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

Date & Time: Nov 8, 1981
Operator:
Registration:
VH-TOL
Flight Phase:
Survivors:
No
MSN:
500-3174
YOM:
1973
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
After takeoff from Merimbula Airport, while climbing, the twin engine airplane went out of control and crashed in the marina of Merimbula. The pilot, sole on board, was killed.

Crash of a Rockwell Shrike Commander 500S in Healy

Date & Time: Aug 12, 1981 at 1000 LT
Operator:
Registration:
N5075E
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Healy - Anchorage
MSN:
500-1855-37
YOM:
1968
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5500
Captain / Total hours on type:
58.00
Circumstances:
After takeoff from Healy, while climbing, the pilot lost control of the airplane that struck trees and crashed near the airport. The pilot was injured and the aircraft was destroyed.
Probable cause:
Collision with trees during initial climb due to inadequate preflight preparation on part of the pilot. The following contributing factors were reported:
- Unfavorable wind conditions,
- Wind gusting 20 knots at airport,
- Wind variable and gusting 50 knots approximately 1,5 mile either side of airport.
Final Report:

Crash of a Rockwell Shrike Commander 500S off Hobart

Date & Time: Apr 27, 1981 at 1814 LT
Operator:
Registration:
VH-EXQ
Survivors:
Yes
Schedule:
Melbourne – Hobart
MSN:
500-1831-28
YOM:
1968
Location:
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1925
Captain / Total hours on type:
77.00
Circumstances:
Due to industrial action, normal domestic airline services had been suspended. The pilot hired the aircraft to convey persons stranded by the strike between Hobart and Melbourne. He submitted a flight plan for the proposed return flight to Melbourne that nominated operations under the Instrument Flight Rules, although he did not hold an appropriate Instrument Rating. The flight to Melbourne was completed without known incident. After refuelling the aircraft and engaging five passengers, the return flight was commenced. A fare was paid by each passenger although the pilot did not hold either a Charter Licence or an appropriate pilot licence. There was considerable cloud in the vicinity of Hobart Airport which, at 1800 hours, was recorded as one okta stratus, base 800 feet; five oktas stratocumulus, base 3000 feet; five oktas altocumulus, base 11,000 feet. The surface wind was a light westerly, and the runway in use was Runway 30. There were rain showers in the area and the runway was wet. The end of daylight was at approximately 1748 hours. When the pilot of VH-EXQ contacted Hobart Tower at approximately 1800 hours, he reported on descent to 7000 feet and 50km from the airport. As the aircraft proceeded, the Aerodrome Controller cleared it for further descent in stages, to provide vertical separation from a preceding aircraft. The only Instrument Landing System (ILS) approach at Hobart Airport was aligned with Runway 12 and the tailwind for a landing in that direction was only two or three knots. In order to expedite their arrivals, the Aerodrome Controller offered the pilot s of both approaching aircraft the option of a straight-in ILS approach to Runway 12 instead of a circling approach to the into-wind Runway 30. Both pilots accepted. At 1803 hours, the preceding aircraft was cleared for an ILS approach. The pilot of VH-EXQ was then advised to expect the same clearance but, to ensure continued separation from the other aircraft, was instructed to make one circuit of the holding pattern at Tea Tree Locator, a navigational radio aid west of the airport. The pilot misunderstood this instruction and, on reaching Tea Tree at about 1805 hours, he continued towards the airport. At 1807 hours, the Aerodrome Controller cleared VH-EXQ for an ILS approach. The pilot acknowledged this instruction in the normal manner and did not advise that he had already commenced the approach. In descending towards the airport the pilot had maintained a high airspeed of nearly 200 knots. From overhead Tea Tree he could see the lights of the preceding aircraft and endeavoured to reduce his speed so as to maintain separation. As a result, the aircraft was still very high as it approached the runway. This was noted by the Aerodrome Controller and, at 1810 hours, he asked the pilot whether he would be able to land on Runway 12 or would prefer to make an approach for Runway 30. The pilot chose the latter and was cleared to a right base leg for Runway 30. The approach to Runway 12 was abandoned and the aircraft turned left onto a close right downwind leg for Runway 30. The landing gear, which had been extended, and the flaps, which had been set at 1/4 down, were not moved from these positions. The pilot reported that at some stage of the approach to Runway 30 he moved the throttles forward to increase power and maintain height. In response the aircraft yawed slightly to the right. Both propeller levers were then pushed fully forward, both throttles were fully opened and the mixture controls were checked in the full-rich position. The aircraft again swung to the right. Identifying this as evidence that the right engine had failed, and after checking from the tachometer that the right propeller was windmilling at about 1500 RPM, the pilot feathered the right propeller and selected the landing gear and flaps up. He believed that he carried out the feathering action at a height of about 300 feet and an airspeed of about 100 knots. At this time the aircraft was heading southwest, towards Single Hill (elevation 680 feet) on the shore of Frederick Henry Bay. The pilot reported that the aircraft would not maintain height or airspeed and he therefore turned left to avoid the hill. The wings were then held level until the aircraft touched down in the bay. After the aircraft turned right at a close base leg position, but then straightened on a southwesterly heading instead of continuing the turn onto final approach, the Aerodrome Controller asked the pilot to confirm that he was tracking for Runway 30. This transmission was not answered and the Aerodrome Controller again called the aircraft. The pilot then reported that he was having trouble with the right engine and he was going to feather. This transmission was made as the aircraft was approaching Single Hill, just before it turned left and descended from view. There were no further transmissions from the aircraft despite a number of calls by the Aerodrome Controller. The Distress Phase of Search and Rescue (SAR) procedures was declared at 1815 hours. The appropriate emergency services were alerted including a helicopter that was on standby for SAR operations. All six occupants were rescued while the aircraft sank and was lost.
Probable cause:
The probable cause of the accident was that, following an apparent loss of power by the right engine, the pilot did not operate the aircraft in the configuration and at the airspeed necessary for safe single-engine flight. The pilot's responses may have been Influenced by operating under Instrument Flight Rules conditions, for which he was not qualified. The cause of the reported loss of power by the right engine was not determined. The following defects were discovered:
- General mechanical wear in left engine,
- Left engine fuel injector system outside manufacturer's specifications,
- Slight timing fault in one magneto on right engine.
Final Report:

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

Date & Time: Jan 21, 1981 at 0032 LT
Registration:
N222FQ
Flight Type:
Survivors:
Yes
Schedule:
College Station - Springfield
MSN:
500-1795-10
YOM:
1968
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
12033
Circumstances:
On approach by night while on a cargo flight from College Station, the pilot failed to realize his altitude was insufficient when the twin engine airplane struck trees and crashed few miles from the runway threshold. The pilot and a passenger were killed while a second passenger was seriously injured.
Probable cause:
Collision with trees on final approach due to improper IFR operation. The following contributing factors were reported:
- Pilot fatigue,
- Low ceiling,
- Fog,
- Snow,
- Visibility two miles or less,
- Witness stated that the pilot got up at 0800LT on January 20 and worked during all day before departing on a four hours flight.
Final Report:

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

Date & Time: Aug 10, 1979 at 1508 LT
Operator:
Registration:
VH-ALH
Flight Type:
Survivors:
No
Schedule:
Whitemark - Melbourne
MSN:
500-1810-20
YOM:
1968
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
8500
Captain / Total hours on type:
100.00
Circumstances:
During the morning of August 9, 1979, the aircraft was refuelled to capacity and three drums, each with a capacity of 20 litres, were also filled with fuel and placed in the baggage compartment. The aircraft, loaded with freight, subsequently departed Essendon at 1335 hours and proceeded to Cambridge where it arrived at 1536 hours. The freight was unloaded and, at 1621 hours, the aircraft departed for Launceston where it arrived at 1653 hours. It was again loaded with freight and departed Launceston at 1720 hours bound for Flinders Island. The aircraft landed at Flinders Island several minutes after the end of daylight, which was at 1745 hours, and the freight was unloaded. On the following day, the aircraft was again loaded with freight and the pilot subsequently reported departure from Flinders Island at 1329 hours, bound for Essendon. The take-off run was observed to be longer than usual for this type of aircraft and its rate of climb appeared to be less than normal. The IFR flight plan notified by the pilot before departure indicated his intention to cruise at an altitude of 4500 feet but, at 1410 hours, he reported to Melbourne Flight Service Unit "request traffic for a descent to proceed VFE we're getting 50 knot head wind here". On being advised that there was no traffic information, the pilot reported leaving 4500 feet. At 1502 hours, the pilot established communication with Essendon Tower, reported approaching Channel 0 at 1500 feet, and "request expedite clearance". He was issued with a clearance to enter controlled airspace at 1500 feet tracking from Channel 0 to Essendon via Clifton Hill. At 1506 hours he reported at Clifton Hill and, at 1507:38 hours, he advised "I'm sorry have a Mayday appear to have a fuel problem we'll have to land on a golf course". On being asked "which golf course?, the pilot replied "oh right where we are now". No further communications were received from the aircraft. The aircraft was observed by witnesses in the Northcote area initially on a north-westerly heading towards Essendon. E was seen to be descending and the sound of the engines was not normal. After flying over the northern section of the Northcote Municipal Golf Course, the aircraft commenced a descending left turn and [passed over a power transmission line which ran in a north-south direction near the western boundary of the golf course. As the turn continued towards an easterly heading, the aircraft again passed over the power line, at a very low height, and in strong tail wind conditions struck trees bordering a fairway while in a slightly left wing down, nose down, attitude. It struck the ground heavily just beyond the trees and the main wreckage travelled a further 73 metres before it came to rest on the edge of a green in the south-eastern corner of the golf course. Detailed examination of the wreckage of the aircraft revealed no evidence of any defect or malfunction which may have contributed to the accident. There was no significant fuel in the fuel systems of the two engines and there was negligible fuel in those cells of the fuel storage system which were undamaged. There was no fire. The pilot was in full time employment as an airline captain with a major operator. He was also involved financially and managerially in Norfish Pty. Ltd. and both he and the Company had financial difficulties at that time. The flight plan submitted by the pilot before departure from Essendon on August 9 contained false names in respect of both the pilot and the operator. Neither the pilot nor Norfish Pty Ltd held a Charter or Aerial Work Licence. The maximum specified take-off weight for the aircraft was 3357 kg. for VFR operations and 3243 kg. for IFR operations. It has been calculated that the gross weight of the aircraft was 3775 kg. when it departed Essendon for Cambridge on 9.8.79 and 3746 kg. when it departed Launceston for Flinders Island on the same day. The calculated gross weight was 4061 kg. when it departed Flinders Island on the day of the accident. Although fuel was available at Cambridge and Launceston, the aircraft was not refuelled after it 'departed from Essendon. The three 20 litre drums were located in the aircraft wreckage and, although all were damaged, detailed examination indicated that they ruptured under the action of hydraulic shock and that they wert filled at the time of the accident. The total operating time of the aircraft from departure Essendon until the time of the accident was consistent with a fuel endurance which could be expected in the circumstances leading to this accident.
Probable cause:
The cause of the accident was that the aircraft was operated with insufficient fuel to safely complete the flight.
Final Report:

Crash of a Rockwell Shrike Commander 500S near Chirimena: 3 killed

Date & Time: Jun 27, 1979
Registration:
YV-827P
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Porlamar - Caracas
MSN:
500-3221
YOM:
1974
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The twin engine airplane departed Porlamar Airport on a flight to La Carlota-Francisco de Miranda Airport in Caracas. After passing Cape Codera, the pilot reported his position to ATC. Shortly later, while cruising in bad weather, the airplane struck the slope of a mountain located in the region of Chirimena. All three occupants were killed.

Crash of a Rockwell Shrike Commander 500S in Sevaruyo

Date & Time: Jan 27, 1979
Operator:
Registration:
CP-1127
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
While on a positioning flight, the pilot reported engine fire to ATC and attempted an emergency landing when the airplane crashed in flames in a desert area located near Sevaruyo. The aircraft was destroyed by a post crash fire and the pilot was slightly injured.

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

Date & Time: Nov 17, 1978 at 0850 LT
Registration:
N2973F
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Gallup - Albuquerque
MSN:
500S-3062
YOM:
1970
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
1467
Captain / Total hours on type:
517.00
Circumstances:
While taking off from Gallup-Senator Clark Airport, the twin engine airplane encountered difficulties to gain height, stalled and crashed in flames. The passenger was killed while the pilot was seriously injured. The aircraft was destroyed.
Probable cause:
Stall during initial climb due to inadequate preflight preparation on part of the pilot. The following contributing factors were reported:
- Failed to maintain flying speed,
- Airframe ice,
- Improper operation of powerplant and powerplant controls,
- Frost on aircraft,
- Turbochargers not used on takeoff.
Final Report:

Crash of a Rockwell Shrike Commander 500S in Hammondsport: 3 killed

Date & Time: Sep 11, 1978 at 1925 LT
Registration:
N40MA
Survivors:
Yes
Schedule:
Raleigh - Hammondsport
MSN:
500-3234
YOM:
1975
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
6300
Circumstances:
While on approach to Hammondsport-Taylor-Van Gelder Airstrip in excellent weather conditions, the pilot failed to realize his altitude was too low when the airplane struck a mountain and crashed few miles from Hammondsport. Two passengers were rescued while three other occupants were killed.
Probable cause:
Stall on final approach after the pilot misjudged distance and altitude and failed to maintain flying speed. The following contributing factors were reported:
- Obstructions to vision,
- Sunglare,
- Haze,
- Aircraft was approaching toward rising terrain.
Final Report:

Crash of a Rockwell Shrike Commander 500U in Santa Rosa de Calamuchita: 4 killed

Date & Time: Feb 2, 1978
Operator:
Registration:
T-138
Flight Phase:
Flight Type:
Survivors:
No
MSN:
500-1757-46
YOM:
1968
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
Crashed in unknown circumstances, killing all four occupants.
Crew:
Cpt García, pilot,
S/O Valdivieso, mechanic.
Passengers:
S/O Domingo Oscar Alcaraz,
Mr. Elio Milone.