Loss of separation

Fokker B.V. F27 MK 50, VH-FNB

Safety Action

Local safety action

Following the investigation, Airservices Australia has:

  1. Withdrawn the use of OPD coordination between the tower and TMA and, restricted the use of Local Instruction 8-22-TM for use between TMA positions.
  2. Briefed controllers to pass sequence information to tower as per Local Instructions 8-23TM in a timely manner and to ensure that handover/takeover procedures are carried out as per local instructions 1-5-TM.
  3. Instructed TWR and TMA Team Leaders to promote team work across streams at all times and ensure each unit provides back up support at all times, especially during quiet periods.
  4. Added a section to local instructions for the control of overshooting aircraft including an instruction to provide a "next" call to DEP for all aircraft conducting overshoot at Perth.
  5. Instructed controllers to pass the current clearance issued to aircraft operating within 5nm of Perth airport to the ADC by the TMA controllers. However this does not absolve the ADC from obtaining information which may be pertinent to separation responsibilities.

Significant Factors

  1. The approach controller, by issuing departure instructions without reference to the Departures controller, did not comply with local instructions.
  2. The aerodrome controller accepted overshoot instructions that placed the two aircraft in close proximity.
  3. The aerodrome controller did not provide assistance to the departure and approach controllers with regard to aircraft operating within close proximity to the aerodrome.
  4. The sole reliance on the use of Operational Data Information for coordination left room for ambiguity to exist in the controllers understanding of an aircraft's intended track.

Analysis

The information flow between the approach and departures controllers was not in accordance with local instructions, because approach was issuing overshoot instructions for an aircraft that would require a clearance from departures. The aerodrome controller, by coordinating with approach instead of departures, compounded this and may have reduced the departures controllers' situational awareness.

The use of Operational Data Information for coordination between units was accepted as a standard operating procedure. On some occasions the overuse and over reliance on Operational Data Information coordination may lead to a lack of situational awareness. Controllers were aware of what was intended to happen after the overshoot but there were no visual cues as to what the aircraft was doing. The approach and departures controllers coordinated via hotline for Departures to retain the Cessna on frequency and place the aircraft on a close right downwind. However, there was no way for the aerodrome controller to know this unless the controller had queried the aircraft's current clearance. This may have led the approach controller to discount the Cessna from his mental traffic picture.

Summary

A Fokker 50 was conducting a practice Instrument Landing System (ILS) approach for runway 24 at Perth, with an intended overshoot to Cunderin. A Cessna 172 was tracking via Northam to Perth with an intended overshoot to Jandakot. Other traffic in the area at the time was a helicopter tracking from Perth to Mundijong.

At 1133 Western Standard Time the crew of the Fokker was conducting the overshoot onto a radar heading which placed the aircraft in close proximity to the Cessna. The pilot of the Cessna sighted the Fokker and turned and descended to avoid that aircraft.

Perth Air Traffic Control had two runway specific traffic management plans. These were North-East (duty runways 03/06) and South-West (duty runways 21/24). Airspace ownership changed dependent on the plan in use and the airspace was divided as Terminal Control Area South (TMA S) and Terminal Control Area North (TMA N), the division occurring along the 281/077 radials from the Perth VOR. At the time of the occurrence the plan placed North-East and TMA S under the control of approach (APP) and TMA N under the control of departures (DEP).

The Perth Aerodrome Controller (ADC) had assumed responsibility for the Aerodrome control position approximately 10 minutes prior to the occurrence. The departure controller had received a handover 10 minutes prior to the incident and was unaware that the Fokker would turn back towards the Cessna.

The relative positions and intended tracks of both the Fokker and the Cessna were such that the departure controller was required to maintain vertical separation until within approximately 5 NM of the aerodrome, with the Fokker passing under the Cessna near Parkerville.

The aerodrome controller coordinated with the approach controller for departure instructions for the helicopter. The approach controller issued the instruction "right unrestricted you separate all the inbounds". The aerodrome controller accepted this and the instructions were issued without reference to the departure controller. The aerodrome controller subsequently coordinated with the approach controller for the overshoot instructions for the Fokker. The approach controller issued the instruction "left 120 unrestricted", but shortly after revised the instruction to, "separate with the helicopter, or keep him on runway heading for a bit to get him above". The aerodrome controller advised that the left turn onto a heading of 120 degrees would suffice. The approach controller issued the overshoot instruction without reference to the departure controller.

Coordination between the tower controllers and the Terminal Control Area controllers utilises the Operational Data Information contained within the radar label display. Coordination between approach and departures is via hotline communications.

Temporary Local Instruction (TLI) SDW/98/160 page 47 Section 5 paragraph 12.3 provides a choice of units to coordinate for aircraft overshooting Perth with the proviso "as appropriate." That section was contained in a letter of agreement between the Tower and Terminal Control Area and specifically dealt with overshooting aircraft.

The same TLI at page 65 Section 6 paragraph 2.1.1 advised that "In all instances the next call must be to DEP". This instruction was headed "Management of Departing IFR Aircraft-Perth" and dealt with Perth Departures from the non-duty runway. That paragraph specifically required the aerodrome controller to coordinate with the departures controller for departure instructions on aircraft departing from the non-duty runway but did not mention the procedure to be followed for overshooting aircraft from the non-duty runway.

Occurrence summary

Investigation number 199900192
Occurrence date 19/01/1999
Location 4 km E Perth, Aero.
State Western Australia
Report release date 12/05/2000
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Loss of separation
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Fokker B.V.
Model F27
Registration VH-FNB
Serial number 20107
Sector Jet
Operation type Air Transport High Capacity
Departure point Perth, WA
Destination Perth, WA
Damage Nil

Aircraft details

Manufacturer Cessna Aircraft Company
Model 172
Registration VH-AUC
Serial number 17275190
Sector Piston
Operation type Flying Training
Departure point Wongan Hills, WA
Destination Jandakot, WA
Damage Nil

Fokker B.V. F28 MK 4000, VH-EWD

Summary

Perth ATS assigned the aircraft an altitude of FL330 on descent from FL370. However, the radar mode C display of the aircraft showed the aircraft descending through FL330 to a final level of FL323. When the air traffic controller queried the crew, the pilot verified FL330. The mode C readout then showed the aircraft climbing and then maintaining FL330. When the aircraft descended below FL330, a Fokker F28 was at FL310, and positioned 4 NM away.

Occurrence summary

Investigation number 199805323
Occurrence date 20/11/1998
Location 228 km N Perth, Aero.
State Western Australia
Report release date 20/08/1999
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Loss of separation
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Fokker B.V.
Model F28
Registration VH-EWD
Serial number 11208
Sector Jet
Operation type Air Transport High Capacity
Departure point Karratha, WA
Destination Perth, WA
Damage Nil

Aircraft details

Manufacturer Saab Aircraft Co.
Model A340
Registration 9V-SJB
Serial number 32-40062
Sector Turboprop
Operation type Air Transport High Capacity
Departure point Singapore
Destination Perth, WA
Damage Nil

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

Analysis

The complexity of the traffic sequence for the ADC was increased by the amount of traffic in the area, and by the fact that the pilot of the turbojet aircraft conducted a go-around. However, had the ADC instructed the Cheetah pilot to report prior to turning base or final for runway 30, he would have had some options to better manage the traffic sequence. The ADC could have also utilised one of the other controllers to assist in the sequencing of the traffic, by monitoring the flight of the Cheetah.

Once the ADC recognised that the use of the intersecting runways was not possible, the use of the appropriate and complete RTF for the situation would have assisted in minimising the possibility for conflict. Under the circumstances, the use of the RTF for emergency conditions may have been appropriate. In his haste to ensure that the Dash 8 received the instruction to hold, the ADC compounded the situation by not allowing the crew time to acknowledge the take-off clearance prior to issuing the hold instruction. Had the ADC transmitted after the crew had completed their acknowledgment, it is probable that they would have clearly received, and been able to safely respond to, the hold instruction.

The use of land-and-hold-short procedures for the particular runways in use was not an option for the ADC.

Summary

The aerodrome circuit was active with a number of aircraft conducting circuit training, or inbound for landing. Both runways 35 and 30 were in use. Runway 30 intersected runway 35 approximately 750 m from its threshold. The tower was staffed with three controllers operating the aerodrome control (ADC), coordination and surface movement control positions.

The ADC had instructed the crew of a De Havilland Dash 8 (Dash 8) to line up for a departure from runway 35. The pilot of an American Aircraft Corporation Cheetah (Cheetah) had been instructed to continue approach for runway 30. The ADC cleared the Dash 8 crew for take-off and then looked towards the final approach path for runway 30 to monitor the approach of the Cheetah. As the ADC completed the transmission to the Dash 8 crew, he saw that the Cheetah was on short final and immediately transmitted an instruction to the Dash 8 crew to hold their position. This instruction was over-transmitted by the acknowledgment of the take-off clearance by the pilot in command of the Dash 8. The ADC commenced to issue a land-and-hold-short instruction to the pilot of the Cheetah; however, seeing that the Dash 8 was starting its take-off roll, he ceased the transmission and issued a further instruction to the Dash 8 crew to hold position. This instruction was over-transmitted by the Cheetah pilot reporting that he was initiating a go-around. The Dash 8 became airborne prior to the intersection of the runways, however, the crew held their aircraft at approximately 50 ft above ground level while the Cheetah passed approximately 100 ft above and slightly behind the Dash 8.

The automatic voice recording of the radio transmissions from the ADC during this period indicated that there were few or no intervals between any of his transmissions. The pilot of another aircraft that was operating in the circuit heard the hold-short instruction. The crew of the Dash 8 reported that they did not hear either of the hold-short instructions.

The ADC had formulated a traffic plan but this changed when a turbojet aircraft he thought was going to conduct a full-stop landing on runway 35, conducted a touch-and-go. The ADC had instructed the crew of the Dash 8 to line up on runway 35 after the approach of the turbojet aircraft, and had amended the approach of the Cheetah to runway 30 to facilitate the departure of the Dash 8. The ADC did not instruct the pilot of the Cheetah to report at a position that would have enabled him to adjust the traffic sequence if required. There was also a delay between the time the ADC approved the Dash 8 crew to line up, and the eventual issue of the departure instructions and a clearance. This delay was due to radio transmissions from the pilot of the turbojet aircraft, as well as the coordination of inbound traffic with the approach controller. During this period, the Cheetah pilot had continued his approach to runway 30. The ADC did not check the position of the Cheetah in relation to the intersection of the runways prior to issuing the take-off clearance to the Dash 8 crew. That was done as he was completing the transmission of the take-off clearance to the crew. As a final action to resolve the conflict between the aircraft, the ADC proposed to issue a land-and-hold-short instruction to the pilot of the Cheetah; however, the landing distance available (590 m) to the pilot did not meet the distance required (900 m) for land-and-hold-short operations.

The Manual of Air Traffic Services details the radiotelephony phraseology (RTF) to be used by controllers to cancel take-off clearances or to stop a take-off in emergency conditions. The ADC used only part of the required RTF for the cancellation of the take-off clearance. He did not use the RTF for an emergency situation.

Occurrence summary

Investigation number 199804856
Occurrence date 07/11/1998
Location Canberra, Aero.
State Australian Capital Territory
Report release date 23/07/1999
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 De Havilland Canada/De Havilland Aircraft of Canada
Model DHC-8
Registration VH-TQF
Serial number 067
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Canberra, ACT
Destination Sydney, NSW
Damage Nil

Aircraft details

Manufacturer American Aircraft Corp
Model AA-5
Registration VH-TXA
Serial number AA5A-0241
Sector Piston
Operation type Private
Departure point Unknown
Destination Canberra, ACT
Damage Nil

Boeing 767-238, VH-EAL

Summary

A Piper Seminole was being flown from Essendon airport, which is located 5 NM south-east of Melbourne airport, to Bendigo. The extended centrelines of the respective northerly runways, which were being used for arrivals and departures, are approximately 3 NM apart. The wind at the time was northerly at 25 kts.

The pilot of the Seminole was instructed to maintain runway heading of 350 degrees and climb to 6,000 ft. After take-off the aircraft was identified on radar by the Melbourne departures north (DEPN) controller.

Six minutes later the crew of a Boeing 767 (B767) was cleared to take-off from runway 34 at Melbourne, for Sydney, and to maintain runway heading on climb to 5,000 ft. After take-off the aircraft was identified on radar by the DEPN controller who cleared the crew to climb to flight level (FL) 200.

Traffic was light, with four departing and one arriving aircraft being managed by the DEPN controller. The controller was aware of the need to maintain either vertical or lateral separation between aircraft departing from Melbourne and the Seminole, and was also conscious that the present heading of the Seminole was not in the direction of Bendigo. He had previously radar vectored a departing Boeing 737 ahead of the Seminole, and planned to do the same with the B767, however, he observed that the B767 did not appear to be climbing as fast as he had expected. Consequently, the controller would have to take both the B767 and the Seminole further to the north before achieving sufficient vertical or lateral separation to enable him to allow the aircraft to resume their respective planned routes. The minimum required separation was either 3 NM lateral or 1,000 ft vertical.

When the B767 was approximately 7 NM to the south-west of the Seminole the controller believed he could vector the B767 to pass behind it, thus minimising any delay to both aircraft. The controller did not issue instructions to ensure vertical separation prior to turning the B767.

The B767 was vectored right, onto a heading of 040 degrees. Shortly after, the Seminole was vectored left onto a heading of 270 degrees. The DEPN controller then instructed the B767 crew to continue the right turn onto 060 degrees as the aircraft was passing approximately 4,500 ft, and instructed the pilot of the Seminole to turn right onto 290 degrees. The B767 crew was requested to expedite the turn onto 090 degrees. Shortly after, the crew reported receiving a traffic alert and collision avoidance system (TCAS) resolution advisory, indicating the crew should maintain the current altitude of approximately 5,400 ft due to a conflicting aircraft. The crew complied, and advised the DEPN controller accordingly. The controller advised the crew that they had passed another aircraft that was to their left. Separation was reduced to 1.5 NM lateral and 600 ft vertical. The B767 crew did not sight the other aircraft.

The B767 crew subsequently reported that the wind at 5,000 ft was westerly at 50 kts. This would have had the effect of increasing the groundspeed of the B767 as it turned towards the east. Consequently, the rate of closure between the B767 and the Seminole would have been greater than anticipated by the controller, and it was probably at that stage he became aware that the aircraft might pass with less than the required separation. However, his subsequent instructions were unable to rectify the situation. Had the controller continued to employ separation assurance techniques, the occurrence would probably not have eventuated.

Occurrence summary

Investigation number 199804849
Occurrence date 25/10/1998
Location 19 km NE Melbourne, (VOR)
State Victoria
Report release date 20/08/1999
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Loss of separation
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer The Boeing Company
Model 767
Registration VH-EAL
Serial number 23306
Sector Jet
Operation type Air Transport High Capacity
Departure point Melbourne, VIC
Destination Sydney, NSW
Damage Nil

Aircraft details

Manufacturer Piper Aircraft Corp
Model PA-44
Registration VH-ZWI
Serial number 44-7995219
Sector Piston
Operation type Unknown
Departure point Essendon, VIC
Destination Bendigo, VIC
Damage Nil

Boeing 737-377, VH-CZN

Safety Action

Local safety action

The Airservices Australia investigation report included a number of recommendations for consideration by Melbourne Centre management. A precis of those recommendations and responses follows:

  1. Recommendation - A controller who has just completed familiarisation should not oversight the familiarisation of another officer.

    This recommendation was not implemented. It remains the responsibility of individual controllers to assess whether they are capable of monitoring another officer.

  2. Recommendation - Amend the flight progress strip presentation for waypoints Oodnadatta and AGAGO.

    That recommendation was implemented.

  3. Recommendation - Review flight progress board presentation and sector workload.

    A workload review was conducted and the sector will be split horizontally. This is scheduled for implementation in November 1999.

  4. Recommendation - The coordinator position to be staffed with sufficient lead-time.

    A notice reminding controllers to employ the coordinator in sufficient time to enable adequate briefing and traffic assessment to be conducted has been included in console operational documents.

  5. Recommendation - Familiarisation should not take place when traffic density dictates that a coordinator is required.

    The recommendation was implemented.

  6. Recommendation - Review alternate methods for annotating potential conflict situations.

    No change was made.

Summary

A Boeing 737 (B737), VH-TJT, was en route from Darwin to Adelaide via air route J187 at flight level (FL) 370. Another B737, VH-CZN, was en route from Ayers Rock to Sydney via air route G222, also at FL370, which was a standard level for the direction being flown by both aircraft. The air routes converged, and eventually crossed at Oodnadatta. Both aircraft were under procedural (non-radar) control by Melbourne Sector 1. The sector console was staffed by a controller who was undergoing re-familiarisation prior to being checked for return to controlling. He was being supervised by a controller who had recently returned after a six month break from full-time operational controlling.

The controller had calculated estimates for Oodnadatta of 1518 and 1520 respectively for CZN and TJT. At 1515, when the crew of TJT reported at SARAH, 40 NM north-north-west of Oodnadatta, the controller became aware that there was no separation standard being applied between the two aircraft, so he instructed the crew of TJT to descend immediately to FL350. The crew reported on descent and indicated that their traffic alerting and collision avoidance system (TCAS) showed an aircraft 33 NM ahead, over Oodnadatta. The crew of TJT subsequently reported maintaining FL350 at 1520. As a result, there was a breakdown of the required vertical separation standard of 2,000 ft.

Both controllers had earlier noted the possibility for conflict between the two aircraft and annotated their respective flight progress strips with an Oodnadatta position, and the calculated estimates for that position. The estimates were annotated at different locations on the strips. There was no local instruction for the standardisation of the annotation of the Oodnadatta position or similar positions that marked the intersections of the various route crossings in the area. During the following 90 minutes, the traffic level steadily increased and the two controllers had discussed the need for a coordinator. The sector was normally operated as a solo operator position; however, there were periods when there were significant or complex traffic levels and there were procedures to enable the controller to be assisted by a coordinator in such cases.

Approximately 10 minutes prior to the occurrence, the controllers requested the assistance of a coordinator and as a consequence, a third controller joined them at the console. At this stage, the traffic situation was very busy, with approximately 70 flight progress strips being monitored and with additional strips being discarded or added to the board as flights progressed through the sector. The coordinator controller had little opportunity to obtain an adequate handover/takeover brief from the two controllers already at the position. The third controller assumed the coordinator position and endeavoured to action any items that he considered required attention as he attempted to gain some idea of the traffic disposition. He was unable to monitor the Sector 1 controller's air-ground-air program on a continuous basis due to the conduct of coordination actions. The work at the console was difficult, with three controllers working in an area normally used by only two controllers.

As a result of a combination a factors, the potential confliction between CZN and TJT, although recognised earlier by both controllers, was subsequently overlooked as the sector workload increased. It was only when the crew of TJT reported at SARAH that action was undertaken resolve the situation.

Airservices Australia carried out an investigation of this occurrence under the overall supervision of a Bureau officer. The significant factors that contributed to this occurrence were found to be;

  1. The two controllers manning the Sector 1 position were not operating at their optimum level of performance due to a lack of recency.
  2. Following an increase in Sector 1 traffic density, the controllers' recognition that they required coordination assistance to manage the increased workload was too late to provide any effective relief.
  3. The amount and disposition of traffic in the sector led the controllers to be distracted to a point where they were unable to adequately monitor all sector traffic.
  4. The controllers' annotation of flight progress strips did not alert them to the possibility for a conflict between CZN and TJT.

Occurrence summary

Investigation number 199804690
Occurrence date 29/10/1998
Location Oodnadatta, (NDB)
State South Australia
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 737
Registration VH-CZN
Serial number 24303
Sector Jet
Operation type Air Transport High Capacity
Departure point Ayers Rock, NT
Destination Sydney, NSW
Damage Nil

Aircraft details

Manufacturer The Boeing Company
Model 737
Registration VH-TJT
Serial number 24445
Sector Jet
Operation type Air Transport High Capacity
Destination Adelaide, SA
Damage Nil

Boeing 747-438, VH-OJP

Safety Action

Local safety action

The operator issued a standing instruction to all crews reminding them to ensure that company procedures were adhered to when communicating to air traffic control via the CPDLC.

Bureau of Air Safety Investigation safety action

As a result of this and similar occurrences, the Bureau of Air Safety Investigation is investigating a perceived safety deficiency. The deficiency relates to the use of controller pilot datalink communication (CPDLC) messages by air traffic control and pilots for the exchange of operational information.

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

Summary

A Boeing 747 (B747) was en route from Auckland to Melbourne, maintaining flight level (FL) 330. The aircraft was experiencing some turbulence. The crew were communicating with Auckland air traffic control via controller pilot data link communications (CPDLC) and were awaiting a response to a request to climb to FL350.

The crew had observed on their traffic alerting and collision avoidance system (TCAS) that another aircraft was crossing their route from the south-east to the north-west at FL350. They were aware that a clearance to climb to FL350 would not be available until that aircraft had passed. The other aircraft was a B737 en route from Wellington to Brisbane. The air routes intersected at the VIMAV reporting point. At 2002 the B737 crew reported at VIMAV maintaining FL350. At 2005, the B747 passed VIMAV.

At about 2010, the B747 crew received a conditional clearance to climb to FL350 at 2018. The delay in the climb approval was required to establish a 15-minute time standard between the two aircraft at the intersection of the air routes. The B747 crew immediately commenced climb to FL350 after the message was received. At 2012 they dispatched a message reporting they were maintaining FL350. When air traffic control notified the crew via high-frequency radio that they had not complied with the clearance, the crew descended the B747 to FL330. The B747 TCAS did not register an alert during the period that separation was infringed.

Normal company CPDLC practice for the B747 crew was for the non-flying pilot to read out the message on the screen, and for this to be confirmed by the flying pilot. Once the message and the subsequent response were confirmed by the two crew members the non-flying pilot dispatched the message to air traffic control.

The investigation found that the crew, for reasons unknown, had mis-interpreted the datalink message as an immediate clearance to climb. It is possible that, due to the turbulence being experienced, the crew acted hastily to acknowledge the message and climb the aircraft to reduce passenger discomfort. It is likely that either one or both of the crew were not as vigilant in their checking of the message as they would have been under less demanding circumstances.

Occurrence summary

Investigation number 199804135
Occurrence date 25/09/1998
Location 19 km W VIMAV
State International
Report release date 15/07/1999
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-OJP
Serial number 25545
Sector Jet
Operation type Air Transport High Capacity
Departure point Auckland, NEW ZEALAND
Destination Melbourne, VIC
Damage Nil

Aircraft details

Manufacturer The Boeing Company
Model 737
Registration ANZ161
Sector Jet
Operation type Air Transport High Capacity
Departure point Wellington, NEW ZEALAND
Destination Brisbane, QLD
Damage Nil

Loss of separation Boeing 767, N601EV and a Boeing 747, 9M-MPD, 9 km south of Bindook, New South Wales, on 21 September 1998

Safety Action

Local Safety Action

The airline has issued a fleet notice to B767 crews, reminding pilots to be more vigilant when flying into Sydney, and alerting them to the inadequacy of holding information.

BASI Safety Action

As a result of this occurrence, the Bureau of Air Safety Investigation is currently investigating a perceived safety deficiency.

The deficiency relates to the depiction of holding patterns on en-route charts, the appropriateness of the use of non-standard holding patterns, and associated radiotelephony phraseology.

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

Summary

Air traffic control had issued the crew of a foreign Boeing 767 (B767) with an instruction to hold at Bindook. Although the published holding procedure required a left pattern, the crew turned the aircraft for a right pattern. The right turn subsequently placed the aircraft into conflict with a Boeing 747, which was being radar vectored to the south of Bindook. Separation was reduced to approximately 700 ft vertically, and 4 NM laterally. The required separation standard was 1,000 ft, or 5 NM.

An investigation revealed that the crew did not locate the holding pattern on the Jeppesen terminal chart. The depiction of the holding pattern was difficult to distinguish from other markings on the chart and the pattern was not displayed on the appropriate Standard Arrival Route (STAR) chart. In addition, the holding pattern was not loaded in the aircraft's flight management computer database. The Captain of the B767 reported that in the USA, where a holding pattern is not displayed, or in the absence of other information, a "default" right hand pattern is to be flown. There is no such procedure in Australia. As a result, the Captain elected to fly a right hand pattern without checking with air traffic control for holding pattern information.

Occurrence summary

Investigation number 199803921
Occurrence date 21/09/1998
Location 9 km S Bindook
State New South Wales
Report release date 17/08/1999
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 767
Registration N601EV
Sector Jet
Operation type Air Transport High Capacity
Departure point Taipei, TAIWAN
Destination Sydney, NSW
Damage Nil

Aircraft details

Manufacturer The Boeing Company
Model 747
Registration 9M-MPD
Sector Jet
Operation type Air Transport High Capacity
Departure point Melbourne, VIC
Destination Sydney, NSW
Damage Nil

Fairchild SA227-DC, VH-WAI

Safety Action

Local Action

ATC Management at Perth has made the following recommendations:

  1. the use of runway 11/29 be restricted to only when operationally required;
  2. local Instructions be amended to ensure the SMC retains the flight progress strip on an aircraft until the aircraft is no longer under the SMC's control; and
  3. local ATC management to continue with its aim of having runway 11/29 withdrawn from operational use due to the traffic management complexities created by its use.

BASI Safety Action

As a result of this and other occurrences, the Bureau of Air Safety Investigation is investigating a safety deficiency.

The deficiency relates to the use of conditional clearances for runway entry and runway crossings by vehicles and aircraft, and the procedures used by air traffic controllers to alert themselves that vehicles or aircraft are on an active runway.

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

Significant Factors

The SMC did not conduct an effective scan of the airfield prior to advising the ADC of "no traffic".

The ADC did not conduct an effective scan of runway 11 or the flight progress strip display prior to clearing the C402 to land.

The flight progress strip display, and the controller's management of the console, did not provide the controllers with an accurate representation of the traffic situation.

The airfield layout increased the potential for a runway incident.

Summary

The crew of a Metro 23 was cleared by the surface movement controller (SMC) at Perth to enter runway 11 and taxi to the threshold of runway 21 prior to departure. However, as the aircraft approached the runway 11 holding point, the crew checked the final approach path and saw a Cessna C402 landing on runway 11 in front of them.

A subsequent investigation revealed that the SMC had previously been using runway 11/29 as a taxiway for vehicle and aircraft movements. The procedure for release of the runway from the aerodrome controller (ADC) to the SMC was for both the ADC and SMC to de-select their respective runway 11/29 selection buttons. Both buttons would become illuminated when selected on, indicating that the runway was active. De-selecting each button had the reverse effect. Should the button be selected or de-selected on one side only, both lights would flash to alert the controllers to a mismatch.

In addition to the use of the runway selection buttons, both controllers were to coordinate off-line with each other using the phrase "runway 11/29 released to you" or "runway 11 active" as appropriate. Any traffic that might be on the runway would also be coordinated. Those procedures were detailed in the Perth Tower Local Instructions.

Just prior to the incident, the SMC had control authority for runway 11/29, and the runway 11/29 selector buttons were in the de-selected position. When the crew of the Metro requested a taxi clearance, the SMC cleared them to taxi to runway 21, entering runway 11 at taxiway Echo. The threshold of runway 21 is at the midway point of runway 11/29 and access to the threshold of runway 21 was achieved by taxiing via runway 11. Once details of the Metro were no longer required by the SMC, the flight progress strip for the aircraft was placed into the top transfer slot on the ADC's side of the console. This procedure was also documented in Perth Tower Local Instructions.

Three minutes after the taxi clearance was issued, the ADC elected to land a C402 on runway 11. Prior to issuing the landing clearance, the ADC selected the runway 11/29 selector button to indicate to the SMC that the ADC was taking control authority for runway 11/29. Because the SMC no longer held a flight progress strip as a memory marker, he also turned on his selector button and advised the ADC "no traffic runway 11". The ADC did not notice the Metro, which had not yet entered taxiway Echo, nor did he notice the flight progress strip in the top transfer slot. The ADC subsequently cleared the C402 to land on runway 11.

Occurrence summary

Investigation number 199803910
Occurrence date 14/09/1998
Location Perth, Aero.
State Western Australia
Report release date 10/07/2000
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 Fairchild Industries Inc
Model SA227
Registration VH-WAI
Serial number DC-874B
Sector Turboprop
Operation type Charter
Departure point Perth, WA
Destination Sunrise Dam, WA
Damage Nil

Aircraft details

Manufacturer Cessna Aircraft Company
Model 402
Registration VH-CKN
Serial number 402B0121
Sector Piston
Operation type Unknown
Departure point Jandakot WA
Destination Perth, WA
Damage Nil

Boeing 747-338, VH-EBX

Summary

The crew of a Boeing 747 (B747), maintaining flight level (FL) 390, en route from Cairns to Nagoya, was contacted by the crew of a Boeing 767 (B767), en route from Auckland to Osaka. The B767 crew reported that they had been approved by air traffic control to climb from FL370 to FL390, and that their position was 44 NM south-east of ASEDA, which is located within the Tokyo oceanic control area. The B747 crew reported that they were 54 NM south-east of ASEDA at FL390. Subsequently, the B767 crew advised that they would limit their climb to FL385. Shortly after that exchange the sector controller instructed the crew of the B767 to descend to FL370 due to traffic.

An investigation found that the sector controller was managing five aircraft tracking north on air route A597, together with an aircraft crossing A597. The controller was concerned that the longitudinal separation between the B767 and another following aircraft at FL370 would reduce to less than the required standard, which was either 2,000 ft vertically or 15 minutes longitudinally. Consequently, the controller instructed the B767 crew to climb, but failed to appreciate that the B767 would conflict with the B747 at FL390. However, the controller subsequently recognised that an error had been made and issued alternative instructions.

Occurrence summary

Investigation number 199803491
Occurrence date 24/08/1998
Location 100 km SSE Aseda, (IFR)
State International
Report release date 04/05/1999
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-EBX
Serial number 23688
Sector Jet
Operation type Air Transport High Capacity
Departure point Cairns, QLD
Destination Nagoya, JAPAN
Damage Nil

Aircraft details

Manufacturer The Boeing Company
Model 767
Sector Jet
Departure point Auckland, NEW ZEALAND
Destination Osaka, JAPAN
Damage Nil

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

Safety Action

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

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

Significant Factors

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

Analysis

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

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

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

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

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

Summary

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

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

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

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

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

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

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

The controller

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

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

Information from the crew of VH-TNU

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

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

Brisbane arrival procedures

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

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

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

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

Sight and Follow procedures

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

Occurrence summary

Investigation number 199802964
Occurrence date 03/08/1998
Location 13 km E Brisbane, Aero.
State Queensland
Report release date 20/08/1999
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Loss of separation
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer De Havilland Canada/De Havilland Aircraft of Canada
Model DHC-8
Registration VH-TNU
Serial number 203
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Williamtown, NSW
Destination Brisbane, QLD
Damage Nil

Aircraft details

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