retracted because of inattention to flight instruments. The darkness and reduced visibility during climbout contributed to a sensory illusion which completely obscured the fact of descent from the pilot.
Probable cause:
The Board determines that the probable cause of this accident was the pilot's inattention to flight instruments during takeoff in conditions of reduced visibility.
Final Report:

Crash of a Douglas DC-6 in Ilha Grande

Date & Time: Jun 10, 1958 at 1145 LT
Type of aircraft:
Operator:
Registration:
LV-ADV
Flight Phase:
Survivors:
Yes
Schedule:
Rio de Janeiro – Buenos Aires
MSN:
43034
YOM:
1947
Country:
Crew on board:
6
Crew fatalities:
Pax on board:
16
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
While in cruising altitude, the engine number four oversped. The engine was shut down and the propeller was feathered. A little later, the engine number two suffered severe vibrations and it was also decided to shut it down and to feather its propeller. Due to insufficient power, the aircraft started to descend with a rate of 500 feet per minute. The captain eventually decided to attempt an emergency landing on Ilha Grande. The airplane belly landed on a beach and came to rest. All 22 occupants were uninjured.
Probable cause:
Double engine failure for undetermined reason.

Crash of a Douglas DC-6V in Norköpping

Date & Time: Nov 28, 1957
Type of aircraft:
Operator:
Registration:
SE-BDP
Flight Type:
Survivors:
Yes
Schedule:
Norköpping - Norköpping
MSN:
43747
YOM:
1953
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was performing a local training flight out from Norrköping-Kungsängen Airport. In flight, the captain informed ATC that an engine caught fire and obtained the permission for an emergency landing. Following technical issues, the crew was unable to lower the undercarriage and a belly landing was carried out. The airplane slid for several yards and came to rest in flames. All five crew members escaped uninjured while the aircraft was destroyed.
Probable cause:
Engine failure.

Crash of a Douglas DC-6A in New York: 20 killed

Date & Time: Feb 1, 1957 at 1802 LT
Type of aircraft:
Operator:
Registration:
N34954
Flight Phase:
Survivors:
Yes
Schedule:
New York – Miami
MSN:
44678
YOM:
1955
Flight number:
NE823
Crew on board:
6
Crew fatalities:
Pax on board:
95
Pax fatalities:
Other fatalities:
Total fatalities:
20
Captain / Total flying hours:
16630
Captain / Total hours on type:
85.00
Copilot / Total flying hours:
8943
Copilot / Total hours on type:
17
Aircraft flight hours:
8317
Circumstances:
Northeast Airlines Flight 8232 a DC-6A, N34954, was scheduled to originate at La Guardia Field, a nonstop to Miami, Florida, with a departure time of 1445. This aircraft and the same crew operating as Flight 822, had arrived at LaGuardia from Miami at 1250. The crew consisted of Captain Alva V. R. Marsh, First Officer Basil S. Dixwell, Flight Engineer Angelo V. Andon, and Stewardesses Doris Steele, Catherine Virchow, and Emily Gately. A short time before the scheduled departure time the crew and passengers boarded the aircraft. Snow, which had started at LaGuardia at 1202, began to accumulate on the aircraft's horizontal surfaces after its arrival at the LaGuardia ramp position. Snow removal by ground personnel, during preflight, was ineffective because of the continuing snowfall. Accordingly, about 1600 the aircraft was taxied, with all occupants aboard, to a nose hangar on the west side of the airport for snow removal. This was accomplished and at 1745 the crew advised LaGuardia ground control that they were ready to taxi from the nose hangar for the IFR, departure to Miami. Flight 823 was then cleared to runway 4 and was advised that the wind was northeast 10, the altimeter setting 30.12, and a time check of 1747-1/2. Air Route Traffic Control cleared the flight as follows. "Cleared to Bellemead, maintain 7,000 feet." A supplementary climb-out clearance was then given: "After takeoff, a left turn direct Paterson, direct Chatham, cross 081-degree radial of Caldwell 4,000 feet or above, cross Paterson between 5,000 and 6,000 feet and cross the northwest course of Idlewild not above 6,000 feet." Both clearances were repeated and acknowledged. Takeoff clearance was issued at 1800 and a tower controller saw the aircraft airborne at approximately 1801.2 The controller advised the flight to contact LaGuardia radar departure control on 120.4 mcs. This message was acknowledged but the radar controller did not receive a call from the flight; however, he did observe a target on the scope that indicated an aircraft over the runway. The next two sweeps on the scope disclosed the target beyond the end of the runway. A subsequent sweep indicated that the target was turning left. The target then disappeared from the scope. The LaGuardia tower controllers observed a large flash at approximately 1802 in the vicinity of Rikers Island, the approximate center of which is about one mile north of the point where the aircraft left the runway. It was learned at 1819, by telephone, that Northeast Airlines Flight 823 had crashed on Rikers Island. The airplane was destroyed by a post crash fire and 20 passengers were killed.
Probable cause:
The Board determines that the probable cause of the accident was the failure of the captain to (1) properly observe and interpret his flight instruments and (2) maintain control of his aircraft. The following findings were reported:
- The weather at the time of takeoff was above the prescribed company minimums,
- The aircraft, immediately following takeoff, made a left turn of approximately 119 degrees and a descent,
- The pilot and flight crew did not observe or interpret any instrument indication of a left turn or descent,
- The heading indications of both fire-seized course indicators corresponded closely to the impact heading of the aircraft,
- These instruments had been functioning properly until the time of impact,
- There was no failure or malfunction of the powerplants,
- There was no airframe failure or control malfunction,
- There was no electrical power failure or malfunction of instruments prior to ground impact,
- There was no fire prior to ground impact,
- As a result of fuselage deformation the main cabin door jammed, hindering evacuation of passengers,
- The main cabin lighting system became Inoperative during deceleration and the emergency inertia lights did not actuate.
Final Report:

Crash of a Douglas DC-6B in Paris-Orly: 34 killed

Date & Time: Nov 24, 1956 at 0018 LT
Type of aircraft:
Operator:
Registration:
I-LEAD
Flight Phase:
Survivors:
Yes
Schedule:
Rome – Milan – Paris – Shannon – Gander – Boston – New York
MSN:
45075
YOM:
1956
Flight number:
LAI451
Country:
Region:
Crew on board:
10
Crew fatalities:
Pax on board:
25
Pax fatalities:
Other fatalities:
Total fatalities:
34
Captain / Total flying hours:
10000
Circumstances:
After liftoff from runway 26 at Paris-Orly Airport, the four engine aircraft encountered difficulties to gain height, hit successively two houses, stalled and crashed in a huge explosion about 600 meters past the runway end. The aircraft disintegrated on impact and debris were scattered for about 200 meters. A passenger was seriously injured while all 34 other occupants, among them the Italian Director Guido Cantelli, were killed.
Probable cause:
The Commission was unable to find any malfunctioning of the aircraft or its equipment which would make it possible to determine why the aircraft followed the observed flight path. The Commission, therefore, believes that:
- the aircraft's slight loss of altitude soon after take-off was the main cause of the accident. There is no explanation for this loss of altitude,
- although the regulations in force were observed, the presence of unmarked obstructions in the take-off path constituted an aggravating factor,
- the initial and direct cause of the accident remains unknown.
Final Report:

Crash of a Douglas R6D-1 into the Atlantic Ocean: 59 killed

Date & Time: Oct 10, 1956 at 2210 LT
Type of aircraft:
Operator:
Registration:
131588
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Lakenheath – Lajes – McGuire
MSN:
43691
YOM:
1953
Country:
Region:
Crew on board:
10
Crew fatalities:
Pax on board:
49
Pax fatalities:
Other fatalities:
Total fatalities:
59
Circumstances:
The crew was performing a flight from RAF Lakenheath to McGuire AFB with an intermediate stop at Lajes, Azores Islands. At 2055LT, while cruising at an altitude of 15,000 feet, the crew informed ATC about his position and everything was ok. More than hour later, at 2210LT, the aircraft went out of control and crashed into the Atlantic Ocean about 590 km southwest of Land's End, Cornwall, UK. The crew was unable to send any distress call. Few debris such as life vests and the nose wheel were found. All 59 occupants have been killed. It was reported that some debris recovered showed traces of fire, leaving open several assumptions.

Crash of a Douglas DC-6B in Cold Bay: 15 killed

Date & Time: Aug 29, 1956 at 2045 LT
Type of aircraft:
Operator:
Registration:
CF-CUP
Survivors:
Yes
Schedule:
Vancouver – Cold Bay – Tokyo – Hong Kong
MSN:
43843
YOM:
1953
Flight number:
CP307
Location:
Crew on board:
8
Crew fatalities:
Pax on board:
14
Pax fatalities:
Other fatalities:
Total fatalities:
15
Captain / Total flying hours:
9522
Captain / Total hours on type:
2906.00
Copilot / Total flying hours:
12782
Copilot / Total hours on type:
465
Aircraft flight hours:
10513
Circumstances:
Flight 307 departed Vancouver, British Columbia at 1347 Bering standard time en route to Hong Kong, China, with a refueling stop at Cold Bay, Alaska and an intermediate stop at Tokyo, Japan, carrying a crew of 8 and 14 passengers. At 2011 the flight reported 100 miles out, estimating Cold Bay at 2036. It reported being over the Cold Bay range station outbound on a standard instrument approach at 2035, and at 2042 as completing a procedure turn and proceeding inbound. This was the last transmission from the flight. At 2045 the aircraft was observed to descend from the overcast north of the airport for a landing on runway 14 and cross the field at low altitude to the intersection of the two runways. At this point a shallow left turn was started and the aircraft went out of sight southeast of the airport. Shortly afterwards a fire was observed and it was ascertained that the aircraft had crashed. Eleven passengers and 4 crew members were fatally injured. The aircraft was destroyed by impact forces and a post crash fire.
Probable cause:
The probable cause of this accident was the full retraction of the wing flaps at low altitude during a circling approach without necessary corrective action being taken by the crew. Considering that very little altitude was gained after the application of power it is probable that a circling approach had been decided upon when the left turn from runway 14 was made. Since the wing flaps during the circling approach would be extended 20 degrees, and since they were found in the fully retracted position, it is believed that they were retracted shortly before impact. Fully retracted wing flaps at this time would explain the feeling of experienced by the off-duty flight crew member.
Final Report:

