Loss of separation

Boeing 737-376, VH-TAF

Safety Action

Local Safety Action

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

ATSB Safety Action

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

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

Significant Factors

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

Analysis

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

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

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

Summary

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

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

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

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

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

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

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

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

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

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

Occurrence summary

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

Aircraft details

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

Aircraft details

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

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

Safety Action

Local safety action

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

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

Australian Transport Safety Bureau (ATSB) Safety Action

The ATSB is investigating safety deficiencies relating to:

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

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

Significant Factors

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

Analysis

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

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

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

Summary

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

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

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

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

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

Occurrence summary

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

Aircraft details

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

Aircraft details

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

Saab SF-340B, VH-EKN

Summary

A Cessna 340 (C340) departed Sydney at 1036, on climb to flight level (FL) 120, tracking via Shellys and Yass to Deniliquin. At 1047 a Saab 340B (Saab) departed Sydney for Canberra on climb to FL120, also tracking via Shellys. Once both aircraft were established in cruise there was a rate of closure of about 100 kt between them. As the Saab passed over Shellys, the Melbourne Sector 12 controller observed on radar that the lateral separation between the two aircraft was reducing to less than the required standard of 5 NM. The controller instructed the Saab to turn left though 90 degrees and advised the crew that there was traffic in their 2-o'clock position at 2 NM. The crew reported sighting the C340. Subsequent radar analysis established that the lateral distance between the aircraft had reduced to 2 NM.

The traffic level in the sector was low, with six aircraft on frequency. The controller had been operating the radar display on the 100 NM scale to enable him to readily observe boundary traffic or approaching flights. The display was centred on Shellys at the time of the occurrence. The controller was closely monitoring the progress of three aircraft that were tracking between Wollongong and Canberra. Two aircraft were in a step climb, while the third was overtaking and outclimbing the first two. The controller believed that he was maintaining an adequate scan of the radar display and was unable to provide a reason for not appreciating the effect of the high rate of closure between the two occurrence aircraft.

The morning shift of the adjacent sector to the west of Sector 12 had transitioned to The Advanced Australian Air Traffic System (TAAATS) approximately two and one-half weeks prior to the occurrence. This had resulted in the implementation of a number of changes to Sector 12 coordination procedures. Those changes were only required during the morning shift. During the afternoon the adjacent sector reverted to the same air traffic control system as that being used by Sector 12. The controller subsequently reported that while the amended coordination procedures were understood, they required conscious thought to action them.

During the morning, and at the time of the occurrence, coordination between the sector and Nowra Air Traffic Control had been restricted by communications problems and the controller was using a "hotline" and a telephone for coordination. There was no telephone available on the Sector 12 console so the controller was required to reach across to use one from an adjacent console.

The investigation did not establish the reason why the controller was unaware of the impending conflict until there was insufficient time to resolve the situation. It is probable that a combination of low traffic levels, possible fixation on the Wollongong - Canberra traffic situation, and some distraction due to amended coordination requirements, was sufficient to reduce the controller's normal level of vigilance.

Occurrence summary

Investigation number 199902615
Occurrence date 10/05/1999
Location Shelleys, (NDB)
State New South Wales
Report release date 29/07/1999
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 Saab Aircraft Co.
Model 340
Registration VH-EKN
Serial number 372
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Sydney, NSW
Destination Canberra, ACT
Damage Nil

Aircraft details

Manufacturer Cessna Aircraft Company
Model 340
Registration VH-MAG
Serial number 3400166
Sector Piston
Operation type Unknown
Departure point Sydney, NSW
Destination Deniliquin, NSW
Damage Nil

Boeing 737-376, VH-TJA

Summary

A Boeing 777 (B777) was tracking via an ARBEY Six standard arrival route (STAR) at 8,000 ft for a landing on runway 34 at Melbourne. A Boeing 737 (B737) departed runway 27 for Maroochydore and was cleared to track via the DOSEL Eight standard instrument departure (SID) on climb to 7,000 ft. Because the SID and STAR tracks crossed north of Melbourne aerodrome the departure controller planned to maintain the minimum vertical separation standard of 1,000 ft between the two aircraft until they had passed, and then clear the aircraft to climb/descend once the 3 NM lateral radar separation standard had been established between them. However, prior to the B737 reaching the crossing point the controller instructed the crew to cancel the SID and to track direct to Mudgee, believing that the track adopted by the B737 would result in the aircraft passing in front of the B777 with greater than the required radar standard.

When a Boeing 767 (B767) subsequently departed from runway 27 on climb to 5,000 ft the controller thought that he only had to separate that aircraft from the B777. Consequently, he instructed the crew of the B777 to descend to 6,000 ft. The crew acknowledged and advised that they had left 8,000 ft. The controller was about to instruct the crew of the B737 to climb to a higher level when he saw that the separation between the B737 and the B777 was going to reduce to less than the required standard. The controller issued instructions to both crews in order to maintain radar separation, however, the distance between the two aircraft reduced to 2.25 NM laterally and 200 ft vertically.

Both aircraft were fitted with traffic alert and collision avoidance systems (TCAS) and each crew received traffic advisories followed by a short resolution advisory. By the time the controller had issued turn instructions the advisories had ceased. Each crew had sighted the other aircraft just prior to the conflict. The short-term conflict alert (STCA) function of The Australian Advanced Air Traffic System (TAAATS) also operated during the occurrence.

The departure and approach control positions had recently transitioned to TAAATS, and the departure controller had been operating the new equipment for about 2.5 weeks. Immediately prior to the occurrence the controller had been discussing the operation of the route adherence monitor (RAM) function of TAAATS with another controller, and was attempting to establish the degree to which an aircraft would have to be off-track before the RAM activated.

When the controller instructed the B777 crew to descend, his impression was that he had resolved the possibility for conflict between the B737 and the B777. However, the track to Mudgee for the B737 did not provide the required lateral separation with the arriving B777. The controller had initially used separation assurance techniques to establish separation between all the aircraft. However, to facilitate the departure climb for the B737 the controller issued instructions to that crew which required him to more diligently monitor the track and altitudes of aircraft under his control. He then became distracted by non-essential manipulation and discussion of the system during a critical phase of the traffic management sequence. Consequently, he did not appreciate that the lateral distance between the B737 and the B777 was insufficient to maintain separation. Had the controller maintained vertical separation between the two aircraft, or had vectored the B737 behind the B777, it is unlikely that the incident would have occurred.

The situational awareness of both crews, the operation of the TCAS, and the STCA were all active defences in the incident.

Occurrence summary

Investigation number 199902459
Occurrence date 22/05/1999
Location 15 km NNW Melbourne, Aero.
State Victoria
Report release date 27/08/1999
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 The Boeing Company
Model 737
Registration VH-TJA
Serial number 24295
Sector Jet
Operation type Air Transport High Capacity
Departure point Melbourne, VIC
Destination Maroochydore, QLD
Damage Nil

Aircraft details

Manufacturer The Boeing Company
Model 777
Registration 9V-UA1
Sector Jet
Operation type Air Transport High Capacity
Departure point SINGAPORE
Destination Melbourne, VIC
Damage Nil

Boeing 737-376, VH-TAG

Safety Action

As a result of this incident, Airservices Australia recommended that:

  1. Team leaders brief controllers on the necessity to provide separation assurance where that assurance is not provided on system routes.
  2. Override facilities are to be used.

A cross familiarisation program between the tower and terminal control staff was developed and an education program was devised to ensure both areas have a better understanding of standard system routes.

The Manual of Air Traffic Services (MATS) 6.2.1.2 has been amended to allow controllers to cancel a SID during hours of darkness and instruct crews to depart on runway track using the climb gradient specified in the cancelled SID.

Analysis

This scenario only occurred prior to first light, which occurred after 0600 from approximately the end of March until early September. The problem with the SIDs converging during daylight hours was normally overcome by the cancelling of the SID and the issuing of a radar departure instruction while the aircraft is on the ground prior to departing RWY 03, thus providing separation assurance.

Prior to first light, separation assurance could have been achieved by DEP applying vertical separation between aircraft departing these runways, or by exercising control over aircraft release times to ensure that a radar standard would exist between them.

The DEP controller did not ensure separation between the B737 and the preceding BAe146 by permitting the trainee to issue an instruction of "unrestricted" to the ADC.

The crew of the BAe146 provided a prompt to the controller by requesting a clearance direct to Ballidu shortly before commencing a turn off runway heading. However, the crew were advised by the DEP trainee that the request was understood and that he "will advise".

A second prompt occurred to the training officer when the crew of the B737 called on the DEP frequency reporting that they were leaving 1,800ft. It appears that this prompt alerted the training officer to the developing situation, as he then instructed the trainee to turn the BAe146.

The training officer at this point still did not intervene directly, but instead indicated to the trainee that he needed to give the crew of the BAe146 a heading in order to resolve the situation more quickly. The provision of traffic information or use of "immediate" may have been appropriate under the circumstances.

That the training officer did not intervene until after the incident had largely been resolved was indicative of inattention to the operational situation and a lack of understanding of the criticality of the situation. The training officer displayed a lack of control over the trainee at a time when the issue of precise instructions and a need to alert the crew of the situation was critical. Instructions issued to the trainee were in general terms rather than the specific terminology that the situation demanded.

The task of the ADC in this instance was to manage the runway departures in accordance with instructions from the DEP controller. The ADC and ADC trainee, both understood that the primary responsibility for separation for aircraft on the 03 and RWY 06 PEPPA3 SID, lay with the DEP controller.

The ADC advised that he continued to visually monitor both aircraft via their departure tracks, even though responsibility for separation lay with the DEP controller. He also advised that at no stage did he offer to take, or accept any, responsibility from the DEP controller for separation of the aircraft.

When asked by the DEP controller whether he could monitor, the response of "Yes, I'm monitoring" was intended to indicate that he had the aircraft in sight and that, at that time, by visual observation their tracks had begun to diverge. He was thus indicating that he was able to monitor that the aircraft tracks were not likely to come together, but was not indicating any acceptance of responsibility for separation.

The training configuration utilised by the ADC and DEP was such that the trainers were unable to directly override their trainees. Use of available override systems would have made it easier for the trainers to readily communicate with the crews.

Summary

An infringement of the 3NM radar separation standard occurred at 0606 western standard time approximately 5NM to the northeast of Perth. The aircraft involved were a British Aerospace 146 (BAe146) that departed Perth on a RWY 03 BIU2 standard instrument departure (SID) followed shortly after by a Boeing 737 (B737) that departed on a RWY 06 PEPPA3 SID.

The 03 BIU2 SID is designed to provide system separation with military airspace to the north of Perth and, as a consequence joins the 06 PEPPA3 SID at position REDIL, 8NM to the northeast of Perth. Military airspace was not active at the time of the incident.

The aircraft were under the control of the Perth Departures (DEP) controller at the time. The responsibility for the provision of separation of aircraft on these two SIDs was defined in Perth Local Instructions as the responsibility of the DEP controller.

The DEP controller was monitoring a trainee controller on DEP who was approaching the final stages of rating training. The controller did not use an "override" box that would have allowed him to override the trainee and transmit instructions to the crews.

The aerodrome controller (ADC) advised the trainee DEP controller that the B737 was next for take-off. The trainee DEP controller issued the ADC an unrestricted clearance for the B737 to depart.

The crew of the BAe146 heard the B737 being cleared for take-off and realised that the two aircraft were on conflicting departure routes. The crew asked the trainee DEP controller for a clearance direct to Ballidu in an attempt to resolve the situation. The controller advised the crew that he "would advise" when the direct clearance was available.

The B737 departed and the crew contacted DEP control and advised that they were leaving 1,800 ft. The crew of the BAe146 monitored the proximity of the B737 visually and on the Traffic Alert and Collision Avoidance System (TCAS). The TCAS equipment did not provide a traffic or resolution advice.

The DEP controller did not intervene directly and prompted the trainee to turn the BAe146 away from the B737. The trainee then issued an instruction to the crew of the Bae146 to cancel the SID and track direct to Ballidu. The DEP controller then instructed the trainee to give the crew of the BAe146 a heading in order to resolve the situation. The trainee responded by instructing the crew of the BAe146 to turn left heading 360 degrees for separation. The trainee then instructed the crew of the B737 to turn right heading 090 degrees for separation.

Traffic information was not passed to either crew, nor was the word "immediate" used in passing heading instructions. There was no relay of the urgency of the situation to either crew by phraseologies used by the trainee. At that time the training officer utilised the APP console handset to contact the ADC on the hotline. The ADC was asked by the DEP controller "can you just monitor", to which the response from the ADC was "Yes I'm monitoring". The DEP controller later reported that in his mind it was a request for the ADC to provide visual separation between the aircraft. He also reported that the response received from the ADC indicated to him that the ADC had been providing separation throughout the event by visual monitoring of the aircraft.

The ADC was monitoring a trainee controller by use of a headset. The "B", or training system handset, was not being utilised. The ADC was unable to override the trainee without actually taking over the ADC handset from the trainee.

The DEP controller was not aware of the training on the ADC position and the ADC controller was not aware of the training on the DEP position.

Recorded radar data indicated that separation reduced to 1.4NM with a vertical separation of 200ft. The aircraft were separated by 1.5NM while at the same level. Minimum required radar separation for these aircraft while not 1,000ft vertically separated was 3NM.

The procedures in use were the standard procedures applicable for the use of runways 03/06 for departing aircraft prior to first light. These procedures required the issue of departure instructions for aircraft departing at night or in IMC to be in the form of a SID. It was not permissible for a controller to cancel a SID and issue a radar departure instruction while the aircraft is on the ground prior to first light. It was only permissible in these circumstances to cancel the SID after the aircraft was airborne and had reached the Minimum Vectoring Altitude (MVA). In the case of the 03 BIU2 SID, this situation provided a very short window of opportunity between the aircraft reaching the MVA and commencing a right turn off runway heading. Reliance on controller intervention to cancel this SID and issue a maintain runway heading instruction in order to maintain separation with SID departures from RWY 06 provided no separation assurance.

Occurrence summary

Investigation number 199902419
Occurrence date 06/05/1999
Location 9 km ENE Perth, (VOR)
State Western Australia
Report release date 05/09/2001
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Loss of separation
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer The Boeing Company
Model 737
Registration VH-TAG
Serial number 23478
Sector Jet
Operation type Air Transport High Capacity
Departure point Perth, WA
Destination Adelaide, SA
Damage Nil

Aircraft details

Manufacturer British Aerospace
Model BAe 146
Registration VH-JJP
Serial number E2037
Sector Jet
Operation type Air Transport High Capacity
Departure point Perth, WA
Destination Broome, WA
Damage Nil

Boeing 737-377, VH-CZO

Safety Action

As a result of this occurrence, the Bureau of Air Safety Investigation is currently investigating two safety deficiencies. The first relates to the inappropriate use of MATS 6-2-3 paragraph 32 by aerodrome controllers. The second relates to the non-application of MATS 6-3-1 paragraph 2 by controllers employed in the Brisbane aerodrome control tower.

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

Significant Factors

  1. The controller did not withhold the take-off clearance for CZO when there was no reasonable assurance that separation would exist between the aircraft when CZO commenced the take-off roll.
  2. The lack of visibility of the A4S taxiway at night from the control tower required that aerodrome controllers instruct pilots to confirm when clear of the runway.

Analysis

The difficulty in accurately locating aircraft on the high-speed taxiway A4S at night from the control tower is evidenced by the controller twice assuming that OGG had departed the runway and entered the taxiway. The awareness among local controllers of this difficulty should have encouraged the use of procedures to ensure the maintenance of required standards. However, the controller only recognised that his visual assessment was incorrect when advised by the crew of OGG. It is likely that the controller subsequently assessed that as CZO had not lined up, it was not necessary to cancel the clearance, but the two aircraft should simply be monitored.

The procedures relating to take-off clearances permitted a degree of discretion by the controller. However, that discretion was conditional upon a valid determination of collision risk and the maintenance of separation standards. Consequently, MATS 6-2-3 paragraph 32 was not appropriate to the issuing of the take-off clearance, as the controller had not positively identified the relative positions of the aircraft.

Summary

The aerodrome controller cleared VH-CZO for a night-time take-off from the Brisbane runway 01, believing that VH-OGG, after landing, had vacated the runway onto the high-speed taxiway A4S. At the time, CZO was at the A7 holding point. The crew of OGG alerted the controller (and the crew of CZO) that they were on the active runway. Shortly after, the controller asked the crew to confirm that they were on taxiway A4S and was advised that they were not. Aware that CZO had not lined up on the runway, the controller did not cancel the take-off clearance, but monitored the situation until OGG vacated the runway at taxiway A4.

The high-speed taxiway A4S was 1,900 m from the runway 01 threshold, and taxiway A4 was 2,310 m from the 01 threshold. Taxiway A4 required that the crew turn the aircraft through 90 degrees to exit the runway.

Taxiway A4S was equipped with uni-directional centreline lighting, which was not visible from the control tower. This made it difficult in conditions of reduced visibility for controllers to determine that an aircraft had vacated the runway and was on the high-speed taxiway. However, in visual meteorological conditions at night, it was not normal practice for controllers to ask crews to report when their aircraft was clear of the runway.

The Manual of Air Traffic Services (MATS) 6-3-1 paragraph 2 stated:

"When take-off or landing separation is based on the position of the preceding landing or taxiing aircraft and visual determination, particularly at night or in reduced visibility, is limited by poor azimuth resolution or other factors, the pilot of that aircraft shall be instructed to report when the aircraft has:

  1. crossed and is clear of a runway intersection; or
  2. stopped short of a runway strip; or
  3. vacated the runway."

The MATS 6-2-3, paragraph 31 stated:

"Before clearing an aircraft for take-off, and immediately before take-off is commenced, the tower controller shall make a visual check from the control tower to determine as far as practicable, that the take-off path is not obstructed. If the take-off path is obstructed, take-off clearance shall be withheld or cancelled as appropriate, until the obstruction no longer exists."

The prescribed separation standard was detailed in MATS 6-3-4 paragraph 24. The standard required that a departing aircraft shall not be permitted to commence take-off until the landing aircraft has vacated and is taxiing away from the runway.

The controller cleared CZO for take-off using the provisions of MATS 6-2-3 paragraph 32. This paragraph stated:

"Take-off clearance need not be withheld until prescribed separation exists if, in the opinion of the controller, no collision risk exists and there is reasonable assurance that separation will exist when the aircraft commences take-off roll."

Occurrence summary

Investigation number 199902114
Occurrence date 23/04/1999
Location Brisbane, Aero.
State Queensland
Report release date 11/10/1999
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-CZO
Serial number 24304
Sector Jet
Operation type Air Transport High Capacity
Departure point Brisbane, QLD
Destination Cairns, QLD
Damage Nil

Aircraft details

Manufacturer The Boeing Company
Model 767
Registration VH-OGG
Serial number 24929
Sector Jet
Operation type Air Transport High Capacity
Departure point Sydney, NSW
Destination Brisbane, QLD
Damage Nil

Boeing 737-377, VH-CZC

Safety Action

As a result of the investigation, Airservices Australia have: Designed a new runway 15 SWIFT standard instrument departure to minimise the possibility of conflict in similar circumstances. This procedure is scheduled for publication on 24 February 2000; and Initiated regular discussion sessions amongst Cairns air traffic controllers to, among other things, review techniques used with successive departures. The first of these meetings took place on 24 June 1999.

Significant Factors

  1. The runway 15 SWIFT standard instrument departure allowed the possibility of a following aircraft turning inside a preceding aircraft.
  2. The performance of the B737-400 series aircraft was superior to that of the B737-300 series aircraft.
  3. The use of minimum departure separation standards was inappropriate.
  4. The decision of the approach/departures controller to concentrate on data entry tasks during the departure sequence was not sound practice.

Analysis

Controllers at Cairns considered that the aircraft were "like types" for the purposes of departure standards and neither the aerodrome controller nor the approach/departures controller considered increasing the separation requirements specified in Local Instructions. However, Boeing 737-400 series aircraft are known to normally out-perform the Boeing 737-300 series.

Separation standards used for consecutive departures allowed controllers to increase the minimum distance at their discretion. On this occasion it was not increased and, although the runway departure standard was not breached, the decision did not allow for any unexpected manoeuvre by either aircraft. Both crews acted in accordance with the standard instrument departure and the closure was the effect of aircraft performance.

The approach/departures controller elected to input data to the air traffic computer during the departure sequence. Although these actions were necessary, they were labour intensive and diverted his attention from the air situation display. They were not urgent and the decision resulted in the controller not having his full attention on the relative positions of the aircraft when they first appeared on the display.

The design of the SWIFT 2 standard instrument departure did not guarantee separation assurance. Whenever the second aircraft reached 4,000 ft prior to the first aircraft (whatever the reason) a reduction in horizontal separation was likely.

Summary

VH-CZC, a Boeing 737-300, had taxied at Cairns for departure from runway 15 bound for Sydney.

VH-TJW, a Boeing 737-400, had taxied after CZC, also for a departure from runway 15 bound for Brisbane.

Both crews had been cleared via the runway 15 SWIFT 2 standard instrument departure. That procedure required crews to turn their aircraft at the earlier of 400 ft or the departure end of the runway and then track to 030 degrees M until climbing through 4,000 ft. At that point the aircraft should be turned right onto a track of 170 degrees M to intercept the 139 degrees radial of the Cairns VOR (VHF navigation aid). The SWIFT 2 standard instrument departure was designed to counter the limitations of high terrain surrounding Cairns aerodrome and the tracking requirements of inbound aircraft from the south and east.

At 0604:15 Eastern Standard Time, the aerodrome controller coordinated the two planned departures with the approach/departures controller using the phrase "next CZC followed by TJW". The reply was "CZC unrestricted, TJW unrestricted". That instruction authorised the aerodrome controller to allow the takeoffs in accordance with Cairns Local Instruction TOWER-20, which stated that the aerodrome controller must ensure that 3 NM separation between aircraft would exist prior to the second aircraft passing the upwind end of the runway.

At 0604:48, the crew of CZC was cleared for take-off and at 0606:43, the crew of TJW was cleared for take-off. Radar analysis showed that both aircraft commenced a left turn at approximately 400 ft at, or about, the departure end of the runway and that the required 3 NM spacing was achieved.

The approach/departures controller had approved a request for a change of level from a pilot of an aircraft that had departed Cairns approximately 7 minutes earlier. After issuing the departure clearances, the controller commenced the process of making the change in the air traffic computer; an action that required nine clicks of the mouse. In order to make this change, the controller looked away from the air situation display (which was on the main screen) and used the auxiliary screen to observe the flight plan window while using the keyboard to input the data.

While the controller was performing the information change task, the crews of the departing aircraft contacted him as required. The controller acknowledged the radio broadcasts then returned to the data input task. He did not continue to check the positional information on the air situation display. A few moments later, he glanced at the display and realised that TJW had turned earlier than CZC and was also out-climbing that aircraft. As he was about to take corrective action, the controller saw that TJW had climbed through 4,000 ft and had commenced the right turn onto a heading of 170 degrees M. The manoeuvre had placed TJW on a track inside that of CZC and led to a rapid reduction of horizontal separation to less than the required standard of 3 NM. The vertical separation standard of 1,000 ft had not been achieved at the time. Radar analysis showed that the aircraft passed 1.7 NM horizontally and approximately 400 ft vertically apart.

The controller immediately cancelled the standard instrument departure for TJW and issued the crew with a radar heading of 100 degrees M to ensure that, although separation standards would be breached, TJW would pass behind CZC. The crew of TJW reported that they had the other aircraft in sight and monitored their flight path to ensure that they remained clear of that aircraft. Both crews subsequently reported that they received a traffic alert and collision avoidance system (TCAS) advice.

CZC, the B737-300 series aircraft, had taken 1 minute and 56 seconds to reach 4,000 ft whereas TJW, the B737-400 series aircraft, took only 1 minute and 27 seconds to pass the same altitude. In addition, the initial opening speed created by the departure spacing off the runway had reduced to zero within 1 minute and 30 seconds of the departure of TJW.

Occurrence summary

Investigation number 199902003
Occurrence date 03/05/1999
Location 13 km E Cairns, Aero.
State Queensland
Report release date 09/06/2000
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Loss of separation
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer The Boeing Company
Model 737
Registration VH-CZC
Serial number 23655
Sector Jet
Operation type Air Transport High Capacity
Departure point Cairns, QLD
Destination Sydney, NSW
Damage Nil

Aircraft details

Manufacturer The Boeing Company
Model 737
Registration VH-TJW
Serial number 26961
Sector Jet
Operation type Air Transport High Capacity
Departure point Cairns, QLD
Destination Brisbane, QLD
Damage Nil

Cessna 310, VH-JOR

Significant Factors

  1. Coordination between the tower and terminal staff was unprofessional and led to confusion as to the status of visual approaches.
  2. Various controllers had different interpretations of the meaning of "west" in relation to aircraft approaches.
  3. A significant deterioration in the prevailing weather conditions coincided with the start of a busy arrival sequence.

Analysis

As the flow controller was planning the arrival sequence, he needed to take account of the type of approach available to each aircraft. Even though visual approaches from the south-west had been in use during the morning, tower staff had advised the terminal area controllers that they were no longer available. However, the flow and approach controllers elected to continue with the plan that had the C310 as number one in the sequence and hoped that the pilot would be able to complete a visual approach. The conversations between tower and terminal area controllers in regard to the status of aircraft approaches took place between various control positions, each in partial isolation. Consequently, there was no coordinated response between tower and terminal area staff, and some confusion arose as to the status of such approaches.

As the C310 had been the first aircraft in a busy traffic sequence, the C310 needed to be repositioned when the pilot was unable to make a visual approach. When this re-sequencing occurred, pressure was on the system to try to make up some time to allow for the re-introduction of the C310. In order to minimise the delay, the approach controller had attempted to reduce the distance between the C310 and the AC50 by use of techniques that were not appropriate for the prevailing weather conditions.

Summary

The Cessna 310 (C310) was the first aircraft in a busy arrival sequence and had been programmed by the flow controller for a visual approach to right base for runway 15. The weather had been fluctuating around marginal visual meteorological conditions for some hours and although the cloud base was generally 2,500 ft, it was lower in passing, heavier showers. The visibility was generally 8 km but reduced to 3,000 - 4,000 m in the showers.

When the pilot of the C310 reported that he was unable to establish visual contact with the ground, the approach controller had to change the arrival plan and vector the aircraft to the east of the aerodrome to facilitate further descent. This amendment to the traffic management plan was intended to assist the pilot to become clear of cloud but it necessitated extra track miles for the aircraft. Consequently, an adjustment to the arrival sequence was required and the C310 became number three in the landing order. This change also meant that the timing of sequential landings had fallen behind that which the flow controller had planned and following aircraft would need to be delayed.

The Aero Commander 500 S (AC50) was the fourth aircraft in the sequence and had been held outside controlled airspace by the approach controller until a separation standard could be guaranteed with the other aircraft.

During the course of these events, several verbal exchanges took place between various tower and terminal control area staff regarding the availability of visual approaches in the deteriorating weather conditions. It was agreed that all jet aircraft, and other aircraft arriving from the north and west, would be processed for instrument landing system (ILS) approaches. While these conversations were taking place, the weather had deteriorated such that the cloud base was 1,500 ft and the visibility was generally 3,000 - 4,000 m.

The terminology of what was "north and west" was never positively determined. The flow controller thought that the track of the C310 (via Copperlode Dam - approximately 210 degrees from Cairns) was south-west and not west. Other controllers considered anything west of 180 degrees was "west" and would not have used this track for a visual approach under the prevailing weather conditions.

When the pilot of the C310 reported that he was "visual", the approach controller authorised a visual approach and transferred the pilot to the tower control frequency. Shortly after, he issued a clearance for the AC50 to enter controlled airspace at 1,000 ft. He judged that, as their observed ground speeds were similar, he would be able to maintain the required radar standard of 3 NM while keeping the aircraft comparatively close to each other in order to minimise delays in the landing sequence.

As he was monitoring the progress of the aircraft, the approach controller noticed that the groundspeed of the C310 had reduced on final approach and that the 3 NM separation with the AC50 was unlikely to be maintained. He asked the aerodrome controller if he could use the "sight and follow" procedure, which would allow the pilot of the AC50 to establish and maintain visual separation with the C310 and, consequently, allow the distance between the aircraft to reduce to below 3 NM. However, due to the deteriorating weather and his resultant inability to sight the aircraft, the aerodrome controller declined the request.

As the AC50 closed on the C310, the approach controller realised that the 3 NM standard was not going to be maintained and asked the aerodrome controller to visually separate the two aircraft, a procedure that would again allow the aircraft to proceed with less than the required radar standard. Once again, the aerodrome controller declined the request as he could not see the aircraft in the prevailing weather conditions.

The approach controller then decided to re-sequence the AC50 and issued instructions for the pilot to turn away from the approach. As the aircraft turned, the horizontal separation reduced to 2.8 NM. An infringement of separation standards had occurred.

Occurrence summary

Investigation number 199901797
Occurrence date 24/03/1999
Location 9 km NNW Cairns, Aero
State Queensland
Report release date 29/05/2000
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Loss of separation
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Cessna Aircraft Company
Model 310
Registration VH-JOR
Serial number 4040642
Sector Piston
Operation type Charter
Departure point Kidston, QLD
Destination Cairns, QLD
Damage Nil

Aircraft details

Manufacturer Aero Commander
Model 500
Registration VH-UJB
Serial number 3152
Sector Piston
Operation type Air Transport Low Capacity
Departure point Lizard Island, QLD
Destination Cairns, QLD
Damage Nil

Boeing 747-438, VH-OJC

Safety Action

Local Safety Action

Airservices Australia Sydney District is investigating whether there is a need to roster staff for the flow position prior to 0600, to ensure that aircraft arriving at the end of the curfew are sequenced appropriately. This task is scheduled for completion by October 1999. In the interim, the evening shift centre coordinator controller will monitor the forecast weather and pending traffic numbers for the following morning, and provide staff for flow duties if warranted

Summary

The Sydney approach radar controller was operating a combined departures/approach service during the early morning shift when staffing was minimal, and had been on duty since 0245.

For noise abatement reasons, runway 34 was the preferred runway for arrivals prior to 0600, but was not utilised due to an excessive downwind component. As a result, a number of inbound aircraft were required to hold, in order to land on runway 16 after 0600. The approach controller was required to nominate to the adjacent sector controllers the minimum longitudinal spacing required between successive arriving aircraft. Local procedures recommended a 15 NM spacing. The approach controller requested and was provided with 10 NM longitudinal spacing between aircraft, including a Boeing 747 (B747) approaching from the south-west, which was sequenced to land ahead of a Boeing 767 (B767) arriving from the north. The controller was also managing a number of other arriving aircraft.

Independent visual approaches (IVAs) to runways 16L and 16R were in use. The approach controller subsequently amended the initial arrival sequence when it became apparent that the B767 would arrive earlier than the B747. This placed those aircraft as number two (runway 16L) and three (runway 16R) respectively in the arrival sequence.

The crew of the B767 were vectored to intercept the runway 16L localiser at approximately 30 NM, and instructed to report when they had that runway in sight. The B747 crew had been instructed to turn right onto a heading of 120 degrees in order to intercept the runway 16R localiser. They were subsequently cleared to make a visual approach after reporting that they had runway 16R in sight. However, as the B747 turned onto final, the aircraft drifted to the left through the centreline of the 16R approach path, triggering a resolution advisory, from its traffic alert and collision avoidance system (TCAS), for the crew to descend. The approach controller observed the close proximity of the aircraft and issued instructions to both crews to turn their respective aircraft from final using a "breakout" procedure. The B767 was sighted by the B747 crew as their aircraft passed through the final approach path. The lateral distance between the aircraft was reduced to 0.3 NM at a time when the vertical separation was 500 ft.

Normally, IVAs are conducted by a director controller using specific procedures, which included the use of a 20 NM scale on the radar display, and a map for intercept guidance. In this instance the approach controller had his display set to a scale greater than 20 NM, and did not use the IVA map. Controllers are also required to provide a radar vector not exceeding 30 degrees for intercept of the localiser. The vector issued to the B747 crew provided a 36-degree intercept of the localiser. Moreover, crews subject to IVA procedures are responsible for a number of actions detailed in the Aeronautical Information Publication (ENR 1.1 - 48, paragraph 36.3.1) including, "ensuring that the runway centreline is not crossed during intercept".

Just prior to the occurrence, two controllers arrived to commence the morning shift from 0600. One of these would have normally replaced the overnight controller; however, due to the number of arriving aircraft, these controllers were instructed to staff the director and flow control positions. A third controller arrived and was waiting to take over from the approach controller when the incident occurred. However, the approach controller's workload prevented him from handing over responsibility for the position at that time.

The approach controller limited his options by coordinating the provision of a 10 NM spacing between successive arriving aircraft. As a result, when the crew of the B747 allowed their aircraft to pass through the extended centreline there was limited margin for error, resulting in an immediate traffic confliction. The performance of the controller was probably degraded by the effects of fatigue and workload. The performance of the B747 crew was likely to have been affected by similar factors.

The provision of additional staff prior to 0600 to provide either a flow or director controller to assist the approach controller, or to relieve the approach controller earlier, would have reduced the approach controller's workload during a critical period.

Occurrence summary

Investigation number 199901401
Occurrence date 07/04/1999
Location 22 km NNW Sydney, (VOR)
State New South Wales
Report release date 26/07/1999
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 VH-OJC
Serial number 24406
Sector Jet
Operation type Air Transport High Capacity
Departure point SINGAPORE
Destination Sydney, NSW
Damage Nil

Aircraft details

Manufacturer The Boeing Company
Model 767
Registration VH-RML
Serial number 22980
Sector Jet
Operation type Air Transport High Capacity
Departure point Brisbane, QLD
Destination Sydney, NSW
Damage Nil

Saab SF-340B, VH-KDQ

Summary

A Saab SF-340B (Saab) was conducting a scheduled passenger service from Canberra to Sydney and had been assigned descent to 7,000 ft by the Approach South radar controller in order to maintain the minimum vertical separation standard of 1,000 ft, between the Saab and a Piper Chieftain. The Chieftain was ahead in the approach sequence and had been assigned descent to 6,000 ft. The two aircraft were separated laterally by distances greater than the minimum radar separation standard of 3 NM, but their respective tracks were converging.

The controller requested the Saab crew to expedite descent to 7,000 ft. That instruction was read back by the pilot in command, however, the readback was indistinct. The controller repeated the request "Expedite descent to 7,000 ft". The pilot in command acknowledged that transmission with the aircraft's callsign. Shortly after, the controller observed that the altitude readout for the Saab was indicating that the aircraft was descending through 7,000 ft. The controller queried the Saab crew to confirm that they were maintaining 7,000 ft, then instructed the crew to turn left onto a heading of 360 degrees due to the traffic ahead. As the crew responded to that instruction, the lateral and vertical separation between the Saab and the Chieftain reduced to 1.5 NM and 500 ft respectively.

The traffic sequence had been busy, with the controller endeavouring to change the landing sequence by placing the Saab ahead of the Chieftain. The controller was required to monitor the lateral and vertical separation between a number of aircraft as two standard arrival routes converged. As a consequence, the controller was required to establish vertical separation to ensure separation was maintained between all aircraft as they approached an area of lateral conflict.

All radio transmissions between the controller and the Saab were recorded. A review of the recorded information indicated that the altitudes assigned by the controller, and the readbacks from the Saab crew, were clear and distinct except for the response to the controller's initial request to expedite descent. The Saab crew were unable to explain why they were not alerted to the possibility of an incorrect altitude following the controller's reiteration of the request to expedite descent to 7,000 ft.

The Aeronautical Information Publication GEN 3.4-10 paragraph 4.4 details readback requirements for flight crew. For other than a route clearance, "the key elements of clearances, instructions or information must be read back ensuring sufficient detail is included to clearly indicate compliance". A level instruction must be read back. In this occurrence, the controller did not expect a readback of the altitude, because the previously assigned altitude had not changed. The indistinct response from the Saab crew caused the controller to doubt that his request had been understood, so he repeated the request. When that transmission was acknowledged by the pilot in command, the controller believed that the crew now understood his request to expedite descent to 7,000 ft.

The Saab crew believed that an altitude clearance of 6,000 ft had been issued between the time the controller assigned them 7,000 ft, and when the controller requested that they expedite descent to 7,000 ft. However, the recorded transmissions did not include any reference to 6,000 ft directed to, or received from, the Saab crew during that period.

Occurrence summary

Investigation number 199901070
Occurrence date 17/03/1999
Location 28 km WSW Sydney, (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 Saab Aircraft Co.
Model 340
Registration VH-KDQ
Serial number 340B-325
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Canberra,, ACT
Destination Sydney, NSW
Damage Nil

Aircraft details

Manufacturer Piper Aircraft Corp
Model PA-31
Registration VH-JVD
Serial number 31-7852041
Sector Piston
Operation type Air Transport Low Capacity
Departure point Shepparton, VIC
Destination Sydney, NSW
Damage Nil