Loss of separation

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

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

Boeing 737-376, VH-TAI

Safety Action

As a result of this investigation, and a number of similar occurrences, the Bureau of Air Safety Investigation issued a report (B98/90) of an investigation of systemic issues at the Sydney Terminal Control Unit. Nine recommendations were made in the report, the following four of which are considered valid for this investigation:

"R980157

Airservices Australia review the application of the "teams" concept within the Sydney Terminal Control Unit to ensure that teams are resourced appropriately and that there is an ongoing commitment to the provision of adequate training in order to achieve a high level of controller proficiency and standardisation."

"R980158

Airservices Australia ensure that adequate refresher training is undertaken by controllers in order to provide for high levels of controller proficiency and standardisation and so that the integrity of safety cases, in which refresher training is deemed to be a mitigating strategy for identified hazards, is maintained."

"R980159

Airservices Australia reassess the human factor hazard analysis for both Stage One and Stage Two of the LTOP safety cases so that the mitigating strategies applied to identified hazards adequately allow for the fundamental limitations of human performance. In reassessing this hazard analysis, BASI recommends that Airservices Australia seek the assistance of human performance expertise."

"R980160

Airservices Australia consider restructuring the current roster operating in the Sydney Terminal Control Unit to ensure that contemporary fatigue management research is translated into meaningful duty hour regulations. In any restructure of the roster, BASI recommends that Airservices Australia expand its absentee management program to include individuals who expose themselves to the risks of fatigue by participating in excessive amounts of overtime and/or emergency duty."

Summary

Sydney airport and associated airspace was being operated in accordance with Mode 9 of the Long-Term Operating Plan. A Boeing 737 (B737) departed runway 34R for Melbourne and was cleared initially to 5,000 ft on a MARUB ONE standard instrument departure (SID), with a Wollongong transition. The SID required the crew to intercept and track via the 075 Sydney VOR radial to 15 NM (waypoint MARUB), and to then turn right and track 144 degrees until passing 9,000 ft.

At the same time, another B737 inbound to Sydney on a CHEZA THREE standard arrival route (STAR) for a landing on runway 34R had passed waypoint WHALE, located 20 NM east of Sydney, and was maintaining 7,000 ft in accordance with its clearance.

The Departures South controller cancelled the 5,000 ft altitude restriction for the departing B737 and issued a clearance for the aircraft to climb to Flight Level 280. The 5,000 ft restriction would have assured separation with the inbound B737. When the altitude restriction was removed, the controller relied on monitoring the flight paths of both aircraft and intervening, if necessary, to maintain separation.

When the departing B737 turned right to track 144 degrees in accordance with the SID, there was a breakdown in separation between the two aircraft. Separation was reduced to 2.5 NM horizontally and 500 ft vertically, whereas the required standard was either 3 NM or 1,000 ft. Traffic information was passed to the crew of the departing B737, who sighted the other B737 while passing behind it.

The Departures South controller was relatively inexperienced, having held a control rating in the Sydney Terminal Control Unit for only three weeks. The controller was distracted from the monitoring role by coordination activities with Bankstown control tower, and by radio transmissions to other aircraft. The controller also considered himself to have been fatigued as a result of local rostering practices.

Occurrence summary

Investigation number 199802135
Occurrence date 12/06/1998
Location 28 km E Sydney, (VOR)
State New South Wales
Report release date 18/06/1999
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 737
Registration VH-TAI
Serial number 23483
Sector Jet
Operation type Air Transport High Capacity
Departure point Sydney, NSW
Destination Melbourne, VIC
Damage Nil

Aircraft details

Manufacturer The Boeing Company
Model 737
Registration FODGX
Sector Jet
Operation type Air Transport High Capacity
Departure point Noumea, New Caledonia
Destination Sydney, NSW
Damage Nil

Boeing 737-33A, VH-CZU

Safety Action

As a result of this investigation, and a number of similar occurrences, the Bureau of Air Safety Investigation undertook a systemic investigation into factors underlying air safety occurrences in Sydney Terminal Area airspace and issued report B98/90 on 18 August 1998. Nine recommendations were made in the report; the following three were considered relevant to this investigation.

R980157

"The Bureau of Air Safety Investigation recommends that Airservices Australia review the application of the "teams" concept within the Sydney Terminal Control Unit to ensure that teams are resourced appropriately and that there is an ongoing commitment to the provision of adequate training in order to achieve a high level of controller proficiency and standardisation."

R980158

"The Bureau of Air Safety Investigation recommends that Airservices Australia ensure that adequate refresher training is undertaken by controllers in order to provide for high levels of controller proficiency and standardisation so that the integrity of safety cases, in which refresher training is deemed to be a mitigating strategy for identified hazards, is maintained."

R980159

"The Bureau of Air Safety Investigation recommends that Airservices Australia reassess the human factor hazard analysis for both Stage One and Stage Two of the Long Term Operating Plan safety cases, so that the mitigating strategies applied to identified hazards adequately allow for the fundamental limitations of human performance. In reassessing this hazard analysis, BASI recommends that Airservices Australia seek the assistance of human performance expertise".

The following responses were received from Airservices Australia on 16 November 1998:

[R980157]

"A recent review of Sydney ATS has resulted in a "spill" of all management positions and a subsequent recruitment program which will be completed by 16 November 1998 to coincide with the Airservices' Business Transformation program.

The first step in this review has been to ensure that the management structure of the facility can operate effectively and that appropriate skills are available within the team. The manner in which the teams operate is the subject of a concurrent review process.

In support of these reviews, a consultant has completed a wide ranging review of supervision within air traffic services and its application within Teams.

Recommendations from these studies will be introduced into the Sydney rostering committee deliberations examining a better framework for TCU rosters. Sydney ATS management plan to introduce a revised roster in the TCU by 1 February 1999.

Team Leader training is recognised as vital to the success of teams and during October and November all Team Leaders will complete a series of Human Factors and Team Resource training modules. To further ensure that Team Leaders are better equipped to perform their duties a specific training programme for each Team Leader will be developed by 22 December 1998".

Response classification: CLOSED - ACCEPTED

[R980158]

"Airservices provides familiarisation training in various forms before the introduction of new procedures and to maintain controller skill levels. This ongoing programme has been augmented by an additional period of refresher training which all TCU controllers will undertake during the remainder of this year".

Response classification: CLOSED - PARTIALLY ACCEPTED

[R980159]

"The LTOP Stage One and Stage Two Safety Cases have been subject to review by independent experts in the field as well as being the subject of a number of post implementation reviews. Recommendations arising from those reviews have been progressively evaluated and applied as appropriate.

Airservices will consider augmenting its review processes with human factors expertise in future".

Response classification: OPEN

Significant Factors

  1. Appropriate separation assurance techniques were not implemented by either controller.
  2. Coordination between controllers was ineffective.

Analysis

The investigation revealed that each controller had different expectations of the intentions of the other. The DN controller had expected the AN controller's Metro would continue on its current track, and that the two aircraft tracks would cross. Conversely, the AN controller expected to keep his aircraft inside the track of the departing B737. Neither the coordination nor communication between controllers was effective. The unexpected turn onto downwind by the Metro, towards the B737, reduced the distance available for the B737 to climb safely above the Metro. The DN controller attempted to stop the B737 at 6,000 ft, but that instruction, combined with the rate of climb of the aircraft, was unable to prevent a breakdown of the vertical separation standard.

Summary

A Boeing 737 (B737) departed runway 34R on an ENTRA ONE standard instrument departure (SID), on climb to 5,000 ft. Immediately after departure, the crew established communication with the Departures North (DN) controller.

A Metro, inbound to Sydney from the north, was being radar vectored for a wide downwind leg to runway 34R, maintaining 7,000 ft, having earlier been diverted to the east for sequencing with preceding slower traffic. Although this track placed the aircraft in DN airspace, the Metro crew, as instructed, remained in communication with the Approach North (AN) controller. On request, the AN controller had been granted approval by the DN controller for the Metro to transit through the DN controller's airspace. The weather conditions were fine, and runway 34 parallel operations had been in progress for 18 minutes.

The DN controller had elected to provide vertical separation between the two aircraft by issuing instructions that would enable the B737 to climb above the Metro. This plan was coordinated with the AN controller. A clearance to climb to flight level 280 was issued to the crew of the B737, with a request to expedite climb through 8,000 ft. As this transmission was being made by the DN controller, the AN controller instructed the crew of the Metro to turn right onto a heading of 170 degrees for the downwind leg.

Subsequently, it was perceived by the DN controller that the effective climb performance of the B737 would be insufficient to ensure that the required separation standard of 1,000 ft vertically or 3 NM horizontally between the two aircraft would be maintained. The controller amended the clearance and instructed the crew of the B737 to maintain 6,000 ft. However, because the B737 was climbing at 4,500 ft/min, it had climbed to 7,000 ft before the crew were able to stop the climb and commence descent. As there was now less than 3 NM between the aircraft, both controllers passed traffic information to the crew of their respective aircraft. The crew of the B737 sighted the Metro, passing beneath that aircraft with approximately 600 ft of vertical separation. The crew of the Metro did not sight the B737.

During the two years since the AN controller had been rated, the system in which he was working had changed significantly due to noise-sharing arrangements at Sydney (Kingsford-Smith) Airport. The controller's training and endorsement had been undertaken and achieved in a less complex environment. The unpredictability of the more complex arrangements required a high degree of coordination for which the controller had not been adequately trained.

Conversely, the DN controller had gained his initial rating in the days when air traffic control was more reactive and dynamic than the present more regulated system. In the previous, less structured air traffic control environment that the controller had been trained in, there had been undocumented procedures that everyone was aware of. Those procedures were passed on from controller to controller as skills were developed and refined. The DN controller expected that his intentions and plan would be readily interpreted by the AN controller.

Occurrence summary

Investigation number 199801905
Occurrence date 29/05/1998
Location 22 km NE Sydney, Aero.
State New South Wales
Report release date 16/09/1999
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 737
Registration VH-CZU
Serial number 27267
Sector Jet
Operation type Air Transport High Capacity
Departure point Sydney, NSW
Destination Coolangatta, QLD
Damage Nil

Aircraft details

Manufacturer Fairchild Industries Inc
Model SA227
Registration VH-NEK
Serial number AC-615B
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Tamworth, NSW
Destination Sydney, NSW
Damage Nil

Boeing 747, CCA174

Safety Action

As a result of this occurrence, the Bureau of Air Safety Investigation is investigating a perceived safety deficiency relating to the use of non-standard language by air traffic controllers during communications with flight crew from a non-English speaking background.

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

Analysis

The instructions passed to the pilot of the B747 may have been unnecessarily complex, given that the pilot was from a non-English speaking background. The controller's transmission was not as definitive as it could have been and included extraneous, non-standard phraseology.

The response from the crew may have indicated to the controller that his transmission was not understood, in that the word "into" indicated a possible turn to intercept the localiser. In addition, the controller did not query the unintelligible transmission.

Summary

The Boeing 747 (B747) was on descent for an arrival at Sydney. The crew was being radar vectored to runway 16R for sequencing behind a SAAB 340 that was being radar vectored to runway 16L. Procedures at Sydney had different air traffic controllers responsible for directing the traffic to each of the parallel runways. The Director West controller positioned aircraft on final for runway 16R and the Director East for runway 16L.

The Director West controller was sequencing the B747 and assigned a heading of 060 degrees magnetic with an instruction to report when the crew had the field in sight.

The crew of the B747 reported the field in sight and the Director West controller told the crew to expect to go right up to the localiser, with a right turn to intercept from the eastern side. The crew acknowledged with a partly unintelligible transmission that included the words "roger" (unintelligible) "localiser into".

Almost immediately, the crew of the B747 turned their aircraft away from the assigned heading onto a heading of 110 degrees to intercept the runway 16R localiser. They advised air traffic control that they were now right heading 110. This particular heading placed the aircraft in potential conflict with the SAAB. The Director West controller instructed the crew of the B747 to maintain a heading of 060 degrees to ensure that the aircraft passed behind the SAAB. The Director East controller passed traffic information regarding the B747 to the crew of the SAAB.

Although the crew of the SAAB reported that they had the B747 sighted, radar separation between the two aircraft was reduced to 2.5 NM during the manoeuvre. The separation standard required was either 3 NM horizontally or 1,000 ft vertically. Analysis of the radar data indicated that vertical separation between the two aircraft was reduced to approximately 800 ft when the 3-NM radar separation standard was infringed.

Occurrence summary

Investigation number 199800870
Occurrence date 17/03/1998
Location 20 km NNW Sydney, Aero.
State New South Wales
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 747
Registration CCA174
Sector Jet
Operation type Air Transport High Capacity
Departure point Melbourne, VIC
Destination Sydney , NSW
Damage Nil

Aircraft details

Manufacturer Saab Aircraft Co.
Model 340
Registration VH-EKG
Serial number 367
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Ballina, NSW
Destination Sydney , NSW
Damage Nil

Boeing 747-338, VH-EBW (QF16)

Safety Action

Local safety action

As a result of their investigation into the occurrence, Aeronautical Radio of Thailand Ltd has proposed to:

  1. Issue a local instruction to prevent controllers approving climb and descent for aircraft operating in the area adjacent to the FIR boundary, or in those areas where crews of aircraft conduct frequency changes.
  2. Issue a local instruction requiring the inclusion of the KATKI position on flight progress strips for all aircraft using the intersecting routes.
  3. Amend the aeronautical charts to have KATKI annotated as a compulsory reporting point for routes G463 and B219.
  4. Review all route intersections in the FIR similar to the KATKI position and amend existing procedures if required.
  5. Review the procedural control facilities, including the provision of adequate flight progress strip bays, and the capability for continuous control frequency monitoring by the procedural controller.

Factual Information

Air Traffic Control services

Sector 3 was responsible for the provision of air traffic control in that part of the Bangkok FIR to the south of Bangkok, and for associated portions of the Phnom Penh and Ho Chi Minh FIR'S. The Sector 3 console had three positions: a radar control position with a radar display located on the left, a procedural control position in the centre, and a radar assistant position on the right. The radar controller was responsible for separating all aircraft in the sector. This included aircraft outside radar coverage. The Sector 3 procedural controller was responsible for issuing clearances using procedural control, and assisting the radar controller with flight progress strip (FPS) marking and coordination. The procedural controller was required to notify the radar controller of any changes that would affect procedural separation.

The radar controller was the only position with facilities to transmit and receive on the control frequency of 135.5 MHz. The procedural controller could monitor the frequency, but required the radar controller to transmit control instructions to aircraft operating under procedural control.

The console had been originally designed for operations utilising a flight data processor for aircraft flight information, without the need for flight progress strips. As a result, the radar operator and assistant radar positions were not fitted with flight progress strip bays. The flight data processor had subsequently proved to be less effective than planned and the sector had reverted to using flight progress strips. This required the radar and the radar assistant consoles to be fitted with temporary strip holders.

A high level of interaction and cooperation was required between the radar and procedural controllers to effectively manage the sector's airspace. The flight progress strips for each aircraft were required to be retained in the procedural display until the crew reported at the next position. This was to enable controllers to observe that an aircraft was in transit between the previous and next positions. However, due to limited space to display the strips, the Sector controllers had developed a habit of removing flight progress strips at the earliest opportunity to make space for new strips.

The strip for QFI6, annotated for the portion of the route from ALGOR to KABAS, did not include an estimate for KATKI. There were two strips for KAL362: one annotated for the portion of the route before KANTO, and one for KANTO to SINMA. The KANTO strip for KAL362 was located in the same bay as the KABAS strip for QF16. The radar controller removed the KAL362 KANTO strip from the bay after the crew reported at that position, prior to the SINMA position.

When the crew of KAL362 requested climb from FL270 to FL290, the radar controller scanned the flight progress strips at the procedural position. There was a SINMA strip for KAL362, but no other strip to indicate a possible conflict. SINMA was located east of the route of QF16. The procedural controller was carrying out coordination duties at the time, and did not hear the climb request. The radar controller then issued a clearance for the crew of KAL362 to climb to FL290, without consulting with the procedural controller.

Crew awareness

The crew of QFI6 were using the same control frequency as KAL362 when the crew of that aircraft reported at KANTO, and were subsequently approved to climb to FL290. There were reports of radio interference on that frequency, including reports of interference from aircraft operating at lower levels. The crew of QF16 did not recall hearing the crew of KAL362 request climb to FL290, nor the amended clearance and readback.

Significant Factors

  1. The design of the Sector 3 console did not allow for all relevant flight progress strips to be displayed.
  2. The radar controller removed the KANTO flight progress strip after the KAL362 crew reported at that position.
  3. The procedural controller did not hear the request for climb to FL290 by the crew of KAL362.
  4. There was no requirement for the display of KATKI on flight progress strips for all aircraft using the intersecting routes.
  5. The radar controller did not consult with the procedural controller prior to instructing the crew of KAL362 to climb to FL290.
  6. The radar controller did not ensure that vertical separation was maintained between KAL362 and QF16 while the aircraft were in an area of conflict
  7. The crew of QF16 did not hear the request and subsequent approval for KAL362 to climb to FL290.

Analysis

The procedural controller was responsible for issuing clearances to aircraft under procedural control, as was the case in this event. The role of the radar controller was to pass on the clearance to the aircraft. By not consulting with the procedural controller, the radar controller bypassed the established system of control, leading to a breakdown in safety.

The configuration of the Sector 3 console provided insufficient space to adequately display all relevant flight progress strips. As a result, controllers had developed the habit of removing strips at the earliest opportunity, thereby creating the potential for vital information to be missed.

The KANTO flight progress strip for KAL362 should have been retained on the procedural board until the crew reported at SINMA, the next position. The removal of the KANTO strip by the radar controller removed the only reminder available to all controllers that the intended tracks of KAL362 and QFI6 would cross.

Inclusion of the KATKI position on all flight progress strips for aircraft using the intersecting routes would have enabled controllers to more readily assess separation requirements in the procedural airspace. If the strips had required the KATKI position it is probable that the details for QFI6 and KAL362 would have been displayed under the same designator on the board, allowing controllers to recognise the potential conflict.

The inability to monitor the control frequency while conducting coordination reduced the likelihood of the procedural controller maintaining a complete appreciation of the disposition of traffic.

The reason why the crew of QFI6 did not hear the transmissions regarding KAL362 climbing to the same level, while operating on the same frequency within direct line of sight, could not be determined.

Summary

QFI6, a Boeing 747, had departed Bangkok for Melbourne and was tracking southbound on airway G463 at flight level (FL) 290. The aircraft was in contact with Bangkok Area Control Centre (BKK ACC) Sector 3 on 135.5 MHz. Sector 3 was a combined radar and procedural control sector. At 0212:54 QF16 reported passing ALGOR at FL290, estimating KABAS, the flight information region (FIR) boundary, at 0221. Just prior to reaching KABAS, the aircraft would pass the intersection of G463 and B219 at KATKI. These positions were all located beyond radar coverage, over international waters, within the procedural control portion of BKK ACC Sector 3 airspace.

A Korean registered Boeing 747, KAL362, had departed Kuala Lumpur for Seoul, tracking via B219 at FL270. Approaching KANTO, located to the west of KATKI, the aircraft was transferred to the BKK ACC. The crew of KAL362 contacted Bangkok Sector 3 on 135.5 MHz and reported passing KANTO at FL270, estimating KATKI at 0219, and requesting climb to FL290. The next reporting position was SINMA, to the east of KATKI. At 0217:20 Bangkok Sector 3 cleared KAL362 to climb to FL290. KAL362 reported leaving FL270 for FL290. At 0220:21 the pilot in command of QF16 advised the Sector 3 controller of having received a traffic alert and collision avoidance system (TCAS) traffic advisory (TA), and that the aircraft had been climbed to FL300 to avoid a collision with KAL362, but was now descending to FL290.

The crew of QF16 had received a TCAS TA, followed by a resolution advisory (RA) commanding a climb to avoid climbing traffic some 800 ft below. Each crew sighted the other aircraft. The KAL362 crew also received a TCAS TA, followed by a TCAS RA commanding a descent. The crew of KAL362 did not report a traffic confliction.

An investigation carried out by Aeronautical Radio of Thailand Ltd, the Thai air traffic control organisation, indicated that KAL362 was incorrectly given a clearance to climb to FL290 by the Bangkok Sector 3 controller, and that the crews of both QF16 and KAL362 were acting in accordance with the clearances issued to them. The minimum required distance between the aircraft was 1,000 ft vertical separation, or a lateral separation of not less than 15 minutes between their estimated times of arrival at KATKI, the intersection of their intended flight routes.

In accordance with ICAO Aircraft Accident and Incident Investigation Annex 13, paragraph 5.3, the circumstances of this occurrence provide for the State of Registry to institute and conduct any necessary investigation. After consultation with the Korean authorities it was agreed that BASI would take responsibility for the ongoing investigation.

Occurrence summary

Investigation number 199702691
Occurrence date 20/08/1997
Location KATKI
State International
Report release date 01/11/1998
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 747
Registration VH-EBW
Serial number 23408
Sector Jet
Operation type Air Transport High Capacity
Departure point Bangkok, THAILAND
Destination Melbourne, VIC
Damage Nil

Aircraft details

Manufacturer The Boeing Company
Model 747
Registration HL-7476
Sector Jet
Operation type Air Transport High Capacity
Departure point Kuala Lumpur, MALAYSIA
Destination Seoul, Republic of Korea
Damage Nil

Boeing 737-476, VH-TJO

Safety Action

As a result of the investigation, the company operating the A320 has amended its flight-planning process by making a modification to the flight-planning system. In the 6 months following the amendment's implementation, manoeuvring times remained within the working tolerances of position reporting.

As a result of this occurrence, the Bureau of Air Safety Investigation is currently investigating a perceived safety deficiency. The deficiency identified relates to the validation of air traffic services' flight progress strip data for aircraft operating outside radar coverage.

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

Factual Information

Radar

The Adelaide radar did not provide reliable coverage on air route T134. It normally gave coverage for aircraft over Portland and for a few miles east of SUBUM, but only provided intermittent coverage for the remainder of the route segment.

Radio

As air route T134 was predominantly outside VHF coverage, the route was designated for HF operation. The air traffic service unit responsible for HF communication was Perth International Flight Service. This limitation resulted in a delay in passing information between the controller and the crew of the B737 because the flight service officer was the intermediary for all radio transmissions.

Flight planning

The company flight plan for the A320 included a manoeuvring time of 10 minutes at the departure aerodrome. This time was estimated by the flight planner, using a computerised flight planning system, as that required for manoeuvring prior to setting course after the aircraft had become airborne. However, the flight plan indicated the time as an elapsed time from airborne to abeam/overhead Melbourne airport. The air traffic control strip printing system did not provide for a specific manoeuvring segment. Consequently, it added the 10-minute manoeuvring time to the 12-minute flight-planned time to the first enroute navigation aid.

Having added this 10-minute interval to the departure time, all the flight progress strips for the A320 therefore indicated position estimates which were approximately 10 minutes later than the corresponding flight-planned estimates.

The manoeuvring time was introduced by the company to allow for the time between becoming airborne and setting course, which varied depending on considerations such as runway direction, standard departure instructions and wind velocity. The flight crew had the same initial flight-plan information as air traffic control. However, the crew updated their plan to reflect the actual time at which the aircraft set course.

The B737 was operated by a different company and the flight plan did not include provision for a manoeuvring time. The flight progress strip estimates were therefore within the normal tolerance of plus or minus 2 minutes.

Pilot reporting

While under radar observation, pilots were not required to report their position as the controller could see that the aircraft was at the reporting point. If there was a difference between the estimated and actual times of arrival, then it was noticed by both parties and independently corrected. Under these conditions separation standards relied on radar.

When under procedural control, separation standards were based on estimated times of arrival at the reporting points and pilots were required to advise air traffic control of any variation of more than 2 minutes. Separation standards were devised to allow for these variations. Controllers crosschecked known times, as reported by pilots, with the flight plan time intervals to provide a check on the estimated time of arrival for the next position. If this crosscheck was within 2 minutes of the pilots estimate, no further action was required.

Significant Factors

  1. The flight plan for the A320 contained a manoeuvring time for the aircraft prior to setting course.
  2. The air traffic control strip printing system was unable to allow for a discrete manoeuvring time in the strip preparation.
  3. The Melbourne Sector 4 controller did not conduct a crosscheck calculation on the flight progress strip notation for the A320's estimated time of arrival at SUBUM.
  4. The Adelaide Sector 4 and Melbourne Sector 1 controllers did not initiate any check action for the observed significant difference in the time interval for the A320 between Portland and SUBUM.
  5. Air traffic control procedures were such that there was no assurrance that the flight crew's estimated times were the same as those being used by ATC to provide procedural separation.

Analysis

Flight planning

The air traffic control strip printing system's interpretations of the A320's flight plan led to a latent error in the flight progress strips for the A320 that was not present in the B737 strips. The system defence to negate this error was removed when the Melbourne Sector 4 controller did not update the flight progress strip estimated time for the SUBUM position.

Air traffic control procedures

Once the Melbourne Sector 4 controller had read the flight plan estimated time for the A320 at SUBUM, the coordination procedures were such that this incorrect estimate was passed to Adelaide Sector 4 and then from Adelaide Sector 4 to Melbourne Sector 1 without further check. Consequently, when coordination was required to allow the climb of the B737, the two controllers concerned had incorrect information. They did not question the information because it had been based on a radar observation.

Air traffic controllers

Although the flight progress strips showed that a longitudinal separation standard existed, the Melbourne Sector 4 controller did not review the situation before transferring the aircraft to Perth International HF. However, a scan of the strips should have revealed the error because the flight-planned time for the route segment was 45 minutes which, when added to the known time over Portland, would have given an estimate for SUBUM of 1447 rather than 1500.

The decision by the oncoming Adelaide Sector 4 controller to check his longer-range radar display, detected the actual position of the A320 on air route T134 and enabled him to implement remedial action.

Pilot reporting

The aircraft passed over the last radar-observed position and the crews would have made estimates for SUBUM, but were not required to report those estimates to air traffic control. The controller also made estimates for SUBUM and based a procedural separation standard on those estimates. He had no need to check those estimates with the pilots or any other controller. Consequently, when the error was made, there was no crosscheck with which to provide a safety net.

Both flight crews were operating within 2 minutes of their corrected estimates, based on their actual times at Portland, and therefore were not required to report any minor changes.

Consequently, the crews and the controllers were working a procedural standard from two different time bases, neither of which had been crosschecked with the other. In a procedural environment, pilots and controllers must have a single datum on which to base their reporting and separation.

Summary

The Boeing 737 (B737) had departed Sydney for Perth and the crew was maintaining the aircraft at flight level (FL) 280. The planned route was to track overhead Portland, Vic., then via air route T134 across the Great Australian Bight. The reporting point SUBUM was located on air route T134, approximately 220 NM south-south-west of Adelaide.

As the aircraft proceeded towards Portland, it was being radar monitored by the Melbourne Sector 4 air traffic controller. Flight crews were not required to report their positions while under radar observation. Accordingly, the time at which the aircraft was overhead Portland was recorded on the air traffic control flight progress strip by the sector controller, who then calculated an estimated time of passing SUBUM. This estimate was based on the flight-planned time interval from Portland to SUBUM and the actual time at which the controller saw the aircraft pass over Portland. The report was then coordinated to Adelaide Sector 4, which had jurisdiction for the route segment to SUBUM.

The Airbus A320 (A320) departed Melbourne for Perth and was tracking to intercept air route T134 via Portland. The crew was maintaining the aircraft at FL310.

The flight progress strips displayed information obtained from the respective company flight plans and showed that the B737 was estimating Portland at 1355 EST and SUBUM at 1444. They also showed that the A320 was estimating Portland at 1415 and SUBUM at 1500.

The Melbourne Sector 4 controller observed the B737 pass Portland at 1357 and, based on that observation, estimated that the aircraft would be approximately on time at SUBUM and elected not to change the estimated time of 1444. The position report was coordinated with Adelaide Sector 4. Air traffic control procedures allowed for a difference of up to 2 minutes between pilot and controller estimates without requiring a cross-check.

A short time later, the Melbourne Sector 4 controller assessed that the A320 passed over Portland at 1402 (13 minutes ahead of the estimate) but due to other duties, did not immediately notate the flight progress strip or coordinate this position with Adelaide Control.

At 1404, the Melbourne controller realised that he had not informed the Adelaide controller of the A320's Portland position report and commenced the coordination process. He reported the time at Portland as 1402 and the level as FL310. At this moment he realised that he had not made a calculation for the SUBUM estimate and used the estimated time of arrival as written on the flight progress strip as his revised estimate. This action resulted in his flight progress strip indicating that the A320 was going to be "on time" at SUBUM despite being 13 minutes early at Portland.

Communications for both aircraft crews were then transferred to Perth Flight Service on high frequency (HF) radio.

The Adelaide Sector 4 controller accepted the coordination from Melbourne Sector 4 on face value because the Melbourne controller was required to check the accuracy of data he was coordinating. The Adelaide Sector 4 controller checked his flight progress strips and noticed that the A320 was early at Portland but estimated to be "on time" at SUBUM. He considered that this discrepancy was probably due to a flight planning error that had been corrected by the Melbourne controller. His decision was influenced by the fact that both aircraft were estimated to be "on time" at SUBUM. He also considered that as they were vertically separated any error in the estimated times would not be significant, and chose not to pursue the matter any further.

The Adelaide Sector 4 controller then coordinated the Portland position details, including the estimated times of arrival at SUBUM, with Melbourne Sector 1, the control position for air route T134 from SUBUM. As a consequence, Melbourne Sector 1 had flight progress strips that indicated both aircraft being "on time" at SUBUM.

At 1444, the Perth Flight Service officer contacted Melbourne Sector 1 with the position report at SUBUM from the crew of the B737. This report included a request for a climb to FL310. As such a climb would negate vertical separation, the controller was required to establish a 10-minute longitudinal separation standard in order to approve the request. As the flight progress strips indicated estimates for SUBUM at 1444 and 1500, this standard appeared to have been achieved. However, because the B737 had only just entered his area of responsibility, he was required to check with the previous sector (Adelaide Sector 4) before authorising such a change. There had been a change of personnel at Adelaide Sector 4 and, as the oncoming controller also had the same time indications as the Melbourne controller, he agreed to the change and the crew of the B737 was instructed to climb to FL310.

After approving the climb, the Adelaide controller decided to check his radar display on the maximum range and saw that the A320 was only 30 seconds east of SUBUM. He immediately contacted the Melbourne Sector 1 controller to inform him of the confliction.

The Melbourne Sector 1 controller contacted Perth Flight Service and issued an instruction for the crew of the B737 to descend to FL290. Because of the amount of coordination required, it took almost 3 minutes to translate the Adelaide controller's observation into an acknowledged instruction for the B737 to descend. As the B737 had reached FL300 before the crew received the instruction to descend, and as the vertical separation standard was 2,000 ft, an infringement of the separation standards had occurred.

Occurrence summary

Investigation number 199702620
Occurrence date 17/08/1997
Location 6 km S Subum, (IFR)
State South Australia
Report release date 01/12/1998
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-TJO
Serial number 24440
Sector Jet
Operation type Air Transport High Capacity
Departure point Sydney, NSW
Destination Perth, WA
Damage Nil

Aircraft details

Manufacturer Airbus
Model A320
Registration VH-HYK
Serial number 157
Sector Jet
Operation type Air Transport High Capacity
Departure point Melbourne, VIC
Destination Perth, WA
Damage Nil

Breakdown in runway separation standard during landings on runways 16 and 07, Sydney (Kingsford Smith) Airport, New South Wales, on 12 March 1992

Summary

At 0832 hours on 12 March 1992, a Boeing 767 aircraft VH-EAO was cleared to land on runway 16 at Sydney (Kingsford Smith) Airport. At the same time, a Boeing 727 aircraft VH-TBR was on final approach to the intersecting runway 07. During the approach air traffic control monitored the progress of both aircraft on radar.

The B727 was instructed to continue the approach and to expect a late landing clearance. After the B767 landed it was instructed to expedite its movement through the intersecting runway. Subsequently, the B727 crossed the runway 07 threshold before the B767 had cleared the intersection, thereby infringing runway separation standards.

Occurrence summary

Investigation number 199202688
Occurrence date 12/03/1992
Location Sydney (Kingsford Smith) Airport
State New South Wales
Report release date 20/07/1993
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Loss of separation
Highest injury level None

Aircraft details

Manufacturer The Boeing Company
Model 767
Registration VH-EAO
Serial number 23403
Sector Jet
Operation type Air Transport High Capacity
Damage Nil

Aircraft details

Manufacturer The Boeing Company
Model 727
Registration VH-TBR
Serial number 22069
Sector Jet
Operation type Air Transport High Capacity
Damage Nil

Loss of separation involving Boeing 747-400 and Bell 206B111, over Sydney, New South Wales, on 20 June 1992

Summary

The Boeing 747 (QFA 27) was cleared for take-off from runway 16 on a Mudgee One Standard Instrument Departure (SID). This SID procedure required the aircraft to track via the 163 radial of the Sydney VOR (omni) to 3,000 ft and then turn left to track back towards the airfield, passing overhead the Sydney VOR prior to setting course in a north-westerly direction.

The VOR navigational aid is located on Sydney Airport and the SID required the B747 to be at 5,000 ft or higher before passing the VOR. Sydney Air Traffic Control had cleared the aircraft to climb to its initial cruising level, flight level (FL) 310. The Bell 206 (VH-BHU) planned to climb overhead Sydney Airport to FL 125 for a photographic operation.

The Sydney Aerodrome Controller (ADC) cleared the helicopter to climb to FL 125 within the lateral confines of an area between Qantas Maintenance facilities, located on the airport and the Sydney Hilton Hotel which is about 0.5 km west of the airport's northern boundary. Due to suppression of radar returns within 3.5 km of the radar head, which is also located on the airport, the flight path of the helicopter was not detected on any ATC radar screen.

Occurrence summary

Investigation number 199200078
Occurrence date 20/06/1992
Location over Sydney
State New South Wales
Report release date 20/09/1993
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Loss of separation
Highest injury level None

Aircraft details

Manufacturer Bell Helicopter Co
Model 206
Registration VH-BHU
Serial number 2964
Sector Helicopter
Operation type Aerial Work
Departure point Sydney, NSW
Destination Sydney, NSW
Damage Nil

Aircraft details

Manufacturer The Boeing Company
Model 747
Registration VH-OJO
Serial number 25544
Sector Jet
Operation type Air Transport High Capacity
Departure point Sydney, NSW
Destination Hong Kong
Damage Nil