Crash of a Lockheed L-1049 Super Constellation in New York: 44 killed

Date & Time: Dec 16, 1960 at 1033 LT
Operator:
Registration:
N6907C
Survivors:
No
Site:
Schedule:
Dayton – Columbus – New York
MSN:
4021
YOM:
1952
Flight number:
TW266
Crew on board:
6
Crew fatalities:
Pax on board:
38
Pax fatalities:
Other fatalities:
Total fatalities:
44
Captain / Total flying hours:
14583
Captain / Total hours on type:
267.00
Copilot / Total flying hours:
6411
Copilot / Total hours on type:
268
Aircraft flight hours:
21555
Circumstances:
On December 16, 1960, at 1033 e.s.t., a collision between Trans World Airlines Model 1049A Constellation, N6907C, and a United Air Lines DC-8, N8013U, occurred near Miller Army Air Field, Staten Island, New York. Trans World Airlines Flight 266 originated at Dayton, Ohio. The destination was LaGuardia Airport, New York, with one en route stop at Columbus, Ohio United Air Lines Flight 826 was a non-stop service originating at O'Hare Airport, Chicago, Illinois, with its destination New York International Airport, New York. Both aircraft were operating under Instrument Flight Rules. Following the collision the Constellation fell on Miller Army Field, and the DC-8 continued in a northeasterly direction, crashing into Sterling place near Seventh Avenue in Brooklyn, New York. Both aircraft were totally destroyed. All 128 occupants of both aircraft and 6 persons on the ground in Brooklyn were fatally injured. There was considerable damage to property in the area of the ground impact of the DC-8. TWA Flight 266 departed Port Columbus Airport at 0900, operating routinely under Air Traffic Control into the New York area The New York Air Route Traffic Control Center (ARTCC) subsequently advised that radar contact had been established and cleared the flight to the Linden. Intersection, Control of the flight was subsequently transferred to LaGuardia Approach Control. When the flight was about over the Linden Intersection, LaGuardia Approach Control began vectoring TWA 266 by radar to the final approach course for a landing on runway 4 at LaGuardia. Shortly thereafter TWA 266 was cleared to descend to 5,000 feet, and was twice advised of traffic in the vicinity on a northeasterly heading. Following the transmission of this information the radar targets appeared to merge on the LaGuardia Approach Control radar scope, and communications with TWA 266 were lost. United Air Lines Flight 826 operated routinely between Chicago and the New York area, contacting the New York ARTCC at 1012 Shortly thereafter the New York Center cleared UAL 826 to proceed from the Allentown, Pa., very high frequency omni directional radio range station (VOR) direct to the Robbinsville, New Jersey, VOR, and thence to the Preston Intersection via Victor Airway 123. At approximately 1021, UAL 826 contacted Aeronautical Radio, Inc. (ARINC) to advise their company that the No. 2 receiver accessory unit was inoperative, which would indicate that one of the aircraft's two VHF radio navigational receivers was not functioning. A "fix" is established by the intersection of two radials from two separate radio range stations. With one unit inoperative the cross-bearings necessary can be taken by tuning the remaining receiver from one station to the other. This process consumes considerable time, however, and is not as accurate as the simultaneous display of information on two separate position deviation indicators While UAL 826 advised the company that one unit was inoperative, Air Traffic Control was not advised. At 1025 the New York ARTCC issued a clearance for a new routing which shortened the distance to Preston by approximately 11 miles. As a result, this reduced the amount of time available to the crew to retune the single radio receiver to either the Colt' s Neck, New Jersey, or Solberg, New Jersey, VOR in order to establish the cross-bearing with Victor 123, which would identify the Preston Intersection. In the event the crew would not attempt to retune the single VOR receiver, crossbearings on the Scotland Low Frequency Radiobeacon could be taken with the aircraft direction finding (ADF) equipment. This would be a means of identifying the Preston Intersection but, under the circumstances, would require rapid mental calculation in the interpretation of a display which could be easily misread. Several factors support the conclusion that this occurred. Instructions had been issued to UAL 826 for holding at the Preston Intersection the clearance limit, should holding be necessary. Clearance beyond Preston for an approach to Idlewild Airport would be received from Idlewild Approach Control and the transfer of control of the flight from the New York Center to Idlewild Approach Control would normally take place as the aircraft was approaching Preston. UAL 826 was not receiving radar vectors, but was providing its own navigation. After the flight reported passing through 6,000 feet the New York Center advised that radar service was terminated and instructed the flight to contact Idlewild Approach Control. UAL 826 then called Idlewild Approach Control, stating "United 826 approaching Preston at 5,000." This was the last known transmission from UAL 826. At the time UAL 826 advised it was approaching Preston it had in fact gone on by this clearance limit several seconds before and was several miles past the point at which it should have turned into the holding pattern. This is confirmed by the data obtained from the flight recorder which had been installed in the UAL DC-8, as well as by analysis of the communication tapes At a point approximately 11 miles past the Preston Intersection a collision occurred between TWA 266 and UAL 826. Weather at the altitude of the collision and at the time of the accident was such as to preclude flight by visual means.
Probable cause:
The Board determines that the probable cause of this accident was that United Flight 826 proceeded beyond its clearance limit and the confines of the airspace allocated to the flight by Air Traffic Control A contributing factor was the high rate of speed of the United DC-8 as it approached the Preston intersection, coupled with the change of clearance which reduced the enroute distance along VICTOR 123 by approximately 11 miles.
Final Report:

Crash of a Douglas DC-8-11 in New York: 90 killed

Date & Time: Dec 16, 1960 at 1033 LT
Type of aircraft:
Operator:
Registration:
N8013U
Survivors:
No
Site:
Schedule:
Chicago – New York
MSN:
45290
YOM:
1959
Flight number:
UA826
Crew on board:
7
Crew fatalities:
Pax on board:
77
Pax fatalities:
Other fatalities:
Total fatalities:
90
Captain / Total flying hours:
19100
Captain / Total hours on type:
344.00
Copilot / Total flying hours:
8500
Copilot / Total hours on type:
379
Aircraft flight hours:
2434
Circumstances:
On December 16, 1960, at 1033 e.s.t., a collision between Trans World Airlines Model 1049A Constellation, N 6907C, and a United Air Lines DC-8, N 8013U, occurred near Miller Army Air Field, Staten Island, New York. Trans World Airlines Flight 266 originated at Dayton, Ohio. The destination was LaGuardia Airport, New York, with one en route stop at Columbus, Ohio United Air Lines Flight 826 was a non-stop service originating at O'Hare Airport, Chicago, Illinois, with its destination New York International Airport, New York. Both aircraft were operating under Instrument Flight Rules. Following the collision the Constellation fell on Miller Army Field, and the DC-8 continued in a northeasterly direction, crashing into Sterling place near Seventh Avenue in Brooklyn, New York. Both aircraft were totally destroyed. All 128 occupants of both aircraft and 6 persons on the ground in Brooklyn were fatally injured. There was considerable damage to property in the area of the ground impact of the DC-8. TWA Flight 266 departed Port Columbus Airport at 0900, operating routinely under Air Traffic Control into the New York area The New York Air Route Traffic Control Center (ARTCC) subsequently advised that radar contact had been established and cleared the flight to the Linden. Intersection, Control of the flight was subsequently transferred to LaGuardia Approach Control. When the flight was about over the Linden Intersection, LaGuardia Approach Control began vectoring TWA 266 by radar to the final approach course for a landing on runway 4 at LaGuardia. Shortly thereafter TWA 266 was cleared to descend to 5,000 feet, and was twice advised of traffic in the vicinity on a northeasterly heading. Following the transmission of this information the radar targets appeared to merge on the LaGuardia Approach Control radar scope, and communications with TWA 266 were lost.United Air Lines Flight 826 operated routinely between Chicago and the New York area, contacting the New York ARTCC at 1012 Shortly thereafter the New York Center cleared UAL 826 to proceed from the Allentown, Pa., very high frequency omni directional radio range station (VOR) direct to the Robbinsville, New Jersey, VOR, and thence to the Preston Intersection via Victor Airway 123. At approximately 1021, UAL 826 contacted Aeronautical Radio, Inc. (ARINC) to advise their company that the No. 2 receiver accessory unit was inoperative, which would indicate that one of the aircraft's two VHF radio navigational receivers was not functioning. A "fix" is established by the intersection of two radials from two separate radio range stations. With one unit inoperative the cross-bearings necessary can be taken by tuning the remaining receiver from one station to the other. This process consumes considerable time, however, and is not as accurate as the simultaneous display of information on two separate position deviation indicators While UAL 826 advised the company that one unit was inoperative, Air Traffic Control was not advised. At 1025 the New York ARTCC issued a clearance for a new routing which shortened the distance to Preston by approximately 11 miles. As a result, this reduced the amount of time available to the crew to retune the single radio receiver to either the Colt' s Neck, New Jersey, or Solberg, New Jersey, VOR in order to establish the cross-bearing with Victor 123, which would identify the Preston Intersection. In the event the crew would not attempt to retune the single VOR receiver, crossbearings on the Scotland Low Frequency Radiobeacon could be taken with the aircraft direction finding (ADF) equipment. This would be a means of identifying the Preston Intersection but, under the circumstances, would require rapid mental calculation in the interpretation of a display which could be easily misread. Several factors support the conclusion that this occurred. Instructions had been issued to UAL 826 for holding at the Preston Intersection the clearance limit, should holding be necessary. Clearance beyond Preston for an approach to Idlewild Airport would be received from Idlewild Approach Control and the transfer of control of the flight from the New York Center to Idlewild Approach Control would normally take place as the aircraft was approaching Preston. UAL 826 was not receiving radar vectors, but was providing its own navigation. After the flight reported passing through 6,000 feet the New York Center advised that radar service was terminated and instructed the flight to contact Idlewild Approach Control. UAL 826 then called Idlewild Approach Control, stating "United 826 approaching Preston at 5,000." This was the last known transmission from UAL 826. At the time UAL 826 advised it was approaching Preston it had in fact gone on by this clearance limit several seconds before and was several miles past the point at which it should have turned into the holding pattern. This is confirmed by the data obtained from the flight recorder which had been installed in the UAL DC-8, as well as by analysis of the communication tapes At a point approximately 11 miles past the Preston Intersection a collision occurred between TWA 266 and UAL 826. Weather at the altitude of the collision and at the time of the accident was such as to preclude flight by visual means.
Probable cause:
The Board determines that the probable cause of this accident was that United Flight 826 proceeded beyond its clearance limit and the confines of the airspace allocated to the flight by Air Traffic Control A contributing factor was the high rate of speed of the United DC-8 as it approached the Preston intersection, coupled with the change of clearance which reduced the enroute distance along VICTOR 123 by approximately 11 miles.
Final Report:

Crash of an Ilyushin II-14T in Vockerode: 7 killed

Date & Time: Jul 22, 1960 at 0740 LT
Type of aircraft:
Operator:
Registration:
400
Flight Phase:
Survivors:
No
Site:
Schedule:
Dessau - Dessau
MSN:
14 803 004
YOM:
1958
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
The crew was engaged in a weather observation mission. After takeoff from Dessau Airport, instead of climbing and flying under IFR, the captain decided to continue under VFR mode below the clouds and in limited visibility. Ten minutes later, while cruising at an altitude of 500 feet, the airplane struck with its right wing the chimney of a metallurgical complexe and crashed in flames. All six crew members and one person on the ground were killed.

Crash of an Avro 652 Anson C.19 in Ruislip

Date & Time: Jun 1, 1960
Type of aircraft:
Operator:
Registration:
VV298
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
Schedule:
Northolt – Marham
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The twin engine aircraft was engaged in a special flight from RAF Northolt to RAF Marham, carrying two cameraman from the BBC and two crew members. Shortly after takeoff from RAF Northolt, while climbing, the left engine failed. Unable to maintain a safe altitude, the crew attempted an emergency landing when the airplane stalled and crashed on the roof of the Premier Foods egg packing building located in Victoria road in Ruislip, about 1,5 mile north of the airfield. Both passengers were unhurt while both pilots were seriously injured. The aircraft was damaged beyond repair.
Probable cause:
Failure of the left engine after takeoff.

Crash of a Vickers 827 Viscount in Rio de Janeiro: 42 killed

Date & Time: Dec 22, 1959 at 1340 LT
Type of aircraft:
Operator:
Registration:
PP-SRG
Survivors:
No
Site:
Schedule:
Brasilia – Rio de Janeiro
MSN:
401
YOM:
1959
Flight number:
VP233
Country:
Crew on board:
6
Crew fatalities:
Pax on board:
26
Pax fatalities:
Other fatalities:
Total fatalities:
42
Circumstances:
While approaching Rio de Janeiro-Galeão Airport in good weather conditions, the Viscount collided with a Brazilian Air Force Fokker T-21 (S.11) registered 0742. Its pilot was completing a local training flight when the collision occurred about 4 km south of the airfield. While the pilot of the trainer plane was able to eject and was later recovered uninjured, his aircraft crashed in Joaquim de Queiroz street. Out of control, the Viscount dove into the ground and crashed in the Peçanha Póvoas street, in the district of Ramos. Several houses were destroyed and all 32 occupants on board the Viscount were killed as well as 10 people on the ground.
Probable cause:
Failure of both pilots to maintain adequate lookout for other aircraft. Apparently, the pilot of the trainer aircraft was not supposed to cross the approach path of the Viscount.

Crash of a Lockheed L-1049H Super Constellation in Chicago: 11 killed

Date & Time: Nov 24, 1959 at 0535 LT
Operator:
Registration:
N102R
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Chicago – Denver – Los Angeles
MSN:
4824
YOM:
1957
Flight number:
TW595
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
11
Captain / Total flying hours:
12467
Captain / Total hours on type:
1670.00
Copilot / Total flying hours:
6285
Copilot / Total hours on type:
3919
Aircraft flight hours:
3432
Circumstances:
Flight 595, loaded with cargo, took off on runway 31L of Midway at approximately 0531LT bound for Los Angles, California. As the aircraft began a left turn, the crew notified Midway Tower they had received a fire warning on the No. 2 engine and had shut it down. They also informed the tower the flight would return and land. The aircraft proceeded in a continuing left turn around the airport in an elliptical pattern and below the clouds which were based at an altitude of 500 to 600 feet. In the turn to final approach to runway 31 the aircraft banked in excess of 45 degrees during which it developed an excessive rate of sink. When the aircraft reached the tops of the trees its wings were nearly level and its nose was raised in a climbing attitude; however, the descent continued. The wing flaps were being retracted during the last 5 to 10 seconds of the final descent and were found to be symmetrically extended at 24 percent upon impact. The plane crashed into a residential area about one-fourth of a mile southeast of Midway Airport, Chicago, Illinois, killing all persons aboard, demolishing the aircraft, and fatally injuring eight persons on the ground.
Probable cause:
The Board determines the probable cause of this accident to be the maneuvering of the aircraft in a manner that caused it to develop an excessive rate of sink while in the turn to final approach.
Final Report:

Crash of a Morane-Saulnier M.S.760 Paris in Córdoba: 1 killed

Date & Time: Nov 9, 1959 at 0740 LT
Operator:
Registration:
E-210
Flight Type:
Survivors:
No
Site:
Schedule:
Buenos Aires - Córdoba
MSN:
A-18
YOM:
1959
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
While approaching Córdoba AFB, the aircraft was too low, struck three houses and crashed in Ferreyra, about 8 km east of the airbase. The pilot was killed while there were no injuries on the ground.

Crash of a Vickers 621 Viking 1 in Southall: 7 killed

Date & Time: Sep 2, 1958 at 0632 LT
Type of aircraft:
Registration:
G-AIJE
Flight Type:
Survivors:
No
Site:
Schedule:
London – Nice – Brindisi – Athens – Tel Aviv
MSN:
127
YOM:
1946
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Captain / Total flying hours:
13000
Copilot / Total flying hours:
1000
Aircraft flight hours:
2319
Circumstances:
The Viking took off from London Airport at 0554 hours GMT with a crew of 3 for a flight to Nice, Brindisi, Athens and Tel Aviv. Fifteen minutes later the cap tain informed London Airport that he had engine trouble and wished to return to Blackbushe. During the return flight the aircraft initially maintained 7,000 feet. Clearance was given to descend to 3000 feet but the descent was apparently continued to 1,000 feet without informing control. Shortly afterwards the aircraft reported "having difficulty maintaining height" and six minutes later, at 0632LT, it crashed in Southall, about 3 miles from the airport. The aircraft was totally destroyed upon impact as well as several houses. All three crew members and four people on the ground were killed. Fifteen other people on the ground were injured.
Probable cause:
The aircraft was allowed to lose height and flying speed with the result that the pilot was no longer able to exercise asymmetric control. The conduct of the pilot and the whole course of events outlined were contributed to by the deliberate policy of this Company, which was to keep its aircraft in the air and gainfully employed regardless of the regulations or of the elementary requirements which should enjoin consideration for the conditions of working of its employees or the maintenance of its aircraft. Any responsibility of the captain is to be viewed in the light of his position as an employee upon whose shoulders an intolerable burden was placed. At the time of the accident, the airplane was overloaded and the captain was overduty as he had been on duty for 31 hours 30 minutes, a gross breach of Article 34E of the Order, since the maximum permissible flying duty period for a two-pilot crew is 16 hours.
Final Report:

Crash of a Douglas C-118A Liftmaster in Norwalk: 42 killed

Date & Time: Feb 1, 1958 at 1913 LT
Type of aircraft:
Operator:
Registration:
53-3277
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Long Beach – McGuire
MSN:
44648
YOM:
1955
Flight number:
USAF30W/02
Crew on board:
6
Crew fatalities:
Pax on board:
35
Pax fatalities:
Other fatalities:
Total fatalities:
42
Captain / Total flying hours:
7819
Captain / Total hours on type:
1448.00
Copilot / Total flying hours:
701
Copilot / Total hours on type:
439
Circumstances:
The four engine aircraft departed Long Beach Airport at 1908LT bound for McGuire AFB, New Jersey, with 35 passengers and a crew of six on board. Shortly after takeoff, the pilot was cleared to climb to the assigned altitude of 17,000 feet. About five minutes later, while climbing to an altitude of 3,000 feet, the airplane collided with a USN Lockheed P2V-5F Neptune registered 127723. Carrying eight crew members, the Neptune has taken off from Los Alamitos NAS and was completing a local training mission. Following the collision, both aircraft went out of control, dove into the ground and crashed in Norwalk. The Liftmaster crashed on several building and a fuel station, killing all 41 occupants and one woman on the ground. The Neptune crashed in a stone-pit located about 2.5 miles north of the C-118 crash site. Six crew members were killed while two others were seriously injured. The accident occurred by night but in good weather conditions with a visibility above 15 miles.
Probable cause:
It was determined that the collision occurred in an uncontrolled area. Both crews were considered as co-responsible of the accident as they failed to take the appropriate measures to avoid each other and to pay attention to potential traffic. The crew of the C-118 was blamed not giving the priority to the Neptune which was flying to his right.

Crash of a Curtiss C-46A-50-CU Commando in Guatemala City: 2 killed

Date & Time: Nov 6, 1957 at 1135 LT
Type of aircraft:
Registration:
N10425
Flight Type:
Survivors:
Yes
Site:
Schedule:
Guatemala City – Belize City – Saint Petersburg
MSN:
30525
YOM:
1944
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
10729
Captain / Total hours on type:
6333.00
Copilot / Total flying hours:
3213
Copilot / Total hours on type:
710
Circumstances:
The aircraft took off from Runway 01 at La Aurora Airport at 1118LT on a scheduled cargo flight to St. Petersburg, Florida via Belize City in British Honduras. It carried a crew of two and no passengers. The flight was cleared on a visual flight rules flight plan and the take-off gross weight was 44 995 lbs including 575 gallons of fuel. At 1125LT the flight advised La Aurora Airport Control Tower that it was returning for an engine check and was cleared for an approach to Runway 19 at that airport. At approximately 1135LT the aircraft was seen to crash at a point 5,029 feet above sea level in a residential area, 3.3 miles northwest of La Aurora Airport, fatally injuring one adult and one child. Three other persons on the ground and both crew members were seriously injured. The aircraft was demolished by impact and subsequent fire.
Probable cause:
Failure of the crankshaft on the left engine and inability of the aircraft to maintain single engine flight for reasons undetermined after failure of the other engine. The following information from a preliminary report on the crankshaft by the National Bureau of Standards, has been added at the request of the Civil Aeronautics Board, Washington: "The crankshaft contained a large fatigue fracture that originated in the splined section in one of the spline fillets. The fatigue crack had penetrated through the crankshaft wall and progressed in both directions from the origin, initially following a spiral path at an angle of about 45 O to the axis of the shaft and then turning into a plane perpendicular to the shaft axis. The fatigue crack attained a total length of about 600 degrees before the final overload fracture occurred. This was a longitudinal break, about 2-1/2 inches long, between two loops of the spiral crack. The fillet where the fatigue crack started was poorly contoured and contained deep tool marks that evidently had contributed to the cause of the failure. In one fillet near the fracture origin the rough machining had produced an effective radius of about 0.005 inch. The drawing did not specify a minimum radius for the splines. It permitted a maximum radius of 0.015 inch. In the vicinity of the fracture the average hardness of the steel was 421 Vickers or about 43 Rockwell C. This indicates a tensile strength of about 200,000 psi. The drawing did not specify hardness or tensile strength except on case hardened surfaces, calling instead for 'Core Property P. W.A. No. 7, which presumably refers to a Pratt and Whitney heat treatment. The chemical composition of the crankshaft steel complied with the material specification in so far as specified elements were concerned. The steel contained appreciable amounts of molybdenum, chromium and copper, which were not specified, but the presence of these elements in the amounts found would not be expected to reduce the fatigue strength of the shaft. A small fatigue fracture that formed a part of a complete longitudinal break was found in the counterbalance bearing. This fracture apparently occurred because of unusually high loads imposed by the progression of the fatigue crack in the crankshaft. The hardness specified in the drawing for the counterbalance bearing was 34 to 38 Rockwell C. Vickers tests showed that the hardness in the part as submitted ranged from 279 to 354 Vickers or from about 27 to 36 Rockwell C. How- ever, the bearing showed evidence of overheating, which probably reduced the hardness in some areas. Chemical and spectrographic analyses showed that the composition of the counterbalance bearing material complied with the specification. "
Final Report: