de Havilland Canada DHC-8-102 , VH-TNU

Safety Action

Shortly after the incident, the operator of TNU published a memorandum to all company flight crew. It included a description of the event and the lessons to be drawn from it and was published in the March 1999 Issue of Asia Pacific Air Safety under the title "Follow your instincts".

As a result of its response to the occurrence, Airservices Australia held meetings at which the circumstances of the incident, with specific reference to the requirements of sight and follow procedures, were discussed amongst controllers. Additionally, Airservices examined the need for cross-referencing the sight and follow procedures in Chapter 6 Section 4 of MATS with Chapter 8 of MATS. Following this examination, sight and follow procedures were removed and visual separation procedures were revised through Amendment List 23 dated 3 December 1998 of MATS.

Significant Factors

  1. The approach controller changed the approach sequence for TNU.
  2. The sight and follow instructions issued to TNU provided insufficient and inaccurate information.
  3. The crew of TNU misidentified EWM as CZA.
  4. Neither TNU nor CZA was equipped with TCAS.

Analysis

In the circumstances, the controller's decision to change the assigned runway for TNU was inappropriate and not in accordance with Local Instructions. It resulted in additional workload by way of the vectoring instructions, as well as the setting up of the sight and follow procedure, for TNU. There were other options for reducing workload such as vectoring the traffic survey aircraft away from the area. Ultimately, the decision set the scene for the conflict to develop.

The information the controller gave the crew of TNU concerning the aircraft they were to sight and follow was incomplete. Because the crew was not given its number in the approach sequence, there was no reason for other than one aircraft ahead to be sighted. Also, because of the speed differential between the two aircraft, the azimuth information provided by the controller rapidly became inaccurate. These oversights resulted in the misidentification by the crew of TNU of EWM as CZA.

The report by the crew that the traffic had been sighted, and the immediate acceptance by the controller of this information, was, in effect, one assumption reinforcing another. In other words, the crew said what the controller wanted to hear. This had two main effects. It:

  1. confirmed to the crew that they had correctly identified the traffic, effectively implying that there was no other potentially conflicting traffic, and
  2. it enabled the controller to divert his attention away from TNU and CZA to the control of other traffic.

Had either TNU or CZA been traffic alert and collision avoidance system equipped, it is likely that either or both crews would have become aware of the confliction before separation standards were infringed. It is also probable that the seriousness of the occurrence would have been less if the TNU cabin crewmember had reported her observation of CZA to the flight deck crew.

Summary

VH-CZA, a Boeing 737, was inbound to Brisbane and was being sequenced to follow VH-EWM, a BAe 146, for a visual approach to runway 19 via left base. Both aircraft were under the control of the Brisbane Approach radar controller and were being processed via the Coolangatta One Standard Terminal Arrival (STAR). VH-TNU, a Dash 8, was behind CZA and was being processed via the Jacob's Well Four STAR.

The Brisbane Flow Controller had originally assigned TNU to land on runway 14. This required the controller to position the aircraft east of the Jacob's Well - Brisbane track, and for the crew to track direct to the Brisbane Control Tower before joining right base for runway 14. There were two light aircraft operating to the south and southeast of the aerodrome at 1,500 ft on traffic survey work. The controller assessed that these aircraft may have conflicted with TNU overflying the aerodrome for runway 14. As well, there was departing traffic that he considered might also have conflicted with TNU being processed for runway 14. As a result, the controller decided to process TNU for runway 19.

The controller vectored TNU north to a position approximately abeam and above CZA and informed the crew that they were following the traffic which was low and to their right. The crew of TNU advised that they were still in cloud. At this time, TNU was approaching 5,000 ft heading 360 degrees M and CZA was descending through 3,500 ft, heading 310 degrees M. The controller then asked the crew of CZA to fly a close left base, and advised that they were following a blue and white BAe 146 aircraft (EWM) which was over St Helena Island on left base for runway 19. A short time later, the crew of TNU reported visual. The controller acknowledged this transmission and then instructed EWM to contact the tower.

After making a number of transmissions to other traffic, the controller instructed TNU to turn left heading 310 and to descend to 2,500 ft. He asked the crew if they still had the B737 in sight, adding that it was in their 10 o'clock position at 3 NM. The controller instructed CZA to descend to 1,500 ft. The crew of CZA then reported visual and were cleared by the controller for a visual approach via a close left base. After CZA acknowledged this clearance, the crew of TNU reported that they had the traffic sighted. The controller responded that CZA was for a close left base and cleared TNU for a visual approach. He then instructed CZA to contact the tower and asked the crew of TNU to closely follow CZA. The controller then processed a departing aircraft and accepted the transfer of another inbound aircraft onto his frequency. A turn instruction he gave this aircraft was not initially understood and required two further transmissions for clarification. As this exchange concluded, the controller asked the crew of TNU to confirm that they still had visual contact with the B737. The crew responded that they believed that the B737 had landed. The controller immediately instructed TNU to turn right. He then confirmed with the tower controller that TNU was turning away from CZA. CZA subsequently landed normally on runway 19 and TNU was processed for landing on runway 14.

Recorded radar data indicated that the minimum separation between the aircraft was about 200 ft vertically, and 0.8 NM horizontally. This occurred as TNU was instructed by the approach controller to turn away from CZA. The required separation standard in the circumstances was 1,000 ft vertically or 3 NM horizontally. The data also showed that, at the time CZA was given as traffic to TNU, the groundspeed of CZA was 143 kts while that of TNU was 243 kts. When the crew of TNU reported sighting the traffic, the position of CZA relative to TNU was between 7 and 8 o'clock at about 3 NM rather than 10 o'clock as the controller had indicated a short time earlier. At this time, EWM was at about a 10 o'clock position relative to TNU but at a range of 7 NM.

A review of the automatic voice recording of communications between the approach controller, the aircraft, and other agencies confirmed that there was no request from the control tower for TNU to be processed for runway 14. It also confirmed that the crew of TNU was not given their number in the landing sequence.

Neither TNU, nor CZA, was fitted with a traffic collision avoidance system (TCAS).

The controller

The controller involved was highly experienced. He gained his initial ATC ratings in June 1980. He had been rated and endorsed to perform the radar approach controller duties since April 1990.

The incident occurred two hours after he had commenced duty on the Approach South position. The controller stated that he did not consider the traffic levels and/or workload to be unusually high at the time of the incident. He indicated that he changed the traffic sequence with respect to TNU to reduce his workload and improve traffic management for both himself and the tower.

Information from the crew of VH-TNU

The technical crew of TNU said that, in hindsight, they did not sight CZA at any stage during the sequence. Their report to the controller that they believed the aircraft had landed indicated that they had mis-identified EWM as CZA. The vectors they had been given placed the aircraft high and fast on the descent profile. This, coupled with the checklist actions and the request to sight the traffic, created a high cockpit workload situation. Neither pilot could recall being given their number in the landing sequence.

The cabin flight attendant on TNU became aware of CZA when she saw it through a passenger window as she completed the cabin pre-landing checks. She felt some concern regarding the proximity of the aircraft and considered entering the cockpit to confirm that the pilots knew of its presence. In the event, she decided to take no action, as she felt confident that they would have been aware of the situation.

Brisbane arrival procedures

The management of air traffic in the Brisbane Terminal Area (TMA) involved the formulation of a traffic management plan for arriving and departing aircraft. The Terminal Approach Coordinator (TAC) decided upon the plan after liaison with the Traffic Management Coordinator (TMC) in the control tower. Its purpose was to determine the most efficient use of available runways and types of approaches consistent with prevailing weather conditions and traffic density and patterns. Once the plan was agreed, the TAC directed the Flow Controller to sequence the arriving traffic in accordance with the traffic management plan. The task of the radar approach controller was to direct aircraft in accordance with the plan to ensure that aircraft arrived in sequence at appropriate intervals for efficient traffic flow.

In order to make the best use of the available runways and minimise delays, procedures had been developed to assist controllers with arriving aircraft required to overfly the aerodrome from the south for runway 14. These procedures were detailed in Northern District Local Instructions TMA 27, and were designed to assist in minimising workload on both the approach and control tower controllers by providing a standardised technique which allowed departing aircraft to depart and remain clear of the arriving overflying traffic. The instruction stated:

In the case of RWY 19/01 and an arrival from the east/southeast for landing RWY 14, the following shall apply. The arrival shall be positioned east of the JCW-BN VOR track, tracking direct to the CONTROL TOWER assigned A020 and for the ACFT to be on TWR frequency no later than 5NM with no restrictions.

These tracking requirements will ensure that a RWY 19 LAV SID can proceed unrestricted.

Sight and Follow procedures

At the time of the occurrence, visual separation standards were detailed in the Manual of Air Traffic Services (MATS) Chapter 4, Section 8. Air traffic controllers could use the visual separation standard to separate aircraft flying at or below FL125. However, if this standard was used an instruction to maintain visual separation with, or to follow other aircraft, should have been issued in accordance with requirements of MATS Chapter 6 Section 4. Chapter 8 of MATS, "Enroute/Approach Control", did not make reference to sight and follow procedures.

Occurrence summary

Investigation number 199802964
Occurrence date 03/08/1998
Location 13 km E Brisbane, Aero.
State Queensland
Report release date 20/08/1999
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 De Havilland Canada/De Havilland Aircraft of Canada
Model DHC-8
Registration VH-TNU
Serial number 203
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Williamtown, NSW
Destination Brisbane, QLD
Damage Nil

Aircraft details

Manufacturer The Boeing Company
Model 737
Registration VH-CZA
Serial number 23653
Sector Jet
Operation type Air Transport High Capacity
Departure point Sydney, NSW
Destination Brisbane, QLD
Damage Nil

Cessna A185E, VH-HTS

Summary

On Sunday, 26 July 1998, at about 1324 EST, a Cessna A185E floatplane, VH-HTS, crashed onto a ridge forming the southern shore of Calabash Bay NSW. The accident occurred during a go-around manoeuvre following an unsuccessful landing approach to the Berowra water alighting area. At the time of the accident the Calabash Bay area was affected by strong winds, widespread rain and showers, low cloud, and reduced visibility. The aircraft was operated by South Pacific Seaplanes and was undertaking a charter flight from Palm Beach to Berowra. All five occupants, including the pilot, suffered fatal injuries. The aircraft was destroyed by impact forces.

The investigation found that the circumstances of the accident were consistent with uncontrolled flight into terrain. The decision by the pilot to carry out a go-around into a confined area surrounded by steep-sided terrain was the culminating factor in a combination of local factors, organisational deficiencies and inadequate safety defences. Local factors included poor weather conditions, a lack of formal procedures to provide safe methods of operation, and commercial pressures. Organisational deficiencies were identified within South Pacific Seaplanes concerning the management and conduct of charter operations carried out by that company, and in the safety regulation of those operations by the Civil Aviation Safety Authority.

During the investigation a number of safety deficiencies were identified. Safety actions to address those deficiencies are currently being formulated by the Bureau of Air Safety Investigation. A description of those deficiencies, and corresponding safety actions, will be summarised in section 4 of the final report.

Occurrence summary

Investigation number 199802830
Occurrence date 26/07/1998
Location Calabash Bay
State New South Wales
Report release date 25/02/1999
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Loss of control
Occurrence class Accident
Highest injury level Fatal

Aircraft details

Manufacturer Cessna Aircraft Company
Model 185
Registration VH-HTS
Serial number 18501835
Sector Piston
Operation type Charter
Departure point Palm Beach, NSW
Destination Berowra Waters, NSW
Damage Nil

Partenavia P68B, VH-IXH

Factual Information

Personnel information & licence details

The pilot had obtained a Commercial Pilot Licence in January 1996 followed by an Instructor Rating in August 1996. He was issued with a Command Instrument Rating on 25 February 1998 and commenced employment with the aircraft operator.

Flight experience & logbook entries to 19 July 1998

Total hours 1,013.5 (last 90 days 130.4)
Total command 778.7 (130.4)
Total dual 234.8
Total instructional flying 438.1
Multi-engine command 279.5 (130.4)
Instrument flight 43.5 (16.6)
Night 39.0 (12.9)
Last check 2-4 March 1998, initial route check by company chief pilot

The pilot's logbook indicated that he had completed 22 GPS arrival procedures since commencing operations at Wagga Wagga. This included 15 GPS arrival procedures conducted while inbound to Wagga Wagga, five of which were conducted in marginal weather conditions with significant cloud below 1,500 ft above ground level.

The pilot had a normal rest pattern in the days preceding the accident. There was no reported sleep disruption, evidence of fatigue or other factors which might have affected his behaviour. He had last worked 3 days prior to the day of the accident, on a similar schedule to that of the accident flight.

During post-mortem toxicology testing of the pilot, low levels of amphetamine and metabolites of anabolic steroids were detected. Specialist advice indicated that the effects of such compounds were extremely complex and the extent to which they may have influenced the pilot's performance during the flight could not be determined.

Observed weather conditions at Wagga Wagga

A meteorologist with the Bureau of Meteorology conducted an aerodrome observation at Wagga Wagga shortly before the accident. The wind was a light easterly with visibility reducing to 1,500 m in light rain and mist. Significant cloud was observed in the vicinity of the aerodrome and included 1 octa of stratus cloud at 300 ft above ground level and 5 octas of stratus at 600 ft above ground level.

Wreckage and impact information

At the time of the collision with Gregadoo Hill the aircraft was flying wings-level in an attitude consistent with level flight. The main wreckage came to rest over the crest of the hill, approximately 65 m beyond the initial point of impact.

The cockpit and cabin structure, including the wing centre section, was destroyed. Post-impact fire substantially damaged both wings. Damage to the propeller blades and their associated assemblies was consistent with each engine operating under power at the time of impact.

Aircraft information

The aircraft was equipped with two barometric pressure-sensitive altimeters. The left altimeter was part of the pilot's standard instrument panel. The second altimeter was located on the lower far right of the co-pilot's instrument panel. Both altimeters separated from the instrument panel during impact.

Although the internal mechanism of the pilot's left altimeter had been substantially destroyed, it was possible to obtain the setting of the altimeter sub-scale. Examination of the instrument face did not reveal the presence of any witness marks and the indicated altitude at the time of the accident could not be determined.

The QNH set on the left altimeter sub-scale was 1013 hPa, which corresponded with the forecast area QNH at the time of the accident. The QNH information had been provided to the pilot by the en-route controller. With that setting on the altimeter sub-scale, the instrument would have indicated that the aircraft was approximately 150 ft higher than it actually was. Although there was a 5-hPa difference between the area QNH and the actual local QNH at Wagga Wagga, it was within the normal amendment criteria.

Components of the right altimeter were evident at the accident site. The instrument face had been separated from the case and the pre-impact altitude indication could not be determined, as there were no witness marks evident. The QNH sub-scale was set to 1008 hPa. This setting corresponded with the departure aerodrome's QNH and the actual QNH for Wagga Wagga at the time of the accident. There was no automatic broadcast of weather information provided at Wagga Wagga.

The aircraft pitot static system was extensively damaged during the accident. The position of the selector valve for the alternate static source could not be determined.

As there was an actual QNH available from the automatic terminal information service at Albury, the pilot was required to conduct a check of the aircraft's altimeters prior to takeoff. At least one of the instruments was required to indicate within 60 ft of the nominated elevation. An instrument indicating an error of more than 75 ft was to be placarded as unserviceable for flight under the Instrument Flight Rules and an entry made in the aircraft maintenance release to that effect. There was no evidence that either of the aircraft altimeters was outside these tolerances in the period leading up to the accident.

The ADF (navigation aid) receiver installed in the aircraft was tuned to the frequency of the Wagga Wagga non-directional beacon. The number one VOR (navigation aid) receiver was tuned to the frequency of the Wagga Wagga VOR. The VOR omni-bearing selector was set to a course of 013 degrees and this corresponded with the published magnetic track between Albury and Wagga Wagga.

The aircraft's maintenance release was valid at the time of the accident and no entries had been made in relation to outstanding unserviceable items. It was reported that the pilot would inform the chief pilot of any maintenance action required and that would then be coordinated with the maintenance organisation. The aircraft maintenance records contained no outstanding airworthiness issues.

The investigation team was provided with a hand-written note compiled by the pilot, which listed aircraft defects. The list was to be supplied to the aircraft operator and maintenance organisation for the next period of scheduled maintenance and identified items that the pilot considered could require attention. The team assessed the significance of the list and recovered some components from the accident site for more detailed examination. However, no evidence was available to suggest that the listed items had contributed to the circumstances of the occurrence.

Global positioning system (GPS) and instrument approach

The aircraft was equipped with a GPS satellite receiver and the pilot broadcast on the mandatory broadcast zone frequency his intention to conduct the Albury - Wagga Wagga GPS Arrival. This procedure required the pilot to use distance information supplied by the GPS receiver to conduct a progressive descent as the aircraft approached the aerodrome. A ground-based navigation aid provided azimuth guidance to the pilot. The aircraft's navigation equipment was correctly configured for the procedure.

The last position recorded by the GPS receiver closely matched the actual position of the accident site and indicated that the aircraft had 4.20 NM to run to the aerodrome's VOR navigation aid. The last altitude recorded on the GPS receiver was 1,274 ft. At this stage of the approach procedure, the aircraft should not have descended lower than 2,000 ft. Descent to the minimum descent altitude (MDA) could then be made once the aircraft was within 3 NM of the Wagga Wagga VOR.

The MDA published for the GPS instrument arrival procedure was 1,580 ft, with a required in-flight visibility of 2,400 m. Descent to 1,580 ft would position the aircraft 856 ft above the aerodrome elevation. Prior to departing Albury, the pilot had received the latest weather report of broken cloud at 600 ft above ground level and 2,000 m visibility in the vicinity of Wagga Wagga aerodrome.

Before using the GPS receiver for operations under the Instrument Flight Rules, the holder of an instrument rating was required to complete a course of ground training to a specified syllabus. No record was found of the pilot having completed this training and the pilot's employer had provided no formal training in the use of the GPS equipment installed on the aircraft. As the GPS receiver was not equipped with a current data card, it was not approved for use under the Instrument Flight Rules. The aircraft was not equipped with alternative distance measuring equipment.

Significant Factors

  1. The pilot was operating the aircraft in instrument meteorological conditions below the approved minimum descent altitude.
  2. Low cloud was covering Gregadoo Hill at the time of the accident.

Analysis

The pilot had received an accurate appreciation of the weather conditions in the vicinity of Wagga Wagga prior to departing Albury. At that stage it would have been apparent that low cloud and poor visibility were likely to affect the aircraft's arrival. Under such conditions it would not have been possible to land from the GPS arrival procedure.

As the reported cloud base and visibility were both below the minimum criteria, it is difficult to rationalise the pilot's transmission that, according to the latest weather report, he would be visual at the minimum descent altitude. This statement suggests that the pilot had already made the decision to continue his descent below the minimum altitude for the procedure and to attempt to establish visual reference for landing.

Based on the report of broken low cloud in the vicinity of the aerodrome, the pilot would have needed to descend to 1,324 ft above mean sea level to establish the aircraft clear of cloud. This is within 50 ft of the last altitude recorded on the GPS receiver.

Due to the difference between the actual and forecast QNH, the left altimeter would over-read by approximately 150 ft. At the time of the occurrence an otherwise correctly functioning instrument would have indicated an altitude of approximately 1,400 ft.

The pilot had probably set the right altimeter to the local QNH prior to departing Albury. As this setting also corresponded to the actual QNH at Wagga Wagga, that instrument would have provided the more accurate indication of the aircraft's operating altitude. However, because of its location on the co-pilot's instrument panel, it is unlikely that the pilot would have included that altimeter in his basic instrument scan.

It was not possible to assess the extent to which illicit drugs may have influenced the pilot's performance during the flight and affected his ability to safely operate the aircraft.

Summary

The aircraft operator had been contracted to provide a regular service transporting bank documents, medical pathology samples and items of general freight between Wagga Wagga, Albury and Corowa. On the day of the accident a passenger was accompanying the pilot for the day's flying.

The pilot commenced the flight from Corowa to Albury under the Visual Flight Rules, flying approximately 500 ft above ground level. At Albury he obtained the latest aerodrome weather report for Wagga Wagga, which indicated that there was scattered cloud at 300 ft above ground level, broken cloud at 600 ft above ground level, visibility restricted to 2,000 m in light rain and a sea-level barometric pressure (QNH) of 1008 hPa.

At 1715 Eastern Standard Time (EST) the aircraft departed Albury for Wagga Wagga under the Instrument Flight Rules. The pilot contacted the Melbourne en-route controller at 1728 and reported that he was maintaining 5,000 ft.

Although the aircraft was operating outside controlled airspace, the en-route controller did have a radar surveillance capability and was providing the pilot with a flight information service. However, no return was recorded from the aircraft's transponder and at 1732 the pilot reported that he was transferring to the Wagga Wagga Mandatory Broadcast Zone frequency. This was the pilot's last contact with the controller.

Although air traffic services do not monitor or record the Wagga Wagga Mandatory Broadcast Zone frequency, transmissions made on this frequency are recorded by AVDATA for the purpose of calculating aircraft landing charges. This information was reviewed following the accident.

The pilot broadcast his position inbound to the aerodrome on the mandatory broadcast zone frequency and indicated that he was conducting a Global Positioning System (GPS) arrival. He established communication with the pilot of another inbound aircraft and at 9 NM from the aerodrome, broadcast his position as he descended through 2,900 ft.

Approximately 1 minute and 20 seconds later, the pilot advised that he was passing 2,000 ft but immediately corrected this to state that he was maintaining 2,000 ft. He also stated that it was "getting pretty gloomy" and that according to the latest weather report he should be visual at the procedure's minimum descent altitude. The aircraft would have been approximately 6 NM from the aerodrome at this time. This was the last transmission heard from the pilot.

The resident of a house to the south of Gregadoo Hill sighted the aircraft a short time before the accident. He was standing outside his house and stated that the aircraft was visible as it passed directly overhead at what appeared to be an unusually low height. The aircraft then disappeared into cloud that was obscuring Gregadoo Hill, approximately 350 m from where he was standing. Moments later he heard the sound of an impact followed almost immediately by a red flash of light. The noise from the engines appeared to be normal up until the sound of the impact.

The aircraft had collided with steeply rising terrain on the southern face of Gregadoo Hill, approximately 40 ft below the crest. The hill is 4 NM from the aerodrome and is marked on instrument approach charts as a spot height elevation of 1,281 ft. The estimated time of the accident was 1739.

The pilot and passenger sustained fatal injuries.

Occurrence summary

Investigation number 199802757
Occurrence date 20/07/1998
Location 7 km S Wagga Wagga, Aero.
State New South Wales
Report release date 07/04/1999
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Occurrence class Accident
Highest injury level Fatal

Aircraft details

Manufacturer Partenavia Costruzioni Aeronautiche S.p.A
Model P.68
Registration VH-IXH
Serial number 186
Sector Piston
Operation type Charter
Departure point Albury, NSW
Destination Wagga Wagga, NSW
Damage Destroyed

Boeing 737-476, VH-TJQ

Safety Action

During the course of the investigation, it became known that hand-held checklists were being used for single-pilot operations in instrument meteorological conditions.

Consequently, the Bureau of Air Safety Investigation is investigating a perceived safety deficiency. The deficiency relates to the practice of single-pilot IFR flight crew using hand-held checklists during ILS approaches, with a possible loss of situational awareness associated with distraction.

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

Significant Factors

  1. The attention of the pilot under training was partially diverted from safely taxiing the aircraft due to his pre-occupation with a previous event.
  2. The training captain did not provide a timely warning to the pilot under training that he had passed the correct taxiway and was approaching an active runway.

Analysis

The task of taxiing the aircraft after landing was not particularly demanding. The night was fine and clear, there were no works in progress, and both pilots of the Metro were familiar with the airport layout. However, it was apparent that the attention of the pilot under training was partially diverted from taxiing the aircraft by his pre-occupation with how he had performed during the practice ILS approach. The result was that he then mistakenly believed the aircraft was still approaching the entry to taxiway Bravo, when in fact the aircraft had passed that point and was approaching runway 34L.

The training captain noticed that the aircraft had passed the entry to taxiway Bravo, and was about to query the pilot under training when he noticed the other aircraft landing on runway 34L. In hindsight, he should have alerted the pilot under training when it became apparent that the aircraft was not beginning to turn into taxiway Bravo.

Although it was reasonable to have expected the crew of the Metro to enter taxiway Bravo after correctly reading back their taxi clearance, the vigilance and prompt action of the tower controllers acted as a final safety defence to stop the aircraft from entering the runway.

Summary

A Fairchild SA227-AC (Metro) aircraft landed on runway 34R, with an instruction to exit onto taxiway Tango 1 and taxi via taxiway Juliet. The pilot contacted the surface movement controller (SMC) while approaching a mandatory holding point on taxiway Juliet, and was instructed to taxi via taxiway Bravo and hold short of runway 25. The pilot read the instruction back correctly. That instruction required the pilot to continue ahead on taxiway Juliet, passing the entry to taxiway Charlie before turning right into taxiway Bravo.

The tower controllers subsequently observed the Metro taxiing along taxiway Juliet, past the entry to taxiway Bravo, towards runway 34L, which lay a short distance beyond taxiway Bravo. At that time, a Boeing 737 (B737) was touching down on runway 34L. The SMC instructed the pilot of the Metro to stop. As there was no reply, the instruction was immediately repeated, and subsequently acknowledged. The Metro was stopped at the edge of runway 34L, beyond the runway holding point. The pilot of the B737 was also instructed to stop immediately, but the aircraft was too close to the taxiway Juliet intersection to comply. The B737 was steered to the left of the runway centreline to increase separation from the Metro, subsequently passing about 25 m in front of that aircraft, at about 80 kts.

The occurrence happened at night in fine conditions; there were no works taking place in the area; and all relevant taxiway lights, runway holding point lights and movement area guidance signs were reported by the air traffic controllers to have been functioning normally. However, when subsequently interviewed, both pilots asserted that the runway 34L holding point lights on taxiway Juliet were not illuminated. Shortly after the incident an airport safety officer had been requested to conduct an inspection of the ground lighting in the occurrence area. All lighting, including the holding point lights on taxiway Juliet protecting runway 34L, were observed to be functioning normally.

An investigation established that the pilot flying the aircraft was undergoing command training under the supervision of a training captain. A practice Instrument Landing System (ILS) approach had been flown, during which the pilot under training experienced difficulties in maintaining the required flight tolerances. After landing, the pilot correctly obtained and read back the taxi clearance. However, he subsequently failed to notice that the aircraft had passed taxiway Charlie and was approaching the entrance to taxiway Bravo. Believing he was now approaching taxiway Charlie, the pilot continued to taxi along taxiway Juliet, expecting to see the entry to taxiway Bravo.

At about that point, the training captain, noticing that the aircraft had just passed the entry to taxiway Bravo, looked towards the pilot to ask where he was going, but immediately noticed the lights of a landing aircraft on runway 34L. Concerned about the proximity of the other aircraft, he immediately instructed the pilot under training to stop, which coincided with similar instructions from the SMC.

During discussions with the crew of the Metro, it became apparent that, after landing, the pilot under training had been concerned with his performance during the practice ILS approach, and had initiated a brief discussion with the training captain at about the time the aircraft had been taxiing along taxiway Juliet.

Both pilots, who were very familiar with the layout of Sydney Airport, also indicated that the movement area guidance signs (MAGS) were somewhat confusing when indicating the entry to taxiways. However, the pilot under training said that normally he did not refer to the MAGS because of his familiarity with the taxiway layout.

Occurrence summary

Investigation number 199802817
Occurrence date 22/07/1998
Location Sydney, Aero.
State New South Wales
Report release date 03/08/1999
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Loss of separation
Occurrence class Accident
Highest injury level None

Aircraft details

Manufacturer The Boeing Company
Model 737
Registration VH-TJQ
Serial number 24442
Sector Jet
Operation type Air Transport High Capacity
Departure point Brisbane, QLD
Destination Sydney, NSW
Damage Nil

Aircraft details

Manufacturer Fairchild Industries Inc
Model SA227
Registration VH-UUO
Serial number AC530
Sector Turboprop
Operation type Charter
Departure point Brisbane, QLD
Destination Sydney, NSW
Damage Nil

Gates Learjet Corporation 35A, VH-JIG, Avalon Airport, Victoria, on 24 June 1998

Safety Action

As a result of this occurrence, the Bureau of Air Safety Investigation is investigating an apparent safety deficiency concerning recurrency flight training. Any safety recommendation resulting from this issue will be published in the Bureau's Quarterly Safety Deficiency Report.

As a result of this occurrence, the operator has:

  1. Amended the company operations manual to specifically prohibit either a check pilot or trainee accepting any variation to the normal challenge/response check-list procedures; and
  2. Amended the company operations manual to require that all asymmetric landings be conducted in accordance with the requirements of the aircraft flight manual.

Summary

The handling pilot was undergoing a scheduled 6-monthly proficiency check in the Learjet, under the supervision of an experienced instructor who occupied the right control seat. The flight was planned to depart from Essendon and proceed to the Ripley locator, for an entry into the holding pattern, before making a locator approach to Avalon. Three touch-and-go circuits were planned at Avalon, including one 700-ft asymmetric low-level circuit following a simulated engine failure at V1. The aircraft was then to return to Essendon via the Plenty locator for an instrument landing system (ILS) approach.

The instructor briefed the exercise in detail and, because the pilot under check had low experience in the Learjet, it was decided that the instructor would handle all radio communications and conduct the necessary check sequences. The instructor also indicated that it was company policy for the aircraft be landed with less than full flap during an asymmetric landing. The aircraft was to be landed with flap 20 at Vref +10 kts.

The flight proceeded normally up to the point of the simulated engine failure at V1. When the instructor simulated a right engine failure by placing the thrust lever in the IDLE position, the aircraft drifted to the right. Intervention by the instructor enabled the aircraft to return to balanced flight. The handling pilot continued to carry out the 700-ft circuit in the after-take-off configuration of gear UP and flap 8. Flap 20 was selected during the base turn. The aircraft was flared normally with both thrust levers in the IDLE position. As the aircraft settled, a slight vibration was noticed, and both pilots became aware that the landing gear was still selected UP. Go-round power was applied and the aircraft climbed away. The landing gear was cycled normally and the aircraft returned for a full stop landing. A subsequent inspection of the aircraft showed that the only evidence of a runway strike was abrasion of the lower fuselage mounted very high frequency (VHF) blade antenna.

A subsequent investigation revealed that the pilot under check was allocated one hour of Learjet flying every 3 months. The instructor had selected the flight sequences to give the pilot the maximum handling exposure in the limited time available. In doing so, the normal two-crew, challenge and response routines were abandoned and the checks had to be accomplished by the instructor alone. The instructor became distracted by the asymmetric handling issues, and the demands of the low-level circuit, subsequently forgetting the relevant downwind and pre-landing checks. The handling pilot, who had been absorbed with controlling the aircraft, had lost situational awareness and did not notice the lack of check procedures by the instructor, or the lack of a positive gear-down indication.

The approach had been carried out with flap 20 extended, rather than full flap (flap 40), because the operator had previously experienced a partial loss of control during training when attempting an asymmetric go-around at flap 40. However, with flap 20 selected, the landing gear warning system was inhibited, contributing to the late realisation that the landing gear was not extended. The flap 20 asymmetric approach configuration was not in accordance with the manufacturer's flight manual recommendations.

Occurrence summary

Investigation number 199802529
Occurrence date 24/06/1998
Location Avalon, Aero.
State Victoria
Report release date 27/04/1999
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Ground strike
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Gates Learjet Corp
Model 35
Registration VH-JIG
Serial number 35-400
Sector Jet
Operation type Flying Training
Departure point Essendon, VIC
Destination Essendon, VIC
Damage Minor

Boeing 767, ZK-NCJ

Safety Action

As a result of this and other similar occurrences, the Bureau of Air Safety Investigation is currently investigating two perceived safety deficiencies. The deficiencies relate to training requirements for air traffic service officers as a result of changes in airspace and the operation of controller pilot datalink facilities by air traffic service officers.

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

Local safety action

As a result of the occurrence and the subsequent investigations by the Bureau of Air Safety Investigation and Airservices Australia, the Northern District En Route manager implemented the following safety actions:

  1. Establishment of a local training assessment panel for non-ab initio controllers transferring inter-group.
  2. Establishment of controller pilot datalink facility fault reporting and monitoring procedures.
  3. Establishment of monthly meetings to monitor the performance of the SITA (Societe Internationale de Telecommunications Aeronautiques, communications network) controller pilot datalink.
  4. Review and amendment of controller pilot datalink controller operating procedures.
  5. Provision of sufficient staff to enable rostering of three team leaders.
  6. Completion of an audit of operating procedures with a view to standardising flight progress strip marking in the group.
  7. Review of the sector 8 (procedural) training course and initiation of action to amend documents and to re-introduce computer-based training for some elements of the course.

Significant Factors

  1. The considerable number of changes and staff issues within the Ocean sectors in the period prior to the occurrence.
  2. The lack of a procedure to assist rated controllers to develop an inter-group training program.
  3. The inadequate preparation of the group leader for on-the-job training.
  4. The lack of a training pre-brief by the group leader and the sector controller.
  5. The approval of the use of non-standard level by the B767.
  6. The inability of the group leader to maintain an appreciation of the traffic disposition.
  7. The lack of controller pilot datalink training aids and the inadequate installation of the facility at the console.
  8. The distraction and subsequent failure of the sector controller to regularly scan the flight progress strips.

Analysis

Organisational aspects

The group leader had a number of projects and staff issues that had to be addressed and that were constraining his ability to effectively manage the Ocean sectors. Taken individually these issues were probably not significant, but collectively they established the environment in which the Group was required to operate. The en-route manager and the group leader developed a plan to overcome these issues and in the long term develop staff in the Ocean sectors. Part of this plan was for the group leader to train for and obtain Ocean sector endorsements.

Training plan

The group leader developed a revised training plan that was constrained by staff commitments and scheduled ab initio training. However, he was not aware of the differences in the operation of sector 8 in comparison to other procedural sectors. Had he undertaken the classroom or simulator training prior to on the job training, he probably would have had an understanding of the unique aspects and a better overall understanding of the operation of the sector.

The group leader and the nominated supervising controller had only spent a short time together but the latter was aware of the training aspects that had been covered up to the morning of the occurrence. Because of this aspect he probably had a better appreciation than the sector controller did of the group leader's ability. Consequently, he would have been in a better position to recognise that the trainee was not maintaining the traffic situation. He might have been able to assume control of the position at a sufficiently early stage to recognise the conflict.

The current training guide and workbook were based on training ab initio controllers. There was no procedure to assist controllers from another group to modify the training to suit their specific requirements. There would appear to be scope for development of a process for peer review of revised training programs that would ensure that essential training aspects are included in a program.

Supervising controller

The sector controller that offered to supervise the group leader was unaware of the trainee's level of sector knowledge. They did not pre-brief and consequently they probably both had different expectations as to the level of participation of the other in the operation of the sector. This aspect in conjunction with his operation of the controller pilot datalink probably caused the sector controller to be distracted to the extent that he was unable to maintain an adequate scan of the flight progress strips.

Flight progress board management

The approval for the B767 to operate at a non-standard level for the track flown cancelled the defence normally provided to the air traffic system by the use of standard levels.

Controller pilot datalink facilities

The lack of a controller pilot datalink training guide or training aid provides an opportunity for controllers to become distracted to the detriment of the management of aircraft separation. Controllers should be able to develop their controller pilot datalink system skills remote from the operating position.

Operating position

The positioning of the controller pilot datalink and the sector 8 operating console restrict the ability of controllers to maintain an effective scan of the flight progress strip board. Controllers are required to divert their gaze and attention from the board to operate the controller pilot datalink keyboard. Modification of the console layout to enable more ready access to the controller pilot datalink or alternatively, provision of a controller to operate the controller pilot datalink during busy traffic periods would alleviate the problem.

Summary

A Boeing 767 (B767) was en route from Auckland to Hong Kong on air route B333. The crew had been cleared to conduct a cruise climb from FL310 to FL330. While FL310 was a standard level for the track being flown, FL330 was not. A Boeing 737 was en route from Sydney to Port Vila on air route B580. The crew of this aircraft had been cleared to, and was maintaining FL330, which was a standard level for their track. The routes cross at LEMIB a waypoint located approximately 490 NM east of Brisbane. The aircrafts' estimates for LEMIB were within three minutes of each other.

Five minutes prior to reaching LEMIB the crew of the B767 received a traffic alert and collision avoidance system traffic advisory warning. The traffic alert and collision avoidance system indicated that an aircraft was passing from left to right 900 ft above the level of, and 12 NM ahead of the B767. The required separation standard was 2,000 ft vertically.

Air traffic controller training was being conducted at the control position responsible for the area at the time of the occurrence. Following a query by the B767 crew regarding the crossing aircraft to air traffic control and a check of the flight progress strip data it was established that a separation standard had not been applied between the aircraft. There was a breakdown of separation.

Organisational aspects

The trainee was a group leader in the Brisbane Centre responsible for the management of the Tops/Ocean/West group. The group was divided into a number of sectors. Tops consisted of sectors 11, 11k and 12. West consisted of sectors 5 and 5D while Ocean had sectors 8, 8O and 10. Sectors 5D and 8O were radar sectors while all the other sectors were procedural control sectors except sector 11K which was a composite radar/procedural sector.

The group leader had previously held ratings and endorsements for all Tops sectors but had let two endorsements lapse due to workload and retained only the sector 11K endorsement.

The Ocean sectors were to be the first of the group to transition to The Australian Advanced Air Traffic Control System. The Ocean sectors had limited experienced staff plus there were other concerns for management that they believed could be suitably handled by the group leader becoming part of the Ocean teams. He also believed that if he obtained Ocean sector ratings he would be able act as a relief controller if required. Consequently, it was agreed that the group leader would transition with the Ocean sectors.

The group leader intended to undergo training to obtain the appropriate endorsements for the Ocean sectors. On completion of training he would function as one of the three Ocean team leaders as well as retaining group leader responsibility for those sectors. The En-route manager was to assume group leader responsibilities for the Tops and West sectors during the transition. To enable the group leader to commit himself totally to the training, an interim group leader was to be appointed to manage the group. The interim leader took over the group in the week immediately prior to the occurrence.

The Ocean sector staff had, and were, undergoing considerable changes due to: the reorganisation of the sectors; developments relating to contingency plans for Papua New Guinea airspace; management of Honiara airspace; and the transfer of the provision of directed traffic information from flight service international to the sectors and changes required for The Australian Advanced Air Traffic Control System transition. There were also a number of staff management issues that limited the options available to the group leader to meet operational demands.

Training plan

The Ocean sectors had a comprehensive training plan with workbooks for trainees and a training guide for the controller supervising the training. However, the supervisors training guide was unapproved and was in draft form only. The training guide and workbook were developed with the intention of providing a basis for ab-initio training. Training normally commenced with the trainee undertaking four weeks familiarisation at the sector operating positions followed by four days of classroom work, approximately one month in the simulator and finally six weeks of on the job training. During the on the job training phase the trainee would be assessed for competency by the supervising controller.

As the group leader already held radar and procedural ratings and an endorsement for sector 11K he elected to rationalise the ab-initio training program to reduce the time spent training. This aspect was in accordance with Airservices Australia's Civil ATS Operations Administration Manual which described "refresher training" for controllers as:

"training which focuses on change in a person's required competence and includes training concentrating on what a person once knew; what a person should (or does) know but hasn't been applying; and what a person hasn't had an opportunity to apply."

 

The Civil ATS Operations Administration Manual also detailed "local training strategies which recognise refresher training responsibilities include (but are not limited to):

  1. personal study of material, including videos, collated and provided by at the direction of team leaders or line mangers;
  2. use of simulator sessions, either specific to refresher training topics or included in ongoing training; and
  3. use of computer based training (CBT)."

The group leader had reviewed the training material for sector 8 but had not undertaken any classroom or simulator training for the sector. Due to other training commitments the simulator was not immediately available. He planned to join the scheduled Ocean simulator-training program at lesson ten (three weeks after the date of the occurrence) and to complete the lessons through to 23. During the interim period the group leader was to undertake familiarisation training under supervision. He had discussed his training plan with one of the Ocean team leaders responsible for training. There was no process to assist rated controllers intending to train for other ratings/endorsements to develop a suitable training plan.

Supervising controller

A supervising controller had been appointed to oversee the training of the group leader. The group leader's training commenced two days prior to the occurrence. During that time he and the supervising controller had spent approximately three hours together on the first day, none on the second and three hours on the morning of the day of the occurrence. The interruptions to the group leader's training were due to a prior commitment on the first day and the lack of a training position as a result of another controller undergoing familiarisation on the second day.

After spending three hours together on the morning of the occurrence the group leader and the supervising controller conducted a handover of sector 8 to enable them to take a rest period. Subsequently, the supervising controller returned to the console and assumed responsibility for sector 8O, the radar sector.

At 1100 Eastern Standard Time the group leader was waiting at the console expecting the next rostered controller to takeover sector 8O to enable the supervising controller to train the group leader on sector 8. A recently arrived controller offered to supervise group leader on the console instead of taking over sector 8O. Subsequently, this controller and the group leader assumed responsibility for sector 8. The controller had recently completed a stint as a supervising controller for another trainee and had considerable training experience. The nominated supervising controller for training the group leader remained on sector 8O.

The controller was not aware of how much training the group leader had completed and was therefore not aware of the latter's level of knowledge in the position. They did not conduct a pre-training brief to discuss learning aspects to be addressed during the session.

Sector 8 was the only procedural sector that used controller pilot datalink facilities to communicate with flight crews. Between 10% and 20% of all the flights operating through the sector used the controller pilot datalink. As the group leader was unable to operate the controller pilot datalink the controller was required to operate the facility. The controller was also directing and explaining the operation of sector 8 to the group leader while reviewing the flight progress strips for conflictions.

The controller and the group leader were at the position for approximately two hours during which the number of aircraft under their control steadily increased. The group leader noted a number of procedures that were different to what he expected to experience and he found it increasingly difficult to maintain an appreciation of the traffic situation. During this period it became apparent to the controller that the group leader was unfamiliar with the operation of the position.

Just prior to the occurrence the group leader received a request for a clearance from the pilot of an aircraft to enter the oceanic control area on climb to FL250. Because of the proximity of the aircraft to other flight information region boundaries the controller had to coordinate with Nadi and Auckland Centres prior to issuing a clearance. At about the same time, a flight information region boundary position report was received on the controller pilot datalink from a flight. The controller should have transferred this flight to Nadi Centre prior to the position but had not instructed the crew to transfer. Consequently, the position report had to be coordinated by voice intercom.

Flight progress board management

Details of the B737 were annotated on a blue flight progress strip and the sector 8O controller had coordinated the flight at FL330. The B767 flight was on a buff flight progress strip. Blue and buff coloured flight progress strips were used to differentiate between eastbound and westbound flights respectively. Coordination on the B767 was received from Auckland Centre and a clearance for the crew to conduct a cruise climb in the block level FL310 to FL330 was concurred. Requests by crews to conduct a cruise climb were regularly received and approved by the sector 8 controllers.

The recognition and resolution of potential conflicts at positions in the sector where tracks crossed was a regular part of a controller's task. The crossing point of the aircrafts' tracks, LEMIB was not annotated on either flight progress strip. After flight progress strips were activated by a departure report or coordination from another air traffic service unit they were passed to the sector 8 controller for placement on the board. The controller would place flight progress strips under an appropriate designator and then review all flight progress strips for conflictions. Conflicting flight progress strips would then be "cocked" to highlight a problem for subsequent action. Controllers "cocked" a flight progress strip by partially moving a strip out of the display bay.

If the controller identified that there was a potential conflict at a crossing point like LEMIB, a separation standard would be calculated and the respective flight progress strips would be annotated with the position. Once the separation procedure had been applied the flight progress strips would be returned to the bay. In the occurrence the flight progress strips for the aircraft were placed in the bay under the same designator without being cocked. The investigation did not establish why the flight progress strips were placed in the bay without being actioned.

Controller pilot datalink facilities

When the controller pilot datalink had been introduced a simulator had been provided to assist in the training of controllers. The controller pilot datalink simulator had subsequently been removed from the centre following training of the initial group of controllers required to operate the system. There were no facilities to assist controllers to learn how to operate the system prior to conducting the on the job training phase of their training. There was no controller pilot datalink reference material in the training guides. The group leader was not familiar with the operation of the controller pilot datalink.

With the introduction of the controller pilot datalink, two additional positions on sector 8 had been established for a controller to specifically operate the facility during the morning and afternoon shifts. At the beginning of 1998 these positions were disestablished to provide an additional team leader and to enable a controller to undertake operational development tasks. Sector staff had discussed the decision to remove the dedicated controller pilot datalink controller and believed that a controller could adequately manage both the controller pilot datalink and the sector 8 position. There was no workload or safety review conducted prior to amending the roster.

Team management

On the day of the occurrence there were no team leaders rostered for duty to oversee the management of the sector. A full performance controller was fulfilling the team leader functions. This controller had not completed team leader training.

Sector 8

Sector 8 was a procedural sector managing the Class A oceanic controlled airspace east of the coast of Australia, extending to the flight information boundary with New Zealand and Nadi, from just south of Tasmania to a line joining Brisbane and Port Vila. The operation of the sector was considered by controllers to be significantly different from other procedural sectors because of the inclusion of the controller pilot datalink and the different separation standards and procedures used for oceanic control compared to sectors over continental Australia.

Operating position

The sector 8 operating position consisted of a console with a flight progress strip display with the controller pilot datalink keyboard and monitor located on a table on the left side of the console. The sector 8 controller operated the controller pilot datalink and managed the separation of aircraft using flight progress strips placed under location designators on the board. The layout of the facilities required the controller to turn 90 degrees to the right each time the controller pilot datalink was operated.

The sector 8O radar position was located to the left of the procedural console and a map display was fixed to the floor in front of, and midway between both operating positions.

The layout of the operating positions and the additional facilities only enabled a single controller to sit and operate sector 8. Controllers supervising training were required to sit or stand behind the trainee.

Occurrence summary

Investigation number 199802755
Occurrence date 19/07/1998
Location waypoint LEMIB
State International
Report release date 01/01/1999
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 ZK-NCJ
Sector Jet
Operation type Air Transport High Capacity
Departure point Auckland, NEW ZEALAND
Destination HONG KONG
Damage Nil

Aircraft details

Manufacturer The Boeing Company
Model 737
Registration YJAV18
Sector Jet
Operation type Air Transport High Capacity
Departure point Sydney, NSW
Destination Port Vila, VANUATU
Damage Nil

de Havilland Canada DHC-8-201, VH-TQG

Safety Action

As a result of this occurrence, the Bureau of Air Safety Investigation is investigating an apparent safety deficiency relating to the standard of English language used by foreign students during communications with air traffic services. Any subsequent safety output related to this issue will be published in the Bureau's Quarterly Safety Deficiency Report.

Summary

The De Havilland Dash 8 was tracking inbound to Tamworth via the 040 radial of the Tamworth VOR (a radio navigation aid) at 3,500 ft in accordance with air traffic control instructions. Meanwhile, a TB10 Tobago was about to depart Tamworth via the 018 VOR radial, a track that would require the Tobago to turn across the inbound track of the Dash 8. Air traffic control had decided to limit the initial climb of the Tobago to 2,500 ft in order to ensure vertical separation with the Dash 8.

The aerodrome control task was being performed by a trainee controller under the supervision of a rated controller. The pilot of the Tobago was instructed to "line-up" and given an altitude restriction of 2,500 ft, which was read back by the pilot. However, the readback was not clear and the aircraft subsequently took off with both the trainee controller and the rated controller uncertain as to the actual altitude read back by the pilot, who was from a non-English speaking background and had an accent that was, on occasions, difficult to understand. It was subsequently determined that the pilot of the Tobago had understood the controller to say 3,500 ft, and that was the altitude he had read back to air traffic control. The crew of the Dash 8 were given traffic information on the position of the Tobago by air traffic control and commenced a look-out for that aircraft.

Because both controllers were unsure that the 2,500 ft restriction had been correctly acknowledged, it was agreed that the trainee controller would request the pilot of the Tobago to confirm that he was maintaining that altitude. Before that could take place, the pilot of the Tobago asked the controller to confirm his assigned altitude. Again, the transmission was not easy to understand. The trainee controller confirmed 2,500 ft and passed traffic information on the Dash 8 at the same time. The only reply from the pilot of the Tobago was the word "affirm" and his callsign.

In fact, the Tobago had been maintaining 3,500 ft, and it was that later transmission from air traffic control that made the pilot realise he should have been maintaining 2,500 ft. He commenced an immediate descent from 3,500 ft, but did not make any radio transmission to that effect.

The crew of the Dash 8 heard the exchange between air traffic control and the pilot of the Tobago. At almost the same time, they saw the Tobago about 400 m ahead, at the same level. They commenced an immediate descent then realised the Tobago was moving to their right. The aircraft passed with a horizontal separation of approximately 200 m, and no discernible vertical separation. The required standard was 1,000 ft vertical separation until the aircraft had passed.

Occurrence summary

Investigation number 199802472
Occurrence date 27/06/1998
Location 9 km NE Tamworth, (VOR)
State New South Wales
Report release date 27/04/1999
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 De Havilland Canada/De Havilland Aircraft of Canada
Model DHC-8
Registration VH-TQG
Serial number 430
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Armidale, NSW
Destination Tamworth, NSW
Damage Nil

Aircraft details

Manufacturer SOCATA-Groupe Aerospatiale
Model TB10
Registration VH-YTU
Serial number 1603
Sector Piston
Operation type Flying Training
Departure point Tamworth, NSW
Destination Inverell, NSW
Damage Nil

Mooney M2OJ, VH-DXT

Summary

The pilot of the Mooney M20J aircraft had planned to take one of his employees from Jandakot to Laverton via Melita Station, where he intended to deliver a small quantity of equipment. The aircraft arrived overhead Melita Station at about 1730 Western Standard Time, approximately 2 hours and 20 minutes after departure. A station hand reported that the aircraft flew over the upwind threshold of the airstrip at a low level and heading in a southerly direction. The aircraft then appeared to fly a downwind leg of a normal circuit before it banked sharply to the left onto an apparent final approach. The station hand then saw the aircraft fly quite close to the ground for about half the length of the airstrip, before adopting a nose-high attitude. The engine noise then increased, although it sounded laboured. When the aircraft was about 100 ft above the ground, he heard the engine noise stop. He then saw the aircraft pitch nose-down and impact the ground in a near vertical attitude. The aircraft was destroyed by the impact and the occupants received fatal injuries. There was no fire.

The aircraft wreckage was located 270 m beyond the northern end of the airstrip and 20 m to the right of the extended centreline. The landing gear was extended, and damage evidence indicated that the propeller was not under power at impact. The flaps were extended; however, their exact setting at impact could not be determined.

The fuel boost pump switch was found in the "off" position. However, it could not be established if the switch was in that position before the accident. The engine-driven fuel pump was damaged during the impact and the investigation was unable to determine if it was functioning correctly prior to the accident. If the engine-driven fuel pump had failed while the fuel boost pump switch was turned off, the engine could have failed due to fuel starvation.

The aircraft was fitted with an emergency locator transmitter (ELT) certified to US Federal Aviation Administration Technical Standard Order (TSO)-C91. Although it appeared to be correctly mounted and connected, The ELT did not activate at the time of the accident. Its instrument panel mounted switch was selected to "arm" and the ELT unit's switch was selected to "auto". The investigation could not determine why the ELT had not operated during the accident. When tested during the investigation, it operated normally.

The Melita Station airstrip, with a useable length of approximately 900 m, was adjacent to the homestead and was aligned approximately north-south. There was no airstrip lighting at Melita; however, runway lighting was available at Laverton.

At the time of the accident, the wind was calm and there was no cloud. The temperature was about 15 degrees Celsius. The station hand stated that although it was twilight, he was able to carry out his tasks without artificial lighting. Airservices Australia advised that the end of daylight on the day of the accident was 1733. The aircraft's flight manual indicated that the aircraft was equipped for night flight.

The pilot held a private pilot licence and a night visual flight rules rating, and was endorsed on the aircraft type. During his aviation medical examination, the pilot indicated that he had a significant family cardiac history. The post-mortem examination established that one of the pilot's coronary arteries was approximately 90 per cent blocked.

The aircraft departed Jandakot with both fuel tanks full. Each tank contained approximately 121 L of useable fuel. Reference to the aircraft's flight manual indicated that fuel usage for the flight should have been between 90 L and 100 L. The pilot's operating handbook (POH) warned that if the selected fuel tank contained less than 30.3 L of fuel, take-off manoeuvres and prolonged sideslips may cause a loss of engine power. Had the engine been drawing fuel from only one tank during the flight from Jandakot to Melita, there would have been approximately 20 L to 30 L of fuel remaining in that tank on arrival at Melita. The nose-high pitch attitude that the aircraft was seen to adopt shortly before the accident might have caused a loss of engine power had the selected fuel tank contained less than 30.3 L. Immediately after the impact, fuel was seen flowing from the aircraft and a strong smell of fuel was evident for some time afterwards. The aircraft's weight and centre of gravity were estimated to have been within the prescribed limits at the time of the accident.

The loss of control during the apparent go-around was consistent with the engine losing power and the aircraft stalling at a height from which recovery was not considered to be possible. The POH warned that the aircraft might lose up to 290 ft of altitude during a stall at maximum weight.

The investigation was unable to establish the reason for the engine failure and did not identify any pre-existing aircraft defects that might have influenced the circumstances of the accident. The significance of the effects of the pilot's medical condition could not be determined.

Occurrence summary

Investigation number 199802458
Occurrence date 29/06/1998
Location 15 km S Leonora, Aero.
State Western Australia
Report release date 27/08/1999
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 Mooney Aircraft Corp
Model M20
Registration VH-DXT
Serial number 24-1081
Sector Piston
Operation type Business
Departure point Jandakot, WA
Destination Melita Station, WA
Damage Destroyed

British Aerospace Plc BAe 146-300 , VH-EWM

Safety Action

This occurrence was one of 12 similar occurrences which involved GPWS warnings to crews of BAe146-300 aircraft at the same position on the runway 35 ILS final approach at Canberra. As a result, the Bureau of Air Safety Investigation is currently investigating a perceived safety deficiency related to these warnings. Any safety output issued as a result of this analysis will be published in the Bureau's Quarterly Safety Deficiency Report.

Summary

While flying a coupled instrument landing system (ILS) approach to runway 35 at Canberra, the crew received a ground proximity warning system (GPWS) "terrain" warning at 470 ft above ground level. As the aircraft was in visual conditions at the time, the crew elected to continue the approach.

The crew reported that, at the time of the warning, the aircraft was established on the ILS glideslope and descending at 650 ft/min. However, the T-VASIS indicated one dot low. Immediately prior to the warning, the radio altimeter indication rapidly increased, and then decreased, apparently triggering the warning.

Occurrence summary

Investigation number 199802426
Occurrence date 19/06/1998
Location Canberra, (ILS)
State Australian Capital Territory
Report release date 01/01/1999
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category E/GPWS warning
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer British Aerospace
Model BAe 146
Registration VH-EWM
Serial number E3179
Sector Jet
Operation type Air Transport High Capacity
Departure point Brisbane, QLD
Destination Canberra, ACT
Damage Nil

Cessna 337A, VH-YGM, 1 km west-south-west of Bundaberg Aerodrome, Queensland

Summary

The aircraft crashed shortly after taking off from runway 25. It caught fire and was destroyed. Witnesses reported that the aircraft commenced the take-off roll with the rear propeller not rotating.

Wreckage examination confirmed that the rear engine was not operating at impact. No fault was found which would have prevented normal operation of that engine and no fault was found in any other system or component of the aircraft.

Occurrence summary

Investigation number 199802140
Occurrence date 07/06/1998
Location 1km WSW Bundaberg, Aerodrome
State Queensland
Report release date 09/03/1999
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 Cessna Aircraft Company
Model 337
Registration VH-YGM
Serial number 3370401
Sector Piston
Operation type Private
Departure point Bundaberg, Qld
Destination Ballina, NSW
Damage Destroyed