Crash of a Douglas DC-6B near Cairo: 52 killed

Date & Time: Feb 20, 1956 at 0345 LT
Type of aircraft:
Operator:
Registration:
F-BGOD
Survivors:
Yes
Site:
Schedule:
Saigon – Calcutta – Karachi – Bahrain – Cairo – Paris
MSN:
43835
YOM:
1953
Location:
Country:
Region:
Crew on board:
9
Crew fatalities:
Pax on board:
55
Pax fatalities:
Other fatalities:
Total fatalities:
52
Circumstances:
The aircraft was on a scheduled flight from Saigon to Paris, France and had left Karachi for Cairo on 19 February at 1715 hours Greenwich Mean Time with 9 crew and 55 passengers aboard. The flight was routine until 0230 hours (20 February) when the aircraft reported to Cairo Air Traffic Control that it had passed Suez (60 miles east of Cairo) at 0224 at a flight level of 8 500 feet, flying VFR and was descending. At 0240 it reported the Cairo aerodrome in sight and being 15 miles out, was granted an authorization for a VFR approach and at the same time was given the QFE and QNH, 29.42 and 29.73 respectively. Contact was established with Cairo approach and the aircraft requested and received landing instructions oh 118.5 megacycles and was asked to call down wind. This message was acknowledged and was the last heard from the flight. Several attempts to contact the aircraft on all available frequencies were made but were unsuccessful. At 0450 hours the wreckage was sighted 18 miles southeast of the aerodrome. Only 6 crew members and 6 passengers survived.
Probable cause:
The accident was due to the failure of the pilot-in-command to monitor the co-pilot during a direct approach procedure and the reliance of the latter on his instruments exclusively to fix his position relative to the runway at an altitude below the minimum safe altitude. The factor of crew member fatigue can- not be ruled out
Final Report:

Crash of a Douglas DC-6B near Longmont: 44 killed

Date & Time: Nov 1, 1955 at 1903 LT
Type of aircraft:
Operator:
Registration:
N37559
Flight Phase:
Survivors:
No
Schedule:
LaGuardia – Chicago – Denver – Portland – Seattle
MSN:
43538
YOM:
1952
Flight number:
UA629
Crew on board:
5
Crew fatalities:
Pax on board:
39
Pax fatalities:
Other fatalities:
Total fatalities:
44
Captain / Total flying hours:
10086
Captain / Total hours on type:
703.00
Copilot / Total flying hours:
3578
Copilot / Total hours on type:
1062
Aircraft flight hours:
11949
Circumstances:
After a routine radio ramp check, Flight 629 taxied to runway 08R (80 degrees, right) and at 1844 the flight was in runup position where it was given ATC clearance for the flight to Portland, the first intended landing. The clearance, in part, included compulsory radio reports from the flight upon passing the Denver Omni and when climbing through 18,000 feet to its assigned flight altitude, 21,000 feet. Following takeoff the flight reported its "off time" to the company as 1852 and thereafter reported passing the Denver Omni at 1856. The latter communication was the last from the flight. About 1903 the Denver tower controllers saw two white lights, one brighter than the other, appear in the sky north-northwest of the airport and fall to the ground. Both lights were observed 30-45 seconds and seemed to fall with approximately the same speed. There was then a momentary flash originating at or near the ground which illuminated the base of the clouds, approximately 10,000 feet above. When the controllers observed the lights they initiated action to determine if any aircraft were in distress. Radio calls were made to all aircraft in the Denver area of responsibility and all except flight 629 were accounted for. It was soon learned that the flight had crashed and all 44 occupants had been killed. It was later confirmed that the disintegration of the aircraft in the air was caused by a bomb. Two weeks later, on November 15, investigators confirmed that an explosive device has been placed on board by John Gilbert Graham aged 23 who signed a US$ 37,500 life-insurance for his mother who was on board. Convicted guilty for murder and terrorism, he was sentenced to death penalty and executed on January 11, 1956.
Probable cause:
The Board determines that the probable cause of this accident was the disintegrating force of a dynamite bomb explosion which occurred in the number 4 baggage compartment. The following findings were reported:
- At 1903, eleven minutes after departure, an in-flight disintegrating explosion occurred aboard Flight 629,
- The aircraft was climbing normally and was on course when the explosion occurred,
- Physical evidence showed conclusively the explosion took place in the number 4 baggage compartment of the aircraft,
- The violence of the explosion and the physical evidence proved the explosion was not caused by any system or component of the aircraft,
- Physical evidence at the scene and laboratory tests confirmed that the explosive material was dynamite, in the form of a bomb,
- There was no evidence found to indicate malfunction or failure of the aircraft or its components prior to the explosion.
Final Report:

