Crash of a Lockheed L-188A Electra in LaGuardia

Date & Time: Sep 14, 1960 at 0800 LT
Type of aircraft:
Operator:
Registration:
N6127A
Survivors:
Yes
Schedule:
Boston – New York – Saint Louis
MSN:
1117
YOM:
1960
Flight number:
AA361
Crew on board:
6
Crew fatalities:
Pax on board:
70
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
14082
Captain / Total hours on type:
279.00
Copilot / Total flying hours:
18310
Copilot / Total hours on type:
460
Aircraft flight hours:
1573
Circumstances:
The Electra scheduled as Flight 361 departed Boston at 0716LT with its destination St Louis, Missouri, and with a planned intermediate stop at LaGuardia Airport. About ten minutes prior to departure a crew change was made when a check pilot boarded the aircraft to flight-check the flight engineer. This check pilot, by mutual agreement with the crew and in accordance with existing company policy, took over the left or pilot-in-command seat with the previously assigned captain moving to the jump seat. The trip was routine until final approach at LaGuardia. On final approach, the airplane aircraft was too low and struck a dyke with its main landing gear and crash landed. Approximately half of the 76 persons on board suffered minor injuries or shock; no one was killed. The aircraft was severely damaged by impact forces and fire.
Probable cause:
The Board determines that the probable cause of this accident was the failure of the pilot to properly plan and execute the approach to a landing. Factors which may have contributed were the shortened runway and the unmarked upper portion of the dike.
Final Report:

Crash of a Boeing 707-123 in Calverton: 5 killed

Date & Time: Aug 15, 1959 at 1642 LT
Type of aircraft:
Operator:
Registration:
N7514A
Flight Type:
Survivors:
No
Schedule:
Calverton - Calverton
MSN:
17641
YOM:
1959
Flight number:
AA514
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
18000
Captain / Total hours on type:
210.00
Copilot / Total flying hours:
22498
Copilot / Total hours on type:
9
Aircraft flight hours:
736
Circumstances:
The crew was completing a local training flight at Calverton-Peconic River Airport, Long Island, New York. While approaching runway 23 at an altitude of 1,000 feet, the airplane yawed to the right, stalled and crashed in a field located three miles from the airport. The airplane disintegrated on impact and all five crew members were killed.
Probable cause:
The Board determines the probable cause of this accident was the crew's failure to recognize and correct the development of excessive yaw which caused an unintentional rolling maneuver at an altitude too low to permit complete recovery.
Final Report:

Crash of a Lockheed L-188A Electra in New York: 65 killed

Date & Time: Feb 3, 1959 at 2356 LT
Type of aircraft:
Operator:
Registration:
N6101A
Survivors:
Yes
Schedule:
Chicago – New York
MSN:
1015
YOM:
1958
Flight number:
AA320
Crew on board:
5
Crew fatalities:
Pax on board:
68
Pax fatalities:
Other fatalities:
Total fatalities:
65
Captain / Total flying hours:
28135
Captain / Total hours on type:
48.00
Copilot / Total flying hours:
10192
Copilot / Total hours on type:
36
Aircraft flight hours:
302
Circumstances:
At approximately 2356LT, the aircraft crashed into the East River while attempting an instrument approach to runway 22 at LaGuardia Airport. There were 73 persons on board, including one infant. The captain and one stewardess were killed; the first officer, flight engineer, and the remaining stewardess survived. Of the 68 passengers, 5 survived. The Board believes that a premature descent below landing minimums was the result of preoccupation of the crew on particular aspects of the aircraft and its environment to the neglect of essential flight instrument references for attitude and height above the approach surface. Contributing factors were found to be: limited experience of the crew with the aircraft type, fealty approach technique in which the autopilot was used in the heading mode to or almost to the surface, erroneous setting of the captain's altimeter, marginal weather in the approach area, possible misinterpretation of altimeter and rate of descent indicator, and sensory illusion with respect to height and attitude resulting from visual reference to the few lights existing in the approach area.
Probable cause:
The Board determines the probable cause of this accident was premature descent below landing minimums which was the result of preoccupation of the crew on particular aspects of the aircraft and its environment to the neglect of essential flight instrument references for attitude and height above the approach surface. Contributing factors were:
- Limited experience of the crew with the aircraft type,
- Faulty approach technique in which the autopilot was used in the heading mode to or almost to the surface,
- Erroneous setting of the captain's altimeter,
- Marginal weather in the approach area,
- Possible misinterpretation of altimeter and rate of descent indicator,
- Sensory illusion with respect to height and attitude resulting from visual reference to the few lights existing in the approach area.
Final Report:

Crash of a Vickers 724 Viscount in New York

Date & Time: Nov 10, 1958 at 1101 LT
Type of aircraft:
Operator:
Registration:
CF-TGL
Flight Phase:
Survivors:
Yes
Schedule:
New York - Montreal
MSN:
43
YOM:
1955
Flight number:
TCA604
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The Viscount was parked at gate to board passengers when it was struck by a Seaboard & Western Airlines' Lockheed L-1049D Super Constellation which was performing training flight LN800 at Idlewild Airport. The Constellation began its takeoff run on runway 31R of the New York International Airport at 1100. When an airspeed of 117 knots (V 2) was reached, the aircraft became airborne and climbed to an altitude of approximately 25 feet. At this altitude severe control difficulty was encountered, causing the aircraft to veer suddenly to the left and the left wing to lower 20 to 30 degrees. This wing struck the runway and from this point on directional control of the aircraft was lost. The aircraft skidded In a westerly direction into a temporary terminal area and came to rest after striking the Viscount. All five crew members from the Constellation were injured while the Viscount was empty. Both aircraft were totally destroyed by fire.
Probable cause:
The Board determines that the probable cause of this accident was an unwanted propeller reversal at a low altitude occurring immediately after takeoff. A contributing factor was the inadequate overhaul procedure employed by the propeller manufacturer.
Final Report:

Crash of a Lockheed L-1049D Super Constellation in New York

Date & Time: Nov 10, 1958 at 1101 LT
Operator:
Registration:
N6503C
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
New York - New York
MSN:
4165
YOM:
1954
Flight number:
LN800
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
12652
Captain / Total hours on type:
1634.00
Copilot / Total flying hours:
13642
Copilot / Total hours on type:
2488
Aircraft flight hours:
11980
Circumstances:
Seaboard & Western's Flight LN-800, a training flight, began its takeoff run on runway 31R of the New York International Airport at 1100. When an airspeed of 117 knots (V 2) was reached, the aircraft became airborne and climbed to an altitude of approximately 25 feet. At this altitude severe control difficulty was encountered, causing the aircraft to veer suddenly to the left and the left wing to lower 20 to 30 degrees. This wing struck the runway and from this point on directional control of the aircraft was lost. The aircraft skidded In a westerly direction into a temporary terminal area and came to rest after striking a parked Trans Canada Air Lines Vickers 724 Viscount. All five crew members were injured while the Viscount was empty.
Probable cause:
The Board determines that the probable cause of this accident was an unwanted propeller reversal at a low altitude occurring immediately after takeoff. A contributing factor was the inadequate overhaul procedure employed by the propeller manufacturer.
Final Report:

Crash of a Fairchild C-123B-6-FA Provider at Mitchel AFB: 1 killed

Date & Time: Oct 15, 1958
Type of aircraft:
Operator:
Registration:
54-0614
Flight Type:
Survivors:
Yes
Schedule:
Mitchel - Mitchel
MSN:
20063
YOM:
1954
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The crew as completing a local night training mission at Mitchel AFB. After touchdown, the airplane encountered difficulties to stop within the remaining distance, overran, went through a fence and a road, colliding with three cars before coming to rest. All four crew members were injured and the aircraft was damaged beyond repair. On the ground, one driver was killed while four other people were also injured.

Crash of a Martin 404 in Massena

Date & Time: Nov 14, 1957 at 1530 LT
Type of aircraft:
Operator:
Registration:
N492A
Survivors:
Yes
Schedule:
New York – Albany – Plattsburgh – Malone – Massena
MSN:
14240
YOM:
1952
Flight number:
EA0183
Crew on board:
3
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
11870
Captain / Total hours on type:
535.00
Copilot / Total flying hours:
738
Copilot / Total hours on type:
155
Aircraft flight hours:
15617
Circumstances:
Eastern Air Lines Flight 18 is a scheduled operation serving the carrier's route between New York City and Massena, New York, and its intermediate stops at Albany, Plattsburg, and Malone, New York. On November 14, at 1245, the flight originated on schedule, its flight crew consisting of Captain Joseph W. Harpham, First Officer Robert Casper and Flight Attendant Nancy A. Price. The flight followed routine preparation and was in accordance with an IFR (Instrument Flight Rules) flight plan. The general weather conditions over most of the route were forecast to be good. The flight proceeded through the intermediate stops in a routine manner, with most passengers deplaning at Albany and Flattsburg. Just prior to reaching Malone the instrument flight plan was canceled in good weather conditions. The flight landed at Malone at 1502. Continuing uneventfully, Flight 18 departed Malone at 1510. The gross takeoff weight of the Martin 404 was 35,977 pounds, 8,923 pounds under the maximum allowable. According to the load manifest the load was properly distributed within the center of gravity limitations. The first officer made the takeoff, climbed the aircraft approximately 2,500 feet, and flew it to Massena. Captain Harpham from his left seat, supervised the flight and performed the duties of copilot. At 1516, when about eight miles east of Richards Field, Captain Harpham reported the flight's position, then asked for and received landing information, which included the surface wind as “northeast 5 to 10 knots," and the active runway 4 (150 feet wide and 4,000 feet long). First Officer Casper established a downwind leg at 1,200 feet to execute a rectangular left-hand pattern for landing on runway 4. The flight was viewed briefly by ground observers during the pattern before reaching the final landing approach and it seemed entirely normal. As the aircraft drew closer to the threshold it seemed high and thereafter assumed an abnormally steep descent. As it approached the runway surface the aircraft assumed a flareout attitude, however, the rate of descent continued with little visible abatement. Consequently, N492A contacted the runway surface with great force at which time the right powerplant separated from the aircraft. The aircraft rebounded and again contacted with great force. It then rolled forward and gradually off the runway to the right. Before stopping it crossed a taxiway and the left powerplant fell free, accompanied by a small fire in the engine and the empty nacelle area. As the aircraft stopped Captain Harpham shut off the fuel and electrical services and ordered the loading ramp lowered. The passengers and crew quickly evacuated by this exit without difficulty or reported injury. At 1522, two minutes after the accident, weather conditions were reported as: Ceiling 4,000 feet broken, 10,000 feet, overcast; visibility 3 miles; haze; wind northeast 6 knots.
Probable cause:
The Board determines that the probable cause of this accident was the captain's incorrect technique during the final approach which resulted in an abnormally steep nose-down attitude and high rate of descent, the latter not being sufficiently arrested before touchdown. The following findings were reported:
- The first officer operated the aircraft in the traffic pattern,
- During the turn to the base leg and while on base leg, an overriding was allowed to drift the aircraft closer to the airport,
- From a higher and closer than normal position on final approach, the captain took control of the aircraft and continued the approach,
- The throttles were closed, landing flap was extended, and the aircraft was slowed to 95 knots,
- The aircraft descended in an abnormally steep nose-down attitude and at a high rate of descent,
- The altitude remaining was insufficient for the aircraft in its existing configuration to regain adequate flareout speed,
- The flareout attitude was accomplished; however, the rate of descent continued with little abatement,
- The aircraft contacted the runway with great force causing major structural damage,
- Important limits in the approach technique were not included as part of company pilot training,
- There was no malfunction or failure of the aircraft prior to the runway contact.
Final Report:

Crash of a Douglas C-124 Globemaster II in Binghamton

Date & Time: Sep 4, 1957
Operator:
Registration:
51-5173
Flight Type:
Survivors:
Yes
Schedule:
Larson - Binghamton
MSN:
43583
YOM:
1951
Crew on board:
9
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The approach to Binghamton Airport was completed at an insufficient altitude. On short final, the aircraft struck a concrete wall. Upon impact, the undercarriage were torn off and the aircraft crash landed. There were no casualties but the aircraft was written off.

Crash of a Grumman HU-16E in Floyd Bennett Field: 4 killed

Date & Time: Aug 22, 1957
Operator:
Registration:
1259
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Floyd Bennett Field - Floyd Bennett Field
MSN:
G-106
YOM:
1952
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
The crew was performing a test flight after the aircraft had undergone an intermediate inspection in which the control columns were removed and inspected for fatigue cracks in the bottom casting. The plane was cleared for take-off and instructed to turn right immediately after take-off to avoid other traffic. Take-off was normal but immediately after leaving the runway the plane banked slightly to the left, hesitated, and then banked and then banked very rapidly to the left until it was in a 90° bank. The left wing tip struck the ground and the plane broke in two and crashed. Four crew members were killed while two others were injured.
Those killed were:
Lcdr Claude S. Labaw,
Lt Rolland A. Faucher,
AD3 Matthew R. Ross,
AT3 Gerald R. Fox.
Probable cause:
The Accident Board was not able to determine the cause of this accident but certain items all pointed strongly toward reversed aileron control cable rigging as the most probably cause.

Crash of a Boeing KC-97G-28-BO Stratotanker off Plattsburgh: 5 killed

Date & Time: Jul 18, 1957
Type of aircraft:
Operator:
Registration:
52-2737
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
16768
YOM:
1952
Crew on board:
8
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
Shortly after takeoff from runway 17 at Plattsburgh Airport, while climbing, the airplane lost height, stalled and crashed into Lake Champlin. Three crew members were rescued while five others were killed.
Probable cause:
The accident was the consequence of a loss of power on two engines simultaneously.