Crash of a Douglas DC-6 in New York

Date & Time: Feb 24, 1967 at 0225 LT
Type of aircraft:
Operator:
Registration:
N8224H
Flight Phase:
Survivors:
Yes
Schedule:
Philadelphia - Boston
MSN:
43741/290
YOM:
1952
Crew on board:
5
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6232
Captain / Total hours on type:
3348.00
Circumstances:
While cruising at an altitude of 15,500 feet over Holmdel, New Jersey, the aircraft suffered an explosive decompression of the cabin. A 60 by 125 inches 'panel' detached from the fuselage and struck the engine number three, causing the detachment of its propeller. The crew started an emergency descent and was able to complete an emergency landing at New York Airport. All 14 occupants were evacuated safely while the aircraft was later declared as damaged beyond repair.
Probable cause:
Fatigue fracture of the fuselage and explosive decompression caused by an inadequate maintenance and inspection on part of the ground maintenance personnel. Investigations reported that at the time of the decompression, the cabin was pressurized for 2,500 feet while the aircraft was flying at an altitude of 15,500 feet.
Final Report:

Crash of a Douglas DC-7B in Charlotte

Date & Time: Jul 20, 1964 at 1858 LT
Type of aircraft:
Operator:
Registration:
N831D
Survivors:
Yes
Schedule:
New York – Charlotte
MSN:
45340
YOM:
1957
Flight number:
EA702
Crew on board:
5
Crew fatalities:
Pax on board:
52
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
18022
Captain / Total hours on type:
4241.00
Aircraft flight hours:
19134
Circumstances:
The DC-7 touched down on runway 05 following an ILS approach. Reverser were applied, but the no. 1 engine reverser didn't respond. The pilot moved the no. 4 throttle to idle. The plane had then reached a rough part of the runway (a 1000 feet area, beginning 2750 feet down the runway). The DC-7 was turning slightly right, but this was corrected with left brake and rudder and left nose wheel steering. Severe vibration then caused the plane to veer sharply right off the runway, causing the nose gear to collapse. It appeared that the nose wheel strut collar had failed from both the left and right sides.
Probable cause:
Improper reversing technique resulting in the use of excessive directional corrective forces during which the aircraft struck an unsuitable runway condition. Unsuitable runway condition, resulting from inadequate runway maintenance. Inadequate supervision by the captain.
Final Report:

Crash of a Douglas DC-7D in Richmond

Date & Time: Jul 17, 1964 at 1833 LT
Type of aircraft:
Operator:
Registration:
N809D
Survivors:
Yes
Schedule:
New York – Richmond
MSN:
44860
YOM:
1955
Crew on board:
5
Crew fatalities:
Pax on board:
71
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
16244
Captain / Total hours on type:
1862.00
Aircraft flight hours:
25106
Circumstances:
On final approach to Richmond-Byrd Field Airport, the pilot was cleared to land on runway 15 but the airplane was slightly below the glide. This caused the right main gear to struck the ground 150 feet short of runway threshold and to be sheared off at impact. The aircraft slid on the runway for 4,752 feet before coming to rest. All 76 occupants were evacuated safely while the aircraft was considered as damaged beyond repair.
Probable cause:
The pilot misjudged altitude and distance and undershot during landing.
Final Report:

Crash of a Douglas DC-7 at Chambers Field NAS

Date & Time: Sep 26, 1961
Type of aircraft:
Operator:
Registration:
N317A
Flight Type:
Survivors:
Yes
Schedule:
New York - Norfolk
MSN:
44138
YOM:
1954
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was performing a positioning flight from New York to Chambers Field NAS at Norfolk to pick up troops on behalf of the US Army. On approach, the primary hydraulic system failed. Nevertheless, the crew was able to continue the approach and the aircraft touched down 275 feet past the runway threshold. After a course of 1,400 feet, the airplane veered off runway to the left and struck an embankment before coming to rest. All five crew members were uninjured while the aircraft was damaged beyond repair.
Probable cause:
Loss of directional control during the landing roll caused by improper use of propeller reversing and braking. The following factors contributed to the accident:
- The captain's inadequate familiarity with the aircraft systems and procedures under normal system hydraulic failure,
- Failure of the hydraulic system for an undetermined reason.

Crash of a Convair R4Y-1Z at Bader Field AFB

Date & Time: Feb 23, 1961
Type of aircraft:
Operator:
Registration:
140378
Flight Type:
Survivors:
Yes
Schedule:
New York - Andrews
MSN:
140
YOM:
1954
Crew on board:
4
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft was performing a flight from New York to Andrews AFB, carrying a crew of four and four passengers, among them Paul B. Fay Jr. who should be appointed under-secretary of the US Navy. While descending to Andrews, the crew was informed about poor weather conditions at destination and the captain decided to divert to Bader Field. Few minutes later, the electric system failed. The pilot-in-command was able to land on runway 04 at Bader Field but after touchdown, he was unable to activate the reverse thrust due to the electric failure. Unable to stop withing the remaining distance, the aircraft overran and eventually plunged into the Bay of Thorofare. All eight occupants were quickly rescued while the aircraft was lost.
Probable cause:
Failure of the electric system in flight.

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 a Lockheed L-1049E-55 Super Constellation in Montego Bay: 37 killed

Date & Time: Jan 21, 1960
Operator:
Registration:
HK-177
Survivors:
Yes
Schedule:
New York – Montego Bay – Barranquilla – Bogotá
MSN:
4556
YOM:
1954
Flight number:
AV671
Country:
Crew on board:
7
Crew fatalities:
Pax on board:
39
Pax fatalities:
Other fatalities:
Total fatalities:
37
Circumstances:
Avianca Flight 671, a Lockheed Super Constellation, took off from New York-Idlewild for a flight to Bogotá via Montego Bay and Barranquilla. En route to Montego Bay, the no. 3 engine malfunctioned and was stopped. The flight diverted to Miami, arriving there at 16:57. A replacement propeller governor was fitted, but during pre-flight checks a further defect in the no. 2 engine was found. This was rectified and the flight departed Miami at 00:12, the copilot being the pilot flying. Upon arrival near Montego Bay, clearance was given for a standard instrument approach. The airfield was sighted following the procedure turn at 2,000 feet and the approach was continued visually. Following a heavy touchdown, the plane bounced and landed back on the runway and skidded down the runway in flames, coming to rest inverted, 1,900 feet from the runway threshold and 200 feet to the left. Five crew members and four passengers survived while 37 other occupants were killed. The airplane was destroyed by fire.
Probable cause:
The adoption of a final approach path resulting in a heavy landing during which a major structural failure occurred in the port wing in the immediate vicinity of Station 80 joint caused by the transmission of stresses through the undercarriage in excess of those which would be encountered if the rate of sink of the aircraft at the time of impact had been controlled within the designed maximum of 10 feet per second. The primary responsibility for the safety of an aircraft and its complement is vested in the captain. However, there is evidence of mitigating circumstances in that the errors of judgement that precipitated the disaster reflect some deficiency of knowledge which should have been instilled in the training and flight proficiency checking of the pilots of HK-177. A measure of responsibility for the accident must, therefore, devolve on the supervisory and advisory authorities for the overall conduct of the operation.

Crash of a Douglas DC-6A/B in Shannon

Date & Time: Jun 22, 1959
Type of aircraft:
Operator:
Registration:
N5026K
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Shannon – New York
MSN:
44426
YOM:
1954
Location:
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Immediately after applying takeoff power, the crew of the DC-6 heard a loud noise and the takeoff was abandoned. A visual check before the plane stopped revealed that the no. 4 engine had separated from the wing. A fire erupted and spread after evacuation, destroying the aircraft. It appeared that the no. 4 propeller had failed and that the unbalanced loads on the engine mounts caused separation of the entire engine. All crew and passengers survived but six dogs the cargo hold died in the accident.
Probable cause:
The accident was caused by fatigue failure of No.1 blade of No.4 propeller. Laboratory findings showed that the failure was caused by previous blade bending resulting in the disruption of the compressive stresses in the shot peened area of the propeller blade.

Crash of a Lockheed L-1049E-55 Super Constellation off New York: 74 killed

Date & Time: Jun 20, 1956 at 0132 LT
Operator:
Registration:
YV-C-AMS
Flight Phase:
Survivors:
No
Schedule:
New York – Caracas
MSN:
4561
YOM:
1954
Flight number:
LV253
Crew on board:
10
Crew fatalities:
Pax on board:
64
Pax fatalities:
Other fatalities:
Total fatalities:
74
Circumstances:
The four engine christened 'Rafael Urdaneta' departed New York-Idlewild Airport at 2306LT and proceeded to the south. One hour and twenty minutes later, while flying along the US coast, the crew contacted ground and received the permission to return to New York following the failure of the number two engine. The crew was unable to feather the propeller and the aircraft suffered severe vibrations. Ten minutes later, while the crew was trying to dump the fuel, a fire erupted. The aircraft went out of control, dove into the sea and crashed about 40 miles southeast of New York. The airplane disintegrated on impact and all 74 occupants were killed.
Probable cause:
Although the accident was observed by witnesses, its cause cannot be determined with absolute certainty. However, it would be logical to assume that the vibration which resulted from the loss of control of propeller no.2 caused one of the inside wing attachments to loosen or break at some point between the fuel tank and the dump chute at the symmetrical point of vibration (behind engine no.3).
Final Report:

Crash of a De Havilland DH.104 Dove 2A in Grove City: 2 killed

Date & Time: Aug 30, 1953
Type of aircraft:
Registration:
N4962N
Flight Type:
Survivors:
No
Schedule:
New York – Grove City
MSN:
04326
YOM:
1952
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The twin engine aircraft was completing a flight from New York City to Grove City. On approach, it crashed in unknown circumstances in a field, killing both occupants, a pilot and his passenger.