Crash of a Boeing 307 Stratoliner near Madras

Date & Time: May 10, 1958
Type of aircraft:
Registration:
N75385
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
2002
YOM:
1940
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Parked since few months on a regional airport, the aircraft was recently purchased by a new owner who wanted to know the exact consumption of oil and fuel. A test flight was scheduled with two test pilots. To be able to perform a longer flight, additional fuel tanks were installed in the cabin. While cruising at a relative low altitude, the crew informed ATC that a fire erupted in the cabin and elected to make an emergency landing. The airplane crash landed in flames in a field located 15 miles from Madras and came to rest. While both pilots were able to evacuate with no injury, the aircraft was destroyed by fire.
Probable cause:
Additional fuel tanks were installed in the cabin to perform the test flight but it was determined that these fuels tanks were not sealed and were leaking. The technicians who installed the fuel tanks on board were aware of the fact that these tanks were leaking, but since they had not been able to find the source of the leaks, they decided to install them despite a major risk of fire. In flight, some fuel leaked from a tank and ignited while in contact with an incandescent element whose nature remains unknown. In such conditions, the crew was unable to continue the test flight and an emergency landing was therefore necessary.

Crash of a Douglas DC-7 near Las Vegas: 47 killed

Date & Time: Apr 21, 1958 at 0830 LT
Type of aircraft:
Operator:
Registration:
N6328C
Flight Phase:
Survivors:
No
Site:
Schedule:
Los Angeles – Denver – New York
MSN:
45142
YOM:
1956
Flight number:
UA736
Crew on board:
5
Crew fatalities:
Pax on board:
42
Pax fatalities:
Other fatalities:
Total fatalities:
47
Circumstances:
United Airlines Flight 736 departed Los Angeles International Airport at 0737 hours Pacific standard time with 42 passengers and 5 crew aboard. It was a scheduled passenger flight to New York, which was proceeding normally in accordance with an IFR flight plan along Victor Airway 16 to Ontario, California, and Victor Airway 8 to Denver. The aircraft was cleared to a cruising altitude of 21 000 ft msl and advised to climb in VFR weather conditions. At 0735 the flight reported to Aeronautical Radio that it was over Ontario at 12 000 ft and was climbing in VFR conditions. Then at 081 1 it reported over Daggett at its cruising altitude of 21 000 ft and estimated that it would reach Las Vegas (omni range station) at 0831, This was the last position report made by the flight. At approximately 0745 hours that morning F-100F, 56-3755, took off from Nellis Air Force Base, Las Vegas, Nevada on an instrument training flight carrying an instructor and a trainee pilot. The flight was in accordance with a VFR local flight plan filed with Nellis Operations and the local traffic control tower. At approximately 0823, 755 called Nellis VFR Control and reported that it was "inbound on KRAM" ( a local commercial radio broadcast station). The flight requested an altitude assignment from which it would conduct a simulated ADF instrument jet penetration utilizing KRAM. The VFR controller assigned 755, 28 000 ft and advised it to report over the radio station. At approximately 0828, the flight reported that it was over KRAM requesting a penetration. The VFR controller cleared it for an immediate penetration and requested that it report the penetration turn. 755 then reported leaving 28 000 ft. There were no &her reports from the flight in connection with this procedure. At 0830 the offices of Aeronautical Radio at Los Angeles, Denver and Salt Lake City heard an emergency message from the United flight.. . . . " United 736, Mayday, midair collision, over Las Vegas. " At the same time, as nearly as can be determined, there was an unrecorded emergency transmission from the F-1 00F. This message was heard by the VFR controller and by the two pilots of another F-100F. All were agreed that the first portion of the emergency transmission was "Mayday, Mayday, this is 755. " The last part of the message was either, "We've had a flameout" or 'We're bailing out." The aircraft collided at 21 000 ft over a position later determined to be about 9 miles southwest of the Las Vegas VOR station, on Victor Airway 8, approximately 1-3/4 miles to the right (southeast) of the centerline. Both aircraft fell out of control and crashed killing the 47 persons on board the DC-7 and both pilots of the F-100F.
Probable cause:
The probable cause of this collision was a high rate of near head-on closure at high altitude; human and cockpit limitations; and the failure of Nellis Air Force Base and the Civil Aeronautics Administration to take every measure to reduce a known collision exposure.
Final Report:

Crash of a Douglas C-133A-10-DL Cargomaster in Ellendale: 4 killed

Date & Time: Apr 13, 1958 at 0843 LT
Type of aircraft:
Operator:
Registration:
54-0146
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Dover - Dover
MSN:
44716
YOM:
1954
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total hours on type:
585.00
Copilot / Total hours on type:
60
Circumstances:
The four engine aircraft left Dover AFB runway 32 at 0828LT on a local training flight. Fifteen minutes later, while cruising at a relative low altitude of 2,000 feet, the airplane went out of control, dove into the ground and crashed in flames in a dense wooded area located near Ellendale. The airplane was destroyed by impact forces and all four crew members were killed.
Crew:
Cpt Raymond R. Bern, pilot,
1st Lt Herbert T. Palisch, copilot,
T/Sgts Marvin A. Aust, flight engineer,
T/Sgt Edward L. McKinley Jr., flight engineer.
Probable cause:
Its is believed the accident was the result of icing conditions encountered at low height (2,000 feet). Tests showed that ice formed in a tube through which the doomed plane’s control cables passed.

Crash of a Douglas SC-47A at McChord AFB: 3 killed

Date & Time: Apr 13, 1958
Operator:
Registration:
42-93183
Flight Type:
Survivors:
No
Schedule:
McChord - McChord
MSN:
13066
YOM:
1944
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
Crashed in unknown circumstances at McChord AFB while completing touch-and-go maneuvers. All three crew members were killed, among them T/Sgt Roy Edwin Craft.

Crash of a Vickers 745D Viscount in Saginaw: 47 killed

Date & Time: Apr 6, 1958 at 2319 LT
Type of aircraft:
Operator:
Registration:
N7437
Survivors:
No
Schedule:
New York – Detroit – Flint – Saginaw – Chicago
MSN:
135
YOM:
1956
Flight number:
CA067
Crew on board:
3
Crew fatalities:
Pax on board:
44
Pax fatalities:
Other fatalities:
Total fatalities:
47
Captain / Total flying hours:
16050
Captain / Total hours on type:
1702.00
Copilot / Total flying hours:
2030
Copilot / Total hours on type:
975
Circumstances:
At 2306, four minutes after takeoff, the flight, pursuant to clearance instructions, reported to Flight tower that it was at 3,600 feet and was departing the Flint outer marker. At this time the tower requested the estimated time of arrive at Tri-City and was advised that it was 2315. Flight 67 was then given the following clearance: "ARTC (Air Route Traffic Control) clears Capital 67 to hold north of the Saginaw omni range, one minute pattern, right turn, maintain 3,600 feet. Expect further clearance 2320, change to company frequency for this clearance." This clearance was acknowledged and, as per instructions, the frequency was changed to that of the company at Detroit. At 2310, Capital at Detroit relayed the following clearance to the flight: "ARTC clears Flight 67 for approach at Saginaw (Tri-City) Airport. Report time on the ground to Saginaw radio." These instructions were verified. The flight then called Saginaw ATCS (Air Traffic Communication Station) and was given the local 2300 weather observation and the runway in use, No. 5. The Tri-City Airport does not have a traffic control tower. The 2300 Saginaw weather was reported as: Measured ceiling 900 feet, overcast, visibility 3 miles, light snow showers, temperature 34; dewpoint 33; wind north-northeast 18, peak gusts to 27 knots; altimeter 29.48, comments--drizzle ended and snow showers began at 2225. At 2316 Trip 67 advised Saginaw radio that it was over the airport. A short time later, ground witnesses observed the lights of the aircraft when it was on the downwind leg of the traffic pattern. The aircraft was seen to make a left turn onto base leg and at this time the landing lights of the aircraft were observed to come on. During this portion of the approach the aircraft was flying beneath the overcast, estimated to be 900 feet, and appeared to be descending. When turning on final, Trip 67 flew a short distance beyond the extended centerline of the runway and the turf was seen to steepen for realignment with the runway. Soon after this the aircraft was observed to level off and then to descend steeply and strike the ground. A large fire immediately erupted. The aircraft was totally destroyed and all 47 occupants have been killed.
Probable cause:
The Board determines that the probable cause of this accident was an undetected accretion of ice on the horizontal stabilizer which, in conjunction with a specific airspeed and aircraft configuration, caused a loss of pitch control.
Final Report:

Crash of a Fairchild C-119C-17-FA Flying Boxcar near Bridgeport: 3 killed

Date & Time: Mar 27, 1958 at 1615 LT
Operator:
Registration:
49-0195
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Sheppard - Carswell
MSN:
10432
YOM:
1949
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
En route from Sheppard AFB to Carswell AFB, while cruising at an altitude of 6,000 feet in poor weather conditions, the aircraft collided with a USAF Douglas C-124 Globemaster II. Registered 52-0981, the C-124 was en route from Kelly AFB to Tinker AFB with 15 people on board. Following the collision, both aircraft dove into the ground and crashed in a field located near Bridgeport. All 18 occupants on both aircraft were killed.
Probable cause:
It was determined that the collision was the result of an error on part of the C-119's crew who failed to respect the instructions transmitted by ATC, asking them to fly at an altitude of 7,000 feet. For undetermined reason, the crew continue his route at the insufficient altitude of 6,000 feet, crossing the track of the C-124 which was flying at the same level. Low visibility caused by poor weather conditions was considered as a contributing factor.

Crash of a Douglas C-124 Globemaster II near Bridgeport: 15 killed

Date & Time: Mar 27, 1958 at 1615 LT
Operator:
Registration:
52-0981
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Kelly - Tinker
MSN:
43890
YOM:
1952
Crew on board:
10
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
15
Circumstances:
En route from Kelly AFB to Tinker AFB, while cruising at an altitude of 6,000 feet in poor weather conditions, the four engine aircraft collided with a USAF Fairchild C-119C-17-FA Flying Boxcar. Registered 49-0195, the Flying Boxcar was en route from Sheppard AFB to Carswell AFB with a crew of three on board. Following the collision, both aircraft dove into the ground and crashed in a field located near Bridgeport. All 18 occupants on both aircraft were killed.
Probable cause:
It was determined that the collision was the result of an error on part of the C-119's crew who failed to respect the instructions transmitted by ATC, asking them to fly at an altitude of 7,000 feet. For undetermined reason, the crew continue his route at the insufficient altitude of 6,000 feet, crossing the track of the C-124 which was flying at the same level. Low visibility caused by poor weather conditions was considered as a contributing factor.

Crash of a Douglas DC-7C in Miami: 9 killed

Date & Time: Mar 25, 1958 at 0006 LT
Type of aircraft:
Operator:
Registration:
N5904
Flight Phase:
Survivors:
Yes
Schedule:
Dallas – Miami – Panama City – Rio de Janeiro
MSN:
45072
YOM:
1957
Flight number:
BN971
Crew on board:
5
Crew fatalities:
Pax on board:
19
Pax fatalities:
Other fatalities:
Total fatalities:
9
Captain / Total flying hours:
20672
Captain / Total hours on type:
241.00
Copilot / Total flying hours:
13250
Copilot / Total hours on type:
257
Aircraft flight hours:
3306
Circumstances:
Braniff International Flight 971 was originally scheduled to depart New York, New York, for Miami, Florida, on March 23, 1958, at 2355 but this leg of the flight was not made owing to shortage of equipment and scheduling difficulties on that date. N 5904 was ferried from Dallas, Texas, to Miami, arriving at 1915 on March 24 for use as Flight 971. The aircraft was serviced and made reedy for the trip to Panama City, Panama, the first scheduled stop on the route to Rio de Janeiro, Brazil. The crew consisted of Captain Thomas D. George, First Officer John C. Winthrop, Jr., Second Officer Charles F. Fink, Steward Alberto Zapatero, and Stewardess Madelon Campion. The flight departed the Miami terminal at 2356, taxied to runway 27R where engine runup was made, after which a normal takeoff was accomplished. Shortly after takeoff, and in accordance with tower clearance, a climbing right turn was started. During the turn the No. 3 engine malfunctioned and a fire developed in that area. The airplane, still in a right turn, started to lose altitude rapidly. While traveling in a north-northeasterly direction it struck in an open marsh containing scattered trees and underbrush. Rescue operations were immediately initiated but were seriously hampered by heavy ground traffic of sightseers attracted to the area. Several of the passengers and crew members were airlifted by U. S. Coast Guard helicopters direct to hospital grounds in Miami and the others were removed to nearby ambulances and taken to hospitals.
Probable cause:
The Board determines that the probable cause of this accident was the failure of the captain to maintain altitude during an emergency return to the airport due to his undue preoccupation with an engine fire following takeoff. The following findings were reported:
- Weather was not a factor in the accident,
- The flight was properly planned and dispatched,
- Smoke from No. 3 engine on the prior flight was reported to the ferry crew by the Miami tower and the crew should have written up this item in the aircraft log,
- Shortly after a routine takeoff No. 11 cylinder of the No. 3 engine failed, resulting in a fire in flight,
- Emergency measures (i.e., propeller feathering, extinguisher, fuel shutoff) were promptly taken by the crew,
- Full power was available from the other three engines and there was no impairment of structure or control of the airplane,
- The captain made a decision to return to the airport and, in attempting to do so, altitude was not maintained and the aircraft struck the ground.
Final Report:

Crash of a Lockheed RC-121D Super Constellation at McClellan AFB

Date & Time: Mar 22, 1958 at 1118 LT
Operator:
Registration:
54-2308
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
McClellan - McClellan
MSN:
4390
YOM:
1956
Crew on board:
4
Crew fatalities:
Pax on board:
14
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5613
Captain / Total hours on type:
3583.00
Copilot / Total flying hours:
1664
Copilot / Total hours on type:
372
Circumstances:
The crew departed McClellan AFB on a topographic and geographical mission off the Californian coast. Shortly after takeoff from runway 16, while climbing to an altitude of 500 feet, the engine number two caught fire. The crew obtained the authorization to return for an emergency landing and the captain completed a 180 turn to intercept the glide. Doing so, the airplane lost 200 feet while flying over a populated area and the speed dropped to 120 knots. On final, the captain told his colleagues he was unable to reach the airport so he attempted an emergency landing in an open field located 1,5 mile short of runway 16. On touchdown, the airplane slid for several yards, lost its right wing and came to rest in flames. All 18 occupants were injured, five of them seriously, and the aircraft was destroyed by fire.
Probable cause:
The cause of the fire on engine number two could not be determined. At the time of the accident, ceiling was broken at 2,000 feet and overcast at 4,000 feet with light rain and a wind from the southeast at 10 knots, gusting 22 knots.

Crash of a Lockheed 18-56 LodeStar near Grants: 4 killed

Date & Time: Mar 22, 1958 at 0240 LT
Type of aircraft:
Operator:
Registration:
N300E
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Burbank – Tulsa – New York
MSN:
2312
YOM:
1942
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
7680
Captain / Total hours on type:
386.00
Copilot / Total flying hours:
4500
Copilot / Total hours on type:
3500
Aircraft flight hours:
3910
Circumstances:
The flight had made routine position reports from its assigned altitude of 11,000 feet until passing over Winslow, Arizona. Shortly after the last routine report at 11,000 feet a higher altitude was requested of Air Traffic Control because of encountering icing conditions. The request was granted and the aircraft reported, five minutes later, being at 13,000 feet between cloud layers. The last report was over Zuni, New Mexico, estimating Grants at 0249, 19 minutes later. Ten minutes after this report a ground explosion at an elevation of 7,200 feet m. s. 1. was observed by another flight and by ground witnesses. The wreckage of N300E was found in the area of the witnessed explosion. The right engine master rod bearing had failed in flight and the right propeller was feathered; however, complete loss of control followed and the aircraft struck the ground in a very steep angle of descent. As far as can be determined, there was no failure of the aircraft structure or controls prior to ground impact. The aircraft had anti-icing equipment installed and the pilots were experienced in Lodestar operation. There is evidence of the aircraft being considerably over its maximum allowable weight at departure and it is believed that the comparatively sudden failure of an engine at 13,000 feet created a situation, made more critical by virtue of the then existing weight, in which the pilot was unable to maintain control of the aircraft. All four occupants were killed, among them the American film producer Mike Todd, husband of Elizabeth Taylor, who was flying with his scenarist Art Cohn. The twin engine airplane was christened 'The Liz'.
Probable cause:
The Board determines that the probable cause of this accident was the loss of control of an overloaded aircraft following the failure of an engine at a cruising altitude which was critical for single-engine operation. The loss of control was aggravated by surface ice accretion.
Final Report: