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Crash of a Piper PA-61 Aerostar (Ted Smith 601P) in Teutonic Bore: 1 killed

Date & Time: May 28, 1980 at 1137 LT
Operator:
Registration:
VH-KXY
Flight Phase:
Survivors:
Yes
Schedule:
Teutonic Bore – Leonora – Perth
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
2810
Captain / Total hours on type:
149.00
Circumstances:
The aircraft was engaged on the return segment of a flight from Perth to Teutonic Bore, with an intended refuelling stop at Leonora. After embarking the two passengers and their baggage, the pilot started the engines and taxied for a take-off into the north, on the 1350 metre long main strip. The weather conditions were fine with a northerly surface wind of about 7 knots. The initial part of the take-off run was apparently normal but, after travelling some 400 metres and at about the point of rotation, one of the passengers noted an engine power surge. The take-off was continued, the aircraft became airborne and shortly afterwards the landing gear was retracted. After the aircraft had slowly climbed straight ahead to an altitude of about 200-300 feet above ground level, the passenger heard a marked change in the engine noise and felt the aircraft decelerating. The extent of the power loss and the absence of any yawing force indicated both engines had lost power simultaneously. Level flight straight ahead was reportedly maintained for an estimated 10 seconds and then the aircraft entered a descending left turn. At about this time the pilot, in response to a query from the passenger, advised that he intended to return to the airstrip but then stated "we're going down", or words to that effect. The terrain in the area was generally firm and flat. It was lightly covered with scrub and there was occasional small trees but a safe landing with only minimal damage was possible. When VH-KXY struck the ground the gear and flaps were retracted and the rate of descent was high. The aircraft was in a level attitude but yawed approximately 45 degrees to the right. After the initial impact, the aircraft slid across the ground on a track of 220 degrees magnetic for 67 metres before coming to rest. There was no post-impact fire. One passenger was able to exit via the cabin door by his own efforts. The other occupants were trapped in the wreckage and were rescued some 30 minutes later by persons who attended the accident. The pilot died shortly after being removed from the aircraft.
Probable cause:
The probable cause of the accident was that, following a substantial loss of power by both engines, the pilot did not carry out the procedures necessary for a safe forced landing. The cause of the loss of power by both engines has not been determined.
Final Report:

Crash of a Cessna 340A in Goulburn: 1 killed

Date & Time: May 15, 1979 at 1851 LT
Type of aircraft:
Operator:
Registration:
VH-TDU
Flight Phase:
Survivors:
Yes
Schedule:
Melbourne – Ballarat – Bendigo – Albury – Goulburn – Sydney
MSN:
340-0349
YOM:
1974
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
3500
Copilot / Total flying hours:
1060
Copilot / Total hours on type:
3
Circumstances:
The pilot contacted Sydney Flight Service Center at 1849, advised he was taxiing for runway 22 and that he would call again on departure. No further transmissions were received from the aircraft. VH-TDU completed an apparently normal take off and the landing gear was retracted. Shortly after it became airborne, it entered a gradual descending left turn and flew into the ground. The initial impact was on the left wing tip, approximately 1700 metres south of the departure end of Runway 22, at a speed of about 125 knots. The aircraft bounced, rolled inverted and again struck the ground some 100 metres further to the east. It then ;slid across the ground for a further 230 metres. A small fuel-fed fire broke out in the right wing but died out after several minutes. Five occupants were slightly injured while the captain was killed. Examination of the wreckage found no evidence of pre-existing mechanical malfunction or defect, apart from an open circuit in the gyro motor of the pilot's turn co-ordinator instrument. The instrument was not subjected to mechanical damage during impact and it is likely the fault existed prior to the accident. It could not be determined whether the pilot was aware that the instrument was unserviceable. All other instruments, including the primary flight instruments used in aircraft attitude control, were found to be serviceable and calibrated within specified limits. There was no evidence of pilot incapacitation prior to impact. Injuries were such that he was unable to recall details of the final flight. The passengers were not aware of any abnormality until the aircraft struck the ground. The pilot's current log book was not located. Therefore, while it is known that he had considerable experience at flying Cessna 340 aircraft, his hours on this type are unknown.
Probable cause:
There is insufficient evidence to establish the cause of the accident but the most likely explanation is that the pilot, influenced by fatigue, did not adequately refer to the flight instruments during the take-off and initial climb.
Final Report:

Crash of a Piper PA-61 Aerostar (Ted Smith Aerostar 601) in Charleville

Date & Time: Feb 1, 1979 at 0125 LT
Operator:
Registration:
VH-CPH
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Charleville – Mount Isa
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After lift-off at 85 knots, the pilot noted a positive rate of climb before retracting the landing gear and flaps. He then felt the aircraft sink and noted a high indicated rate of descent. Although full power was applied the descent continued until the aircraft struck the runway in a slightly nose-up attitude. The aircraft slid across the overrun area and through a fence before coming to rest. Fire broke out and engulfed the wreckage. At the time of the accident the aircraft weight was more than 200 kg above the maximum allowable and the centre of gravity was 142 mm forward of the forward limit. The pilot had been unable to retain control of the aircraft during the initial climb phase when the flaps were retracted at a relatively low airspeed.
Probable cause:
Overweight at takeoff.
Final Report:

Crash of a Rockwell Grand Commander 680 near Katherine

Date & Time: Jan 22, 1978
Operator:
Flight Type:
Survivors:
Yes
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing a drug smuggling flight and attempted to land on an abandoned airstrip located about 6 km west of Katherine. After the mishap, the crew set afire the airplane and left before being arrested by the police. On board was a load of 200,000 opium sticks for a total value of 3 millions US$.

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 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 De Havilland DH.60 Moth in Melbourne

Date & Time: Nov 22, 1959
Type of aircraft:
Operator:
Registration:
VH-UGM
Flight Type:
Survivors:
Yes
Schedule:
Melbourne - Melbourne
MSN:
453
YOM:
1928
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Built in 1928, the aircraft was restored for three years and has just been delivered to its new owner, J. O. Richardson, three days prior to the accident. The pilot, sole on board, was completing a local flight at Moorabbin Airport. On final approach, the engine failed. The aircraft stalled and crashed short of runway. The pilot was injured and the aircraft was destroyed.
Probable cause:
Engine failure on final approach.

Crash of an Avro 652 Anson I in Le Touquet

Date & Time: Dec 11, 1950
Type of aircraft:
Operator:
Registration:
VH-BDX
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Le Touquet – Croydon
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed on takeoff at Le Touquet Airport for unknown reason. Both occupants were uninjured while the aircraft was damaged beyond repair. The aircraft was already damaged in a wheels-up landing near Cranbrook, Kent, after an engine failure over the English Channel on February 6, 1950. It suffered a second accident on November 18, 1950 near Boulogne, France.

Crash of an Avro 652 Anson I into the Tuggerah Lake

Date & Time: Dec 9, 1950
Type of aircraft:
Operator:
Registration:
VH-AYE
Flight Phase:
Flight Type:
Survivors:
Yes
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
En route from Toowoomba, the aircraft suffered an engine failure while approaching Central Coast, NSW. The pilot attempted an emergency landing into the Teggurah Lake. The aircraft came to rest in shallow water and was considered as damaged beyond repair. The pilot was unhurt. The aircraft was owned by T. M. S. Hall.