Crash of a GAF Nomad N.24A in Lake Tekapo

Date & Time: Jul 20, 1987 at 1900 LT
Type of aircraft:
Operator:
Registration:
ZK-NMD
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Lake Tekapo - Hamilton
MSN:
36
YOM:
1977
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After takeoff from Lake Tekapo, the aircraft encountered difficulties to gain height the stalled and crashed past the runway end. The pilot, sole on board, was seriously injured.
Probable cause:
It was determined that the stall during initial climb was the consequence of an excessive accumulation of frost on fuselage and wings. The aircraft was not deiced prior to takeoff.

Crash of a Cessna 402C in Bundaberg: 4 killed

Date & Time: Jun 21, 1987 at 0318 LT
Type of aircraft:
Operator:
Registration:
VH-WBQ
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Bundaberg - Brisbane
MSN:
402C-0627
YOM:
1982
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
The flight had been arranged to transport a critically injured patient to hospital in Brisbane. The pilot evidently experienced some difficulty in starting one of the engines. However, witnesses reported that the engines sounded normal as the aircraft commenced moving from the parking area. At 0310 hours the pilot contacted Brisbane Flight Service Unit and reported that the aircraft was taxying. He advised that he was in a hurry, and indicated that he would provide details of the flight after takeoff. Two minutes later he advised that takeoff was being commenced from Runway 14. No further transmissions were received from the aircraft. The aircraft was seen to become airborne and shortly afterwards enter a fog bank. Other witnesses subsequently reported hearing the sounds of an impact. The flight had been arranged to transport a critically injured patient to hospital in Brisbane. The pilot evidently experienced some difficulty in starting one of the engines. However, witnesses reported that the engines sounded normal as the aircraft commenced moving from the parking area. At 0310 hours the pilot contacted Brisbane Flight Service Unit and reported that the aircraft was taxying. He advised that he was in a hurry, and indicated that he would provide details of the flight after takeoff. Two minutes later he advised that takeoff was being commenced from Runway 14. No further transmissions were received from the aircraft. The aircraft was seen to become airborne and shortly afterwards enter a fog bank. Other witnesses subsequently reported hearing the sounds of an impact. The flight had been arranged to transport a critically injured patient to hospital in Brisbane. The pilot evidently experienced some difficulty in starting one of the engines. However, witnesses reported that the engines sounded normal as the aircraft commenced moving from the parking area. At 0310 hours the pilot contacted Brisbane Flight Service Unit and reported that the aircraft was taxying. He advised that he was in a hurry, and indicated that he would provide details of the flight after takeoff. Two minutes later he advised that takeoff was being commenced from Runway 14. No further transmissions were received from the aircraft. The aircraft was seen to become airborne and shortly afterwards enter a fog bank. Other witnesses subsequently reported hearing the sounds of an impact. The investigation revealed that the aircraft had collided with a tree 800 metres beyond the aerodrome boundary, while tracking about 10 degrees to the right of the extended centreline of the runway. It had then continued on the same heading until striking the ground 177 metres beyond the initial impact point. The wreckage was almost totally consumed by fire.
Probable cause:
The extensive fire damage hampered the investigation of the accident. The surviving passenger believed that the aircraft was on fire before the collision with the tree. No other evidence of an in-flight fire could be obtained, and it was considered possible that the survivor's recall of the accident sequence had been affected by the impact and the fire. Such discrepancies in recall are not uncommon among accident survivors. The elevator trim control jack was found to be in the full nose-down position, but it was not possible to establish whether the trim was in this position prior to impact. Such a pre-impact position could indicate either a runaway electric trim situation or that, in his hurry to depart, the pilot had not correctly set the trim for takeoff. The aircraft was known to have had an intermittent fault in the engine fire warning system. The fault apparently caused the fire warning light to illuminate, and the fire bell to sound, usually just after the aircraft became airborne. The pilot was aware of this fault. It was considered possible that, if the fault occurred on this occasion as the aircraft entered the fog shortly after liftoff, the pilot's attention may have been focussed temporarily on the task of cancelling the warnings. During this time he would not have been monitoring the primary flight attitude indicator, and would have had no external visual references. It was also possible that, if for some reason the pilot was not monitoring his flight instruments as the aircraft entered the fog, he suffered a form of spatial disorientation known as the somatogravic illusion. This illusion has been identified as a major factor in many similar accidents following night takeoffs. As an aircraft accelerates, the combination of the forces of acceleration and gravity induce a sensation that the aircraft is pitching nose-up. The typical reaction of the pilot is to counter this apparent pitch by gently applying forward elevator control, which can result in the aircraft descending into the ground. In this particular case, the pilot would probably have been more susceptible to disorientating effects, because he was suffering from a bronchial or influenzal infection. Although all of the above were possible explanations for the accident, there was insufficient evidence available to form a firm conclusion. The precise cause of the accident remains undetermined.
It is considered that some of the following factors may have been relevant to the development of the accident
1. The pilot was making a hurried DEPARTURE. It is possible that he did not correctly set the elevator trim and/or the engines may not have reached normal operating temperatures before the takeoff was commenced.
2. Shortly after liftoff the aircraft entered a fog bank, which would have deprived the pilot of external visual references.
3. The aircraft had a defective engine fire warning system. Had the system activated it may have distracted the pilot at a critical stage of flight.
4. The aircraft might have suffered an electric elevator trim malfunction, or an internal fire, leading to loss of control of the aircraft.
5. The pilot may have experienced the somatogravic illusion and inadvertently flown the aircraft into the ground. The chances of such an illusion occurring would have been increased because the pilot was evidently suffering from an infection.
Final Report:

Crash of a Britten-Norman BN-2A-20 Islander near Lae: 2 killed

Date & Time: Jun 20, 1987
Type of aircraft:
Registration:
P2-KAD
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Ogeranang – Lae
MSN:
800
YOM:
1977
Location:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The twin engine airplane was completing a cargo flight from Ogeranang to Lae, carrying two pilots and a load of coffee. While cruising at an altitude of 8,700 feet in marginal weather conditions, the aircraft struck the slope of a mountain located in the Rawlinson Mountain Range. The wreckage was found 32 km from Lae. Both occupants were killed.
Probable cause:
Controlled flight into terrain.

Crash of a Fletcher FU-24-950M near Matakana: 1 killed

Date & Time: May 6, 1987 at 1453 LT
Type of aircraft:
Operator:
Registration:
ZK-CBI
Flight Phase:
Survivors:
No
MSN:
88
YOM:
1962
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
An aerial topdressing operation was being undertaken from a sloping airstrip located on a headland near Matakana. The fertilizer to be applied was granulated superphosphate totaling 60 tonnes. The aircraft arrived at the airstrip and while waiting for the loader to arrive the pilot walked the length of the runway, then requested that the farmer cut down some saplings at the end of the strip that might obstruct his climb out path. Upon arrival of the loader the pilot instructed the driver to place 18 hundredweight (cwt) or 915 kgs of fertilizer in the aircraft. This was done, along with the addition of some fuel, and the first flight of the operation commenced. The driver did not observe the take off but while reloading his vehicle at the bin noticed a cloud of fertilizer dust off the end of the strip, indicating that the pilot had jettisoned the load. A few minutes later the driver sighted the aircraft briefly through a gap in the trees. It was flying, apparently normally, at about sowing height and on a reciprocal course to the take off direction. A faint trail of fertilizer was coming from the hopper. The plane then disappeared behind some trees and the driver did not see it again. Just after losing sight of the aircraft he saw what seemed to be a piece of red paper fluttering to the ground. When the aircraft failed to land a search was made and the wreckage of ZK-CBI was found in dense scrub about 350 metres to the left of the departure end of the airstrip. The pilot, sole on board, was killed. The investigator found that the pilot had initiated jettisoning the load 36 metres before the boundary fence. It was not clear whether the plane was still on the ground or was airborne at a low speed when a collision with the concrete post and wire fence occurred. Two posts had almost completely severed both halves of the " all flying " tailplane or stabilator. The outboard left hand section was retained by the trim tab only. The outboard part of the right hand side of the stabilator later detached and was found 150 metres from the crash site. With this degree of damage to the tailplane horizontal control must have been difficult, but the pilot was able to clear a low ridge ahead and fly out over a large basin where a 180 degree turn was completed in order to land back on the airstrip. Before the approach could be completed however, the outer part of the RH side of the stabilator separated and the aircraft dived steeply to the ground. The aircraft was destroyed by the severe impact. Fire did not break out. This was not a survivable crash.
Probable cause:
The probable cause of this accident was that the pilot did not initiate the jettisoning of the load in time to restore the take off performance which had been degraded by the kikuyu grass on the airstrip. The following findings were reported:
- The aircraft was loaded within approved limits.
- Kikuyu grass growing on the airstrip caused a significant deterioration in the acceleration of the plane on take off.
- The aircraft was capable of normal operation before the collision with the fence.
- The collision caused critical damage.
- Some minutes after the collision about 1/4 of the total horizontal stabilizer area separated from the aircraft causing it to become uncontrollable in pitch and dive to the ground.

Crash of a Fletcher FU-24A-950 in Orari Gorge: 1 killed

Date & Time: Apr 13, 1987 at 1700 LT
Type of aircraft:
Operator:
Registration:
ZK-DZA
Flight Phase:
Survivors:
No
MSN:
201
YOM:
1974
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
ZK-DZA was engaged in an aerial topdressing operation at Orari Gorge Station, situated about 16 km north-northwest of the small town of Geraldine in Canterbury. The day's work had commenced at 08:12 and by 16:30 100 tonnes of superphosphate fertilizer had been distributed over the farm in about 100 sorties. These operations had been uneventful apart from two instances of the engine stopping while idling on the ground. One of these events occurred at the start up after the lunch break and the other was after the halt taken at about 16:30 to enable the attachment of a Transland spreader unit to the plane. The pilot was unconcerned at these unwanted stoppages as the engine had a tendency to do this in warm ambient temperatures, and he attributed it to " vapour lock ". At about 16:55 the pilot took off again to spread a mixture of 575 kg of selenium pellets and between 100 and 150 kg of superphosphate over a higher area of the farm. The aircraft weight and CG were within the permitted limits. About five minutes later the loader driver heard " a thump " and on looking around sighted the plane on the side of a hill about one kilometer northwest of his location. The driver immediately radioed base to get them to inform the station manager that a crash had occurred. There was one eyewitness to the accident. A farmer working about 4 km away saw the Fletcher flying away from him and dropping a short trail of fertilizer before making " a funny move sideways " and then coming to a stop on the ground. He immediately returned to his house and telephoned Orari Gorge Station to raise the alarm. Station personnel arrived at the crash scene by 4WD vehicle within ten or fifteen minutes. They found the aircraft wrecked and the pilot dead. Fire had not occurred. The crash site was on a steep grassy slope 1,700 feet amsl. The aircraft had contacted the ground in roughly a landing attitude, at high rate of sink, and drifting to the left. It was severely damaged, with the main undercarriage legs separated and the nose leg folded back under the fuselage. The engine was displaced and the spreader torn off. Of the rest of the airframe only the tail section remained intact. Deceleration was rapid.The ground slide covered a distance of sixteen metres. This was not a survivable accident.
Probable cause:
The weather was calm with only high cloud. Examination of the engine revealed no evidence that it may have lost power in flight. An autopsy carried out on the pilot showed that he had received a broken neck and a ruptured heart in the impact. He was suffering from a moderately severe coronary heart disease at the time of death. The crash investigator concluded that this very experienced pilot may have had a heart attack and been seriously incapacitated in flight, prompting him to attempt an immediate emergency landing on the hillside.

Crash of an Embraer EMB-110P2 Bandeirante off Hoskins: 14 killed

Date & Time: Feb 6, 1987
Operator:
Registration:
P2-RDM
Survivors:
Yes
Schedule:
Rabaul - Hoskins
MSN:
110-262
YOM:
1980
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
15
Pax fatalities:
Other fatalities:
Total fatalities:
14
Circumstances:
While descending to Hoskins Airport, the crew encountered poor weather conditions with thunderstorm activity and severe turbulences. Control was lost and the aircraft crashed in the sea few km offshore. Three passengers were rescued while 14 other occupants were killed.
Probable cause:
Loss of control due to severe atmospheric turbulences.

Crash of a Cessna 402B in Mount Dianne: 5 killed

Date & Time: Feb 2, 1987 at 0639 LT
Type of aircraft:
Operator:
Registration:
VH-TLQ
Survivors:
Yes
Schedule:
Cairns – Mount Dianne
MSN:
402B-1236
YOM:
1977
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
The aircraft was the first of a group of four aircraft being used to return staff to an alluvial gold mine after a weekend break. The weather in the area of the destination was not suitable for a visual arrival and the aircraft was initially held for several minutes in an area five kilometres to the south of the strip, awaiting an improvement in the weather. The aircraft was then flown towards the strip and the pilot reported to a following aircraft that there had been a lot of rain and that the strip looked wet. He also advised that he intended to carry out a precautionary circuit and check if it was safe to land. No further transmissions were received from VH-TLQ. The wreckage of the aircraft was subsequently found burning in a river valley, 300 metres west of the threshold of runway 34. Surviving passengers stated that the aircraft struck trees shortly before impact. There were no ground witnesses. The aircraft had impacted the ground in a steep nose down left wing low attitude, at a low forward speed, then cartwheeled up rising ground before coming to rest inverted, 42 metres from the point of impact. The cabin area was destroyed by an ensuing fire.
Probable cause:
An inspection of wreckage did not reveal any mechanical defect or failure that could have contributed to the accident. The reasons for the apparent loss of control of the aircraft could not be determined.
Final Report:

Crash of a De Havilland DH.114 Heron 2B in Nadi: 11 killed

Date & Time: Dec 27, 1986 at 1348 LT
Type of aircraft:
Operator:
Registration:
DQ-FEF
Survivors:
Yes
Schedule:
Savusavu - Nadi
MSN:
14056
YOM:
1955
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
12
Pax fatalities:
Other fatalities:
Total fatalities:
11
Circumstances:
On final approach to Nadi Airport runway 21, at an altitude of 500 feet, the right flap jammed in a 35° angle while the left one was down at 60°. This caused the aircraft to roll to the left and to crashed short of runway. Both pilots and nine passengers were killed while three others were seriously injured.
Probable cause:
Unsecured non-standard flap attachment pin migrated upward and lodged in a lightening hole.

Crash of a De Havilland DHC-2 Beaver near Walcha: 1 killed

Date & Time: Dec 22, 1986
Type of aircraft:
Operator:
Registration:
VH-AAY
Flight Phase:
Survivors:
No
Schedule:
Winterbourne - Winterbourne
MSN:
136
YOM:
1951
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
Superphosphate spreading was being carried out, with the aircraft uplifting one tonne loads about every 6 minutes. Fuel endurance with both tanks full was approximately 2 hours. The pilot was conducting his 25th takeoff for the day, about one hour after refuelling. Witnesses observed that the aircraft did not become airborne at the usual point, two-thirds of the way along the 675 metre strip. Lift-off finally occurred at the end of the strip, but almost immediately afterwards the aircraft clipped a fence. It was seen to sink slightly, before climbing at a steeper than normal angle until some 250 metres beyond the fence. At this point the nose dropped suddenly and the aircraft dived into rising ground in a steep nose down attitude. Fire broke out on impact and consumed much of the wreckage. The pilot, sole on board, was killed.
Probable cause:
Preliminary investigation revealed that the fuel selector was in the "off" position. This had been the first occasion that the pilot had flown this particular aircraft. The fuel selector in this aircraft was different to that in the other Beaver the pilot had operated. In the previous aircraft, rotating the fuel selector through 180 degrees anti-clockwise changed the selection from the rear to the forward fuel tanks. In the accident aircraft, a similar movement of the selector changed the selection from the rear tank to the "off" position. This difference had not been brought to the pilot's attention, and it was possible that he had not thoroughly familiarized himself with the aircraft prior to commencing operations. It was considered likely that the takeoff had been commenced with the fuel selector positioned to the almost empty rear tank. During the takeoff roll, the fuel low quantity bell and associated light had activated, and the pilot had changed the fuel selector by feel, while continuing with the takeoff. With the fuel supply turned off, the engine had failed from fuel starvation, and the aircraft had subsequently stalled at too low a height above the ground to permit recovery before impact.
Final Report:

Crash of a Douglas C-47B-35-DK at Edinburgh AFB

Date & Time: Oct 17, 1986
Operator:
Registration:
A65-114
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
16712/33460
YOM:
1945
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Just after liftoff, both engines failed simultaneously. The aircraft stalled and hit the runway surface. On impact, the left main gear collapsed and the aircraft came to rest. There were no casualties but the aircraft was considered as damaged beyond repair and later transferred to the South Australian Aviation Museum in Port Adelaide.
Probable cause:
Double engine failure for unknown reasons.