Crash of a Douglas C-124C Globemaster II in Palm Beach: 3 killed

Date & Time: Aug 21, 1956
Operator:
Registration:
52-1005
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Palm Beach - Palm Beach
MSN:
43914
YOM:
1952
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The crew was completing touch-and-goes at Palm Beach Airport. After takeoff, while climbing, a technical issue occurred on the engine number two that lost a propeller blade which penetrated the fuselage, cutting several control cables. Engines number three and four stopped immediately, causing the aircraft to bank right and to crash in a tree nursery. Three crew members were killed while three others were injured. The aircraft was destroyed.
Probable cause:
Loss of a propeller blade on engine number two.

Crash of a Fairchild C-82A-20-FA Packet in Boca Raton: 5 killed

Date & Time: Aug 8, 1956 at 0505 LT
Type of aircraft:
Operator:
Registration:
N4832V
Survivors:
No
Schedule:
Miami - Boca Raton
MSN:
10070
YOM:
1944
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
4976
Captain / Total hours on type:
186.00
Copilot / Total flying hours:
3179
Copilot / Total hours on type:
170
Aircraft flight hours:
1016
Circumstances:
N4832V departed Masters Field, Miami, Florida, for Boca Raton Airport at 0448, August 8, 1956. Aboard the aircraft were Pilot Charles W. Day, Copilot Rae F. Howry, and three company insecticide-mixer personnel. The purpose of the direct 36-mile flight was the movement of the aircraft, crew and mixer personnel to the Boca Raton Airport from which the spraying operation was to be conducted. The takeoff of N4832V was followed immediately by another company operated C-82, N4829V and the two aircraft proceeded at an altitude of approximately 500 feet. N4829V flew to the left, slightly above and to the rear of N4832V until reaching Boca Raton. Both aircraft arrived over the city of Boca Raton shortly after 0500 and proceeded north and west the mile or so to the airport. Dawn was breaking and the runways, although unlighted, were plainly visible. N4832V made a eight turn for approach to runway 04. After passing over more than one-third of the length of the 5,000-foot runway a go-around was initiated. The aircraft then Immediately went into a climbing left turn. During this turn the aircraft stalled and crashed, killing all five occupants.
Probable cause:
The Board determines that the probable cause of this accident ins loss of power on the left engine and the drag-induced effect of the unfeathered left propeller, resulting in loss of directional control daring an attempted go-around. The following findings were reported:
- During approach to the airport serious malfunctioning of the left engine occurred,
- An improperly planned final approach resulted in runway misalignment and necessitated a go-around,
- During the attempted go-around the left engine rear master rod bearing failed resulting in loss of power on the left engine,
- The propeller was not feathered for single-engine operation,
- The lack of left engine power at low at low airspeed, and the drag resulting from the unfeathered left propeller resulted in loss of directional control,
- During the resulting left turn the aircraft was stalled and entered an "over-the-top" spin.
Final Report:

Crash of a Douglas C-118A Liftmaster at McGuire AFB: 46 killed

Date & Time: Jul 13, 1956 at 1537 LT
Type of aircraft:
Operator:
Registration:
53-3301
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
McGuire – Stephenville – Lakenheath
MSN:
44672
YOM:
1955
Flight number:
A441/13
Crew on board:
10
Crew fatalities:
Pax on board:
56
Pax fatalities:
Other fatalities:
Total fatalities:
46
Captain / Total flying hours:
4183
Captain / Total hours on type:
1137.00
Copilot / Total flying hours:
1454
Copilot / Total hours on type:
642
Circumstances:
The Liftmaster was engaged in a transatlantic flight from McGuire (Fort Dix) Airbase to Lakenheath, UK, with an intermediate stop at Stephenville. Less than two minutes after takeoff from McGuire AFB runway 24, while climbing, the four engine aircraft encountered poor weather conditions, stalled and crashed in a dense wooded area located 1,4 mile from the airfield. Eight crew members and 38 passengers, among them civilians, were killed while 20 other occupants were injured.
Probable cause:
It was reported that weather conditions were poor at the time of the accident with thunderstorm activity around the McGuire Airbase, a horizontal visibility of 1,500 meters, clouds from 600 to 1,800 feet and wind gusting up to 30 knots with turbulences. The assumption that the aircraft encountered strong downdraft caused by a micro-burst was not ruled out.

Crash of a De Havilland DH.104 Dove in Moses Point: 1 killed

Date & Time: Jul 2, 1956
Type of aircraft:
Operator:
Registration:
N26W
Flight Phase:
Survivors:
No
MSN:
04352
YOM:
1952
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
Crashed in unknown circumstances, killing the pilot, sole occupant.

Crash of a Douglas DC-7 in the Grand Canyon: 58 killed

Date & Time: Jun 30, 1956 at 1032 LT
Type of aircraft:
Operator:
Registration:
N6324C
Flight Phase:
Survivors:
No
Site:
Schedule:
Los Angeles – Chicago – New York
MSN:
44288
YOM:
1955
Flight number:
UA718
Crew on board:
5
Crew fatalities:
Pax on board:
53
Pax fatalities:
Other fatalities:
Total fatalities:
58
Captain / Total flying hours:
16492
Captain / Total hours on type:
1238.00
Copilot / Total flying hours:
4540
Copilot / Total hours on type:
230
Aircraft flight hours:
5115
Circumstances:
United Air Lines Flight 718 was regularly scheduled from Los Angeles to Chicago, Illinois. On June 30, 1956, it took off from runway 25L (left) of the Los Angeles International Airport at 0904 (three minutes after TWA 2). Flight 718 was on an IFR flight plan to Chicago via Green Airway 5 Palm Springs inter-section, direct Needles, direct Painted Desert, direct Durango, direct Pueblo, direct St. Joseph. Victor Airway 116 Joliet, Victor Airway 84 Chicago Midway Airport. The flight plan proposed a .JPG"> airspeed of 288 knots., a cruising altitude of 21,000 feet, and a departure time of 0845. The flight crew consisted of Captain Robert F. Shirley, First Officer Robert W. Harms, Flight Engineer Gerard Flore, and Stewardesses Nancy L. Kemnitz and Margaret A. Shoudt. Flight preparations and dispatch of United 718 were routine and the aircraft departed with 3,850 gallons of fuel. The company load manifest showed the gross weight of the aircraft at takeoff to be 105,835 pounds, which was less than the maximum allowable of 114,060 pounds; the latter weight was restricted from a maximum of 122,200 pounds for the aircraft because of a landing limitation at Chicago. The load was properly distributed with respect to the center of gravity limitations of the aircraft. After takeoff the flight contacted the Los Angeles tower radar controller, who vectored it through the overcast over the same departure course as TWA 2. United 718 reported "on top" and changed to Los Angeles Center frequency for its en route clearance. This corresponded to the flight plan as filed; however, the controller specified that the climb to assigned altitude be in VER conditions. Flight 718 made position reports to Aeronautical Radio, Inc., which serves under contract as United company radio. It reported passing over Riverside and later over Palm Springs intersection. The latter report indicated that United 718 was still climbing to 21,000 and estimated it would reach Needles at 1000 and the Painted Desert at 1034. At approximately 0958 United 718 made a position report to the CAA communications station located at Needles. This report stated that the flight was over Needles at 0958, at 21,000 feet, and estimated the Painted Desert at 1031, with Durango next. At 1031 an unidentified radio transmission was heard by Aeronautical Radio communicators at Salt Lake City and San Francisco. They were not able to understand the message when it was received but it was later determined by playing back the recorded transmission that the message was from United 718. Context was interpreted as: "Salt Lake, United 718 . . . ah . . . we're going in."
Probable cause:
The Board determines that the probable cause of this mid-air collision was that the pilots did not see each other in time to avoid the collision. It is not possible to determine why the pilots did not see each other, but the evidence suggests that it resulted from any one or a combination of the following factors: Intervening clouds reducing time for visual separation, visual limitations due to cockpit visibility, and preoccupation with normal cockpit duties, preoccupation with matters unrelated to cockpit duties such as attempting to provide the passengers with a more scenic view of the Grand Canyon area, physiological limits to human vision reducing the time opportunity to see and avoid the other aircraft, or insufficiency of en route air traffic advisory information due to inadequacy of facilities and lack of personnel in air traffic control. The following findings were reported:
- Approaching Daggett, TWA 2 requested its company radio to obtain 21,000 feet as an assigned altitude, or 1,000 on top,
- Company radio requested 21,000 feet IFR from ARTC. This vas denied by ARTC. Request was then made for 1,000 on top. This was approved and clearance issued. The flight climbed to and proceeded at 21,000 feet,
- As an explanation for the denial of 21,000 feet, TWA 2 was furnished pertinent information on UA718,
- The last position report by each flight indicated it was at that time at 21,000, estimating the Painted Desert line of position at 1031,
- The Salt Lake controller possessed both position reports at approximately 1013, at which time both flights were in uncontrolled airspace,
- Traffic control services are not provided in the uncontrolled airspace and according to existing Air Traffic Control policies and procedures the Salt Lake controller was not required to issue traffic information; none was issued voluntarily,
- A general overcast with some breaks existed at 15,000 feet in the Grand Canyon area,
- Several cumulus buildups extending above flight level existed; one was nearly over Grand Canyon Village and others were north and northeast in the area of the collision,
- The collision occurred at approximately 1031 in visual flight rule weather conditions at about 21,000 feet,
- The collision in space was above a position a short distance west of the TWA wreckage area, 17 miles west of or approximately 3-1/2 minutes' flying time from the Painted Desert line of position,
- Under visual flight rule weather conditions it is the pilot's responsibility to maintain separation from other aircraft,
- At impact the aircraft relative to each other converged at an angle of about 25 degrees with the DC-7 to the right of the L-1049. The DC-7 was rolled about 20 degrees right wing down and pitched about 10 degrees nose down relative to the L-1049,
- There was no evidence found to indicate that malfunction or failure of the aircraft or their components was a factor in the accident.
Final Report:

