Crash of a Rockwell Turbo Commander 680 near Bangkok: 2 killed

Date & Time: Jul 22, 1984
Operator:
Registration:
HS-TFB
Survivors:
Yes
Schedule:
Tak - Bangkok
MSN:
680-1573-28
YOM:
1966
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
On final approach to Bangkok-Don Mueang Airport, the crew encountered engine trouble when the airplane stalled and crashed in a rice paddy field located 12 km from the runway 19 threshold. Three occupants were killed while five others were injured.

Crash of a Rockwell Turbo Commander 680TV in Castle Rock

Date & Time: Jul 11, 1984 at 1616 LT
Registration:
N932E
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Seattle - Hillsboro
MSN:
680-1588-39
YOM:
1966
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5000
Captain / Total hours on type:
75.00
Circumstances:
The aircraft was on a cross country trip. On previous flights over the same route, two refueling stops were made. During this trip, no refueling was accomplished, and while en route, the low fuel warning light came on. The pilot declared an emergency and was vectored and assigned the lowest possible IFR altitude. Shortly thereafter, both engines quit. When he enquired about nearby airports, the pilot was told there were none and advised to find a road or suitable area to land. The pilot overshot a road after feathering both engines and crashed on an embankment. There was no smell of fuel at the scene of the crash. Both props were in the feathered position. The pilot was injured.
Probable cause:
Occurrence #1: loss of engine power (total) - nonmechanical
Phase of operation: descent
Findings
1. (c) aircraft preflight - inadequate - pilot in command
2. Refueling - not performed - pilot in command
3. (c) fluid, fuel - exhaustion
4. (c) fuel supply - inadequate - pilot in command
5. Aircraft performance, two or more engines - inoperative
----------
Occurrence #2: forced landing
Phase of operation: descent - emergency
Findings
6. Propeller feathering - performed - pilot in command
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: landing - flare/touchdown
Findings
7. (f) terrain condition - high vegetation
8. (f) terrain condition - uphill
9. (f) terrain condition - rough/uneven
Final Report:

Crash of a Rockwell 680W Turbo II Commander in Atlanta

Date & Time: Nov 20, 1982 at 1930 LT
Operator:
Registration:
N5058E
Flight Type:
Survivors:
Yes
Schedule:
Charlotte - Atlanta
MSN:
680-1787-17
YOM:
1968
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3420
Captain / Total hours on type:
143.00
Aircraft flight hours:
2306
Circumstances:
The pilot reported that on the previous flight, the center fuel tank gauge was malfunctioning and indicated 800 lbs even when it was full with 1400 lbs. After landing at Charlotte, NC, it was still indicating 800 lbs. Before takeoff, the center tank was refilled. While en route about 40 miles west of Atlanta, GA, the pilot noted that the fuel gauge indicated 500 lbs and was dropping rapidly. A few minutes later, both engines flamed out. Vectors were obtained to fly to the nearest airport. During the descent, the engines were restarted. The pilot intercepted the ILS and remained high on the glide slope. The weather at the airport was reported as 100 feet overcast, visibility 1/4 mile with fog and rain. The aircraft broke out of the clouds approximately 2/3 of the way down the runway, then continued off the end of the runway and went thru ILS antenna array. An exam revealed the center fuel cap was missing, it was found in the grass near the parking ramp at Charlotte. The fuel cap was found to be worn and would not lock securely.
Probable cause:
Occurrence #1: loss of engine power(total) - non mechanical
Phase of operation: cruise - normal
Findings
1. (f) engine instruments,fuel quantity gauge - incorrect
2. (f) operation with known deficiencies in equipment - performed - pilot in command
3. (c) fuel system,cap - worn
4. (c) fuel system,cap - separation
5. (c) fluid,fuel - loss,partial
6. (c) fluid,fuel - starvation
7. Aircraft performance,two or more engines - inoperative
----------
Occurrence #2: overrun
Phase of operation: landing - roll
Findings
8. Emergency procedure - performed - pilot in command
9. Precautionary landing - performed - pilot in command
10. (f) weather condition - low ceiling
11. (f) weather condition - fog
----------
Occurrence #3: on ground/water collision with object
Phase of operation: landing - roll
Findings
12. (f) object - approach light/navaid
Final Report:

Crash of a Rockwell Turbo Commander 680 near Dumfries

Date & Time: Nov 15, 1982
Registration:
N89DA
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
680-1702-78
YOM:
1967
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The twin engine airplane crashed in unknown circumstances in a field near Dumfries, about 15 km southeast of Montego Bay, Jamaica. Both pilots were not found and the airplane was damaged beyond repair. It was engaged in an illegal contraband mission.

Crash of a Rockwell Turbo Commander 681 in Winnemucca: 2 killed

Date & Time: Jan 27, 1981 at 2230 LT
Operator:
Registration:
N500JP
Survivors:
Yes
Schedule:
Reno - Winnemucca
MSN:
681-6003
YOM:
1969
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total hours on type:
60.00
Circumstances:
The approach to Winnemucca was completed by night and poor weather conditions. On final, the airplane struck the ground below airport elevation and crashed. The pilot and a passenger were killed while a second passenger was seriously injured.
Probable cause:
Controlled collision with ground on final approach due to improper IFR operation. The following contributing factors were reported:
- Rain,
- Snow,
- Turbulences associated with clouds and thunderstorms,
- Obstructions to vision,
- Weather slightly worse than forecast.
Final Report:

Crash of a Rockwell Turbo Commander 680W II off South Bimini

Date & Time: Mar 23, 1980
Registration:
N93RA
Flight Phase:
Flight Type:
MSN:
680-1722-2
YOM:
1968
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances into the sea off South Bimini Airport. Occupant fate unknown.

Crash of a Rockwell 680W Turbo Commander II near Niedernach: 1 killed

Date & Time: Dec 27, 1978 at 1045 LT
Operator:
Registration:
D-IMON
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Essen - Innsbruck
MSN:
680-1819-33
YOM:
1968
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
While in cruising altitude on a positioning flight from Essen-Mülheim Airport to Innsbruck-Kranebitten Airport, the pilot lost control of the airplane that entered a dive and crashed in the Walchensee (Walchen Lake) off Niedernach, Bavaria. The aircraft was destroyed upon impact and the pilot, sole on board, was killed.
Probable cause:
It was reported that the tail separated in flight for unknown reasons.

Crash of a Rockwell 680W Turbo Commander II in Lucerne Valley

Date & Time: Nov 11, 1978 at 0300 LT
Registration:
N94HD
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
Schedule:
San Diego - Las Vegas
MSN:
680-1811-28
YOM:
1968
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5420
Captain / Total hours on type:
1105.00
Circumstances:
While in cruising altitude on a flight from San Diego to Las Vegas, the pilot suffered physical impairment. The airplane crashed in a desert area near Lucerne Valley. The pilot was seriously injured and the aircraft was written off.
Probable cause:
Controlled collision with ground after the pilot suffered in-flight physical impairment. Two micrograms per milliliter of benzodiazepine found in his blood sample.
Final Report:

Crash of a Rockwell Hawk Commander 681 in Greenup: 3 killed

Date & Time: Mar 8, 1978 at 1008 LT
Operator:
Registration:
N5NP
Survivors:
No
Schedule:
Milwaukee – Manchester – Huntington
MSN:
680-6042
YOM:
1970
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
9154
Captain / Total hours on type:
1395.00
Circumstances:
En route, the crew encountered engine problems and was cleared to divert to Ashland Airport. While descending in marginal weather conditions (low ceiling, fog and icing conditions), the crew lost control of the airplane that crashed in a field located in Greenup, west of the airport. The aircraft was destroyed and all three occupants were killed. At the time of the accident, weather conditions were below minimums.
Probable cause:
Uncontrolled collision with ground on final approach following a powerplant failure for undetermined reasons. The following contributing factors were reported:
- Failed to follow approved procedures,
- Improper emergency procedures,
- Low ceiling,
- Fog,
- Icing conditions including sleet, freezing rain,
- Partial loss of power on one engine,
- Forced landing off airport on land,
- Visibility half a mile or less,
- Weather conditions below minimums.
Final Report:

Crash of a Rockwell Aero Commander 681 Mestersvig: 2 killed

Date & Time: Jul 23, 1973
Operator:
Registration:
SE-FGE
Flight Type:
Survivors:
No
Schedule:
Mestersvig - Mestersvig
MSN:
681-6033
YOM:
1969
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew was returning to Mestersvig Airport following a mapping mission. On final approach, the twin engine airplane crashed 400 meters short of runway threshold. Both occupants were killed.