Crash of a De Havilland DHC-6 Twin Otter 100 in Tau

Date & Time: Jun 17, 1988 at 1036 LT
Operator:
Registration:
N202RH
Survivors:
Yes
Schedule:
Pago Pago - Tau
MSN:
68
YOM:
1967
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
14
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
19455
Captain / Total hours on type:
3393.00
Aircraft flight hours:
18403
Circumstances:
The captain, who was flying the Twin Otter from the right seat, entered a right hand traffic pattern for landing. A left quartering, 15 knot headwind, was gusting across the airport. Upon turning to the final approach the captain reduced the aircraft's engine power to the low speed range for the visual approach. As the aircraft neared the runway the rate of descent accelerated. The captain's application of full engine power failed to arrest the aircraft's rate of descent and the aircraft impacted the ground short of the runway. All 16 occupants were injured.
Probable cause:
Occurrence #1: undershoot
Phase of operation: approach - vfr pattern - final approach
Findings
1. (c) planned approach - improper - pilot in command
2. (f) weather condition - turbulence
3. (f) weather condition - gusts
4. (c) powerplant controls - delayed - pilot in command
5. Stall/mush - inadvertent - pilot in command
----------
Occurrence #2: in flight collision with terrain/water
Phase of operation: approach - vfr pattern - final approach
Final Report:

Crash of a Rockwell Shrike Commander 500S in Mount Garnet

Date & Time: May 20, 1988 at 1750 LT
Operator:
Registration:
VH-SDI
Survivors:
Yes
Schedule:
Kidston – Cairns
MSN:
500-3188
YOM:
1974
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The pilot was temporarily replacing the pilot who normally flew the aircraft. After arriving at Kidston he checked the fuel quantity gauge and decided that there was sufficient fuel on board for the return flight. As the aircraft approached top of climb, the pilot found that the fuel gauge indicated a lower fuel quantity than he had expected. He re-checked the indicated quantity after the aircraft was established in cruise and decided that sufficient fuel still remained to complete the planned flight. Shortly after passing Mt Garnet both engine fuel flow gauges began to fluctuate and the engines began to surge. The pilot immediately turned the aircraft towards the Mt Garnet strip, but shortly afterwards both engines failed. The pilot attempted to glide the aircraft to the strip, but it collided with trees and came to rest about one kilometre from the runway 27 threshold. All three occupants escaped with minor injuries and the aircraft was damaged beyond repair.
Probable cause:
Both engines had failed due to fuel exhaustion. The pilot normally flew a different type of aircraft, this aircraft only being used by the company to supplement its services. For company aircraft normal route fuel requirements are specified. As a result, there was little need for him to make significant fuel calculations. On this occasion, the pilot found he had little time between his arrival at Cairns and the scheduled DEPARTURE of his next flight. He ordered that only 80 litres of fuel be added to the aircraft tanks. The calculated fuel burn for the proposed return flight to Kidston was approximately 240 litres. However, on DEPARTURE from Cairns it was estimated that only about 220 litres of fuel was in the aircraft tanks. Refuelling facilities were available at Kidston but no fuel was added to the aircraft tanks.
The following factors were considered relevant to the development of the accident:
1. The aircraft design is such that the fuel quantity can only be determined by the gauge, unless the tanks are full.
2. The preflight preparation, in relation to fuel requirements, carried out by the pilot was inadequate.
3. The pilot lacked recent experience at more complex fuel calculations.
Final Report:

Crash of a Piper PA-31-350 Navajo Chieftain off Coffs Harbour: 3 killed

Date & Time: Apr 7, 1988 at 2113 LT
Operator:
Registration:
VH-AOX
Survivors:
Yes
Schedule:
Brisbane – Coolangatta – Coffs Harbour – Port Macquarie
MSN:
31-7552013
YOM:
1975
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The aircraft was operating a scheduled service from Brisbane to Port Macquarie with planned intermediate stops at Coolangatta and Coffs Harbour. Weather conditions over the route were influenced by a widespread unstable airmass. The terminal forecast for Coffs Harbour indicated a surface wind of 360/15, visibility in excess of 10 km, 5 octas stratus at 1000 ft, 5 octas cumulus at 2000 ft. Thunderstorms, associated with visibility reduced to 2000 metres were also forecast for periods of up to 30 minutes. The actual weather conditions at Coffs Harbour were generally consistent with the terminal forecast. Runway 03 was in use throughout the evening. Coffs Harbour airport was equipped with NDB, VOR and domestic DME radio navigation aids. A VOR/DME procedure was published for runway 03 approaches. For aircraft not equipped with DME, a VOR or NDB approach was available using common tracking and minimum altitude criteria. Runway 03 was also equipped with a 6 stage T-VASIS and 3 stage runway lighting. All facilities were reported as functioning normally, with the exception of the VOR which was experiencing intermittent power failures due to the effects of heavy rain. The VOR was able to be reset manually from the Coffs Harbour control tower. Although the tower was scheduled to be unmanned before the arrival of VH-HOX, the duty air traffic controller elected to man the tower until the aircraft had landed. The controller also called out a technician to attend to the VOR. The aircraft was equipped with dual ILS/VOR and ADF receivers, plus International DME. Domestic DME equipment was not fitted to the aircraft, although required by ANO 20.8. After descending in the VOR/NDB holding pattern, the aircraft was cleared for an instrument approach. The pilot had been told of the intermittent operation of the VOR and had said he would revert to the NDB. At that time the weather conditions were fluctuating about the circling minima of 950 feet (QNH) and five km visibility. The controller advised the aircraft of a heavy shower to the south of the field. The aircraft subsequently completed the approach and the pilot reported "visual". The controller said he saw the lights of the aircraft in a position consistent with a right downwind leg for a landing on runway 03. The aircraft was then cleared to land. Shortly after, the controller saw the lights of the aircraft disappear briefly, consistent with the aircraft passing through a localised area of rain/cloud. The lights then reappeared briefly, as though the aircraft was turning onto finals, before disappearing. This was immediately followed by short series of "clicks" on the tower frequency. The aircraft was called immediately but failed to respond to any calls. The accident site was located about 1070 metres short of the landing threshold, and about 750 metres to the right of the extended runway centreline. The aircraft was found to have initially struck a nine metre high tree in a nose low attitude, steeply banked to the right, on a track of 050 degrees. After striking the tree with the outboard section of the right wing, the aircraft struck other trees before hitting the ground and overturning. A fire broke out shortly after the aircraft came to rest. As a result of his remaining on duty, the controller was able to provide immediate notification of the accident to the emergency services. This action facilitated the rescue of survivors.
Probable cause:
A subsequent examination of the aircraft structure, systems and components, found no evidence of any pre-existing defect or malfunction which could have contributed to the accident. The pilot was properly licenced and qualified to conduct the flight. Evidence was provided to show that the pilot had probably flown a total of 930 hours in the previous 365 days, thereby exceeding the ANO 48 limitation of 900 hours. Other breaches of Flight and Duty Limitations were found to have occurred during the previous 12 months, however, during the three months prior to the accident no significant breaches of ANO 48 were found which could have contributed to the accident. Specialist medical advice considered the 30 hour exceedence of the 900 hour limitation was not significant in this accident. Other specialist advice was obtained concerning the possibility of the aircraft being affected by low level windshear or a microburst during the final stage of the night circling approach. It was considered this was not a factor in the accident. Considerable evidence was presented during a subsequent Coroners' Inquest concerning allegations of irregular operating practices by the operator over a period of several years prior to the accident. Much of this evidence was only provided after the granting to witnesses of immunity from prosecution. Despite this, no new evidence was presented which related to the accident flight. The investigation concluded that, on the evidence available, the aircraft was turning onto a short right base leg when it entered a localised area of rain and low cloud. The pilot was required to look out of the right cockpit window to enable him to maintain visual reference with the approach end of the runway. It is considered probable that the pilot briefly diverted his attention from the flight instruments while attempting to maintain that visual reference as the aircraft passed through an area of reduced visibility. During that period the aircraft continued to roll to the right, resulting in an inadvertent loss of height. The pilot was unable to effect a recovery before the aircraft struck trees.
The following factors were considered relevant to the development of the accident:
1. Low cloudbase, with localised rain squalls and reduced visibility.
2. Low level, right hand, night circling approach.
3. Pilot lost visual reference at a critical stage of the approach.
4. Pilot did not initiate missed approach.
5. Pilot probably diverted attention from the flight instruments.
Final Report:

Crash of a Piper PA-60 Aerostar (Ted Smith 600) near Cassilis: 2 killed

Date & Time: Dec 22, 1987 at 1620 LT
Operator:
Registration:
VH-IGV
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Bankstown – Coolah
MSN:
60-0054-123
YOM:
1971
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The pilot was conducting a freight charter flight, and witness evidence confirmed that on DEPARTURE he was occupying the left-hand seat. The pilot was accompanied by a friend who was also a commercial pilot, but not endorsed on this type of aircraft. Approximately 18 minutes prior to the estimated time of arrival at the destination, the pilot reported leaving the cruising altitude of 6500 feet on descent. Several minutes after the descent report had been made, a witness about 50 kilometres from the destination reported seeing the aircraft pull-up into a very steep climb from an extremely low height with its wings level, and then become inverted. It then entered what was described by the witness as a spin or spiral dive, before impacting the ground in a near vertical descent. The pilot was found in the right-hand seat, and the passenger had been thrown clear of the wreckage. It was established that neither seat belt had been fastened at the time of the impact. Although it could not be determined which pilot was flying the aircraft at the time of the pull-up, medical evidence suggested that the pilot occupying the right-hand seat position was handling the controls at the time of ground impact. The weather at the time of the accident was fine and clear, with 10-15 knot winds.
Probable cause:
A thorough examination of the aircraft wreckage did not reveal any malfunction or mechanical failure which may have caused a sudden and severe loss of control. Investigation showed that at the
moment of impact the aircraft was in a near vertical descent, without any rotation about the vertical axis, and the wings were in a stalled condition. No reason was found which could have explained either the low flying, or the steep pull-up. During the investigation it was established that with this aircraft type, a considerable degree of sustained elevator force would need to be applied by a pilot in order to achieve the type of flight path reported by the witness. It is considered that such a control input would need to be deliberately executed.
Significant Factors:
It was considered that the following factors were relevant to the development of the accident:
1. The pilot, or passenger, performed what was apparently a deliberate steep pull-up from low-level. The reason for the pull-up was not established.
2. Loss of control occurred as a consequence of the aircraft becoming stalled.
3. There was insufficient height for the pilot to effect recovery following the loss of control.
Final Report:

Crash of a Britten-Norman BN-2A-20 Islander in Papua New Guinea

Date & Time: Dec 15, 1987
Type of aircraft:
Operator:
Registration:
P2-COG
Flight Phase:
MSN:
843
YOM:
1978
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances somewhere in Papua New Guinea in December 1987 (exact date unknown).

Crash of a Fletcher FU-24-950M in Wairakei: 1 killed

Date & Time: Dec 12, 1987
Type of aircraft:
Operator:
Registration:
ZK-CWQ
Flight Phase:
Survivors:
No
MSN:
64
YOM:
1960
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The single engine aircraft crashed in unknown circumstances in Wairakei. The pilot, sole on board, was killed.

Crash of a Britten-Norman BN-2A-2 Islander in Kanabea: 1 killed

Date & Time: Dec 8, 1987
Type of aircraft:
Operator:
Registration:
P2-MIB
Flight Phase:
Survivors:
Yes
MSN:
217
YOM:
1970
Location:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
Crashed shortly after takeoff for unknown reasons. A passenger was killed and three other occupants were injured.

Crash of a Cessna 208 Caravan I off Kaikoura: 2 killed

Date & Time: Nov 27, 1987 at 2355 LT
Type of aircraft:
Registration:
ZK-SFB
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Christchurch - Wellington
MSN:
208-0059
YOM:
1985
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
While cruising by night at an altitude of 11,000 feet on a cargo flight from Christchurch to Wellington, the pilot encountered icing conditions. The airplane went out of control, entered a dive and crashed in the sea off Kaikoura. Both occupants were killed.
Probable cause:
The following findings were reported:
- Icing conditions,
- The aircraft was not equipped with deicing systems,
- The pilot was tired due to a duty period more than 18 hours,
- The pilot loaded and unloaded more than 10 tons of cargo during the day,
- The pilot was soaked by rain while doing so because no foul weather gear was provided,
- The pilot did not have sufficient rest time,
- The pilot did not have a proper brake time and meal,
- The pilot was not properly trained concerning indoctrination course and suffered hypoxia in flight.

Crash of a Douglas C-47B-15-DK in Lae

Date & Time: Nov 18, 1987
Operator:
Registration:
P2-006
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
15192/26637
YOM:
1944
Location:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After liftoff at Lae-Nadzab Airport, one of the engine failed. The crew attempted an emergency landing in a pasture when one wing struck an obstacle. The airplane belly landed and came to rest. There were no casualties.
Probable cause:
Engine failure for unknown reasons.

Crash of a Cessna 402A off Malekolon: 1 killed

Date & Time: Oct 16, 1987
Type of aircraft:
Operator:
Registration:
P2-GKG
Survivors:
No
MSN:
402A-0070
YOM:
1969
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
On approach to Malekolon Airstrip, the twin engine aircraft crashed in unknown circumstances in the sea and sank. Both occupants were killed.