Crash of a Lockheed L-188CF Electra at Ogden-Hill AFB

Date & Time: Mar 19, 1972 at 0007 LT
Type of aircraft:
Operator:
Registration:
N851U
Flight Type:
Survivors:
Yes
Schedule:
Tucson - Ogen-Hill
MSN:
2001
YOM:
1959
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
15000
Captain / Total hours on type:
2500.00
Circumstances:
The crew was completing a ferry flight from Tucson to Ogden-Hill AFB. On approach, while descending to a height of 7,000 feet, the crew got a n°2 prop low oil warning. The engine was shut down but the crew was unable to feather the propeller for unknown reason. Despite the situation, the pilot-in-command was able to continue the approach and landed safely on runway 32. After touchdown, the n°2 prop separated from its mount and debris punctured the n°1 fuel tank. The airplane caught fire and came to rest in flames after a course of 4,000 feet. All three crew members escaped uninjured while the aircraft was partially destroyed by fire.
Probable cause:
Failure of a powerplant and propeller system on approach. The following factors were reported:
- Pressure too low,
- Improper in-flight decisions,
- Inadequate supervision of flight on part of the pilot-in-command,
- Improper use of equipment,
- Improper emergency procedures,
- Fire in engine,
- Low oil level light illuminated and prop oversped during feathering,
- Insufficient oil for unknown reason and engine oil not restored.
Final Report:

Crash of a Cessna 411 near Stockton: 5 killed

Date & Time: Dec 26, 1971 at 1930 LT
Type of aircraft:
Operator:
Registration:
N411Q
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Phoenix - Salt Lake City
MSN:
411-0146
YOM:
1965
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
6900
Circumstances:
While cruising at an altitude of 9,100 pieds by night and in poor weather conditions, the twin engine airplane struck the slope of a mountain located in the region of Stockton, Utah. SAR operations were conducted but eventually suspended few days later as no trace of the aircraft nor the five occupants was found. On 13 May 1972, walkers found the wreckage in an isolated area. The aircraft was totally destroyed by impact forces and the accident was not survivable.
Probable cause:
Controlled flight into terrain. The following factors were reported:
- Inadequate preflight preparation,
- The pilot attempted operation beyond experience/ability level,
- The pilot continued under VFR mode into adverse weather conditions,
- Low ceiling and snow showers,
- Turbulences associated with clouds and thunderstorm activity,
- High obstructions.
Final Report:

Crash of a Lockheed L-188CF Electra at Ogden-Hill AFB

Date & Time: Aug 24, 1970 at 0708 LT
Type of aircraft:
Operator:
Registration:
N855U
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Ogden-Hill – Mountain Home – Spokane – Great Falls – Minot – Grand Forks
MSN:
2012
YOM:
1959
Flight number:
UV9524
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
16395
Captain / Total hours on type:
1022.00
Circumstances:
The airplane was engaged in a cargo flight from Ogden-Hill AFB to Grand Forks AFB, North Dakota, with intermediate stops in Mountain Home, Fairchild AFB (Spokane), Great Falls and Minot, carrying various equipment for the US Army. After liftoff from runway 32, while climbing, the pilot raised the landing gear when the airplane pitched down to 15°. It lost height and struck the ground 8,200 feet past the runway end, slid for about 2,600 feet before coming to rest in flames. All three crew members were injured and the aircraft was destroyed.
Probable cause:
Loss of control during initial climb caused by an inadequate preflight preparation on part of the crew who failed to follow the approved procedures. The following contributing factors were reported:
- Inadequate preflight on part of the flight engineer,
- Lack of action on part of the flying crew,
- Pressure to low on the hydraulic system, hydraulic pumps,
- Nosed over after takeoff, unable to control pitch,
- One hydraulic pump used while the company requested use of all three pumps for takeoff.
Final Report:

Crash of a Rockwell 1121B Jet Commander in Salt Lake City: 2 killed

Date & Time: Dec 16, 1969 at 0610 LT
Operator:
Registration:
N403M
Flight Phase:
Survivors:
No
Schedule:
Salt Lake City - Seattle
MSN:
1121-132
YOM:
1969
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
9423
Captain / Total hours on type:
1195.00
Circumstances:
During the takeoff roll at Salt Lake City Airport, the crew completed the rotation too early. The aircraft stalled then crashed in flames near the runway. The aircraft was destroyed and both pilots were killed.
Probable cause:
Premature liftoff on part of the flying crew. The following factors were considered as contributing:
- The pilot-in-command failed to obtain flying speed,
- Physical impairment,
- Crew fatigue,
- Improperly loaded aircraft-weight and/or CofG,
- Icing conditions including sleet and freezing rain,
- Obstructions to vision.
Final Report:

Crash of a Rockwell Aero Commander 560 near Park City: 2 killed

Date & Time: Feb 23, 1968 at 1430 LT
Operator:
Registration:
N2784B
Flight Phase:
Flight Type:
Survivors:
No
Site:
MSN:
560-284
YOM:
1956
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
2385
Captain / Total hours on type:
86.00
Circumstances:
While performing a cargo flight, the crew encountered poor weather conditions. The captain decided to make a 180 turn to gain height when the twin engine aircraft struck the slope of a mountain located near Park City. The aircraft was destroyed upon impact and both occupants were killed.
Probable cause:
It was determined that the crew continued under VFR mode into adverse weather conditions. At the time of the accident, the visibility was reduced due to fog, rain and snow.
Final Report:

Crash of a Beechcraft Queen Air 80 in Salt Lake City

Date & Time: Dec 9, 1967 at 1515 LT
Type of aircraft:
Operator:
Registration:
N814B
Flight Phase:
Survivors:
Yes
MSN:
LD-18
YOM:
1962
Crew on board:
2
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4356
Captain / Total hours on type:
109.00
Circumstances:
Shortly after takeoff, while in initial climb, both engines failed simultaneously. The captain raised the undercarriage and attempted an emergency landing. The airplane belly landed in a field and came to rest near the airport. All five occupants were injured, one of them seriously. The aircraft was destroyed.
Probable cause:
Inadequate preflight preparation on part of the crew. Failure of both engines due to lack of lubrication caused by a thick and cold oil that was not pre-heated before flight.
Final Report:

Crash of a Beechcraft 65-88 Queen Air in Woods Cross: 2 killed

Date & Time: Dec 6, 1966 at 1517 LT
Type of aircraft:
Operator:
Registration:
N886E
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Salt Lake City - Salt Lake City
MSN:
LP-10
YOM:
1966
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
13000
Captain / Total hours on type:
100.00
Circumstances:
The crew departed Salt Lake City Airport for a local training flight. Three minutes after passing 9,000 feet, still climbing to reach FL130, the crew informed ATC about smoke in the cockpit. Shortly later, the aircraft entered an emergency descent until il crashed in Woods Cross, about 6 miles northeast of the airport. The aircraft owned by Thomas J. Carter was destroyed and both pilots were killed.
Probable cause:
The exact cause of the accident could not be determined with certainty.
Final Report:

Crash of a Douglas DC-3A near Salt Lake City: 13 killed

Date & Time: Nov 27, 1965 at 0715 LT
Type of aircraft:
Operator:
Registration:
N485
Flight Phase:
Survivors:
No
Site:
Schedule:
Lake City – Provo – Albuquerque
MSN:
4848
YOM:
1942
Flight number:
EDD065
Crew on board:
4
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
13
Captain / Total flying hours:
12361
Captain / Total hours on type:
1443.00
Circumstances:
The airplane was on a charter flight from Salt Lake City to Albuquerque with an intermediate stop at Provo, carrying football supporters. Four minutes after its departure from Salt Lake City Airport, the crew encountered poor weather conditions when, at an altitude of 5,500 feet, the airplane struck the slope of a mountain located 22 miles south of Salt Lake City. The wreckage was found 11 feet below the summit (5,449 feet) and was destroyed upon impact. All 13 occupants were killed, among them the captain Garth Edde who founded Edde Airlines in 1960. At the time of the accident, the airplane was one mile east of the intended track.
Probable cause:
It was determined that the crew flew under VFR mode in adverse weather conditions. The crew exercised poor judgment.
Final Report:

Crash of a Boeing 727-22 in Salt Lake City: 43 killed

Date & Time: Nov 11, 1965 at 1752 LT
Type of aircraft:
Operator:
Registration:
N7030U
Survivors:
Yes
Schedule:
New York – Cleveland – Chicago – Denver – Salt Lake City – San Francisco
MSN:
18322
YOM:
1965
Flight number:
UA227
Crew on board:
6
Crew fatalities:
Pax on board:
85
Pax fatalities:
Other fatalities:
Total fatalities:
43
Captain / Total flying hours:
17743
Captain / Total hours on type:
334.00
Copilot / Total flying hours:
6074
Copilot / Total hours on type:
84
Aircraft flight hours:
1781
Circumstances:
Flight 227 took off from New York-LaGuardia (LGA) for a flight to San Francisco (SFO) via Cleveland (CLE), Chicago (MDW), Denver (DEN) and Salt Lake City (SLC). The aircraft took off from Denver at 16:54 and climbed to its assigned cruising altitude of FL310. At 17:38 flight 227 began its descent for Salt Lake City. The flight proceeded in accordance with radar vectors. After a radar handoff to Salt Lake City Approach Control new clearance altitudes were given. At 17:47 the approach controller advised, "United seventy twenty seven ... five miles south of Riverton Fan Marker coming on localizer course cleared for ILS runway three four left approach." The pilot replied "Okay we're slowed to two fifty (Knots) and we're at ten (10,000 feet) we have the runway in sight now, we'll cancel and standby with you for traffic." Control of the flight was transferred to the tower and at 17:49:40 landing clearance was issued. The aircraft crossed the outer marker over 2,000 fee & above the ILS glide slope. The rate of descent during the final approach exceeded 2,000 ft/min, approximately three times the United Air Lines recommended rate of descent for landing approaches. The first officer attempted to apply power but the captain stopped him. Power was then applied too late to arrest the rate of descent. The airplane touched down 335 feet short of the threshold of runway 34L. The right and left main landing gear began to separate and the airplane slid onto the runway. Severe upward and rearward impact forces from the right main Landing gear assembly produced a large impact hole and ruptured fuel lines and the no. 3 generator leads between fuselage station 1030 and 1130 on the right side. The fuel was ignited by sparks from the fuselage scraping on the runway and/or the severed generator leads. 13 passengers were uninjured while 35 people were wounded. 43 other occupants were killed.
Probable cause:
The Board determines the probable cause of this accident was the failure of the Captain to take timely action to arrest an excessive descent rate during the landing approach.
Final Report:

Crash of a Beechcraft E18 in Delta: 1 killed

Date & Time: Mar 5, 1964 at 1900 LT
Type of aircraft:
Operator:
Registration:
N5645D
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
BA-358
YOM:
1958
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
8634
Circumstances:
While in cruising altitude, the pilot informed ATC that both engines failed and elected to divert to the nearest airport. While losing speed and height, the airplane crash landed in a field located in Delta. All three passengers were injured while the pilot was killed.
Probable cause:
Engine failure caused by icing. Improper operation or failed to use the anti-icing and/or de-icing equipment on part of the pilot.
Final Report: