Country
code

Queensland

Crash of a Vickers 832 Viscount near Winton: 24 killed

Date & Time: Sep 22, 1966 at 1303 LT
Type of aircraft:
Operator:
Registration:
VH-RMI
Flight Phase:
Survivors:
No
Schedule:
Mount Isa – Longreach – Brisbane
MSN:
416
YOM:
1959
Flight number:
AN149
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
20
Pax fatalities:
Other fatalities:
Total fatalities:
24
Captain / Total flying hours:
14288
Captain / Total hours on type:
10003.00
Copilot / Total flying hours:
2803
Copilot / Total hours on type:
249
Aircraft flight hours:
18634
Aircraft flight cycles:
6586
Circumstances:
On 22 September 1966, the Viscount 832 aircraft registered VH-RMI, was engaged on a regular public transport service, designated Flight 149, from Mt. Isa to Longreach in Queensland, Australia, with a crew of four and twenty passengers on board. The flight departed from Mt. Isa at 1208 hours Australian Eastern Standard Time climbing to Flight Level 175 with an expected time interval of 73 minutes to Longreach. The flight progressed, apparently uneventfully, until 1252 hours when the Longreach Flight Service Unit heard the crew of VH-RMI say that it was on an emergency descent and to stand by. Two minutes later the aircraft advised that there were fire warnings in respect of Nos. 1 and 2 engines, that one of these warning conditions had ceased and that the propeller of the other engine could not be feathered. At 1259 hours information from the crew of VH-RMI, relayed to Longreach through the crew of another aircraft in the vicinity, indicated that there was a visible fire in No. 2 engine and that the aircraft was diverting below 5 000 ft to Winton. The town of Winton is located some 20 miles to port of the planned track and is 90 miles short of Longreach. No further communications were received from the aircraft but at 1303 hours a number of people located in the Winton area saw black smoke in the air west of the town, and it was subsequently established that this was associated with VH-RMI which had crashed in light timber on level ground some 131 miles short of the Winton aerodrome. The aircraft disintegrated on impact and all 24 occupants have been killed.
Probable cause:
The probable cause of the accident was that the means of securing the oil metering unit to the No. 2 cabin blower became ineffective and this led to the initiation of a fire within the blower, which propagated to the w$ng fuel tank and substantially reduced the strength of the main spar upper boom. It is probable that the separation of the oil metering unit arose from an out-of-balance condition induced by rotor break-up but the source of the rotor break-up could not be determined.
The following findings were reported:
- The crash of the aircraft followed the failure in an upward direction of the port wing between No. 1 and No. 2 engines at approximately 1302:30 hours Eastern Standard Time when the aircraft was at a height of 3 500 ft to 4 000 ft above ground level,
- The port wing failed as a result of a weakening of the main spar due to a fire in No. 2 cell of No. 2 fuel tank,
- The fire originated in the No. 2 cabin blower and travelled through the rear of No. 2 engine nacelle and port wheel bay to the fuel tank,
- The fire in No. 2 cabin blower was initiated as a result of a rotor break-up, the blower subsequently being driven in an out-of-balance condition by the quill shaft long enough for the metering unit to become separated from the rear end cover by the resulting vibration,
- The metering unit continued to be driven after separation and lubricating oil continued to be supplied. The driven rotor lost its rear stub shaft radial location and caused metal-to-metal contact which generated a temperature sufficiently high to ignite the oil in that area,
- It is not possible on the evidence to determine what was the cause of the rotor break-up.
Final Report:

Crash of a De Havilland Australia DHA-3 Drover 3 in Thargomindah

Date & Time: Jan 5, 1966
Operator:
Registration:
VH-FDR
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
5006
YOM:
1951
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Take off was abandoned when, in moderate quartering wind, the pilot was unable to maintain directional control. The aircraft moved sideways off the strip and both undercarriage struts were torn away after striking rocks. All three occupants escaped uninjured while the aircraft was considered as damaged beyond repair.
Probable cause:
Loss of control during takeoff due to quartering wind.

Crash of a De Havilland DH.89B Dominie in Brisbane

Date & Time: Oct 25, 1965
Operator:
Registration:
VH-BIF
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Brisbane - Brisbane
MSN:
6903
YOM:
1945
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances at Brisbane-Archerfield Airport while completing a local training flight with skydivers. Both occupants were uninjured while the aircraft was considered as damaged beyond repair.

Crash of a Douglas DC-4-1009 in Brisbane: 2 killed

Date & Time: May 24, 1961 at 0435 LT
Type of aircraft:
Operator:
Registration:
VH-TAA
Flight Type:
Survivors:
No
Schedule:
Sydney – Brisbane
MSN:
43065
YOM:
1946
Flight number:
TN1902
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
13019
Captain / Total hours on type:
378.00
Aircraft flight hours:
46006
Circumstances:
The crew was completing a cargo flight from Sydney to Brisbane. On short final in good weather conditions, the four engine aircraft crashed in unknown circumstances. The wreckage was found few hours later at Bulwer Island, about 1,5 km southeast of runway 01 threshold. The aircraft was destroyed by impact forces and a post crash fire and both pilots were killed.
Probable cause:
The accident occurred during the pre-landing circuit when the captain tried to leave his seat under the influence of a disordered cardiac function and, in the course of so doing, collapsed across the engine control console in such a way as to bring all four throttle levers to the closed position depriving the first officer of the throttle movement necessary to avoid a crash-landing off the airport.
Final Report:

Crash of a Fokker F27 Friendship off Mackay: 29 killed

Date & Time: Jun 10, 1960 at 2205 LT
Type of aircraft:
Operator:
Registration:
VH-TFB
Survivors:
No
Schedule:
Brisbane – Maryborough – Rockhampton – Mackay
MSN:
10112
YOM:
1959
Flight number:
TN538
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
25
Pax fatalities:
Other fatalities:
Total fatalities:
29
Aircraft flight hours:
2420
Aircraft flight cycles:
3396
Circumstances:
The Fokker F-27 aircraft was on a regular passenger flight from Brisbane (BNE) to Mackay (MKY) via Maryborough (MBH) and Rockhampton (ROK). The aircraft departed Brisbane at 17:11 and arrived at Maryborough at 17:52. It then took off at 18:12 on the next portion of the trip to Rockhampton where it landed without incident one hour later. Just prior to the landing at Rockhampton, the aircraft was advised of a special weather report which indicated shallow ground fog at Mackay to a height of 20 ft with a visibility of 880 yd, and also that an alternate aerodrome would be required for the rest of the flight. The flight departed Rockhampton at 19:52. On departure the air traffic controller at Mackay was advised that the expected flight time to Mackay was 52 minutes at an altitude of 13000 ft, that Townsville had been selected as the alternate. At 20:17 the aircraft reported at the prescribed reporting point, Charon Point, 80 miles south of Mackay at 130000 ft and gave its estimated time of arrival at Mackay as 20:40. It was advised that Mackay Airport was closed to landings at that time, and the situation remained the same when the aircraft reached the point at which it would normally have commenced its descent to Mackay. The captain indicated that he would continue the flight at 13000 ft and would hold over Mackay at that altitude. At 20:45 the ATC Officer advised the pilot that visibility was fluctuating between 2 and 2-1/2 miles along runway 14/32. The pilot replied that the airport lighting, the city area, and the surrounding country could be clearly seen, but that a belt of fog extending about 10 miles was situated to the southwest of the airport and was moving in a slightly northeasterly direction across the airport. The pilot then requested landing instructions. The aircraft was cleared to make a visual approach with a view to landing on runway 14. He reported on final approach, and at 20:55 the aircraft was cleared to land. As the aircraft approached close to the runway threshold at a height of about 50 feet, the pilot advised that a small patch of fog had suddenly appeared on the approach to the runway. It then flew along the runway at a height of approximately 50 ft and commenced to climb away. The pilot advised that he would look at the approach to runway 32. The ATC Officer next observed the aircraft descending to approach runway 32. It reached a height of approximately 200 ft, but before crossing the threshold it began to climb along the line of the runway, and the pilot requested permission to hold over Mackay at 5000 ft until an improvement in the weather occurred. This procedure was approved. The aircraft continued to hold over Mackay until about 22:00. At approximately 22:02 the ATC Officer noted the conditions improved rapidly and visibility was continually improving. When the aircraft was thus informed, it replied: "Roger tower, will commence let down to approach on runway 32". The aircraft was cleared for a visual approach and was given the wind (calm) and QNH (1019 mb) and was asked to report on final approach. Nothing more was heard from the flight. During the approach the airplane contacted the sea and crashed, some 12 km short of the runway.
Probable cause:
The investigation was not able to determine a probable cause of this accident. No evidence was found of material or structural defects, fire or an explosion on board, or any commotion or unusual act by any person in the aircraft. It is possible that something happened within the last 2-3 minutes as a result of which the pilot was unaware of his actual rate of descent. This could have been either caused by the instruments not accurately recording the altitude, or by the pilot relying on visual observation of his surroundings without paying (sufficient) attention to the instruments. The accident happened at night with very few visual clues.

Crash of a De Havilland DH.60 Moth near Home Hill

Date & Time: May 1, 1960
Type of aircraft:
Operator:
Registration:
VH-UGN
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Home Hill - Home Hill
MSN:
411
YOM:
1927
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The single engine airplane crash in unknown circumstances near the Burdekin River in Home Hill. The sole occupant was unhurt while the aircraft owned by Paddy F. Nielsen was damaged beyond repair.

Crash of a Lockheed L-414-56 Hudson in Horn Island: 6 killed

Date & Time: Jun 24, 1957 at 1535 LT
Type of aircraft:
Operator:
Registration:
VH-AGO
Flight Type:
Survivors:
No
Schedule:
Horn - Weipa Mission
MSN:
414-6429
YOM:
1942
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
6
Aircraft flight hours:
3083
Circumstances:
At 0735 hours, the aircraft departed Horn Island with only the normal crew on board to conduct aerial photography over the northern portion of the Cape York Peninsula. The aircraft returned to Horn Island at about midday and was refueled to full tanks. The crew lunched with the crew of World Wide Aerial Surveys Hudson VH-SMM which was also conducting aerial photography in the area. After lunch the three passengers boarded VH-AGO which set course for Weipa Mission at 1516 hours. At 1523 hours, Captain Linfoot advised the communication station on Thursday Island that he was returning to Horn Island with engine trouble and requesting that VH-SMM be held on the ground at Horn Island to render assistance if required. Following a baulked approach at Horn Island, the aircraft crashed on a tidal mud shelf 1.25 miles north-west of Horn Island Aerodrome at approximately 1535 hours. It was subsequently established that the port engine had seized as a result of a master rod bearing failure. The inquiry determined that VH-AGO had a total time of 3083 hours with 260 hours since last overhaul.
The following account of the accident is extracted from "Aviation Safety Digest":
"The aircraft was temporarily based at the Weipa Mission aerodrome, northern Queensland, with the normal crew consisting of a pilot, a navigator and a photographic assistant. On the day before the accident the aircraft was flown on a private flight from Weipa Mission to the Horn Island aerodrome with three non-paying passengers aboard in addition to the crew. The aircraft remained overnight at Horn Island, and early on the following morning took off with the normal crew, and carried out survey work over a period of some four hours. The aircraft returned to Horn lsland at about midday and was refueled. During the same morning another Hudson aircraft (VH-SMM of WWAS. Ed.) engaged on photographic survey work had arrived at the aerodrome and the two crews lunched together. Both aircraft were prepared for departure and the three passengers again boarded the Weipa Mission aircraft, which took-off first and set course at 1518 hours E.S.T. intending to climb to 7,000 feet en route for Weipa, 45 minutes flying time to the south. Five minutes after departure the pilot of this aircraft advised the communication station at Thursday Island that trouble had developed in the port engine and that he was returning, to land at Horn Island. He also asked that the other Hudson aircraft be held on the ground in case some assistance was needed. At the stage that this message was relayed to the captain of the second Hudson the aircraft was lined up for take-oft but immediately vacated the strip. The captain watched the circuit and approach of the other aircraft from a position clear of, but adjacent to, the threshold of Runway 08. The returning aircraft was seen to cross Runway 08 and then turn downwind at a height of 1,500-1,700 feet and proceed with a left-hand circuit towards the threshold of that runway. As the aircraft turned on to final approach at about the normal distance from the threshold but still unusually high, the ground observers noticed that the undercarriage had not been extended. The aircraft continued to descend in this configuration and it seemed likely at this stage that a wheels-up landing would be made well down the strip. When the aircraft had reached a point approximately 600 feet from the threshold and 150 feet above ground level the undercarriage was observed to extend and it was also noticed that the port propeller was feathered. At this point there appeared to be no wing flap extended and the aircraft crossed the strip threshold at a height of more than 100 feet and at a speed estimated to be well in excess of the normal approach speed. Soon after the aircraft had passed the threshold it was seen to roll and turn to port and this motion continued until the aircraft disappeared from view at such a height and angle of bank that an accident seemed imminent. The pilot of the Hudson on the ground immediately took-off and located the wrecked aircraft on a coral mud shelf just beyond the northern shore of the island. Ground parties discovered that the aircraft had been virtually destroyed by very high impact forces and the six occupants had lost their lives."
Those on board at the time of the crash were:
Joseph (Joe) Linfoot (Captain)
Hermione Ivy (Josie) Linfoot (Wife of the Captain)
Graham Holstock (Navigator)
Harold Corrigan (Camera Operator)
William Frank Mitchell (Director of Mitchell Aerial Services Pty Ltd, Cairns)
Lionel Kenneth George Jeffery (a pilot intending to join Adastra).
Source & photos:
http://www.adastron.com/adastra/aircraft/hudson/vh-ago.htm
Probable cause:
The official report found that a baulked approach was initiated at or near the threshold of Runway 08. It was concluded that given the speed and height of the approach, a baulked approach was essential to avoid over-running the airstrip. The reference to a council truck may be related to the fact that the DCA groundsman was directed to drive his vehicle on to the runway to prevent Hudson VH-SMM from taking-off at the request of the captain of VH-AGO.

Crash of a De Havilland Australia DHA-3 Drover 2 near Camooweal

Date & Time: Apr 26, 1957
Registration:
VH-ANZ
Flight Type:
Survivors:
Yes
Schedule:
Camooweal - Alice Springs
MSN:
5017
YOM:
1951
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crash location was 57 miles south of Camooweal near the NT/Queensland border. TAA Captain Richard Paul was relieving TAA Captain Harry Moss as resident NTMS pilot at Alice Springs, NT. Paul had just departed Camooweal to return to Alice Springs, carrying the doctor and nurse. They had been asked to look out for a missing stockman on horseback. Some 40 miles out of Camooweal, the pilot sighted a lone horseman. Preparations were being made in the circling aircraft to drop a message in order to establish the rider’s identity when the aircraft struck level ground near the Border Fence and slid some 85 metres before coming to rest in a substantially damaged condition. The horse rider ignored the circling aircraft and rode away, unaware the aircraft had crashed. An RFDS Drover and ground parties reached the site later the same day. The two passengers were returned to Camooweal in a vehicle. However Dick Paul needed urgent medical attention, and was flown to Mount Isa hospital by the RFDS Drover. His condition required urgent transfer to Brisbane, and no airline flight was available. A BOAC Britannia on scheduled service Darwin-Brisbane agreed to divert to collect him but Mount Isa runways were unsuitable and nearest location with required runway length was Cloncurry. A TAA DC-3 carried him from Mount Isa to Cloncurry, but the Britannia's main wheels broke through the taxiway surface pavement after landing. It was unable to move. With no other choice, Captain Paul was re-loaded on board the TAA DC-3 which then took him to Brisbane, where he recovered in hospital. The Britannia was stranded at Cloncurry for 3 days and its passengers accommodated with families in town.
Source:
http://www.goodall.com.au/australian-aviation/drover/drover.htm

Crash of an Avro 694 Lincoln 31 on Mt Superbus: 6 killed

Date & Time: Apr 9, 1955 at 0414 LT
Type of aircraft:
Operator:
Registration:
A73-64
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Townsville – Brisbane
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
10 Squadron RAAF had received a telephone call late on Good Friday night from the Townsville hospital seeking an emergency evacuation to Brisbane of a critically jaundiced 2 day old baby, Robyn Huxley. As most of the Squadron's air crew were on leave or stand-down over Easter, the Commanding Officer of 10 Squadron, Wing Commander John Costello decided to pilot the Squadron's only serviceable aircraft, A73-64, for the evacuation flight. The crew consisted of the new Commanding Officer Wing Commander Costello who had flown Sunderlands during the war against the German U Boats in the Atlantic, the Senior Navigation Officer, Squadron Leader Finlay, who was a wartime Pathfinder navigator, the squadron Chief Signaler, Flight Lieutenant Cater, and the squadron Senior Engineering Officer, Squadron Leader Mason. The baby girl and nurse Mafalda Gray were positioned in the long-nosed section of the Lincoln bomber. The aircraft took off from Garbutt airfield at 00.30 am on Saturday 9 April 1955. The aircraft encountered some cloud and rain as it approached southern Queensland. The aircraft had to fly at a relatively low altitude to ensure the baby had a comfortable flight. At 4.05 am the aircraft contacted Brisbane Air Traffic Control to advise that they were flying in cloud at 6,000 feet. They advised that they would arrive in Brisbane in about 10 minutes time and sought a clearance to reduce altitude to 5,000 feet. Brisbane Air Traffic Control advised that they were cleared to drop to 5,000 feet and if they wished they could drop to 4,000 feet for the approach to Eagle Farm airfield. A short time later Brisbane Air Traffic Control contacted them with weather information and asked them to confirm when they had obtained a visual fix on the town of Caboolture. No further reports were heard from the Lincoln bomber. There were no low clouds in the Brisbane area at that time. Some time later, reports came in that an aircraft, later confirmed as a Lincoln, was heard to circle over the town of Bell at about 3.30 am. Bell is located about 18 miles north east of Dalby. Clearly A73-64 was well off course. The weather south of Bell was overcast with scattered rain. At 4.14 am some members of the Brisbane Bushwalking Club heard a large aircraft fly overhead followed by the noise of an impact and some large explosions. By their estimation it had slammed into a nearby mountain in the Main Range region of the Border Ranges near Emu Vale. This was later confirmed to be Mount Superbus, the highest mountain (1,375 meters) in southern Queensland. A small group from the Bushwalking club was dispatched immediately to Emu Vale to notify the relevant authorities. Five hours later a Canberra bomber from Amberley airbase was able to confirm the location of the still burning wreckage of Lincoln, A73-64 just below the summit of Mount Superbus. Ground rescue crews were dispatched to the site. They quickly confirmed that there were no survivors.
Crew (10th Squadron):
W/Cdr John Peter Costello, pilot,
S/Ldr Charles Surtees Mason, copilot,
S/Ldr John Watson Finlay, navigator,
F/Lt William George Stanley Cater, signaler.
Passengers:
Baby Robyn Huxley,
Sister Mafalda Gray.
Source: http://www.ozatwar.com/ozcrashes/superbus.htm

Crash of a Douglas C-47A-5-DK off Mackay: 2 killed

Date & Time: Mar 14, 1954 at 0420 LT
Operator:
Registration:
VH-BBV
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Mackay – Rockhampton
MSN:
12360
YOM:
1944
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
One minute after its takeoff from Mackay Airport, while climbing by night, the twin engine aircraft went out of control and plunged into the sea off Mackay. The aircraft was destroyed and both crew members were killed. The crew was completing a cargo flight from Mackay to Rockhampton, carrying a load of newspapers.
Probable cause:
The assumption that the loss of control was the result of a bird strike was not ruled out.