Australia

Fokker F-27, registered VH-EWL, was operating as East-West Airlines Flight 752/753 from Sydney (SYD) to Orange, Bathurst and back to Sydney. The flight departed from Sydney at 17:06 hours and proceeded to Orange without incident. The flight then departed from Orange at 18:10 hours and, flown by the First Officer, the aircraft cruised at an altitude of 5250 feet which is the lowest safe altitude for the route. There was no cloud below the aircraft and the visibility was unrestricted. At Bathurst the weather was reported as a five knot wind from the north-east and the altimeter setting was 1021 millibars. The crew commenced the descent from a position about 5.5 km west of the aerodrome, in visual conditions, with the lights of the city of Bathurst and the runway lights clearly visible. Initially, it was intended to overfly the aerodrome and then make a left-hand circuit preparatory to landing on runway 17, but when the captain saw what appeared to be a light rain shower slightly east of the runway 35 threshold, and which might have involved penetration during a left-hand circuit to runway 17, he decided to land on runway 35 instead. At 1817:30 hours the captain called Sydney Flight Service reporting that the aircraft had arrived in the Bathurst circuit area. The aircraft, which was still being flown by the First Officer, was turned some 90 degrees to the right and it joined the left downwind leg of the traffic circuit for a landing on runway 35. The aircraft proceeded downwind a little further than is usual then turned onto base leg of the circuit by which time all cockpit checks had been completed except for setting the engine fuel trims to 'full increase'. The captain states that whilst the aircraft was on the base leg he checked that the water methanol lights were on, and that the fuel trim indicators were at 'full increase'. The aircraft was turned onto final approach for landing, at which time the landing gear was down, 26.5 degrees of wing flap had been extended, it was aligned with the runway centre-line and no drift was evident. Flight conditions were smooth. Light rain was then encountered and the windscreen wipers were switched on to operate at slow speed. The flight path appeared to be normal at an airspeed of 110 knots reducing to 100 knots with the rate of descent stabilised at some 700 ft/min. At about this time the aircraft passed over the Great Western Highway (730 metres south of the runway 35 threshold) and at the normal height of about 300 feet above terrain; two or three noticeable turbulence bumps were then encountered and the aircraft commenced to drift to the left of the runway alignment. The aircraft heading was altered a few degrees to the right and the approach was continued in light to moderate turbulence with the rain intensity increasing to heavy as the aircraft approached the runway threshold; the windscreen wipers were then selected to operate at high speed. At approximately 200-250 feet above terrain and prior to reaching the runway threshold, on the command of the Captain, the First Officer initiated a go-around because the aircraft had drifted too far to the left of the runway centre-line to safely effect a landing. The First Officer placed the power levers in the position for maximum power and he rotated the aircraft, by reference to the flight instruments, to the normal body attitude of 8 to 9 degrees for initial climb. The response of the engines appeared normal to the crew and they believed that full 'wet' power was being developed. Immediately after the engine power increased the captain raised the wing flaps from the setting of 26.5 degrees to 16.5 degrees, and he retracted the landing gear. At the commencement of the go-around the aircraft was still in conditions of turbulence and heavy rain and that, initially, the aircraft maintained its altitude; the indicated airspeed then decayed rapidly to 73 knots at which time the aircraft was estimated to be 80-100 feet above the runway. As the indicated airspeed decreased the First Officer lowered the nose of the aircraft slightly but still maintained a climbing attitude. At about this time the captain took hold of his control wheel but the First Officer continued to fly the aircraft by reference to his flight instruments. The indicated airspeed remained at 73 knots for a few seconds then rapidly increased to about 80-85 knots; it was not fluctuating and the turbulence had ceased. The rear fuselage of the aircraft then impacted the ground heavily just outside the boundary of the flight strip, at a point 1240 metres north of the runway 35 threshold, 48 metres to the right of the runway centre-line. The aircraft slid along on the fuselage for a distance of 625 metres during which the starboard engine was torn out of the wing. Cockpit impact drill was initiated by the flight crew during the ground slide and completed when the aircraft came to rest. The crew and passengers evacuated the aircraft at which time there was little or no rain at their location and there was a light breeze from a southerly direction.

The crew was involved in a local spraying mission in the region of Hamilton, Tasmania. While cruising at an altitude of 500 feet, the pilot-in-command initiated a left turn and descended till 50 feet when the airplane struck power cables. On impact, the left wing was torn off and the aircraft crashed in flames. Both occupants were killed.

The crew departed Bankstown on a local training flight. While circling near the airport, the Dove collided with a private Piper PA-30-160B Twin Comanche registered VH-WWB that was approaching Bankstown Airport on a flight from Sydney with also two people on board. Following the collision, both aircraft dove into the ground and crashed in a residential area located about 3 NM from the airfield. Both aircraft were destroyed and all four occupants were killed. Fortunately, there were no casualties on the ground. It is believed that the crew of the Dove encountered radio problems before the accident.

The crew was completing a positioning flight to Broome to pick up oil rig workers to Portuguese Timor on behalf of the Burma Oil Company. The approach and landing were completed in heavy rain falls due to monsoon. After touchdown, the airplane went out of control, veered off runway and lost its undercarriage and engines before coming to rest. All three crew members escaped uninjured while the aircraft was damaged beyond repair.

During the takeoff roll, al loss of hydraulic pressure forced the crew to abort. Unable to stop within the remaining distance, the twin engine airplane overran and came to rest against an embankment. Both pilots were injured and the aircraft was damaged beyond repair.
Photos via www.aussieairliners.org

Upon landing on a grassy runway on Trefoil Island, the airplane went out of control, veered off runway, lost its undercarriage and came to a halt. Both occupants were unhurt while the aircraft was damaged beyond repair.

The aircraft departed Adelaide-Parafield Airport on a charter flight to Moomba, carrying seven passengers and a passenger on behalf of Santos Ltd. At the time of the accident, it as owned and operated by Ansett Transport Industries (Operations) Pty Ltd trading as Ansett General Aviation. During initial climb, while flying in clouds at an altitude of 700 feet heading 270°, the twin engine airplane went out of control, entered a left turn and subsequently stuck the ground at high speed in a shallow dive, some 13 miles northeast of Adelaide Airport. The airplane disintegrated on impact and all eight occupants were killed. The accident was not survivable.

At approximately 0745 hours Central Standard Time on 20 January 1972, there was an in-flight fire in a Beech 65-80 Queen Air aircraft, registered VH-CMI, which resulted in the separation of the starboard engine and the starboard outer wing. The aircraft subsequently struck the ground some seven miles south-west of Alice Springs Airport in the Northern Territory. At the time of the accident, the aircraft was engaged in operating a charter flight for the purpose of carrying passengers, mail and freight from Alice Springs to Ayers Rock. The aircraft was destroyed by fire and impact forces and the pilot and the six passengers were killed.

The area to be seeded was a flooded rice paddy, rectangular in shape and approximately 1,650 feet east/west by 800 feet north/south, with the western bank 95 feet to the east of a river. There was an extensive area of dense timber, generally about 70 feet in height, on the western side of the river and a line of trees along the eastern bank. After making an aerial inspection of the area the pilot arranged for the two men who were to act as markers to take up positions on the banks of the paddy in preparation for easterly and westerly seeding runs commencing along the southern side. The first run was made into the east, approaching over the timbered area and towards the low sun. run was then made to the west followed by a steep pull-up and turn over the trees. The third run, again into the east, was commenced but no seed was dropped on this occasion possibly because of difficulties in observing and lining up with the marker at the western end of the paddy. The next run was to the west and was apparently normal and this was followed again by a steep pull-up and turn over the trees. Towards the end of the turn the aircraft was at an estimated height of 100 feet above the trees which was higher than on the previous turn in this area and may have resulted from an endeavour to observe each of the two markers in order to line up for the next run. The aircraft commenced a steep descent, with the wings level, consistent with an approach for a seeding run to the east. A few seconds later, when about 250 feet short of the rice paddy, the aircraft struck the sparsely foliated upper branches of a tree which extended about 20 feet above the other trees in the vicinity and the starboard elevator was torn off. With no apparent power reduction, and little change of direction, the aircraft rolled steeply to the left, descended and, after travelling a further 150 feet, struck another tree on the eastern side of the river. The wings and empennage were torn off and the fuselage fell through the tree to the ground and burst into flames.

Belly landed at Townsville Airport for unknown reasons. There were no casualties but the aircraft was damaged beyond repair.