Crash of a Douglas DC-6 in Ronkonkoma: 3 killed

Date & Time: Apr 4, 1955 at 1555 LT
Type of aircraft:
Operator:
Registration:
N37512
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
New York-Idlewild – Ronkonkoma – LaGuardia
MSN:
43001
YOM:
1947
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
9763
Captain / Total hours on type:
549.00
Copilot / Total flying hours:
9018
Copilot / Total hours on type:
1156
Aircraft flight hours:
22068
Circumstances:
N37512, under the command of Captain S. C. Hoyt, UAL New York area flight manager, departed New York International Airport at 1428 on a Visual Flight Rules flight plan for an estimated two-hour flight in the vicinity of MacArthur Field, Islip. The aircraft was properly dispatched on a routine check flight, and Captains V. H. Webb and H. M. Dozier were aboard for the purpose of receiving their periodic instrument proficiency check. Upon completion of the checks, the flight was scheduled to return to LaGuardia Airport. At 1501 the flight reported to the company by radio that they were “doing air work around Hempstead.” Another message was received by the company at 1527 reporting that the flight was going to make an ILS (Instrument Landing System) approach at Islip (MacArthur Field). Shortly thereafter, the flight contacted the MacArthur tower, requesting approval for an ILS approach and landing. Permission was granted by the tower, and a normal landing was made on runway 32. The aircraft was taxied to the intersection of runways 28 and 32 and the crew prepared for takeoff. The 1532 MacArthur weather observation showed scattered clouds at 20,000 feet, broken clouds at 25,000; visibility over 15 miles; temperature 53; dew-point 30; wind NNW at 20 knots, gusts to 30 knots. When the flight departed New York International Airport, weather was approximately the same and the forecast for the New York area indicated that it would be similar over the area for the duration of the flight. At 1548, the MacArthur controller cleared the flight to take position on runway 32 and take off. The aircraft took position on the runway but did not immediately take off, hence a second takeoff clearance was transmitted at 1550. The gross weight of the aircraft at takeoff from MacArthur Field was approximately 61,050 pounds, which was well below the maximum allowable. The load was correctly distributed with respect to center of gravity limits. The aircraft became airborne approximately, 1,500 to 1,800 feet down the runway. The takeoff appeared normal, as did the initial portion of the climb, and the aircraft remained on the runway heading. When about 50 feet high, the right wing lowered and the aircraft started turning to the right, at which time the landing gear was retracting. The aircraft continued a climbing turn and the degree of bank increased to approximately vertical by the time the heading changed about 90 degrees and the aircraft had attained an estimated altitude of 150 feet. The nose dropped sharply and the aircraft dived into the ground, striking on the right wing and nose. It then cartwheeled and came to rest right side up. An intense fire started and consumed a large portion of the wreckage in spite of the prompt arrival of fire fighting equipment on the field.
Probable cause:
The Board determines that the probable cause of this accident was unintentional movement of No. 4 throttle into the reverse range just before breaking ground, with the other three engines operating at high power output, which resulted in the aircraft very quickly becoming uncontrollable once airborne. The following findings were reported:
- No evidence of failure or malfunctioning of the structure powerplants, propellers, or electrical system was found,
- In reducing power to zero thrust during an instrument takeoff with a simulated engine out, No. 4 propeller was unintentionally reversed before the aircraft became airborne,
- Evidence indicated that No. 4 throttle was moved out of reverse by the pilot into the forward position in an attempt to unreverse, but the reverse warning flag was not lifted, resulting in increased reverse thrust,
- An outboard propeller on a DC-6 reversing as the aircraft becomes airborne, in conjunction with high power output of the other three engines, at takeoff configuration and airspeed causes the aircraft to become almost immediately uncontrollable,
- There was insufficient time and altitude for any pilot corrective measures to become effective.
Final Report: