Crash of a Rockwell Aero Commander 560 in Hibbing

Date & Time: May 19, 1971 at 1525 LT
Registration:
N445TK
Flight Type:
Survivors:
Yes
Schedule:
Chicago - International Falls
MSN:
560-209
YOM:
1955
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1983
Captain / Total hours on type:
100.00
Circumstances:
En route from Chicago to International Falls, while in cruising altitude, the crew encountered poor weather with icing conditions. The pilot-in-command was cleared to divert to the nearest airport and started to descend. On approach to Hibbing-Chisholm Airport, the crew did not land but initiated a go-around. After passing over the runway end, control was lost and the airplane crashed in a field. The aircraft was destroyed and both pilots were seriously injured.
Probable cause:
Inadequate preflight preparation on part of the crew. The following factors were reported:
- Rain, snow and icing conditions including sleet and freezing rain,
- Airframe ice,
- Adverse/unfavorable weather conditions,
- Icing conditions forecasted,
- No de-icing equipment on aircraft,
- First approach missed.
Final Report:

Crash of a Rockwell Aero Commander 560 in Helendale: 2 killed

Date & Time: Mar 19, 1971 at 1145 LT
Registration:
N2727B
Flight Type:
Survivors:
No
Schedule:
Van Nuys – Helendale
MSN:
560-227
YOM:
1955
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
400
Captain / Total hours on type:
4.00
Circumstances:
While on approach to Helendale Airport, the twin engine aircraft speed was too low. The left wing dropped and the airplane dove into the ground and crashed in flames. Both occupants were killed. They were completing an electrical chute device drop test from Van Nuys Airport.
Probable cause:
The pilot-in-command failed to maintain flying speed. The following factors were reported:
- Lack of familiarity with aircraft.
Final Report:

Crash of a Rockwell Aero Commander 560f in Latham: 2 killed

Date & Time: Aug 16, 1970 at 1045 LT
Registration:
N560F
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Portsmouth - Dayton
MSN:
560-1034-13
YOM:
1961
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
2249
Captain / Total hours on type:
750.00
Circumstances:
En route, the pilot informed ATC about an engine failure and elected to divert to the nearest airport. While flying at low height, the airplane struck power cables and tree tops before crashing onto the ground. The wreckage was found in an isolated area three days later. The airplane was destroyed and both occupants were killed.
Probable cause:
The cause of the engine failure could not be determined.
Final Report:

Crash of a Rockwell Aero Commander 560F in Chavantes

Date & Time: Sep 23, 1969
Registration:
PT-BKN
MSN:
560-1197-45
YOM:
1962
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances.

Crash of a Rockwell Aero Commander 560A in Crossville: 5 killed

Date & Time: Mar 29, 1969 at 1129 LT
Operator:
Registration:
N2761B
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Benton Harbor - Atlanta
MSN:
560-442
YOM:
1956
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
889
Captain / Total hours on type:
236.00
Circumstances:
While in cruising altitude in poor weather conditions, the pilot lost control of the airplane that entered a dive and crashed few dozen seconds later in a huge explosion. All five occupants were killed.
Probable cause:
The accident was probably caused by the combination of the following factors:
- The pilot attempted operation with known deficiencies in equipment,
- The pilot failed to obtain/maintain flying speed,
- Icing conditions including sleet, freezing rain,
- Turbulences associated with clouds and thunderstorms,
- Airframe ice,
- Ice carburetor,
- The pilot entered known icing conditions with no prop or airframe de-icing systems on aircraft.
Final Report:

Crash of a Rockwell Aero Commander 560F near Wolf Creek: 3 killed

Date & Time: Dec 8, 1968 at 1055 LT
Registration:
N6257X
Flight Phase:
Survivors:
No
Schedule:
Great Falls - Missoula
MSN:
560-1115-33
YOM:
1961
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
7157
Captain / Total hours on type:
107.00
Circumstances:
While in cruising altitude, the pilot encountered poor weather conditions with thunderstorm activity, turbulences, high winds and freezing rain. Under VFR mode, he lost control of the airplane that dove into the ground and crashed. All three occupants were killed.
Probable cause:
The accident was probably caused by the combination of the following factors:
- The pilot continued under VFR mode into adverse weather conditions,
- Loss of control for undetermined reason,
- Icing conditions including sleet and freezing rain,
- Turbulences associated with clouds and thunderstorms,
- Flew into known turbulences.
Final Report:

Crash of a Rockwell Aero Commander 560A in Málaga: 6 killed

Date & Time: Nov 9, 1968
Registration:
HK-1079
Survivors:
Yes
Schedule:
Bucaramanga – Málaga
MSN:
560-292
YOM:
1956
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
Crashed in unknown circumstances while approaching Málaga Airport on a taxi flight from Bucaramanga. A passenger survived while six other occupants were killed.

Crash of a Rockwell Aero Commander 560 in Dilley

Date & Time: Mar 22, 1968 at 1450 LT
Operator:
Registration:
N855LB
Flight Type:
Survivors:
Yes
MSN:
560-176
YOM:
1954
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
2100
Captain / Total hours on type:
500.00
Circumstances:
On final approach to Dilley Airpark, both engines stopped simultaneously. The pilot lost control of the airplane that stalled, struck trees and crashed in Hilltop, northeast of the airport. Both occupants were seriously injured and the aircraft was destroyed.
Probable cause:
Complete failure of both engines due to fuel exhaustion. Inadequate preflight preparation on part of the pilot who was inattentive to fuel supply.
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 Rockwell Aero Commander 560E in Kingshill: 2 killed

Date & Time: Dec 12, 1967 at 1140 LT
Registration:
N8448C
Flight Type:
Survivors:
No
Schedule:
Christiansted - Christiansted
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
10850
Captain / Total hours on type:
500.00
Circumstances:
The crew was completing a local training flight at Christiansted-Alexander Hamilton Airport. While approaching from the north, the airplane stalled and crashed in Kinsghill, about 2 miles north of the airfield. The aircraft was destroyed and both pilots were killed.
Probable cause:
Loss of control while practicing single engine approach. The crew failed to maintain flying speed and inadequate flight supervision.
Final Report: