Crash of a Beechcraft 60 Duke near Hatch: 6 killed

Date & Time: Jan 20, 1974 at 1813 LT
Type of aircraft:
Operator:
Registration:
N35D
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Eagle - Las Vegas
MSN:
P-43
YOM:
1969
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
En route from Eagle to Las Vegas by night, the pilot encountered strong headwinds and severe icing conditions. In low ceiling, he lost control of the airplane that dove into the ground and crashed in a mountainous terrain located near Hatch. The wreckage was found four days later, on January 24, and all six occupants have been killed.
Probable cause:
Uncontrolled descent following poor judgment and improper in-flight decisions on part of the pilot. The following factors were reported:
- Icing conditions including sleet and/or freezing rain,
- Ice propeller,
- Airframe ice,
- Inadequate preflight preparation,
- Improperly loaded aircraft and CofG,
- Miscalculated fuel consumption,
- Low ceiling,
- Adverse winds aloft,
- Strong headwinds,
- Low fuel,
- Severe icing conditions,
- Continued flight thru icing conditions until non maintained altitude,
- Wreckage found four days later.
Final Report:

Crash of a Cessna 402 near Peach Springs: 10 killed

Date & Time: Oct 16, 1971 at 0945 LT
Type of aircraft:
Operator:
Registration:
N3250Q
Flight Phase:
Survivors:
No
Schedule:
Las Vegas - Grand Canyon
MSN:
402-0050
YOM:
1967
Crew on board:
1
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
10
Captain / Total flying hours:
2441
Captain / Total hours on type:
415.00
Circumstances:
The twin engine airplane departed Las Vegas Airport on a charter flight to Grand Canyon, carrying nine passengers, tourists from the US, France and Germany. En route, the pilot encountered poor weather conditions and elected to turning around when he lost control of the airplane that dove into the ground and crashed about 39 miles north of Peach Springs. The wreckage was found a day later in the Shivwits Plateau near Parashant Canyon. The aircraft disintegrated on impact and all 10 occupants have been killed.
Crew:
Wayne Leeth.
Passengers:
James Allen Jr,
Florence Allen,
Mr. R. Lynch,
Mrs. R. Lynch,
Mr. P. Dosmond, France,
Mrs. P. Dosmond, France,
Paul Haack, West Germany,
Renate Haack, West Germany,
Walter Pilgram, West Germany.
Probable cause:
The pilot continued VFR flight into adverse weather conditions. The following factors were reported:
- Low ceiling, rain and snow.
Final Report:

Crash of a Beechcraft C-45g eXPEDITOR in Prescott: 4 killed

Date & Time: Aug 29, 1971 at 1450 LT
Type of aircraft:
Operator:
Registration:
N74Q
Flight Type:
Survivors:
Yes
Schedule:
Las Vegas – Houston
MSN:
AF-290
YOM:
1953
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
2472
Captain / Total hours on type:
189.00
Circumstances:
En route from Las Vegas to Houston, the left engine failed. The pilot was able to feather the propeller but unable to maintain a safe altitude. He informed ATC about his situation and was cleared to divert to the nearest airport for an emergency landing. While trying to land at a ranch airstrip, the airplane hit a wood pile and crashed in flamers. The pilot and a passenger were seriously injured while four other occupants were killed.
Probable cause:
Failure of the left engine in flight due to cylinder assembly failure. The following factors were reported:
- Material failure,
- Improper in-flight decisions or planning,
- Improper emergency procedures,
- Intentional wheels-up landing,
- Left engine lost power due to cracked n°9 cylinder.
Final Report:

Crash of a Lockheed 18-08 LodeStar in Albuquerque: 11 killed

Date & Time: Dec 5, 1969 at 1500 LT
Type of aircraft:
Registration:
N410M
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Las Vegas - Dalhart
MSN:
2203
YOM:
1942
Crew on board:
2
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
11
Captain / Total flying hours:
8030
Captain / Total hours on type:
30.00
Circumstances:
En route from Las Vegas to Dalhart, Texas, the crew encountered poor weather conditions with icing and turbulences. The VFR rated pilot preferred to continue in such conditions when few minutes later, a structural failure occurred on the left wing that detached. Out of control, the airplane dove into the ground and crashed in a huge explosion in an open field. All 11 occupants were killed.
Probable cause:
Airframe failure in flight and uncontrolled descent caused by the combination of the following factors:
- The pilot-in-command attempted operation with known deficiencies in equipment,
- The pilot-in-command continued VFR flight into adverse weather conditions,
- The pilot-in-command exceeded designed stress limits of aircraft,
- Overload failure of airframe, wings spars,
- Separation in flight,
- Icing conditions, including sleet and freezing rain,
- Airframe ice,
- The left wing failed and separated in flight,
- The pilot type rated for VFR flight only,
- The aircraft was not fitted with de-icing equipment.
Final Report:

Crash of a Fairchild F-27A near Las Vegas: 29 killed

Date & Time: Nov 15, 1964 at 2025 LT
Type of aircraft:
Operator:
Registration:
N745L
Survivors:
No
Site:
Schedule:
Phoenix – Las Vegas
MSN:
29
YOM:
1958
Flight number:
BO114
Crew on board:
4
Crew fatalities:
Pax on board:
25
Pax fatalities:
Other fatalities:
Total fatalities:
29
Captain / Total flying hours:
11171
Captain / Total hours on type:
4055.00
Copilot / Total flying hours:
3249
Copilot / Total hours on type:
811
Aircraft flight hours:
14401
Circumstances:
Weather was poor near Las Vegas with indefinite ceiling at 500 feet, sky obscured, 900 m visibility and light snow. Flight 114 was flying a VOR/DME-3 approach when the plane descended below altitude minima. At 9.7 DME, at an elevation of 3575 feet msl the plane struck rising terrain and crashed. The flight should have been at 4300 feet msl at that point. It appeared that the VOR/DME-3 approach procedure was relatively new, having become effective on October 3, 1964. Until November 15 no approaches using this procedure had been flown. The approach chart depiction for the segment of the approach from the 15 mile fix to the 6 mile fix displayed no descent information on the profile section. However, the profile did show a solid horizontal line between the 6 mile fix and the 3 mile fix, with an altitude of 3,100 feet. Further, the solid line was defined in the Chart Legend as "Flight Path," which implied that a descent to 3,100 feet was proper once the fix to which the flight has been cleared is reached.
Probable cause:
The misinterpretation of the approach chart by the captain which resulted in a premature descent below obstructing terrain.
Final Report:

Crash of a Lockheed L-049 Constellation in Hinsdale: 78 killed

Date & Time: Sep 1, 1961 at 0205 LT
Operator:
Registration:
N86511
Flight Phase:
Survivors:
No
Schedule:
Boston – New York – Pittsburgh – Chicago – Las Vegas – Los Angeles – San Francisco
MSN:
2035
YOM:
1945
Flight number:
TW529
Crew on board:
5
Crew fatalities:
Pax on board:
73
Pax fatalities:
Other fatalities:
Total fatalities:
78
Captain / Total flying hours:
17011
Captain / Total hours on type:
12633.00
Copilot / Total flying hours:
5344
Copilot / Total hours on type:
1975
Aircraft flight hours:
43112
Circumstances:
During engine runup, Flight 529 was given its air traffic control clearance which was: "cleared to the Las Vegas Airport via Victor 6 Naperville, Victor 8 flight plan route, maintain 5,000 feet." The clearance was acknowledged correctly and TWA Flight 529 departed on runway 22L at 0200, making a right turn out of traffic. The 0200 Midway Airport weather was: scattered clouds at 10,000 feet; high overcast, visibility three miles in haze and smoke; wind south eight knots. The Chicago O'Hare Airport weather at 0200 was: partial obscuration; scattered clouds 15,000 feet; high overcast; visibility two and one-half miles in ground fog and smoke; wind south six knots. Radar contact was established with the flight one minute and 34 seconds after the flight acknowledged takeoff clearance and as the aircraft proceeded outbound in a right turn. At 0204, Flight 529 was observed on radar by the departure controller to be five miles west of Midway Airport proceeding on course. Northwest Airlines Flight 105 was cleared for takeoff on runway 22L at Midway, and took off Immediately. The ground controller observed a flash west of Midway Airport at this time and asked Flight 105 if he had seen a flash. Flight 105 advised that they had seen a flash fire and would fly over the area. As Flight 105 reported over the fire, the radar range was noted to be nine miles west of Midway Airport and the radar return of TWA. Flight 529 had disappeared from the scope. It was later determined that Flight 529 had crashed at this site and that the observed ground fire was the result of the accident. The airplane disintegrated in a field and all 78 occupants have been killed.
Probable cause:
The Board determines that the probable cause of this accident was the loss of an AN-175-21 nickel steel bolt from the parallelogiam linkage of the elevator boost system, resulting in loss of control of the aircraft.
Final Report:

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 Martin 404 in Las Vegas

Date & Time: Nov 15, 1956 at 1504 LT
Type of aircraft:
Operator:
Registration:
N40404
Survivors:
Yes
Schedule:
Kansas City – Topeka – Wichita – Amarillo – Santa Fe – Albuquerque – Las Vegas – Los Angeles
MSN:
14104
YOM:
1951
Flight number:
TW163
Crew on board:
3
Crew fatalities:
Pax on board:
35
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
9431
Captain / Total hours on type:
639.00
Copilot / Total flying hours:
9926
Copilot / Total hours on type:
105
Aircraft flight hours:
10451
Circumstances:
Trans World Airlines Flight 163 is a regularly scheduled domestic operation between Kansas City, Missouri, and Los Angeles, California, with intermediate stops at Topeka and Wichita, Kansas; Amarillo, Texas; Santa Fe and Albuquerque, New Mexico; and Las Vegas, Nevada. A scheduled crew change is made at Albuquerque. There, on November 15, 1956. Captain Arthur G. deFabry, First Officer James P. Rapattoni, and Hostess Anne J. Zeman boarded Flight 163 as its crew to complete the remaining segments. The flight was routine to Las Vegas where it landed at 1440. During the short ground time at Las Vegas the aircraft was serviced and the crew performed routine duties for continuation of the flight to Los Angeles. There was no apparent need for maintenance on the aircraft and none was performed. An Instrument Flight Rules flight plan was prepared and filed because of instrument weather conditions over the latter portion of the flight segment to Los Angeles. Weather conditions at Las Vegas, however, were clear. At 1449 Captain deFabry, seated in the captain’s position, taxied N 40404 from the Las Vegas terminal to runup position beside runway 7 where the required pretakeoff checks were accomplished. The aircraft and equipment responded normally. The flight was issued an instrument clearance by Air Route Traffic Control. At this time, according to the company load manifest, the gross weight of the aircraft was 41.801 pounds, well under the maximum allowable for takeoff, 43,650 pounds. The load was properly distributed with respect to the center of gravity limitations of the aircraft. With Captain deFabry operating the aircraft, Flight 163 took off at 1456. The takeoff was routine and was followed by a climbing left turn to gain altitude and establish a southwesterly course toward Los Angeles. At 1501, when over the northern perimeter of the city, First Officer Rapattoni radioed the Las Vegas tower stating the flight was returning to the airport, engine out. The Las Vegas tower controllers immediately notified all other traffic to remain clear and alerted emergency equipment. Flight 163 was cleared to land, any runway, and informed that the wind was calm. Captain deFabry elected to use runway 7 and First Officer Rapattoni notified the tower. Emergency equipment was then dispatched into position on the taxiway parallel to that runway. N40404 was soon observed on a wide base leg for runway 7 and as it turned onto the final approach. Position and altitude of the flight seemed normal. As the aircraft drew closer its extended gear could be seen and its left propeller was clearly visible, stopped and feathered. As the aircraft passed over the runway threshold its alignment position, and altitude seemed good; however, to nearly all observers excessive speed was apparent. The aircraft floated a considerable distance down the runway before touching it. It then bounced several times, after which an application of power was heard, obviously :m an attempt to go around. The Martin climbed, veered to the left, and its left wing gradually lowered. It seemed to “struggle” to continue flight and its airspeed decreased visibly. Seconds later the aircraft struck the ground, left wing low, just inside the airport boundary. Weather conditions at the time of the accident were clear, visibility 65 miles, and the wind was calm. A large cloud of dust, raised by the accident, hung over the scene and gradually lifted nearly vertically in evidence of the calm wind.
Probable cause:
The Board determines that the probable cause of this accident was that during an emergency situation the captain failed to reduce speed during the latter portion of a single-engine approach; this excessive speed resulted in an overshoot and an attempted go-around which was beyond the performance capability of the aircraft under existing conditions. The following findings were reported:
- The prior segments of the flight, the pretakeoff cheeks, and the takeoff at Las Vegas were normal,
- Shortly after takeoff the left engine No. 2 cylinder exhaust valve push rod failed causing backfiring, loss of power, and engine roughness; these conditions necessitated taking the engine out of operation by feathering its propeller,
- Emergency single-engine operation was established, the McCarran tower was notified, and the flight returned to the airport to land,
- The base leg and final approach to runway 7 were normal with respect; to alignment, position, and altitude,
- The flight crossed the threshold with excessive airspeed and floated 2.749 feet before touching the runway,
- A series of bounces occurred as unsuccessful attempts were made by Captain deFabry to force the aircraft on the runway,
- Believing the aircraft could successfully go around at the speed and in the configuration which existed the captain attempted unsuccessfully to do so,
- Prior to the accident company pilot training with respect to single-engine performance of the Martin 404 in the balked landing situation was inadequate,
- Examination showed there was no malfunction of the right engine, landing gear and flap hydraulic systems, or the ADI system.
Final Report:

Crash of a Curtiss C-46E-1-CS in Cheyenne: 3 killed

Date & Time: Oct 9, 1949 at 1754 LT
Type of aircraft:
Operator:
Registration:
NC59485
Flight Type:
Survivors:
No
Schedule:
Las Vegas – Denver
MSN:
2939
YOM:
1945
Flight number:
SL118
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
5514
Captain / Total hours on type:
2654.00
Copilot / Total flying hours:
4583
Copilot / Total hours on type:
2515
Aircraft flight hours:
8585
Circumstances:
At Las Vegas, Trip 11-8 remained on the ground 35 minutes. During this time, the crew obtained weather forecasts for the trip to Denver and had the aircraft serviced with 370 gallons of fuel. These forecasts indicated that between south-western Utah and Denver there would be broken to overcast clouds with bases and tops ranging from 8,000 to 20,000 feet in altitude, and that below 8,000 feet there would be light rain showers with light snow showers above this level. The flight was cleared under Instrument Flight Rules to cruise at 13,000 feet to Grand Junction, Colorado, 14,000 feet to Eagle, Colorado, and 16,000 feet to the Dupont Intersection, 5 miles north of Denver, with Laramie, Wyoming, designated as the alternate airport The computed elapsed time was three hours and five minutes with sufficient fuel aboard to fly five hours and five minutes. A forecast for Denver, at 1700, when the flight was estimated to arrive, indicated a ceiling of 700 feet with icing in the clouds above 8,000 feet. At Laramie, the chosen alternate airport, a ceiling of 2,000 feet occasionally lowering to 1,000 feet was forecast with light rain showers expected to change to light snow showers after dark. At 1403, the flight departed Las Vegas, and two hours and two minutes later, at 1605, reported over Grand Junction at an altitude of 13,000 feet, climbing to 14,000. At this time the flight received from INSAC (Interstate Airways Communication) at Grand Junction the 1530 weather observations for Grand Junction, Denver, Eagle and Pueblo, Colorado. Denver was reported having a variable ceiling of 600 feet, overcast and lower broken clouds, visibility six miles, light rain and wind from the north-northwest at 12 miles per hour. When over Eagle, at 1637, the flight reported at an altitude of 14,000 feet and climbing to 16,000. Forty-five minutes later, at 1708, over the Dupont Intersection the flight reported to the Denver Tower and was given the Denver weather as ceiling 200 feet and visibility two miles. As the ceiling and visibility were expected to remain that way for several hours and as the company's landing minimums for Denver were ceiling 400 feet and visibility one mile, the crew requested a change of flight plan. Rock Springs, Wyoming, was chosen as the new alternate and permission was requested to land at Laramie, weather permitting. Denver Air Traffic Control approved and cleared the flight to Rock Springs to maintain 14,000 feet. Twenty-five miles south of Laramie, at 1732, Trip 11 called the Cheyenne Tower and asked permission to change course and to proceed direct to Cheyenne. This was approved by Denver ATC and the crew was further advised by the tower that there was a squall line between Laramie and Cheyenne. The Cheyenne weather reported to the flight at that time was ceiling 3,500 feet, overcast, lower broken clouds and visibility 20 miles. At 1740, the flight reported over the Cheyenne range at 14,000 feet and a special Cheyenne weather report was given the crew which showed the ceiling had lowered to 900 feet and that there was light sleet, and a visibility of 12 miles. Proceeding out the east course of the Cheyenne range, the flight notified the tower that it was low on fuel, taking on ice, and having difficulty in maintaining altitude. A few minutes later clearance was given the flight to descend to 8,000 feet on the north course of Cheyenne range. 2 This was acknowledged and seconds later it encountered severe turbulence. At approximately 1750, an unreadable transmission was heard by the tower. There was definite hysteria in the voice making this transmission. The tower then called the flight several times but no answer was received. Two minutes later at 1752, the tower received the following transmission "We are O. K and are out of it now." About one-half minute later a noise believed to be caused by a surge of power of the aircraft's engines was heard northwest of the tower. Shortly after this a flash of light was seen about two miles northwest of the airport.
Probable cause:
The Board determines that the probable cause of this accident was the loss of control of the aircraft during an instrument approach to Cheyenne, Wyoming, under conditions of heavy icing and severe turbulence.
The following findings were noted:
- Wings and tail surfaces of the aircraft were not equipped with deicing boots, however, anti-icing equipment had been installed on the propellers,
- Forecasts issued by the U. S. Weather Bureau and available to the crew before departure from Los Vegas, indicated icing conditions would be encountered enroute to Denver,
- At the time the flight departed Las Vegas the weather at Denver was above the company's minimums and was expected to remain above these minimums until the arrival of the flight at Denver,
- Being unable to land at Denver because of adverse weather conditions, the flight proceeded first to Laramie and then to Cheyenne where the weather had been reported as ceiling 3,500 feet, visibility 20 miles,
- The front moved toward Cheyenne more rapidly than was anticipated by either the Weather Bureau or the captain, and it arrived at Cheyenne before a landing could be accomplished,
- During the descent at Cheyenne, the flight encountered severe turbulence and heavy icing.
Final Report:

Crash of a Douglas DC-3A near Lebec: 11 killed

Date & Time: Nov 13, 1946 at 0341 LT
Type of aircraft:
Operator:
Registration:
NC18645
Flight Phase:
Survivors:
No
Site:
Schedule:
Lethbridge – Salt Lake City – Las Vegas – Burbank
MSN:
11662
YOM:
1943
Flight number:
WA023
Crew on board:
3
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
11
Captain / Total flying hours:
4886
Captain / Total hours on type:
4060.00
Copilot / Total flying hours:
3488
Copilot / Total hours on type:
298
Aircraft flight hours:
6229
Circumstances:
At 0324LT, the crew informed ATC about his position at 9,000 feet vertical to Newhall and six minutes later, he obtained the permission to descend. At 0341LT, the aircraft hit the slope of Mt White located 14 miles south of Lebec and disintegrated on impact. All 11 occupants were killed. It appears that at the time of the accident, the aircraft was off track to the east by ten miles due to strong west winds, and it hit the mountain 75 feet below the summit.
Probable cause:
The Board determines that the probable cause of this accident was the action of the pilot in making an instrument letdown without previously establishing a positive radio fix. This action was aggravated by conditions of severe static, wind in excess of anticipated velocities, preoccupation with an unusual amount of radio conversation, and the inoperative Newhall radio range.
Final Report: