Sikorsky S-76A, VH-BHM, Barrow Island Aerodrome, Western Australia, on 4 August 1999

Safety Action

Operator safety action

The operator issued an alert message for its fleet of S76 helicopters to undergo an inspection of the subject area. A defect report was also submitted to the Civil Aviation Safety Authority.

Manufacturer safety action

As a result of this incident and a similar incident experienced by another Australian S76 operator in 1995, and following consultation between the operator, helicopter manufacturer and BASI; the manufacturer conducted a design engineering review of the cyclic stick base hardware to determine if it was possible to reduce the effect of foreign object entry to the tub area.

Following the review, the manufacturer advised that a field modification of the pilot's side bracket was being prepared to increase the gap between the torque tube rig boss and the bracket foot. On 28 August 1999, the manufacturer also advised of its intention to issue an Alert Service Bulletin, in due course, to address the results of the engineering review.

BASI safety action

BASI will monitor the progress of this manufacturer's proposed safety action.

Summary

The pilot of the Sikorsky S76 helicopter reported that while approaching Barrow Island and immediately after he reduced the helicopter's airspeed for landing gear extension, he found that the cyclic could not be moved aft. He also found that with any further forward movement of the cyclic stick, the stick then could not be moved aft of the new position. The pilot froze the cyclic longitudinal position and the helicopter stabilised in a level pitch attitude at about 85 kts indicated airspeed. Using only lateral cyclic movements to manoeuvre the helicopter, the pilot conducted an 80-kt run-on landing on the runway at Barrow Island.

The subsequent maintenance inspection found a panhead type screw at the base of the cyclic stick. The screw had lodged between the lower protrusion on the casting on the end of the cyclic stick torque tube and the lugs on a support bracket. The lodgement of the screw in that location had caused the cyclic restriction experienced by the pilot.

The cyclic stick base hardware was accommodated in a tub-like area formed by the cabin structure supports. A leather boot mounted at the base of the cyclic normally prevented foreign objects from entering the tub. The subsequent maintenance inspection found the leather boot on this helicopter to be intact. With the boot in place, the only possible entry points where a screw could be inserted was through a rigging pin hole in the aft mid-height position of the boot-halves joint, or vertically through an opening provided for the cyclic stick electrical wiring loom. Due to the unlikelihood that a screw could enter the tub area when the boot was fitted, the screw was probably introduced to the area during prior maintenance while the boot was removed.

Occurrence summary

Investigation number 199903789
Occurrence date 04/08/1999
Location Barrow Island , Aero.
State Western Australia
Report release date 20/10/1999
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Control - Other
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Sikorsky Aircraft
Model S-76
Registration VH-BHM
Serial number 760107
Sector Helicopter
Operation type Charter
Departure point Cossack Pioneer, WA
Destination Barrow Island, WA
Damage Nil

Fairchild SA227-DC, VH-DMO, 2 km north-north-east of Latrobe Valley Aerodrome, on 25 July 1999

Safety Action

As a result of this occurrence, the Australian Safety Transport Bureau is currently investigating a safety deficiency relating to procedures allowing straight-in approaches to be flown at aerodromes where there is a greater than usual possibility of conflict with unalerted traffic, such as CTAF aerodromes.

Any safety output issued as a result of this analysis will be published in the Bureau's Quarterly Safety Deficiency Report.

Analysis

The pilot of the Chipmunk did not see the Metroliner. It is likely that the pilot commenced his take-off roll when the Metroliner was at least 3 NM from touchdown. At that distance, the Metroliner may not have been readily detectable by the Chipmunk pilot. His lookout for possible traffic would most likely have been directed towards the circuit and approach of runway 03 rather than towards runway 21 and he would not have been expecting to see traffic approaching from the opposite direction. With the aircraft in the level attitude during take-off, he would have been looking along the runway and his attention would have been focused on maintaining directional control. The Metroliner would most likely have been obscured from the Chipmunk pilot's view by the nose of his aircraft when he subsequently rotated to the climb attitude.

The crew of the Metroliner did not see the Chipmunk until that aircraft was almost overhead theirs. As they had not received any response to their broadcasts on the CTAF, they were relying on visual acquisition of any unalerted traffic as their only defence against a conflict. However, the Chipmunk was a small visual target with little relative movement. In addition, it had no anti-collision lighting and would initially have been below the Metroliner crew's horizon. The contrast between the background and the colour of the Chipmunk was minimal and would have made the aircraft difficult to discern.

The straight-in approach procedure at CTAF aerodromes did not appear to adequately address the limitations of unalerted "see and avoid" principles. The assumption of two pairs of eyes being more likely to detect unalerted aircraft than one pair of eyes, did not prove to be an adequate defence in this incident.

In this instance, the crew of the Metroliner elected to make a straight-in approach in wind conditions that most probably favoured a reciprocal runway direction. Without any response to their broadcast intentions, the crew probably assumed that there was no traffic and believed it was safe to use runway 21. As regulations in force at the time of the occurrence did not include a requirement for an airline operator to assess the circumstances and the likelihood of encountering non-radio traffic at individual locations, it was likely that many crews were conducting straight-in approaches as an expected routine. Had the crew been aware, for example, of the potential for greater numbers of recreational movements at weekends and on public holidays, they may have decided not to conduct the straight-in approach.

Although the company had provided a radiocommunication service to comply with the requirements for this procedure, its effectiveness to alert the crew to other aircraft was restricted by company procedures and by the physical location of the radio operator. The radio operator was not familiar with aircraft movements and had never been instructed to provide runway-in-use information. Had the radio operator been afforded a full view of the entire runway and the approach path of the Metroliner and permitted to issue traffic information, a timely warning may have been broadcast to the crew of the Metroliner about the presence of the Chipmunk.

The pilot of the Chipmunk chose to continue his flight without radio communication and without knowledge of a procedure that could place him in potential conflict with a passenger-carrying aircraft. Knowledge of scheduled aircraft movements at that location may have influenced the pilot to avoid commencing a non-radio flight when the arrival of a scheduled service was imminent.

Summary

Sequence of events

The crew of a Metroliner, conducting a scheduled passenger service from Sydney, reported that at 30 NM from Latrobe Valley, they obtained weather information from their ground agent on the common traffic advisory frequency (CTAF). They recorded the wind as light and variable. At approximately 17 NM, the co-pilot broadcast on the CTAF advising their intention to join for a 5 NM straight-in approach to runway 21. Two similar broadcasts were made, one at 10 NM and the other at 5 NM. At approximately 1 NM from touchdown, the crew saw a Chipmunk aircraft a short distance to their left and about 400 ft above them, travelling in the opposite direction. The crew continued their approach and landing as they considered that there was no further risk of collision.

The Chipmunk pilot was conducting a private flight. He reported that the aircraft radio had undergone maintenance prior to the incident flight and that he was unsure if a functional check of the radio had been made. He determined that the wind was a light north-easterly and elected to use runway 03. He broadcast on the CTAF that he was taxiing, and made a further transmission advising that he was backtracking along runway 03. He did not hear any response to either broadcast and had not heard the aerodrome frequency response unit. He assumed that his aircraft radio was not operating and proceeded with the flight without making any further radio broadcasts.

The pilot of the Chipmunk reported that he did not see any aircraft either when entering the runway or when lining up for takeoff. He departed and climbed away, unaware that the landing Metroliner had passed below him. Although he was aware that scheduled flights operated into the aerodrome, he was not familiar with those schedules. He was also unaware that such aircraft could conduct straight-in approaches to CTAF aerodromes. He reported that although his aircraft was equipped with a landing light, he was not in the habit of using it in daylight conditions.

Witness information

An instructor at the aerodrome reported that, at the time of the occurrence, the Chipmunk and the Metroliner were the only aircraft in the circuit. He added that other aircraft movements that day had been made from runway 03.

Following this incident, another instructor observed the straight-in approach procedure under similar conditions. He stationed himself at a position similar to that of the Chipmunk pilot at takeoff in order to determine the visibility of the approaching Metroliner. He reported that when the crew broadcast their 5 NM position, he was only able to see the aircraft after several seconds of looking. However, at an estimated 3 NM, with the landing gear extended and the taxi light illuminated, it was much easier to see the aircraft.

Weather

Weather conditions at the time of the occurrence were described as fine and clear with good visibility. Witnesses on the ground reported the wind as 5-8 kt from the north-east. Data recorded from the automatic weather station (AWS), indicated that a north-east wind had prevailed from 1100 Eastern Standard Time (EST) onwards. The Latrobe Valley METAR (meteorological observation) at 1304 EST indicated that the wind direction was 070 degrees magnetic and the windspeed was 7-10 kt. Those conditions favoured the use of runway 03.

Straight-in approach procedures

On 26 March 1997, the Civil Aviation Safety Authority permitted multi-crew regular public transport aircraft to conduct straight-in approaches to non-controlled aerodromes other than those within a mandatory broadcast zone. Effective from 1 May 1999, amendment 35 to the Civil Aviation Orders (CAO) part 82.3 incorporated a new sub-section 5A that required the provision of a ground-based radiocommunication service at aerodromes where straight-in approach procedures were conducted. However, following industry concerns about the operator's liability in relation to the provision of traffic information and the cost to airlines of providing such a service, that section was amended. CAO amendment 41 was issued with a new sub-section 5B that restricted the information to be given by the radiocommunication service to wind direction and runways in use at the aerodrome.

The company operating the Metroliner contracted the services of a ground-handling and booking agent to perform the required radiocommunication service, and personnel were trained and approved to provide that service. The procedure required the agent's staff to obtain weather information from the AWS and, when requested, broadcast this information to company pilots on the CTAF. Information about other traffic or the runway in use was not transmitted.

The agent advised that crews could obtain traffic and runway information from other aircraft on the CTAF. Other duties performed by the agent's staff precluded them from continuously monitoring the CTAF for information about other traffic. Additionally, the company radio was situated in the airport terminal and only a limited view of the airfield was afforded through the windows. Visual observation of aerodrome traffic from this location was not possible. The Chipmunk would not have been visible from this vantage point at any time it was taxiing or airborne.

There were no specific company instructions for crews making straight-in approaches at CTAF aerodromes. Company management personnel were satisfied that the procedures contained in the Aeronautical Information Publication were adequate. Company standard operating procedures required the landing and recognition lights to be turned on as aircraft were approaching 10,000 ft when transition checks were being completed. The taxi light was not to be turned on until after the landing gear was extended. The crew reported that that procedure had been followed.

The pilot in command advised that the crew's preferred choice of runway direction at Latrobe Valley on the flight from Sydney was runway 21. This not only reduced flying time but also allowed crews the 3-minute cooldown period for the engines while backtracking to the terminal. It also avoided running the engines near the terminal and creating unnecessary noise.

Determination of the runway in use, as required by the Aeronautical Information Publication (AIP) procedure, was assumed by crews to be either the reported runway being used by other traffic in the circuit or, in the absence of other traffic, runway 21, provided that wind conditions were favourable. The view expressed by the pilot in command was that the straight-in approach procedure offered a better level of safety than that provided by the normal circuit entry and that it was more expedient. He believed that the procedure resulted in less circuit manoeuvring and a reduced risk of traffic conflicts.

Aerodrome traffic

This incident occurred on a Sunday afternoon. The airline operated six services per week into Latrobe Valley but only one of these flights was conducted on a weekend. The pattern of activity at the aerodrome was not recorded however, staff at the Aero Club were able to confirm that most recreational flying activity took place at weekends and on public holidays. Only a small number of aircraft operating from the aerodrome were not radio-equipped. The scheduled movements at Latrobe Valley were not published in any of the aeronautical publications.

Occurrence summary

Investigation number 199903768
Occurrence date 25/07/1999
Location 2 km NNE Latrobe Valley, Aero.
State Victoria
Report release date 23/12/1999
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Separation issue
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Fairchild Industries Inc
Model SA227
Registration VH-DMO
Serial number DC-870B
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Sydney, NSW
Destination Latrobe Valley, VIC
Damage Nil

Aircraft details

Manufacturer De Havilland Canada/De Havilland Aircraft of Canada
Model DHC-1
Registration VH-DHW
Serial number DHC 770
Sector Piston
Operation type Private
Departure point Latrobe Valley, VIC
Destination Yarram, VIC
Damage Nil

de Havilland Canada DHC-8-202, VH-SDA, 407 km north-west of Cairns Aerodrome, on 25 June 2009

Summary

While cruising at flight level 220 between Kimmi and Ablok, approximately 220 NM north-west of Cairns, the crew of the Dash 8 heard a muffled sound that was followed by an increase of the left engine inter turbine temperature. The crew reduced the engine power and returned the aircraft to Cairns.

The engine examination revealed that the reported problem was the result of a failure of the number 5 bearing. The bearing cage contained two cracks and was open. Some roller pockets in the bearing cage were enlarged and distorted, which allowed the rollers to rotate in the plane of the cage. Some other rollers were immobilised and contained large flats. Six of the 12 rollers had a smaller diameter than the rest. Their surface was abraded and smeared, consistent with heavy contact loads.

Because of several similar failures, the engine manufacturer had issued service bulletin number 21472R2, on 25 February 1999, introducing an improved number 5 bearing. The service bulletin advised that engines of serial numbers subsequent to the failed engine were already fitted with the new bearing. It further recommended that number 5 bearings on all other Pratt & Whitney PW100 engine models should be replaced when the engines were disassembled and access was available. The improved bearing had not been installed on this engine.

Occurrence summary

Investigation number 199903738
Occurrence date 25/06/1999
Location 407 km NW Cairns, Aero.
Report release date 15/11/2000
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Abnormal engine indications
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer De Havilland Canada/De Havilland Aircraft of Canada
Model DHC-8
Registration VH-SDA
Serial number 482
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Cairns, QLD
Destination Horn Island, QLD
Damage Minor

Transponder related between a Boeing 747-438, VH-OJB and Tupolev KGA515, Lajak, on 17 July 1999

Summary

While maintaining flight level (FL) 330, the crew of a Boeing 747 (B747) aircraft monitored the position report from the crew of a Tupulov 154 (Tu154) aircraft. This position report indicated that the Tu154 was estimating position LAJAK at 1907 UTC. The B747 was estimating LAJAK at 1906. Both aircraft were maintaining FL 330.

The crew of the B747 advised air traffic control of the conflict, who directed the crew of the Tu154 to descend to FL 290. The aircraft were vertically separated at LAJAK.

Despite the close proximity of the aircraft, the B747's traffic alert and collision avoidance system (TCAS) did not display the TU154. The crew confirmed with air traffic control that the secondary surveillance radar (SSR) transponder mode C function of the Tu154 was operating correctly. The crew of the B747 reported that their aircraft's TCAS system was functioning correctly and that they were able to monitor aircraft at other stages of the flight.

Investigation revealed that some Eastern Bloc SSR transponders may be selected by the crew to output altitude information in either feet or metres. The investigation was unable to determine if the Tu154 was equipped with this type of transponder.

The operator of the B747 issued an alert to all crews regarding the capability of Eastern Bloc transponders to output altitude information in either feet or metres and if metres was selected the aircraft may not be visible on TCAS.

Occurrence summary

Investigation number 199903711
Occurrence date 17/07/1999
Location Lajak (Reporting Point)
State International
Report release date 06/10/2000
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer The Boeing Company
Model 747
Registration VH-OJB
Serial number 24373
Sector Jet
Operation type Air Transport High Capacity
Departure point London, UK
Destination Bangkok, THAILAND
Damage Nil

Aircraft details

Manufacturer Tupolev
Model Tu-154
Registration KGA515
Sector Jet
Operation type Air Transport High Capacity
Damage Nil

British Aerospace Plc 3201, VH-XFC, 9 km north-north-east of Brisbane, on 28 July 1999

Safety Action

Local safety action

The Airservices Australia investigator made the following recommendations:

"The MORETON GROUP Leader to include the application of the "Sight & Follow" procedure as a specific subject in all future Refresher Training programs with case studies for analysis. (e.g. the practicality of sighting traffic same level eleven o'clock at ten miles in a period of high cockpit workload.)

Consideration given to include in MATS 4-5-1 para 10 specific reference to "---their number in the landing sequence ----" and not limit this reference to same page, para 15, second sentence under the title of Visual Separation by Aerodrome Controllers."

Australian Transport Safety Bureau safety action

As a result of this occurrence the Australian Transport Safety Bureau (formerly BASI) is currently investigating a safety deficiency. The deficiency relates to the training provided to Airservices Australia's approach controllers, in particular human factors awareness training on the limitations of human performance.

Significant Factors

  1. The approach controller used the "sight and follow procedure" in an inappropriate circumstance. That is, the controller transferred the responsibility for separation to the pilot in a situation where the positive application of a separation standard may have been more appropriate.
  2. The approach controller requested the crew of the Metroliner to sight the Jetstream in circumstances where a positive sighting may have been improbable.
  3. The crew of the Metroliner sighted and followed the BAe 146 rather than the Jetstream

Analysis

Notwithstanding the different profiles of the two aircraft, type identification of either aircraft would have been virtually impossible to determine at the ranges of the aircraft, that is beyond 6.8 NM. This is because contrast, which is the difference between the brightness of the aircraft against the brightness of the background, reduces with increasing range. Further, target identification would have been hampered by contour interaction. This phenomenon occurs where the outline of a target aircraft interacts with the contours present in the background. This is a particular problem at lower altitudes where aircraft appear against complex backgrounds.

When the crew of the Metroliner was instructed to report when they could see the other aircraft at 11 o'clock, the BAe 146 was the only aircraft discernible to them. With its side profile, the BAe 146 was at the extreme limit of visual acuity and could easily have been mistaken for a Jetstream, particularly as no other aircraft was in their field of vision. The Jetstream, with its head-on profile and greater range, would have been impossible to see at 9.8 NM. Moreover, because its actual position was not correctly described to the crew, they were looking for the Jetstream in the wrong place.

The approach controller may have realised that there was potential for mis-identification of the two aircraft. This is suggested by his action of cautioning the Metroliner crew about the BAe 146 that was on short final. However, the controller did not provide additional information that would have provided an assurance that the pilot was following the correct aircraft.

The identification of the potential conflict and action taken by the aerodrome controller was timely and appropriate. The vigilance and prompt action of the aerodrome controller acted as a safety defence to reduce the possibility of collision between the aircraft.

Summary

There were three aircraft in the approach sequence to land on runway 19 at Brisbane: a British Aerospace 146 (BAe 146), VH-JJS, on final at 2 NM; a British Aerospace Jetstream 3200 (Jetstream), VH-XFC, on right base at 6.5 NM with approximately 8 track-miles to touchdown; and a Fairchild SA226 Metroliner (Metroliner), VH-TFQ, on an oblique left base at 6.5 NM with approximately 10.5 track-miles to touchdown. Analysis of recorded voice data confirmed that the approach controller advised the crew of the Metroliner that they were number 3 in the sequence and that the Jetstream was number 2. Subsequent to that advice, the controller advised the Metroliner crew that the aircraft they were to follow was at 11 o'clock, 10 NM at 1600 ft. They were instructed to report when they could see that aircraft. The crew responded "Traffic sighted". The crew of the Metroliner was then assigned responsibility for separation from the Jetstream by being cleared to manoeuvre as required to make a visual approach and to "follow the Jetstream". In the same transmission, the crew were cautioned about the BAe 146 "on a very short final runway 19" and instructed to contact the tower.

When the crew transferred to the tower frequency, the aerodrome controller realised that the Metroliner was following the wrong aircraft, the BAe 146, and could be in conflict with the Jetstream. The controller instructed the Metroliner crew to orbit their aircraft on left base to increase its separation with the Jetstream. Analysis of recorded radar data indicated that separation between the Metroliner and the Jetstream had reduced to 1.2 NM when they were at the same level.

The crew of the Metroliner did not recall being cautioned about the 146. The aircraft they had sighted and followed was not the Jetstream but the BAe 146, which resulted in the breakdown of separation.

The Manual of Air Traffic Services (MATS) stated in MATS 4-5-1, paragraph 7:

"Correct identification of the aircraft from which separation must be maintained is essential".

Paragraph 10 stated:

"The traffic information provided shall contain as much as is necessary of the following to assist the pilot in identifying the other aircraft:

  1. type, and description if unfamiliar;
  2. level;
  3. position information either by clock reference, bearing and distance, relation to a geographical point, reported position and estimate, or position in circuit;
  4. intentions, or direction in flight."

Analysis of the radar data indicated that at the time the crew was asked to report sighting the aircraft, the BAe 146 was in the Metroliner's 11 o'clock relative position at 6.8 NM and displayed an oblique, side profile. The position of the Jetstream was more to the Metroliner's 12 o'clock relative position, at 9.8 NM and displayed a head-on profile.

Occurrence summary

Investigation number 199903602
Occurrence date 28/07/1999
Location 9 km NNE Brisbane, Aero
State Queensland
Report release date 12/05/2000
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Loss of separation
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer British Aerospace
Model 3200
Registration VH-XFC
Serial number 949
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Roma, QLD
Destination Brisbane, QLD
Damage Nil

Aircraft details

Manufacturer Fairchild Industries Inc
Model SA226
Registration VH-TFQ
Serial number TC-395
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Coolangatta, QLD
Destination Brisbane, QLD
Damage Nil

Aircraft details

Manufacturer British Aerospace
Model BAe 146
Registration VH-JJS
Serial number E2093
Sector Jet
Operation type Air Transport High Capacity
Departure point Unknown
Destination Brisbane, QLD
Damage Nil

Cessna 172H, VH-RLO, on 16 July 1999

Factual Information

The Cessna 172 was being used to assist a ground party of station hands to muster sheep on a station property approximately 46 km south-west of Onslow, WA. The manager of the station reported that the aircraft was being used to spot livestock on the ground and to muster sheep using a pilot-activated siren on the underside of the fuselage.

The aircraft was being flown along a generally east-west track, from one side of the paddock to the other, which gradually progressed towards the northern boundary. Although members of the ground party were unable to estimate the height at which the aircraft was operating, they did report that the aircraft siren was effective in moving the sheep. An experienced mustering pilot stated that a siren fitted to an aircraft would probably be quite ineffective at a height of 500 ft above ground level.

The station manager reported that the pilot appeared to be attempting to position the aircraft to cut off a mob of sheep that had broken away from the group he was following. He saw the aircraft pass approximately overhead and in a westerly direction before it commenced a left turn.

The manager looked away from the aircraft but reported that he could clearly hear its engine, which sounded normal. He immediately looked up when he heard the sound of an impact and saw that the aircraft had crashed approximately 100-200 m from where he was standing.

As a result of the accident the pilot sustained fatal injuries and the aircraft was destroyed. Damage to the aircraft was consistent with it having impacted the ground in a near vertical attitude at a low forward speed. A significant quantity of fuel was later recovered from the aircraft wreckage. There was no evidence that a mechanical defect had contributed to the accident.

The property owners had employed the pilot to fly their aircraft to assist with mustering operations. They stated that they had little knowledge of operating a light aircraft in support of their primary production activities. One of the owners was aware of a mustering type endorsement and reported that despite contacting a number of organisations and authorities, he had experienced difficulty in finding somebody to conduct mustering training for the pilot.

The pilot was issued with his private pilot licence (aeroplanes) on 4 June 1999, 6 weeks before the accident. At the time of the accident, the pilot had accumulated about 191 hours aeronautical experience, which included some helicopter training. No evidence was found to indicate that the pilot had received any formal low-flying training or that he was qualified to conduct mustering operations. Investigators were told the pilot had arranged to do training for a mustering endorsement once he had enough experience to be endorsed.

Flight and duty time limitations are specified for pilots engaged in commercial operations. However, as this mustering operation was being conducted in the private category, there was no requirement for the pilot or the aircraft operator to comply with these limitations. Consequently, the pilot was responsible for determining his daily flying activities. This was done in conjunction with the property owners, property manager and the mustering party. Investigators were told that the pilot typically commenced flying at approximately 0700 local time and continued through the day, until the last paddock had been completed.

During the course of the investigation the pilot's recent flight and duty times were reviewed to determine whether fatigue had been a factor leading to the occurrence. He had flown at least 68 hours in the 9 days since arriving at the station and had not taken a day off during this period. On the day of the accident, he had flown at least 8 hours 30 minutes. He was known to take short breaks from airborne operations about every 4 hours, during which time he would refuel the aircraft.

Analysis

On the day of the accident, the pilot had been flying the aircraft at low level for most of the day, with minimal rest periods. He had only recently qualified for his private pilot licence and a significant portion of his total flying hours had been accumulated in the 9 days before the accident. During this period, he had exceeded the flight and duty times normally permitted for a commercial operation.

Fatigue can diminish human performance, particularly with tasks requiring sustained attention and rapid reaction times. It may impair a pilot's ability to judge distance and speed, and it increases reaction times. It may also lead to poor decision making. Heat, noise and vibration may exacerbate these effects.

A human factors report noted that the pilot had worked long hours in a job in which he was inexperienced and that he probably found this type of flying both physically and mentally demanding. The report concluded that at the time of the accident the pilot was suffering from the effects of fatigue, possibly impairing his ability to safely operate the aircraft. The pilot was not qualified to conduct mustering or low flying operations. Without such qualifications, the pilot was legally required to operate no lower than 500 ft above ground level. At this height, the aircraft may have been of some use in spotting sheep but probably would have been ineffective at mustering.

The pilot had received minimal training to identify the visual illusions associated with low level flight. As such it was considered unlikely he was aware of appropriate techniques to safely manoeuvre the aircraft at low level. Several visual illusions affect pilots of low flying aircraft. An untrained pilot would be particularly susceptible to such illusions, some of which may prevent correct estimation of airspeed or making appropriate control inputs during a critical phase of flight.

The property owners had little aviation experience to help them manage the hazards of this type of operation. Although one of the owners knew that pilots needed special training for mustering, the accident pilot was employed while still unqualified.

Pilot fatigue, a lack of low flying training and no appropriate supervision of a relatively inexperienced pilot were identified as possible contributing factors to the accident. The immediate circumstances of the aircraft impacting the ground could not be established.

Summary

The Cessna 172 was being used to assist a ground party of station hands to muster sheep on a station property approximately 46 km south-west of Onslow, WA. As a result of the accident the pilot sustained fatal injuries and the aircraft was destroyed.

Occurrence summary

Investigation number 199903463
Occurrence date 16/07/1999
Location 46 km SW Onslow, Aero.
State Western Australia
Report release date 08/08/2000
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Collision with terrain
Occurrence class Accident
Highest injury level Fatal

Aircraft details

Manufacturer Cessna Aircraft Company
Model 172
Registration VH-RLO
Serial number 17255432
Sector Piston
Operation type Private
Departure point Minderoo Station, WA
Destination Minderoo Station, WA
Damage Destroyed

Boeing 737-376, VH-TAF

Safety Action

Local Safety Action

The Airservices Australia Occurrence Investigation report (V4) made 18 recommendations intended to review procedures involving training, communication and standardisation.

ATSB Safety Action

As a result of this and other occurrences, the Australian Transport Safety Bureau (ATSB) is currently investigating a safety deficiency relating to the lack of separation assurance techniques applied by air traffic controllers.

Any safety output issued as a result of the analysis will be published in the Bureau's Quarterly Safety Deficiency Report.

Significant Factors

  1. The similarity of the departure instruction to the noise abatement procedure provided the potential for a human error to occur.
  2. The crew of TAF did not comply with the departure instruction issued by air traffic control because the crew confused the instruction with the noise abatement procedure.
  3. The enroute controller did not issue TAF with a procedural clearance that would have provided separation assurance with CZV.

Analysis

The investigation determined that the crew of TAF did not comply with their departure instruction. Separation would not have been infringed if TAF had continued on a heading of 090 M as directed, instead of intercepting the 128 radial. The similarity of the noise abatement procedure to the departure instruction may have diminished the importance of the requirement for the crew to maintain a heading of 090 M after departure.

Although the action of the crew resulted in an infringement of the radar separation standard, the enroute controller did not issue a clearance that assured separation between TAF and CZV. Separation assurance was required in accordance with MATS 4-1-1, paragraph 6. The controller used radar procedures to separate the two aircraft, where non-radar separation should have been applied in accordance with MATS 4-1-1 paragraph 11 because communications and equipment did not allow the application of radar separation.

The enroute controller was not in direct communication with the crews of both aircraft. Moreover, portions of Maroochydore airspace were below radar coverage including airspace below 1,500 ft. Although LOA 98/054 allowed the enroute controller to "assume radar identification of departing aircraft within four minutes of the next call", published procedures did not permit the enroute controller to apply radar separation between radar identified aircraft and aircraft departing Maroochydore that were not identified.

Summary

The crew of VH-TAF, a Boeing 737, was taxiing for runway 18 at Maroochydore (MC) for a departure to Sydney. The route was flight planned, and subsequently cleared, via waypoint TRIKI (128 MC at 22 NM) on air route W196 at flight level (FL) 350. The crew had pre-briefed the noise abatement procedure that was detailed in AIP Australia as follows:

"2.2 Departing Runway 18 - MC to TRIKI: UNLESS OTHERWISE DIRECTED BY ATC. (a) Jet aircraft shall at 500FT, turn left heading 090 degrees M to intercept track. If not able to intercept track from this heading, then maintain heading 090 degrees until 4DME before turning to intercept track".

Another Boeing 737, VH-CZV, was inbound to Maroochydore from Sydney and tracking via TRIKI on W196. The Maroochydore aerodrome controller had received prior coordination on this aircraft, which was on descent to 5,000 ft. Although the BURNET enroute controller was responsible for CZV, the crew was not in two-way communication with the enroute controller. The enroute controller had agreed to allow the crew to transfer frequency direct from Brisbane Approach to Maroochydore Tower. The standard frequency transfer point in accordance with Letter of Agreement (LOA) ND 98/054 was TRIKI. CZV was roughly 32 NM from Maroochydore when the aerodrome controller contacted the enroute controller to coordinate a departure clearance for TAF.

Maroochydore was a non-radar tower and the aerodrome controller was responsible for providing procedural separation to aircraft below 4,500 ft. The enroute controller was responsible for the surrounding airspace overlying and to the south of Maroochydore as defined in the AIP Designated Airspace Handbook. The enroute controller was able to use radar or procedural means to provide air traffic control separation. Radar coverage in the Maroochydore area was generally available above 1,500 ft.

At 1236, the enroute controller advised the aerodrome controller to issue TAF a heading of 090 degrees M and to maintain FL150, a level that would provide vertical separation from a third aircraft overflying at FL160. The aerodrome controller recognised a potential conflict between TAF and CZV, and confirmed with enroute that the enroute controller would accept the responsibility for conflict resolution. The enroute controller accepted the responsibility for providing separation.

The aerodrome controller then issued the following departure instruction to the crew of TAF: "TAF, restriction on departure is to turn left and take up a heading of 090 magnetic, maintain FL 150, clear for take-off, make left turn". The crew correctly read back the instruction. The crew later reported that they interpreted the restriction on departure to be the altitude restriction and believed the heading instruction applied to the noise abatement procedure. At 1238, the crew was instructed by the aerodrome controller to contact the enroute controller to make a departure report.

CZV meanwhile, was approaching TRIKI and the crew reported to the Maroochydore aerodrome controller on descent to 5,000 ft. The aerodrome controller directed the crew to continue tracking direct to Maroochydore and to maintain 5,000 ft. Maroochydore tower then contacted the enroute controller seeking an unrestricted descent clearance for CZV, which was granted but not issued to the crew.

At the same time, TAF was turning right to intercept the 128 radial at 4 NM from Maroochydore and was passing 4,400 ft on climb. The crew contacted the enroute controller at 1239 and reported established on the 128 radial, climbing to FL 150. TAF and CZV were then on reciprocal tracks and closing. In an unsuccessful attempt to preserve the required separation, the crew of TAF was told to turn left onto a heading of 090 M and maintain 5,000 ft. The aerodrome controller who was in two-way communication with the enroute controller over the hotline, found that CZV was passing 5,400 ft on descent. The enroute controller asked the aerodrome controller to direct the crew of CZV to turn right on to 090 M, which was actioned. The enroute controller issued traffic information to the crew of TAF about the relative position of CZV and requested the crew to climb to FL 150 and maintain their best rate of climb. Traffic information was not issued to the crew of CZV about TAF.

At 1240, the required vertical separation of 1,000 ft between the two aircraft reduced to 400 ft when the minimum radar separation of 5 NM was infringed. The application of radar separation and the requirements for issuing clearances were detailed in chapters 4, 9 and 12 of the Manual of Air Traffic Services (MATS).

The enroute controller received a short-term conflict alert (STCA) on the radar display. However, neither of the flight crews reported receiving a traffic alerting and collision avoidance system (TCAS) warning from their respective aircraft's display.

Occurrence summary

Investigation number 199903590
Occurrence date 27/07/1999
Location 37 km SE Maroochydore, (VOR)
State Queensland
Report release date 02/04/2001
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Loss of separation
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer The Boeing Company
Model 737
Registration VH-TAF
Serial number 23477
Sector Jet
Operation type Air Transport High Capacity
Departure point Maroochydore, QLD
Destination Sydney, NSW
Damage Nil

Aircraft details

Manufacturer The Boeing Company
Model 737
Registration VH-CZV
Serial number 23831
Sector Jet
Operation type Air Transport High Capacity
Departure point Sydney, NSW
Destination Maroochydore, QLD
Damage Nil

Boeing 767-324, VH-BZF, 3 km west-north-west of Melbourne (VOR), on 18 March 1999

Safety Action

Local safety action

As a result of the investigation, Airservices Australia Southern District have proposed to:

  1. amend the Melbourne tower training syllabus to ensure that ab initio trainees gain a broad range of experience prior to commencing aerodrome or coordinator training;
  2. require trainees and controllers supervising training to attend a training principles briefing pending the introduction of a workplace training course in the near future;
  3. impose a maximum training session duration of 2 hours; and
  4. amend local instructions relating to traffic management procedures and the use of non-duty runways.

Australian Transport Safety Bureau (ATSB) Safety Action

The ATSB is investigating safety deficiencies relating to:

  1. ab initio aerodrome controller rating training; and
  2. the identification and publication of critical safety areas including the level of separation assurance provided by standard instrument departures.

Any safety outputs issued as a result of the investigation will be published in the Bureau's Quarterly Safety Deficiency Report.

Significant Factors

  1. The supervisor of the trainee, the aerodrome controller, had a lapse in concentration at a critical stage of the departure sequence, having been operating at the position in excess of 3 hours.
  2. The trainee was unfamiliar with terminal area operations/procedures and was unaware of the increase in complexity during runway transition.
  3. Tower training publications' critical safety section and other references did not include potential standard instrument departure or arrival areas of conflict.

Analysis

The concentration level of both the aerodrome controller and the trainee had probably lapsed due to the duration of the training session. Additionally, the aerodrome controller may have been less vigilant in his monitoring of the trainee because of the reduction in aircraft numbers and his perception of the trainee's level of competence in the aerodrome control position.

Provision of information regarding the increase in complexity of traffic management during runway transition and regarding the critical safety aspects of standard instrument departures and arrivals would have provided the trainee with some knowledge to compensate for areas where he lacked experience. On-the-job training does not necessarily expose trainees to all critical elements nor provide sufficient time for them to develop their own traffic management models. Information on such critical areas is required to ensure that safety aspects are understood and considered, particularly during on-the-job training.

A greater awareness of terminal area operations and procedures may have provided the trainee with sufficient knowledge to appreciate that the departing aircraft were not going to be separated by the departure controller. In turn, this may have alerted the trainee to the fact that he was required to provide a separation solution or alternatively coordinate one with the departure controller.

Summary

A Beech 1900 (Beech) departed from runway 27 and was tracking via a STRATHBOGIE 8 standard instrument departure, on climb to 5,000 ft. Shortly after, a Boeing 767 (B767) departed from runway 34 on a DOSEL 8 standard instrument departure, on climb to 5,000 ft. The standard instrument departure tracks intersected approximately 2 NM north of the aerodrome. The departure north radar controller (departure controller) observed that the separation between the two aircraft was not going to be maintained and queried the aerodrome controller in relation to the separation procedure being applied. The aerodrome control position was being operated by a trainee under the supervision of a rated controller. The trainee advised that he thought the departure controller was providing separation. The departure controller instructed the Beech crew to turn left onto a heading of 310 degrees and the B767 crew to turn right onto a heading of 030 degrees. The two aircraft passed at the same altitude, with 1 NM lateral separation. The minimum separation required was either 3 NM laterally or 1,000 ft vertically. There was an infringement of separation standards. The B767 was fitted with a traffic alert and collision avoidance system and the crew received a traffic advisory just prior to the issue of the avoiding instructions from the departure controller.

The trainee and the aerodrome controller had been at the console for about 3 hours and the number of aircraft being managed had reduced slightly following a busy period. The runway mode was being changed from land and hold short operation (LAHSO) using runways 34 and 27, to dedicated departure runway arrangement using those runways. In LAHSO all aircraft depart from runway 27, while in the dedicated departure mode, departures to the south and west use runway 27 and those to the north and east use runway 34. In that configuration, the intersection of aircraft departure tracks is almost eliminated. It was recognised by experienced controllers that the transition period between runway modes required an increased awareness and careful consideration of the traffic management plan to ensure that potential conflicts for departing aircraft were minimised. The trainee was aware of potential problems for each mode but had not been alerted to the potential problems that may occur during a mode transition period. On taxi, the crew of the B767 requested and were approved to use runway 34. The trainee subsequently amended the departure order of the B767 and the Beech to eliminate a requirement to apply a 2-minute wake turbulence separation standard to the Beech aircraft.

The trainee did not appreciate that the aircraft's departure tracks converged north of the aerodrome. The aerodrome controller reported that as the trainee was soon to be checked for a rating his monitoring of the trainee's control was less vigilant than normal. Local instructions stated that the aerodrome controller was responsible for the separation of departing aircraft within 5 NM of the aerodrome and that for departures from different runways, the aerodrome control and departure control positions were jointly responsible for coordinating a separation solution. The departure controller's preference was to depart the B767 before the Beech but he agreed to the trainee's request to change the departure order. Normal practice in this situation was that the aerodrome control position, having initiated the change, was responsible for the separation unless otherwise coordinated. The controllers neither coordinated a separation solution nor clearly established who was responsible for ensuring separation. Both assumed that the other was going to separate the two aircraft. The aerodrome controller was not aware of the developing situation and was only alerted to the infringement following the departure controller's query to the trainee.

The trainee had undergone tower control ab initio training, which included approximately 1 day of training on the vectoring of aircraft. The course did not provide any terminal area (TMA) control training. Controllers undergoing training for tower positions were able to undertake TMA familiarisation. But the tower training syllabus did not require trainees to develop an understanding of, or to be familiar with, TMA operations. TMA familiarisation by tower trainees was conducted on an ad-hoc basis and there was no procedure to assess a trainee's level of understanding of TMA operations.

Melbourne Tower training publications did not provide advice of a preferred duration for training sessions that would maximise the training benefit. The publications did list aspects of critical safety that needed to be covered during training for both trainees or supervising controllers. But the list did not include areas of known conflict for standard instrument departures or standard arrival routes. The publications did not include advice of the potential inherent complexity of runway mode transition.

Occurrence summary

Investigation number 199903436
Occurrence date 18/07/1999
Location 3 km WNW Melbourne, (VOR)
State Victoria
Report release date 24/03/2000
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Loss of separation
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer The Boeing Company
Model 767
Registration VH-BZF
Serial number VH-BZF
Sector Jet
Operation type Air Transport High Capacity
Departure point Melbourne, VIC
Destination Sydney, NSW
Damage Nil

Aircraft details

Manufacturer Beech Aircraft Corp
Model 1900
Registration VH-IMH
Serial number VH-IMH
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Melbourne, VIC
Destination Williamtown, NSW
Damage Nil

Robinson R22 Beta, VH-HRU

Summary

The Robinson R22 helicopter had been engaged in cattle mustering operations on the day of the accident. Late in the afternoon the pilot invited one of the stockmen to accompany him on a flight to a nearby tourist resort to purchase bread for the stockcamp. They arrived at Ross River Homestead resort at about 1700 CST and sometime later decided to remain overnight at the resort. Witnesses reported that the pilot had consumed a quantity of alcohol during the course of the evening.

At about 2345-2400 witnesses heard the helicopter engine start and run for a period of time before the helicopter was seen to take-off and depart in a north-easterly direction. It climbed steeply to about 600 ft above ground level, after which the engine noise appeared to change and the aircraft descended quickly until impact with the terrain. Searchers found the wreckage soon after first light the next morning on a flat area of land between hills, approximately 800 m from the resort.

Witnesses reported that at the time of the accident there was no wind. There was a high level cloud overcast and very dark conditions. Examination of the astronomical ephemeris (a table of the moon's position) confirmed that the moon did not rise until approximately 3 hours after the accident. The helicopter was not equipped for flight under the instrument flight rules.

The evidence showed that the helicopter impacted the terrain banked to the right, in a nose-low attitude, and at high forward and vertical speeds. Impact forces destroyed the forward right and central cockpit area of the aircraft. The investigation could find no evidence of pre-existing damage to any of the helicopter's flight control systems. The type of damage to the main and tail rotor blades indicated low power and low rotor RPM at impact. Examination of the engine indicated that it was either at idle or a very low power setting at impact. The investigation determined that sufficient clean fuel of the correct grade was on board the helicopter at the time to power the engine. No defect was identified that may have influenced the circumstances of the accident.

Due to the severity of the impact, the accident was not survivable.

Occurrence summary

Investigation number 199903335
Occurrence date 09/07/1999
Location Ross River Homestead, 80 km E Alice Springs
State Northern Territory
Report release date 03/11/1999
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Collision with terrain
Occurrence class Accident
Highest injury level Fatal

Aircraft details

Manufacturer Robinson Helicopter Co
Model R22
Registration VH-HRU
Serial number 0941
Sector Helicopter
Operation type Private
Departure point Ross River Homestead, NT
Destination Unknown
Damage Destroyed

Collision with terrain, Eagle Aircraft Pty Ltd 150B, VH-EAD, Avalon Aerodrome, Victoria, on 10 July 1999

Summary

Three Eagle 150 aircraft, VH-EAD, VH-FPO and VH-JBA, were engaged on a training flight for an airshow formation routine. The lead aircraft, EAD, was callsign Eagle 1; FPO was Eagle 2 and JBA was Eagle 3. They were operating at heights between 500 ft and 800 ft. Eagle 2 carried a passenger who was a former Royal Air Force pilot with extensive formation flying experience. The other aircraft did not carry passengers.

The training sequence usually included a formation flypast at 500 ft, followed by a break into a bomb-burst manoeuvre. Following the bomb burst, Eagle 1 would pull up steeply to about 800 ft for some low-speed manoeuvres with flaps extended. Eagles 2 and 3 would remain at 500 ft and complete a pass close to each other as they flew in opposite directions. The aircraft would then rejoin for a formation flypast, followed by a break for a stream landing.

On the day of the accident, the pilots practised their routine (except the stream landing) four times. Then, after the bomb burst during the fifth practice, Eagle 1 climbed to between 700 ft and 800 ft for the low-speed manoeuvres with flaps extended, while Eagles 2 and 3 performed their close pass in opposite directions. As the three aircraft were manoeuvring for a rejoin, the passenger in Eagle 2 observed Eagle 1 roll to the right, flick inverted and begin rotating to the right in a steep nose-down attitude. The rotation stopped after about one revolution, but the aircraft flicked a second time. The rotation ceased again after about one revolution, but the aircraft flicked inverted again. The pilot did not effect recovery before the aircraft impacted the ground.

Examination of the wreckage did not reveal any defect that may have contributed to the accident. Measurement of a flap actuator extension indicated that the wing flaps were extended to 32 degrees (91% of the maximum extension available) at the time of impact. The elevator trim tab was set to 18 degrees up, indicating that the aircraft was trimmed for level flight at 61 kts indicated airspeed with the flaps set to 35 degrees.

The weather conditions at the time of the accident were fine, with a slight sea breeze from the south-east at 2 to 3 kts, with a surface temperature of 13 degrees C, visibility of more than 15 km and no low cloud.

The pilot of Eagle 1 held a Private Pilot Licence with a current Class 2 medical certificate. He had accumulated a total of about 780 flying hours including 47 hours on Eagle aircraft, which he had been flying for about 22 months. About 39 hours of his Eagle experience had been gained on X-TS 150 aircraft and about 8 hours on EAD, a 150 B variant. The X-TS 150 variant is powered by a Continental IO-240A engine driving a McCauley 70-inch diameter propeller of 54-inch fixed pitch, whereas the 150 B variant is powered by a Continental IO-240B engine driving a McCauley 70-inch diameter propeller of 57-inch fixed pitch. There are physical differences between the engines but power outputs are the same. The main difference between the variants was the propeller pitch. Consequently, the performance of the 150B variant, having a propeller with a cruise pitch, would be slower to respond to a rapid increase in power than the X-TS 150.

The pilot had completed a formation flying endorsement approximately 3.5 years previously. Since 26 January 1997 he had accumulated about 47 hours of formation flying in Eagle, Piper Cherokee and Cessna 150 aircraft. He did not hold an aerobatic rating. The pilot's last Biennial Flight Review was completed on 22 November 1998 in an Eagle X-TS 150 aircraft. His last flight before the accident flight had been in EAD 4 days before the accident. The pilot's last airshow routine practice was at Avalon on 16 May 1999.

No pre-existing medical or toxological condition that may have contributed to the accident was identified during the pilot's autopsy.

The Eagle 150 B aircraft was granted Certificate of Type Approval 179-1 by the Civil Aviation Safety Authority (CASA), on 11 November 1997. The process of certification included extensive testing of the aircraft in accordance with Joint Aviation Requirements-Very Light Aeroplanes (JAR-VLA).

The stall characteristics of the Eagle were tested in accordance with JAR - VLA 201, 203, 207 and 221. The flight-test program included stalling the aircraft in more than 200 different combinations of configuration, airspeed, deceleration rate, attitude, flight path and G loading. The aircraft met or exceeded the requirements of JAR-VLA, demonstrating generally benign stall characteristics in all configurations when in balanced flight at the point of stall. Entry into a stall from unbalanced flight could result in an incipient spin.

If a pilot releases pressure on the flight controls after entering an incipient spin, the aircraft should cease rotating and assume a steep nose-down attitude. The pilot can then recover the aircraft to level flight. If the pilot immediately begins spin recovery actions as described in the "Pilot's Operating Handbook and Approved Flight Manual" for the Eagle 150 B, the aircraft should be capable of recovery to level flight from a single-turn incipient spin.

In production test flying, EAD had demonstrated normal stall characteristics.

The Flight Manual, Section 3.7 stated in part:

"Intentional spins are prohibited in this aircraft. Should an inadvertent spin occur, the following recovery procedure should be used:

  1. Retard the throttle to idle
  2. Centralise controls
  3. Retract flaps

If the aircraft continues to spin:

  1. Determine the direction of rotation by visual method or by reference to the turn indicator (turn and balance indicator)
  2. Apply and hold full rudder opposite to the direction of rotation
  3. If the aircraft fails to stop rotating, move control column smoothly forward until rotation stops
  4. As rotation stops, centralise controls, roll wings level and pull the aircraft out of the dive".

The section included the following note:

"Rotation may seem to increase in speed when forward controls are applied, this is normal and is to be expected just prior to rotation stopping". In this occurrence, the aircraft was observed to roll steeply to the right and then enter a steep nose-down attitude consistent with a stall followed by an incipient spin. Immediately before this, the aircraft was manoeuvring at low airspeed, with flaps extended. The pilot did not retract the flaps in accordance with the aircraft Flight Manual's spin-recovery procedure, but certification test flying had shown that this should not have affected the aircraft's capability to recover.

The pilot had considerably more experience on the X-TS 150 variant than on the 150 B variant, but it is unlikely that differences between the two variants affected the circumstances of the accident.

At the time of the stall, the aircraft was turning right at low airspeed. The passenger in Eagle 2 was giving advice to the pilot of Eagle 1 concerning manoeuvres to enable Eagles 2 and 3 to rejoin formation more efficiently. It is possible the pilot of Eagle 1 was focussing on the rejoin manoeuvre to the extent that he did not recognise the onset of the stall.

The observed manoeuvres are consistent with a stall from an uncoordinated right turn, followed by an incipient spin from which recovery was not effected. The reason the pilot was unable to recover the aircraft from the spin could not be determined.

Occurrence summary

Investigation number 199903333
Occurrence date 10/07/1999
Location Avalon, Aero.
State Victoria
Report release date 22/03/2001
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Collision with terrain
Occurrence class Accident
Highest injury level Fatal

Aircraft details

Manufacturer Eagle Aircraft Australia
Model 150
Registration VH-EAD
Serial number 021
Sector Piston
Operation type Private
Departure point Moorabbin, VIC
Destination Moorabbin, VIC
Damage Destroyed