Crash of a Lockheed L-1049 Super Constellation in the Grand Canyon: 70 killed

Date & Time: Jun 30, 1956 at 1031 LT
Operator:
Registration:
N6902C
Flight Phase:
Survivors:
No
Site:
Schedule:
Los Angeles – Kansas City – Washington DC
MSN:
4016
YOM:
1952
Flight number:
TW002
Crew on board:
6
Crew fatalities:
Pax on board:
64
Pax fatalities:
Other fatalities:
Total fatalities:
70
Captain / Total flying hours:
14922
Captain / Total hours on type:
7208.00
Copilot / Total flying hours:
6976
Copilot / Total hours on type:
825
Aircraft flight hours:
10519
Circumstances:
On June 30, 1956, at 0901, Trans World Airlines Flight 2, a regularly scheduled passenger service, took off from runway 25 of the Los Angeles Inter-national Airport. Flight 2 was on an instrument flight rules (IFR) flight plan from Los Angeles, California, to Kansas City, Missouri, via Green Airway 5, Amber Airway 2, Daggett direct Trinidad, direct Dodge City, Victor Airway 10 Kansas City. The flight plan also proposed a cruising altitude of 19,000 feet, a .JPG"> airspeed of 270 knots, and a departure time of 0830. The Trans World flight crew consisted of Captain Jack S. Gandy, Copilot James H. Ritner, Flight Engineer Forrest D. Breyfogle, night Engineer Harry H. Allen (aboard as an additional crew member), and Hostesses Tracine E. Armbruster and Beth E. Davis. Preparations for Flight 2 were routine except that departure was delayed a few minutes by minor maintenance on the aircraft. The flight was dispatched with 3,300 gallons of fuel and the load manifest showed the gross weight of the aircraft at takeoff was 108,115 pounds, well, under the maximum allowable of 113,200 pounds. The load was properly distributed with respect to center of gravity limitations of the aircraft. As requested. the flight, after takeoff, contacted the Los Angeles tower radar departure controller, and was vectored through an overcast which existed in the Los Angeles area. After reporting "on top" (2,400 feet) the flight switched to Los Angeles Air Route Traffic Control Center (referred to as Los Angeles Center) frequency, 118.9 mcs., for its en route clearance. This clearance specified the routing as filed in the flight plan, however, the controller specified that the flight climb to 19,000 feet in VFR conditions. Immediately thereafter TWA 2 asked for a routing change to Daggett via Victor Airway 210. This was approved in a routine manner. At 0921, through company radio communications, Flight 2 reported that it was approaching Daggett and requested a change in flight plan altitude assignment from 19,000 to 21,000 feet. ARTC (Los Angeles Center) advised they were unable to approve the requested altitude because of traffic (United Air Lines Flight 718). Flight 2 requested a clearance of 1,000 feet on top. Ascertaining from the radio operator that the flight was then at least 1,000 on top, ARTC cleared the flight. At 0959 Trans World 2 reported its position through company radio at Las Vegas. It reported that it had passed Lake Mohave at 0955, was 1,000 on top at 21,000 feet, and estimated it would reach the 321-degree radial of the Winslow omni range station (Painted Desert) at 1031 with Farmington next. This was the last radio communication with the flight.
Probable cause:
The Board determines that the probable cause of this mid-air collision was that the pilots did not see each other in time to avoid the collision. It is not possible to determine why the pilots did not see each other, but the evidence suggests that it resulted from any one or a combination of the following factors: Intervening clouds reducing time for visual separation, visual limitations due to cockpit visibility, and preoccupation with normal cockpit duties, preoccupation with matters unrelated to cockpit duties such as attempting to provide the passengers with a more scenic view of the Grand Canyon area, physiological limits to human vision reducing the time opportunity to see and avoid the other aircraft, or insufficiency of en route air traffic advisory information due to inadequacy of facilities and lack of personnel in air traffic control. The following findings were reported:
- Approaching Daggett, TWA 2 requested its company radio to obtain 21,000 feet as an assigned altitude, or 1,000 on top,
- Company radio requested 21,000 feet IFR from ARTC. This vas denied by ARTC. Request was then made for 1,000 on top. This was approved and clearance issued. The flight climbed to and proceeded at 21,000 feet,
- As an explanation for the denial of 21,000 feet, TWA 2 was furnished pertinent information on UA718,
- The last position report by each flight indicated it was at that time at 21,000, estimating the Painted Desert line of position at 1031,
- The Salt Lake controller possessed both position reports at approximately 1013, at which time both flights were in uncontrolled airspace,
- Traffic control services are not provided in the uncontrolled airspace and according to existing Air Traffic Control policies and procedures the Salt Lake controller was not required to issue traffic information; none was issued voluntarily,
- A general overcast with some breaks existed at 15,000 feet in the Grand Canyon area,
- Several cumulus buildups extending above flight level existed; one was nearly over Grand Canyon Village and others were north and northeast in the area of the collision,
- The collision occurred at approximately 1031 in visual flight rule weather conditions at about 21,000 feet,
- The collision in space was above a position a short distance west of the TWA wreckage area, 17 miles west of or approximately 3-1/2 minutes' flying time from the Painted Desert line of position,
- Under visual flight rule weather conditions it is the pilot's responsibility to maintain separation from other aircraft,
- At impact the aircraft relative to each other converged at an angle of about 25 degrees with the DC-7 to the right of the L-1049. The DC-7 was rolled about 20 degrees right wing down and pitched about 10 degrees nose down relative to the L-1049,
- There was no evidence found to indicate that malfunction or failure of the aircraft or their components was a factor in the accident.
Final Report:

Crash of a Boeing KC-97G-26-BO Stratotanker near Walker AFB: 11 killed

Date & Time: Jun 26, 1956
Type of aircraft:
Operator:
Registration:
52-2700
Flight Phase:
Flight Type:
Survivors:
No
Site:
MSN:
16731
YOM:
1952
Crew on board:
11
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
11
Circumstances:
Few minutes after takeoff from Walker AFB, while climbing by night, a propeller blade detached from the engine number two, penetrated the fuselage and pierced a fuel tank. The aircraft caught fire, exploded and crashed in a desert area located 8 miles south of the airbase. All 11 crew members were killed.
Probable cause:
Loss of a propeller blade during initial climb.

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 Ford 4 in Townsend

Date & Time: Jun 19, 1956
Type of aircraft:
Operator:
Registration:
N9642
Flight Phase:
Survivors:
Yes
Schedule:
Townsend - Townsend
MSN:
4-AT-058
YOM:
1929
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was performing a crop spraying mission at Townsend, Montana. While flying at low height, the left engine lost power and eventually detached. The crew elected to make an emergency landing but the aircraft crashed. Both occupants were slightly injured while the airplane was written off.
Probable cause:
Loss of power on left engine which detached in flight.

Crash of a Lockheed PV-1 Ventura in Jeffersonville: 8 killed

Date & Time: May 15, 1956 at 1038 LT
Type of aircraft:
Operator:
Registration:
N64001
Flight Type:
Survivors:
No
Schedule:
Chicago – Louisville
MSN:
5326
YOM:
1943
Crew on board:
2
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
8
Captain / Total flying hours:
17600
Captain / Total hours on type:
9.00
Copilot / Total flying hours:
2297
Copilot / Total hours on type:
29
Aircraft flight hours:
3109
Circumstances:
The flight was for the purpose of transporting six Crane officials from Chicago, Illinois, to Louisville, Kentucky, to attend a business convention. Departure was from O'Hare-Chicago International Airport on a VFR flight plan (changed en route to IFR) with the Crane Company's Chief Pilot Randolph A. Mulherin in command, and Robert H. Robinette, also a Crane pilot, as copilot. Gross weight upon departure was estimated to be 27,360 pounds; the maximum permissible takeoff weight was 31,000 pounds. Shortly after takeoff the pilot gave a routine report to Chicago radio of his time off as 0908 and his estimated elapsed flight time as one hour and 20 minutes. He did not request weather information at that time. Other radio contacts followed as the flight progressed, the final one being at 1034 over the Jeffersonville intersection. An approach was then started from that point to the Standiford Airport, 6-9/10 miles distant. During this approach the aircraft struck trees and crashed at a point one-half mile north of the Jeffersonville intersection. The airplane was destroyed and all eight occupants have been killed.
Probable cause:
The Board determines that the probable cause of this accident was a critical loss of altitude, due to a complete power loss from the left engine and the drag of its windmilling propeller. The following findings were reported:
- Pilot Mulherin was relatively inexperienced with the subject model aircraft,
- The left engine suddenly lost all power because of a disconnected carburetor control,
- The left propeller was found not feathered,
- Examination of the right engine revealed no significant defect,
- Altitude could not be maintained and the aircraft struck high trees and then plunged steeply to the ground.
Final Report: