Crash of a Rockwell 500U Shrike Commander on Mt Barren Jack: 2 killed

Date & Time: Nov 18, 1989 at 1241 LT
Operator:
Registration:
VH-BMR
Flight Phase:
Survivors:
No
Site:
Schedule:
Canberra – Dalby
MSN:
500-1754-45
YOM:
1968
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
When the survey aircraft failed to arrive at the destination, and on expiry of the SAR time, a search was commenced. Wreckage of the aircraft was subsequently found on the eastern slope of Mt Barren Jack, to the north west of the mouth of Carrolls Creek, and on the planned track for the survey operation. Observers at the Burrinjuck reservoir near the mouth of Carrolls Creek described the weather in the accident area at the time as black clouds spilling over and obscuring the mountain tops. The aircraft collided with trees on the side of the mountain, while banked steeply to the right and in a tail low attitude. The pilot was thrown from the aircraft during the impact sequence. Medical opinion held that there was no evidence of body trauma consistent with the seat belt being fastened at the time of impact. The flight was completed on behalf of the Bureau of Mineral Resources (BMR) and both occupants were killed.
Probable cause:
Because of the destruction of the aircraft by the ensuing fire the status of the seat belt assemblies were unable to be determined. The investigation revealed that both engines were operating at high power at the time of impact. No malfunction or defect could be found with the aircraft which could have contributed to the accident. The survey task required the pilot to adhere strictly to a particular track and the target height for the flight was 500 feet above ground level while maintaining visual contact with the ground at all times. The pilot was suitably qualified to act as pilot in command of survey operations down to a height of 200 feet above ground level. The investigation concluded that the aircraft was being operated at a height substantially lower that 500 feet above ground level prior to the accident. Impact marks, wreckage and mechanical evidence suggest that the aircraft impacted terrain at a time when the pilot was attempting to carry out an evasive manoeuvre to remain clear of terrain. The reason why the aircraft was being operated at such a height and why the pilot delayed turning away from the steeply rising terrain could not be determined.
The following factors were reported:
- The pilot continued the flight into adverse weather conditions.
- The pilot flew the aircraft towards steeply rising terrain at a height substantially lower that 500 feet above ground level.
Final Report:

Crash of a Rockwell Shrike Commander 500S off Caldera: 2 killed

Date & Time: Nov 6, 1988
Registration:
CC-CFL
Flight Phase:
Survivors:
No
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
Crashed in unknown circumstances in the sea off Caldera. Both pilots were killed.

Crash of a Rockwell Shrike Commander 500S in Mount Garnet

Date & Time: May 20, 1988 at 1750 LT
Operator:
Registration:
VH-SDI
Survivors:
Yes
Schedule:
Kidston – Cairns
MSN:
500-3188
YOM:
1974
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The pilot was temporarily replacing the pilot who normally flew the aircraft. After arriving at Kidston he checked the fuel quantity gauge and decided that there was sufficient fuel on board for the return flight. As the aircraft approached top of climb, the pilot found that the fuel gauge indicated a lower fuel quantity than he had expected. He re-checked the indicated quantity after the aircraft was established in cruise and decided that sufficient fuel still remained to complete the planned flight. Shortly after passing Mt Garnet both engine fuel flow gauges began to fluctuate and the engines began to surge. The pilot immediately turned the aircraft towards the Mt Garnet strip, but shortly afterwards both engines failed. The pilot attempted to glide the aircraft to the strip, but it collided with trees and came to rest about one kilometre from the runway 27 threshold. All three occupants escaped with minor injuries and the aircraft was damaged beyond repair.
Probable cause:
Both engines had failed due to fuel exhaustion. The pilot normally flew a different type of aircraft, this aircraft only being used by the company to supplement its services. For company aircraft normal route fuel requirements are specified. As a result, there was little need for him to make significant fuel calculations. On this occasion, the pilot found he had little time between his arrival at Cairns and the scheduled DEPARTURE of his next flight. He ordered that only 80 litres of fuel be added to the aircraft tanks. The calculated fuel burn for the proposed return flight to Kidston was approximately 240 litres. However, on DEPARTURE from Cairns it was estimated that only about 220 litres of fuel was in the aircraft tanks. Refuelling facilities were available at Kidston but no fuel was added to the aircraft tanks.
The following factors were considered relevant to the development of the accident:
1. The aircraft design is such that the fuel quantity can only be determined by the gauge, unless the tanks are full.
2. The preflight preparation, in relation to fuel requirements, carried out by the pilot was inadequate.
3. The pilot lacked recent experience at more complex fuel calculations.
Final Report:

Crash of a Rockwell Shrike Commander 500S in Tolcayuca

Date & Time: May 17, 1988
Operator:
Registration:
ETL-1269
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
MSN:
500-3248
YOM:
1975
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in a hilly terrain in Tolcayuca while completing a training flight. All three pilots were injured.

Crash of a Rockwell Shrike Commander 500S in Louws Creek: 2 killed

Date & Time: May 17, 1988
Operator:
Registration:
C9-AOO
Flight Phase:
Survivors:
Yes
MSN:
500-3179
YOM:
1974
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
En route, the twin engine airplane encountered poor weather conditions and crashed near Louws Creek. One occupant was seriously injured while two others were killed.

Crash of a Rockwell Shrike Commander 500S near Canning Dam: 2 killed

Date & Time: Feb 27, 1986 at 0807 LT
Operator:
Registration:
VH-SDO
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Jandakot - Jandakot
MSN:
500-3263
YOM:
1976
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The flight was planned to check the onboard survey equipment. After departing Jandakot the aircraft operated to the south of the airfield for about 80 minutes before the pilot advised that he would be extending his operation to the east over the Darling Ranges. The aircraft was then sighted, by several witnesses, over the foothills heading in an easterly direction. These witnesses reported that the engines were not operating normally. A short time later, the aircraft was observed to pass over the dam wall at an altitude of about 25 feet and head down a valley in a northerly direction before disappearing from sight. An inspection of the wreckage indicated that the aircraft had collided with two 30 metre high trees, in a nose high attitude at a low forward airspeed, before falling to the ground below the trees. At impact neither engine was delivering power. The fuel system, which was found to be relatively intact, contained only nine litres of fuel.
Probable cause:
It was determined that the engines failed due to fuel starvation following the exhaustion of the useable fuel onboard the aircraft. The pilot was then faced with attempting a landing in unsuitable
terrain. Evidence indicates that the aircraft departed Jandakot with both the fuel quantity indicating systems unserviceable. Although the maintenance documentation for the aircraft did not indicate that these systems were unserviceable, it is believed that the pilot was aware of the maintenance state of the aircraft before departure.
Final Report:

Crash of a Rockwell Shrike Commander 500S in Des Moines: 7 killed

Date & Time: Nov 25, 1985 at 1742 LT
Operator:
Registration:
N81589
Flight Type:
Survivors:
No
Schedule:
Milwaukee - Des Moines
MSN:
500-3297
YOM:
1976
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
7
Captain / Total flying hours:
7020
Captain / Total hours on type:
1553.00
Aircraft flight hours:
3185
Circumstances:
N81589 was following a Boeing 727 on ILS approach in IFR conditions. Approximately 2.5 miles from runway, N81589 suddenly deviated left nearly 90°. 39 seconds later, pilot reported he encountered severe turbulences, then said he was trying to climb. N81589 subsequently flew thru tree tops on rising terrain for approximately 2 city blocks, then hit power lines and a pole and crashed against a tree. No evidence of turbulences due to weather at/near approach altitude. Investigation showed 4.7 miles separation between aircraft when the 727 passed the point of deviation (pod). At pod, the 727 was on the ILS glide slope at 850 feet; N81589's altitude was not determined. Wind was from 120° at 3 to 6 knots, shifting more southerly withalt. Prevailing visibility was 1/2 mile; RVR for runway 12L was 6,000 feet; light rime icing was reported. Witnesses heard power interruption of one engine at pod; but there was no indication of power loss where aircraft hit trees. Radar data showed aircraft slowed to 80 knots at pod, accelerated to 100 knots during deviation, slowed to 70 knots before impact; vmca was 74 knots. Safety board believes the pilot most likely lost control due to slow speed and light airframe icing; possibly encountered wake turbulences. No reason found for loss of engine power. All seven occupants were killed.
Probable cause:
Occurrence #1: loss of control - in flight
Phase of operation: approach - faf/outer marker to threshold (ifr)
Findings
1. (f) light condition - dark night
2. (f) weather condition - low ceiling
3. (f) weather condition - fog
4. (f) weather condition - rain
5. (f) weather condition - icing conditions
6. (c) wing - ice
----------
Occurrence #2: altitude deviation,uncontrolled
Phase of operation: approach - faf/outer marker to threshold (ifr)
Findings
7. (f) airspeed - reduced - pilot in command
8. (c) airspeed - inadequate - pilot in command
9. (c) aircraft handling - not maintained - pilot in command
10. Descent - uncontrolled
11. Directional control - not maintained
12. Remedial action - initiated
13. Level off - performed
----------
Occurrence #3: loss of engine power
Phase of operation: approach
Findings
14. (f) reason for occurrence undetermined
----------
Occurrence #4: in flight collision with object
Phase of operation: approach
Findings
15. (f) terrain condition - rising
16. Proper climb rate - not possible
17. Stall/mush
18. (f) object - tree(s)
19. (f) object - wire, transmission
20. (f) object - utility pole
----------
Occurrence #5: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Rockwell Shrike Commander 500S in Cloquet: 1 killed

Date & Time: Sep 16, 1985 at 2205 LT
Operator:
Registration:
N8139P
Survivors:
No
Schedule:
Brainerd - Cloquet
MSN:
500-3265
YOM:
1975
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
12750
Captain / Total hours on type:
3000.00
Aircraft flight hours:
4317
Circumstances:
The pilot expected the weather to be below minimums but flew the approach anyway. He did not have a second pilot on board per company rules. The aircraft collided with trees about 3 miles from the approach end of runway 17. The pilot, sole on board, was killed.
Probable cause:
Occurrence #1: undershoot
Phase of operation: approach - faf/outer marker to threshold (ifr)
Findings
1. (c) in-flight planning/decision - improper - pilot in command
2. (c) minimum descent altitude - below - pilot in command
3. (c) ifr procedure - improper - pilot in command
4. (f) weather condition - low ceiling
5. (c) overconfidence in personal ability - pilot in command
6. (f) light condition - dark night
----------
Occurrence #2: in flight collision with object
Phase of operation: approach - faf/outer marker to threshold (ifr)
Findings
7. Object - tree(s)
Final Report:

Crash of a Rockwell Shrike Commander 500S off Norfolk Island: 1 killed

Date & Time: Sep 11, 1984
Operator:
Registration:
N9031N
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Pago Pago – Norfolk Island – Sydney
MSN:
500-1867-43
YOM:
1969
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
After takeoff from Norfolk Island Airport, while climbing, the twin engine aircraft lost height and crashed into the sea. The pilot, sole on board, was killed.

Crash of a Rockwell 500S Shrike Commander in Chilpancingo: 4 killed

Date & Time: Jan 31, 1983
Operator:
Flight Phase:
Flight Type:
Survivors:
No
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
After takeoff from Doctor Alfonso G. Alarcón Airport, the twin engine airplane encountered difficulties to gain height and crashed on Mt El Torre located about 3 km from the airfield. All four occupants were killed.