Crash of a Piper PA-31T Cheyenne II in Delta

Date & Time: Jan 17, 1982 at 1435 LT
Type of aircraft:
Registration:
N91TW
Flight Type:
Survivors:
Yes
Schedule:
Delta - Las Vegas
MSN:
31-7820078
YOM:
1978
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4000
Captain / Total hours on type:
520.00
Aircraft flight hours:
340
Circumstances:
Approximately 1/2 mile from the airport after takeoff, the pilot noticed the left front baggage door partly open and made a left turn back toward the airstrip. After the turn, the baggage door came completely open, the left wing dropped immediately and the aircraft stalled. The pilot added full power and lowered the nose. When he raised the nose near the ground, the aircraft shuddered and crashed. Two rescue personnel, both certified pilots, arrived shortly after the accident and found the nose baggage door in the unlocked position with the bayonet pins retracted. A Piper representative stated that if the left side nose baggage door of a PA-31 opened in flight there would be the likelihood of an interruption to the smooth airflow through the prop, possibly reducing the thrust produced by the blades.
Probable cause:
Loss of control in flight while maneuvering to landing area after the pilot failed to maintain flying speed. The following findings were reported:
- Cargo door unlocked,
- Inadequate preflight preparation,
- Aircraft performances deteriorated,
- Inadvertent stall by the pilot.
Final Report:

Crash of a Mitsubishi MU-2B-20 Marquise in Provo: 2 killed

Date & Time: Dec 21, 1979 at 1758 LT
Type of aircraft:
Operator:
Registration:
N200BR
Survivors:
No
Schedule:
Denver - Provo
MSN:
205
YOM:
1971
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
12833
Captain / Total hours on type:
1785.00
Circumstances:
The pilot started the approach to Provo Municipal Airport by night. Due to limited visibility, he was unable to locate the runway as the lights were off. On final, the twin engine airplane crashed in a swamp located near the airport and was destroyed. Both occupants were killed.
Probable cause:
Controlled collision with ground in traffic pattern-circling due to inadequate preflight preparation on part of the pilot. The following contributing factors were reported:
- Improper IFR operation,
- The pilot misjudged altitude,
- Rain,
- Aircraft came to rest in water,
- The runway lights were not activated by the pilot,
- The pilot circled east when the runway was not sited.
Final Report:

Crash of a Lockheed L-188CF Electra in Salt Lake City: 3 killed

Date & Time: Nov 18, 1979 at 0456 LT
Type of aircraft:
Operator:
Registration:
N859U
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Ogden-Hill - Nellis
MSN:
2016
YOM:
1960
Flight number:
3N18
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
20000
Captain / Total hours on type:
3140.00
Copilot / Total flying hours:
3140
Copilot / Total hours on type:
2715
Aircraft flight hours:
41764
Circumstances:
The four engine airplane departed Ogden-Hill AFB at 0445LT on a cargo flight to Nellis AFB on behalf of the USAF, carrying three crew members and 27,552 lbs of cargo. While climbing from 12,000 to 13,000 feet, the flight indicated to Salt Lake departure control that they had lost all electrical power, the flight requested no-gyro vectors to visual flight conditions and clearance for an immediate descent to a lower altitude. During the descent, the aircraft attained a high airspeed and high rate of descent and disintegrated in flight. The three crewmembers were killed and the aircraft was destroyed. The wreckage was dispersed along a path about 1 1/2 miles long on an abandoned airport located about 4 nmi south of the Salt Lake City International Airport.
Probable cause:
The National Transportation Safety Board determines that the probable cause of this accident was a progressive failure in the aircraft's electrical system leading to the disabling or erratic performance of some critical flight instruments and flight instrument lighting while the flight was operating in night instrument meteorological conditions. As a result of these conditions, the flightcrew could not resolve the instrumentation anomalies to determine proper aircraft attitude reference, and became disoriented and lost control of the aircraft. The crew's efforts to regain control of the aircraft imDOSed aerodynamic loads which exceeded design limits of the ahraft and caused it to break up in flight.
Final Report:

Crash of a Cessna 421C Golden Eagle III near Spanish Fork: 5 killed

Date & Time: Jan 9, 1979 at 1710 LT
Operator:
Registration:
N5469G
Flight Phase:
Survivors:
No
Site:
Schedule:
Provo - San Francisco
MSN:
421C-0216
YOM:
1972
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
2629
Captain / Total hours on type:
52.00
Circumstances:
Few minutes after takeoff from Provo Airport, while climbing in marginal weather conditions and limited visibility, the twin engine airplane struck the slope of a mountain located near Spanish Fork, few miles southeast of Provo. The wreckage was found four days later, on January 13. All five occupants were killed.
Probable cause:
Controlled collision with ground from climb to cruise due to improper IFR operation. The following contributing factors were reported:
- Inadequate preflight preparation,
- Low ceiling,
- Fog,
- Snow,
- Visibility 3/4 mile or less.
Final Report:

Crash of a Douglas DC-8-54F near Kaysville: 3 killed

Date & Time: Dec 18, 1977 at 0138 LT
Type of aircraft:
Operator:
Registration:
N8047U
Flight Type:
Survivors:
No
Site:
Schedule:
San Francisco – Salt Lake City – Chicago
MSN:
45880/275
YOM:
1966
Flight number:
UA2860
Location:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
14954
Captain / Total hours on type:
4148.00
Copilot / Total flying hours:
9905
Copilot / Total hours on type:
366
Aircraft flight hours:
29832
Circumstances:
About 0138:28 m.s.t. on December 18, 1977, a United Airlines, Inc., DC-8F-54 cargo aircraft, operating as Flight 2860, crashed into a mountain in the Wasatch Range near Kaysville, Utah. The three flightcrew members, the only persons aboard the aircraft, were killed, and the aircraft was destroyed. Flight 2860 encountered electrical system problems during its descent and approach to the Salt Lake City Airport. The flight requested a holding clearance which was given by the approach controller and accepted by the flight crew. The flight then requested and received clearance to leave the approach control frequency for a "little minute" to communicate with company maintenance. Flight 2860 was absent from the Approach control frequency for 7 1/2 minutes. During that time, the flight entered an area near hazardous terrain. The approach controller recognized Flight 2860's predicament but was unable to contact the flight. When flight 2860 returned to approach control frequency, the controller told the flight that it was too close to terrain on its right and to make a left turn. After the controller repeated the instructions, the flight began a left turn and about 15 seconds later the controller told the flight to climb immediately to 8,000 feet. Eleven seconds later, the flight reported that it was climbing from 6,000 feet to 8,000 feet. The flight crashed into a 7,665-foot mountain near the 7,200-foot level. The aircraft was destroyed and all three crew members were killed.
Probable cause:
The approach controller's issuance and the flight crew's acceptance of an incomplete and ambiguous holding clearance in combination with the flight crew's failure to adhere to prescribed impairment-of-communications procedures and prescribed holding procedures. The controller's and flight crew's actions are attributed to probable habits of imprecise communication and of imprecise adherence to procedures developed through years of exposure to operations in a radar environment. Contributing to the accident was the failure of the aircraft's No.1 electrical system for unknown reasons.
Final Report:

Crash of a Rockwell Grand Commander 690A in Kingston: 1 killed

Date & Time: Nov 12, 1974 at 1804 LT
Operator:
Registration:
N40MP
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Phoenix - Butte
MSN:
690-11116
YOM:
1973
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
2754
Captain / Total hours on type:
200.00
Circumstances:
While cruising by night at an altitude of 17,500 feet on a ferry flight from Phoenix to Butte, the twin engine airplane collided with a USAF General Dynamics F-111A Aardvark registered 67-0055. Following the collision, both aircraft entered a dive and crashed in flames near Kingston. The pilot of the Commander was killed while both military pilots were seriously injured.
Probable cause:
The collision occurred by night when the aircraft was not under radar contact with no control. It is understood that the F-111 crew had a rendezvous with the crew of a USAF Boeing KC-135 refueling plane for a night exercise but he mistook the Commander that was struck from the rear with a 0-10° angle.
Final Report:

Crash of a Rockwell Aero Commander 560 near Bicknell: 2 killed

Date & Time: Nov 2, 1974 at 1015 LT
Registration:
N867G
Flight Phase:
Survivors:
No
Site:
Schedule:
Milford - Grand Junction
MSN:
560-228
YOM:
1955
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
900
Captain / Total hours on type:
200.00
Circumstances:
En route from Milford (Utah) to Grand Junction, Colorado, the pilot encountered poor weather conditions with limited visibility due to clouds, snow falls and icing conditions. In cruising altitude, he lost control of the airplane that entered a dive and crashed in mountainous terrain located near Bicknell. The wreckage was found nine days later on November 11. Both occupants have been killed.
Probable cause:
Loss of control after the pilot continued VFR flight into adverse weather conditions. The following contributing factors were reported:
- Improper in-flight decisions or planning,
- Ice-propeller,
- Airframe ice,
- Low ceiling,
- Snow, blowing snow,
- Icing conditions, including sleet and/or freezing rain,
- Attempted flight in known icing conditions,
- Aircraft had no airframe-prop ice protection.
Final Report:

Crash of a Cessna 402B in Logan

Date & Time: May 31, 1974 at 1440 LT
Type of aircraft:
Operator:
Registration:
N69391
Flight Phase:
Survivors:
Yes
Schedule:
Logan - Roosevelt
MSN:
402B-0529
YOM:
1973
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1485
Captain / Total hours on type:
32.00
Circumstances:
Shortly after takeoff from Logan-Cache Airport, while in initial climb, the front left cargo door opened, detached and struck the tail. The pilot was unable to maintain a safe control of the airplane that crash landed in a field past the runway end. All seven occupants were injured, one of them seriously.
Probable cause:
Inadvertent opening of the front left cargo door during initial climb for undetermined reason. The following factors were reported:
- Material failure and previous damage,
- High density altitude of 6,000 feet,
- Support bar broken.
Final Report:

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 421B Golden Eagle I in Roosevelt: 2 killed

Date & Time: Nov 21, 1973 at 1050 LT
Operator:
Registration:
N2217Q
Flight Phase:
Survivors:
No
Schedule:
Provo - Omaha
MSN:
421B-0017
YOM:
1970
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
18000
Captain / Total hours on type:
458.00
Circumstances:
While in cruising altitude, the pilot encountered problems with the left propeller and lost control of the airplane that dove into the ground and crashed in Roosevelt. The aircraft was destroyed and both occupants were killed.
Probable cause:
Powerplant failure caused by a propeller and accessories (governors) technical issue. The following factors were reported:
- Governors disconnected,
- Failed to maintain flying speed,
- Improper operation of flight controls,
- Physical impairment,
- Suspected mechanical discrepancy,
- Left governors lower spring seat/thrust bearing of pilot valve plunger loose,
- Possibility of hypoglycemic reaction.
Final Report: