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 Boeing KC-97G Stratotanker on Mt Big Shanty: 7 killed

Date & Time: Jan 22, 1957 at 1930 LT
Type of aircraft:
Operator:
Registration:
53-0222
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Westover - Griffiss
MSN:
17004
YOM:
1953
Flight number:
Crony 14
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
The airplane was on a refueling mission and departed Westover AFB at 1330LT bound for Griffiss AFB, Rome, New York. Following an uneventful mission, the crew started the descent to Griffiss AFB but was instructed to follow a holding pattern because a fighter that was short of fuel must land immediately. Twenty-five minutes later, while cruising in poor weather conditions (freezing rain and snow), the airplane struck the snowy Mt Big Shanty (701 meters high) located about 70 miles northeast of Griffiss AFB, in the Adirondack Mountain Range. Rescuers arrived on scene in the early morning of January 24. All seven crew members have been killed, among them Maj Charles D. Mellinger, pilot, and 1st Lt Fred Defrench, copilot.

Crash of a Douglas DC-3 in New York: 1 killed

Date & Time: Jan 19, 1957
Type of aircraft:
Operator:
Registration:
N33374
Flight Phase:
Survivors:
No
MSN:
4369
YOM:
1942
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
Parked at Idlewild Airport, the aircraft was stolen by a technician who was able to takeoff. During initial climb, at an altitude of 150 feet, the airplane stalled and crashed near the runway. The aircraft was destroyed and the 'pilot' was killed.

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 Lockheed PV-1 Ventura near Smithtown: 3 killed

Date & Time: Jan 26, 1956 at 1633 LT
Type of aircraft:
Registration:
N2000C
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Ronkonkoma - Ronkonkoma
MSN:
5243
YOM:
1943
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
800
Captain / Total hours on type:
600.00
Aircraft flight hours:
2216
Circumstances:
N2000C took off at 1625 on January 26, 1956, from MacArthur Field, Ronkonkoma, Long Island, New York, its home base, on a local flight with three pilots. They were Bernard J. Malloy, check pilot, and Pilots Raymond Hamberg and Hugo D. Filangeri. The purpose of the flight was to qualify Pilot Hamberg on the Lockheed PV-1 aircraft, a type he had never piloted. The takeoff of N 2000C was normal, toward the northwest, and made under VFR (Visual Flight Rules) conditions with Pilot Hamberg occupying the left or captain's to scat and Pilot Malloy, as check pilot, seated on the right as copilot; Pilot Filangeri acted as observer. Subsequently the PV-1 was seen over the Smithtown area, flying westerly at an estimated altitude of 2,500-3,000 feet, where a witness reported that the engines sounded normal but that the aircraft appeared to be flying at a slow airspeed. Witnesses stated that shortly thereafter the engine power sounded as though it was cut momentarily and then came back on. At an altitude of approximately 2,000 feet the aircraft was seen to dip down and pull up, slightly nose-high, and then fall off to the left, making two to three turns of a descending spiral, and disappear behind the tree-topped horizon. Flames erupted frost the woods over the point where the aircraft was last seen, followed quickly by a large column of black smoke. All three pilots were killed.
Probable cause:
The Board determines that the probable cause of this accident loss of control resulting in a stall at an altitude too low to effect recovery. The following findings were reported:
- Weather was not a major factor,
- The altitude probably did not exceed 3,500 feet above the ground during the eight minutes the aircraft wan in the air,
- There wan no fire prior to impact,
- There was no evidence of failure of the airframe or malfunction of controls as far as could be drained,
- There was no evidence of power failure of either engine,
- The purpose of the flight was pilot familiarization and included slow flight,
- The aircraft was observed to stall at low airspeed approximately 2,000-2,500 feet above the ground.
Final Report:

Crash of a Douglas A-26C-45-DT Invader at Mitchel AFB: 3 killed

Date & Time: Nov 2, 1955
Type of aircraft:
Operator:
Registration:
44-35737
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Mitchel - Mitchel
MSN:
29016
YOM:
1944
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
While completing a local training flight at Mitchel AFB, the aircraft went out of control and crashed in unknown circumstances in East Meadow, near the airbase. The aircraft was destroyed by impact forces and a post crash fire and all three crew members were killed.

Crash of a North American TB-25N Mitchell at Mitchel AFB: 6 killed

Date & Time: Sep 13, 1955 at 0830 LT
Operator:
Registration:
45-8822
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Mitchel – Wright-Patterson
MSN:
108-47673
YOM:
1945
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
Shortly after takeoff from Mitchel AFB, while climbing to a height of about 300 feet, the crew informed ground about the failure of the right engine. The crew elected to make an emergency landing when the aircraft crashed in a cemetery in Uniondale, bursting into flames. All six occupants were killed.
Crew:
Maj James D. Judy, pilot,
Cpt Richard E. Hall.
Passengers:
Lt Col Morris I. Fass,
S/Sgt John I. Jackson Jr.,
Lee Rogow,
Larry J. Rubrecht.
Probable cause:
Failure of the right engine for unknown reasons.

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:

Crash of a Douglas A-26C-50-DT Invader in Georgetown: 3 killed

Date & Time: Jan 20, 1955
Type of aircraft:
Operator:
Registration:
44-35793
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Griffiss - Turner
MSN:
29072
YOM:
1944
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The crew was completing a flight from Griffiss AFB (Rome) to Turner AGB located in Albany. Enroute, the twin engine aircraft crashed in unknown circumstances in a field located in Georgetown, killing all three crew members.

Crash of a Douglas DC-6B in New York: 26 killed

Date & Time: Dec 18, 1954 at 1400 LT
Type of aircraft:
Operator:
Registration:
I-LINE
Survivors:
Yes
Schedule:
Rome – Milan – Paris – Shannon – Gander – Boston – New York
MSN:
44418
YOM:
1954
Flight number:
LAI451
Crew on board:
10
Crew fatalities:
Pax on board:
22
Pax fatalities:
Other fatalities:
Total fatalities:
26
Captain / Total flying hours:
14734
Captain / Total hours on type:
3356.00
Copilot / Total flying hours:
7546
Copilot / Total hours on type:
3670
Aircraft flight hours:
1424
Circumstances:
After an uneventful instrument flight involving no Air Route Traffic Control routing and control, Flight 451 reported at 1122 to the Idlewild Approach Control as being aver the Mitchell Radio Range Station at 7,000 feet. The flight was then cleared to enter the Scotland holding pattern (located approximately 13 nautical miles southwest of the airport) and was subsequently "laddered down" to the number one position to approach. Between 1147 and 1159 weather conditions deteriorated below the ceiling minimum of 400 feet for landing on runway 22, the runway then in use. The flight continued to hold. At 1159 reported weather conditions improved and I-LINE was cleared for an approach to runway 22 using the back course of the ILS (Instrument Landing System). At 1218 the flight reported it had discontinued this approach. It was then issued missed-approach instructions and returned to the Scotland holding pattern. Shortly thereafter weather conditions were again reported below minimums for runway 22. They were then reported as: Ceiling 300 feet, broken, 2,500 feet, overcast; visibility 2-1/2 miles, light rain and fog; wind south-southeast 20 knots. While holding, the flight was asked by Approach Control if it would be able to make an approach to runway 4, the ILS runway, considering the tailwind component. The flight accepted runway 4 and was cleared at 1307 for an ILS approach. At 1313 the tower was advised by 451 that the approach had been missed. The flight was next offered, and it accepted, a GCA (Ground Controlled Approach). This approach was abandoned at 1324, a missed-approach procedure was followed, and the flight returned to Scotland. At 1327 the Italian Airlines Station Manager, in a message relayed by the tower, asked the flight its remaining fuel, and received the reply that there was three hours of holding fuel. The Station Manager then suggested that the flight hold for 1-1/2 hours and if unable to land to proceed to Washington, D. C. At 1329 the flight acknowledged this message. At 1349 the flight was again cleared for an ILS approach, the third approach to runway 4 and its fourth to the airport. At approximately 1400 the aircraft struck the left pier. The impact was accompanied by a violent explosion and followed by an intense fire. Tower personnel immediately sounded the crash alarm and initiated emergency procedures. At the time of the accident weather conditions were reported as: Ceiling 200 overcast; visibility 2-1/2 miles, light rain and fog; wind south-southeast 16 knots. Italian Airlines' minimums for ILS approaches to runway 4 are ceiling 200 feet and visibility 1/2 mile. The aircraft was destroyed and all 10 crew members and 16 passengers were killed, six others were injured.
Probable cause:
The Board determines that the probable cause of this accident was an erratic approach which resulted in a descent to an altitude too low to avoid striking the pier. A contributing factor to this accident was pilot fatigue due to the particular and difficult circumstances. The following findings were reported:
- The flight made four instrument approaches to the Idlewild Airport, one to runway 22 and three to runway 4,
- The three approaches to runway 4 were made with a downwind component approximately 8 knots,
- There were no language difficulties between the flight crew and control personnel,
- Prior to the last approach weather and altimeter information was given the flight,
- The weather information was adequate for the normal ILS breakout area,
- Radar advisories were given the flight during the ILS approaches and during the last approach the flight was repeatedly advised that it was low with respect to normal ILS altitudes,
- The last approach was apparently made without using the ILS glide path,
- The radio navigational and landing facilities for the airport were functioning normally,
- When the aircraft struck the pier it was nearly level laterally, slightly nose-high, and without appreciable descent,
- Approximately 80 percent of the wreckage was recovered, the examination of which revealed no structural or mechanical failure of the power units, propellers, airframe, controls, or instruments prior to impact,
- The crew reported no mechanical or other difficulty.
Final Report: