Separation issue

Piper PA-28R-201, VH-PRF

Summary

A British Aerospace 146 (BAe 146) was arriving at Alice Springs from the north-east and was instructed by air traffic control to make a visual approach to runway 12 via a left circuit.

A Piper Cherokee Arrow (Arrow) was also arriving at Alice Springs on a flight from Coober Pedy and was instructed to track via visual flight rule route "VFR Route 6". That route tracked via the Stuart Highway, south-west of the aerodrome. As the aircraft passed Mount Polhill (20 NM from the aerodrome) the pilot was cleared to track via the gaol and to then make a visual approach to runway 06.

When the BAe 146 was on final approach the crew sighted the Arrow approximately 1 NM ahead and descending through their level. They commenced a go-around and manoeuvred to the right to ensure that they passed behind that aircraft.

The pilot of the Arrow had misinterpreted some of the controller's instructions and had tracked for a circuit because he was not set up for a straight-in approach. However, in carrying out that action he had not informed the controller of his change of plan and his inability to carry out the instructions received.

Although the controller was looking for the Arrow in order to provide a visual service, he did not see the aircraft because the pilot had been tracking in a direction that the controller was not expecting.

Occurrence summary

Investigation number 200003093
Occurrence date 17/07/2000
Location 12 km SSW Alice Springs, Aero.
State Northern Territory
Report release date 16/10/2001
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Separation issue
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Piper Aircraft Corp
Model PA-28
Registration VH-PRF
Serial number 28R-7837078
Sector Piston
Operation type Private
Departure point Cooper Pedy, SA
Destination Alice Springs, NT
Damage Nil

Aircraft details

Manufacturer British Aerospace
Model BAe 146
Registration VH-JJX
Serial number E2127
Sector Jet
Operation type Air Transport High Capacity
Departure point Cairns, QLD
Destination Alice Springs, NT
Damage Nil

Cessna 172N, VH-IGA

Summary

A member of the public reported seeing a single engine aircraft manouevre suddenly to avoid another aircraft, on an intersecting track, while the aircraft were over Brisbane.

An investigation reviewed radar data and air traffic control automatic voice recordings to establish the sequence of events. The investigation found that VH-OXF, a Beech 300, was tracking for a left base to runway 01 at Brisbane Airport at 2,500 ft, while a Cessna 172, VH-IGA, was tracking north over the suburbs at 1,500 ft. The Brisbane departures controller established that the pilot of the Beech could see and was able to avoid the Cessna before reducing the vertical spacing between the aircraft to less than the vertical separation standard of 1,000 ft. The Beech pilot reported seeing and passing over the top of the Cessna and ready for further descent. The controller issued a clearance for a visual approach. The recorded radar data indicated that the Beech began a steady descent from about the intersection of the aircraft tracks.

The controller's options in relation to ensuring separation between the aircraft were either to:

  1. maintain the Beech at 2,500 ft until there was more than 3 NM lateral separation with the Cessna; or
  2. use visual separation procedures by having a pilot report seeing the other aircraft and then instructing that pilot to avoid the sighted aircraft.

To enable the Beech to descend in preparation for landing, the controller used the second option. Examination of the radar data indicated there was no infringement of separation standards.

The recorded radar data indicated that during the period when the Beech was assigned 2,500 ft, the Mode C altitude intermittently indicated 2,300 ft and 2,400 ft. Mode C altitude has a tolerance of plus or minus 200 ft. The pilot was therefore complying with the air traffic control clearance.

Occurrence summary

Investigation number 200002938
Occurrence date 06/07/2000
Location 11 km WSW Brisbane, Aero.
State Queensland
Report release date 13/09/2000
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Separation issue
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Cessna Aircraft Company
Model 172
Registration VH-IGA
Serial number 17269546
Sector Piston
Operation type Aerial Work
Departure point Archerfield, QLD
Destination Archerfield, QLD
Damage Nil

Aircraft details

Manufacturer Beech Aircraft Corp
Model 300
Registration VH-OXF
Serial number FL122
Sector Turboprop
Operation type Unknown
Departure point Unknown
Destination Brisbane, QLD
Damage Nil

de Havilland Canada DHC-8-201, VH-TQG, 185 km east of Williamtown (NDB), New South Wales, on 15 November 1999

Safety Action

Local safety action

The operator of the Astra has confirmed that flight crew/air traffic control briefings will be conducted before all future calibration flights.

Australian Transport Safety Bureau safety action

As a result of the investigation the Australian Transport Safety Bureau issued the following recommendation:

R20000105

The Australian Transport Safety Bureau recommends that the Australian Defence Force review airspace activation and clearance issue procedures to ensure that flight crews understand and/or are notified of any changes in prohibited/restricted/danger airspace management responsibility.

Significant Factors

  1. The flight crew and air traffic control staff did not brief effectively before the calibration flight.
  2. The Astra crew was unaware that Brisbane Centre was responsible for management of a portion of R577.
  3. The Astra crew was unable to maintain continuous two-way communications with flight service international.
  4. The provision of radar coverage and use of secondary surveillance radar transponders in oceanic airspace assisted in the resolution of the conflict.

Analysis

The briefing planned between the Astra crew and Williamtown Air Traffic Control staff did not occur and as a result, the air traffic control staff were not fully conversant with the Astra crew's intentions. Also, the Astra crew were unaware of the unique delineation in airspace management responsibilities for the area where they intended to operate. These aspects made it difficult for the crew to adequately prepare for contingencies and for air traffic controllers to understand the complex nature of the calibration task.

The Astra crew complied with the clearance issued by Williamtown Air Traffic Control. However, the clearance was issued without air traffic control being fully conversant with the flight profile. The misunderstanding was compounded by the Astra crew believing that their flight would be managed by Williamtown Air Traffic Control. If the crew had been aware of the ramifications of the Jordy Release, it was likely that they would have appreciated that the initial stages of the flight would pass back and forth between R577 and non-controlled airspace. Had they been aware of this fact and that consequently, they were responsible for their own traffic avoidance, the Astra crew may have ensured that air traffic services were advised of the intention to change level well in advance of commencing the climb to FL200. If the crew had been able notify flight service international of their intention to climb from 10,000 ft to FL200 it was probable that they would have been issued with traffic information on the Dash 8 and the conflict may not have occurred.

The operation of the Astra's transponder on the assigned code assisted in the resolution of the situation. An alternative for the crew was to select the transponder to the radio failure code of 7600, which was part of the aviation safety net. Given the complex nature of the task and the communication difficulties being experienced by them at the time, this action may have provided a more timely alert to air traffic agencies. Had air traffic agencies been alerted by the change in code to 7600, it is likely that air traffic control or flight service international officers would have either provided traffic information or initiated action to separate other aircraft in the vicinity of the Astra.

Summary

The Brisbane Ocean sector controller saw on radar an unidentified aircraft climbing through flight level (FL)180. The controller issued traffic information to the crew of a Dash 8 operating an instrument flight rules (IFR) flight from Lord Howe Island to Sydney at FL200. The crew of the Dash 8 sighted the unidentified aircraft at an approximate distance of 5 NM and 1,500 ft below them. The two aircraft passed with 3 NM lateral separation at the same level. The unidentified aircraft was subsequently identified as an Astra conducting an IFR calibration flight. It appeared that the crew of the Astra had not complied with Aeronautical Information Publication (AIP) procedures for changing levels in non-controlled airspace. These procedures require pilots of IFR category aircraft operating in non-controlled airspace to notify the relevant air traffic agencies of any changes in altitude/level. Investigation of the occurrence revealed that the Astra crew were not notified of a change in airspace management for their area of operations.

The Astra crew was conducting a calibration of a new radar that had been installed at Williamtown aerodrome. This required the aircraft to track outbound from Williamtown at 1,500 ft, in a direction clear of local operating areas and air routes, until radar coverage was lost and then return on the reciprocal track while climbing. Once the next altitude or level was reached the crew would immediately turn the aircraft to track outbound again. The manoeuvre was to be repeated at 10,000 ft, FL200, FL300 and FL400 and would conclude with the aircraft completing the task at approximately 220 NM from Williamtown.

The Astra crew had prepared and dispatched written briefs on the task to Williamtown and Brisbane Air Traffic Control (ATC) agencies. However, the calibration task schedule was amended and subsequently conducted 24 hours earlier than originally notified. The brief depicted the calibration flight as being a series of steps with an increase in altitude/level as the distance from Williamtown increased but did not depict that the aircraft would fly the reciprocal track at any stage. After the Astra had departed Williamtown to commence the calibration, the Williamtown approach coordinator briefed the Brisbane Flight Service International officer on the task, based on the briefing and other details as subsequently advised by the crew.

The general practice of the Astra crew was to conduct personal briefings with the responsible air traffic control staff on the day of a calibration task and this was their intention on the day of the occurrence. However, when the Astra arrived at Williamtown, the senior air traffic control officer who had planned to attend the briefing was not available. Consequently, the crew only briefed a technical ground party.

The Astra crew was issued a clearance by Williamtown Air Traffic Control to track via the 100 tactical air navigation aid radial on climb to FL210. On this track the Astra would transit Williamtown restricted area R577 which was promulgated as continuously active, 24 hours a day. The intended track of the Astra entered and exited R577 respectively at 25 NM and 130 NM east of Williamtown. The vertical limits for the area are from sea level to FL600. When not required for military operations a notice to airman (NOTAM) deactivating R577 for specific periods was normally issued by Williamtown Air Traffic Control. A deactivation NOTAM was not issued for the period of the calibration flight.

As an aid to airspace management, Brisbane and Williamtown Air Traffic Control agencies had agreed to automatically release portions of R577 and other restricted areas to Brisbane when the restricted areas were active. This agreement was published in the Northern New South Wales Manual of Air Traffic Services Supplement (MATS SUPP) which in turn was part of both Williamtown and Brisbane operating procedures. The agreement effectively transferred airspace management responsibility for the south-east portion of R577, known as the Jordy Release, from Williamtown Air Traffic Control to Brisbane Centre. The planned track of the Dash 8 passed through the Jordy Release.

The lateral and vertical limits for Australian airspace were published in the Airservices Australia Designated Airspace Handbook (DAH) and depicted on AIP charts. The DAH, charts or a NOTAM can be used for flight crew pre-flight briefing. None of the documents included the MATS SUPP provisions.

A letter of agreement between Brisbane Ocean sector, Brisbane Flight Service International and Sydney Flight Service 4 detailed the airspace management responsibilities for the Jordy Release when transferred to Brisbane Centre. The division of responsibilities was:

  • Ocean sector
    That portion of the release above FL200 between 90 NM and 150 NM from Sydney and above FL245 outside of 150 NM Sydney,
  • Flight Service International
    That portion of the release at FL200 and below that level outside of 90 NM from Sydney, and
  • Sydney Flight Service 4
    That portion of the release below the control area steps inside 90 NM from Sydney.

The Ocean sector controller was required to separate IFR aircraft as if they were in controlled airspace. The officers of both flight service units were required to issue traffic information to pilots of IFR category flights, just as they would have for pilots of IFR flights in non-controlled airspace, in accordance with the Manual of Air Traffic Services (MATS) criteria. Part of the MATS criteria required traffic information to be issued when aircraft were climbing or descending through the level of another aircraft when these aircraft were within 15 NM or 10 minutes longitudinally or laterally. Ocean sector uses radar and procedural control methods to separate aircraft. Radar coverage extends to beyond the eastern limit of R577. Neither of the flight service units had access to radar services.

Because of the flexible airspace management arrangements for the Jordy Release, flight service international officers usually pre-empted requests for confirmation of the availability of planned routes for aircraft inbound to Sydney. Normal practice was to advise crews as early as possible when the area was active with military operations to enable them to commence tracking via alternative routes. The crew of the Dash 8 was not advised that their planned route was unavailable. The crew was subsequently advised to contact the Ocean controller at 140 NM from Sydney for a clearance.

The Astra crew reported that due to R577 being active, they believed that, their flight would be managed by Williamtown air traffic control. The Williamtown coordinator advised flight service international that the crew had been cleared to FL210 but that initially they would maintain 1,500 ft. The coordinator subsequently advised flight service international that the Astra had climbed to 10,000 ft. The Astra crew was instructed that they were leaving the Williamtown restricted area and to transfer to flight service international on high frequency (HF) radio. This was required as they were operating in that portion of R577 being managed by flight service international.

After several attempts, the Astra crew contacted flight service international on HF radio and was advised of another HF frequency to use if they were having communication difficulties. There was no further contact with the crew on HF radio. The flight service international officer attempted unsuccessfully to contact the crew. The problems with the HF radio communication were believed to be the result of propagation difficulties. Once it was apparent to the crew that HF communication was not viable they tried to establish communications with Brisbane Centre via VHF. The crew reported after the occurrence that because they were unable to advise any air traffic service agency of the next climb, from 10,000 ft to FL200, they broadcasted their intention on the VHF emergency frequency, 121.5 MHz. The investigation could not establish whether other crews heard the transmission.

The crew contacted the Nambucca Sector Controller and reported that their position was 120 NM east of Williamtown on the 100 radial and that the aircraft had left 10,000 ft on climb to FL200. The Nambucca controller confirmed that the Astra was tracking west and that at 110 NM from Williamtown the crew would commence a turn to track outbound. The Nambucca controller contacted the Ocean controller to report the Astra's position. At approximately the same time the Ocean controller was issuing a clearance to the crew of EA261 and shortly after noticed an unidentified aircraft approaching the Dash 8. The Nambucca controller issued traffic information to the crew of the Astra, who arrested the climb of their aircraft and then descended to FL185.

The Astra crew did not select the radio failure code of the aircraft's secondary surveillance radar transponder. The investigation did not establish why the crew did not change the transponder code.

Occurrence summary

Investigation number 199905463
Occurrence date 15/11/1999
Location 185 km E Williamtown, (NDB)
State New South Wales
Report release date 11/08/2000
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Separation issue
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer De Havilland Canada/De Havilland Aircraft of Canada
Model DHC-8
Registration VH-TQG
Serial number 430
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Lord Howe Island
Destination Sydney, NSW
Damage Nil

Aircraft details

Manufacturer Israel Aircraft Industries Ltd
Model 1125
Registration VH-FIS
Serial number 045
Sector Jet
Operation type Aerial Work
Departure point Williamtown, NSW
Destination Williamtown, NSW
Damage Nil

Piper PA-28-140, VH-CNM, on 3 September 1999

Summary

The crew of a SAAB, conducting a scheduled passenger service from Griffith to Sydney, broadcast that they were taxiing to depart from runway 06. The pilot of a Cherokee advised that he was on downwind for runway 36. The crew acknowledged this transmission and then established the position and intentions of the pilot of a Dromader who was on an extended downwind leg for a low-level approach to runway 06. The crew of the SAAB then advised that they were entering and backtracking on runway 06. Approximately 90 seconds later, when the crew advised they were rolling on runway 06, the pilot of the Cherokee responded that he was on late finals to runway 36. The crew continued their take-off and overflew the landing Cherokee by a reported 400 feet.

Each aircraft was in radio communication on the Griffith common traffic advisory frequency of 126.7 MHz.

The crew of the SAAB later reported that they had not heard the pilot of the Cherokee respond to their taxiing broadcast. Their attention had been directed toward the pilot of the Dromader who had adjusted his approach to assist their departure. They had not seen the Cherokee and consequently it was not until the pilot reported on late finals to runway 36 that they realised there was a traffic conflict. The crew reported that at this time the SAAB had accelerated to a speed such that rejecting the take-off was potentially more hazardous than continuing.

The higher terrain to the south of the aerodrome may have made the Cherokee more difficult to detect against the background. Additionally, a line of trees to the south of runway 06 obscured the final approach path to runway 36 from the view of pilots at the 06 threshold.

The reason why the crew of the SAAB did not recall hearing the response of the Cherokee pilot to their taxiing report was not determined. However, it is likely that the decision to expedite their departure ahead of the arriving Dromader created a self-imposed high workload that led to a loss of awareness of the Cherokee.

Occurrence summary

Investigation number 199904284
Occurrence date 03/09/1999
Location Griffith, Aero.
State New South Wales
Report release date 28/02/2000
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Separation issue
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Piper Aircraft Corp
Model PA-28
Registration VH-CNM
Serial number 28-7725045
Sector Piston
Operation type Flying Training
Departure point Griffith, NSW
Destination Griffith, NSW
Damage Nil

Aircraft details

Manufacturer Saab Aircraft Co.
Model 340
Registration VH-CMH
Serial number 327
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Griffith, NSW
Destination Unknown
Damage Nil

Fokker B.V. F27 MK 50 , 20107, VH-FNB, 130 km south of Carnarvon (VOR), Western Australia, on 6 August 1999

Safety Action

The key factors involved with this incident are common to other incidents investigated by the Bureau and which were the subject of safety recommendation R19990220 issued by the Australian Transport Safety Bureau (formerly BASI) to Airservices Australia on 19 January 2000.

Local safety action by Airservices Australia

Airservices Australia advised the ATSB that the existing flight service operations will continue until early 2001 when the national program of incorporating directed traffic information into TAAATS will be completed. Airservices is aware of the need to be vigilant in the management of this change process.

Analysis

FNB should have been reported as potential traffic to the crew of FNA since its track was planned to be within 15 NM laterally of FNA's route and because it was climbing through FNA's level.

The flight service officer reported that he would have normally passed traffic information to the pilots when FNB taxied at Carnarvon. However, on this occasion, he did not recognise that the two aircraft were potentially conflicting traffic. Having calculated a release time of 0225 when he expected FNB to be above FL200, in controlled airspace and therefore clear of FNA, he may have assumed that the traffic had no potential for conflict. An indication of his assumption was that he filed the flight strip for FNB soon after the release time; therefore, the potential for conflict of these two aircraft was never recognised by the flight service officer.

The flight service officer did not have a history of inadequately passing appropriate traffic information although he had, on occasion, used inappropriate air traffic control procedures.

The incident probably occurred as a result of a combination of factors. Firstly, the flight service officer reported that he was pre-occupied with his personal situation and was tired. As a result, he probably did not adequately monitor the progress of his routine actions. Secondly, he reported that he might have used a presumed rate of climb for the Fokker 50 as a basis for determining whether the traffic was potentially conflicting. Such a calculation was erroneous and irrelevant because the traffic assessment criteria in the Manual of Air Traffic Services required the traffic information to be passed. The use of this calculation may have been a manifestation of the flight service officer's occasional use of inappropriate procedures. His pre-occupation, tiredness and deviation from standard operating procedures may have contributed to the flight service officer losing situational awareness and as a result, he did not recognise that the flight paths of FNB and FNA were potentially conflicting.

Once the flight service officer had committed to not advising the crews of FNB and FNA of each other's presence, there were no organisational defences available, such as active supervision, to preclude the mistake going unnoticed. As a result, once the flight service officer had made the error, there was no backup.

Because the pilot in command of FNB did not need to take any avoiding action, it is unlikely that the provision of TCAS stopped an accident from occurring. However, the fact that TCAS had alerted the crew of FNB to the close proximity of traffic unknown to them indicated that it would have been the only defence available had the two aircraft been on a collision course. The effectiveness of TCAS in alerting and directing the crew of FNB to proximal traffic also illustrated the weakness of the principle of see-and-avoid.

CONCLUSION

The flight service officer was fatigued and distracted, probably as a result of stress and inadequate rest before commencing his shift. Consequently, he did not adequately monitor the progress of his routine actions and he did not notice that the two aircraft were potentially conflicting traffic. He did not provide traffic information to the pilots of the two aircraft as required by Manual of Air Traffic Services.

Summary

Sequence of events

At 0208 coordinated universal time (UTC) VH-FNB, a Fokker 50, departed Carnarvon for Perth southbound via air route B469 and was climbing to FL210. The two-way air route was a direct track between Carnarvon and Geraldton . VH-FNA, also a Fokker 50, had departed Geraldton for Learmonth and was tracking via the B469 northbound. The crew of FNA had reported to Perth Flight Service at 0201 that the aircraft was on descent to FL180 from FL200. At 0213, they reported at position HAMEL and were estimating overhead Carnarvon at 0246. HAMEL was a reporting point located 120 NM south-south-east of Carnarvon. FNB's estimated time of arrival at HAMEL was 0242.

About 65 NM south-south-east of Carnarvon and approaching FL180, the co-pilot of FNB glanced down at the traffic alert and collision avoidance system (TCAS) display and noticed a return in the 11-o'clock position at about 7 NM at the same level. The pilot in command of FNB, aware that FNA was likely to be in the area, communicated with the crew of FNA and requested their position. At 0226, as the pilot in command of FNA replied, the pilot in command of FNB saw FNA pass approximately 400 ft below his aircraft on a reciprocal track. FNA was not fitted with a TCAS and the crew of FNA did not see FNB. Flight service had not directed traffic information to either crew.

Flight Service procedures

Both aircraft were outside controlled airspace and operating in a directed traffic information environment in which air traffic control does not provide positive separation between air traffic. However, flight service was required to provide aircraft operating under instrument flight rules information on other possibly conflicting military or instrument flight rule traffic. The requirements and parameters for issuing traffic advice by flight service are in the Manual of Air Traffic Services. The procedures in the manual required the flight service officer to provide traffic information to the crews of both FNA and FNB about each other's flight routes because both aircraft were going to be within 15 NM of each other laterally and FNB was climbing through FNA's level.

When aircraft are planned to depart non-controlled airspace and enter controlled airspace, the flight service officer calculates a release time, which is the time at which the flight service officer expects the pilot of the aircraft to be communicating with air traffic control. When air traffic control receives notification from flight service that an aircraft will be entering controlled airspace, the controller calculates a time of acceptance when the aircraft is expected to be on frequency. Neither the release nor acceptance times are coordinated between flight service and air traffic control.

Flight Service Officer actions

The flight service officer was managing the combined sectors of Flight Service 1 and 8 at the time of the incident. Flight service team leaders were responsible for the administration of shifts. They did not provide active supervision of flight service officers at their work positions.

At the time of the incident, the flight service officer was responsible for monitoring 13 VHF and 8 HF frequencies, and 15 aircraft. Of the 15 aircraft, approximately 10 were active and the remainder were pending. Consequently, the flight service officer and his supervisor reported that the workload was considered light to moderate.

The flight service officer reported that he had assessed that after departure it would take FNB 15 minutes to climb through FL200 into controlled airspace. He therefore calculated that FNB would be in controlled airspace at about 0223 and he rounded up his expected release time to 0225. Air traffic control reported that they added a standard 15 minutes to the departure time advised unless the aircraft was known to have a low performance climb, such as the Fokker 50. In this case, 20 minutes was added. Therefore, the expected on-frequency time for FNB would have been 0228 and in accordance with standard practice, communications checks would have commenced by 0231.

The flight service officer reported that he would have normally passed traffic information to the pilots of both aircraft when FNB taxied at Carnarvon. The flight service officer was unable to explain why he did not believe the two aircraft were potentially conflicting. Following the incident, the flight service officer reported that he thought the Fokker 50 would have climbed at about 1,500 ft/min, a figure he reportedly derived from a previous conversation with one of the operator's pilots. Advice from the operator indicated that it was highly unlikely that a Fokker 50 could achieve such a rate-of-climb, particularly at the flight levels at which FNB was operating. The local flight service management reported that flight service did not advocate calculations based on rate of climb as a traffic assessment method.

The flight service officer reported that he filed the flight strip for FNB soon after the release time of 0225, believing the aircraft to be clear of non-controlled airspace.

Human factors

The flight service officer had received some air traffic control training and reported that he had previously used air traffic control techniques to determine whether traffic was in potential conflict. The use of air traffic control techniques was not required or advocated in flight service procedures. The flight service officer had passed a performance check the day before, when the checking officer noted him using some air traffic control procedures to decide what traffic information should be provided. The supervisor counselled him at the time not to use such procedures. The flight service officer reported that he had been using air traffic control techniques for some time to determine what information needed to be passed to aircraft operating outside controlled airspace in an attempt to reduce the amount of, what he considered, unnecessary radio calls. Although the flight service officer had used unapproved procedures in the past, he did not have any history of providing inadequate or inappropriate traffic information. During the investigation, it was reported that other flight service officers who had undergone some air traffic control training were also known to have applied air traffic control procedures in the flight service environment.

The flight service officer reported that Airservices Australia had managed his career within the previous 2 years in such a manner that caused him concern because there was substantial uncertainty related to his future employment. The flight service officer also reported that as a result of this uncertainty, he was facing significant personal issues and was probably pre-occupied by these issues when he started the shift on the day of the incident. He had approached his local management prior to the incident for leave and the request was being processed at the time of the incident.

The flight service officer reported that he was uncertain about his future employment and as a result of this uncertainty he had only a small amount of sleep the night before his shift and was feeling tired at the time of the incident. The flight service officer's immediate supervisor reported that he was unaware that the flight service officer may have been experiencing significant personal stress or that the flight service officer was fatigued when he commenced duty.

Traffic alert and collision avoidance system

Both aircraft belonged to the same operator. The operator was introducing TCAS as each aircraft underwent a major servicing. FNB was the only aircraft in the operator's fleet that had been fitted with TCAS and not all of the operator's pilots had been trained in the use of TCAS. The operator's policy was that unless both pilots in a crew were qualified to use TCAS, then the equipment was only to be used in the traffic advisory (TA) mode. A TA is indicated on the equipment display to the crew when the aircraft are within about 48 seconds of their closest passing, based on projections derived from current flight path and speed.

Occurrence summary

Investigation number 199903790
Occurrence date 06/08/1999
Location 130 km S Carnarvon, (VOR)
State Western Australia
Report release date 24/03/2000
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Separation issue
Occurrence class Incident
Highest injury level None

Aircraft details

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

Aircraft details

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

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

Safety Action

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

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

Analysis

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

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

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

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

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

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

Summary

Sequence of events

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

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

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

Witness information

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

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

Weather

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

Straight-in approach procedures

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

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

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

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

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

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

Aerodrome traffic

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

Occurrence summary

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

Aircraft details

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

Aircraft details

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

Beech Aircraft Corp 1900D, VH-IMH

Summary

The crews of all four aircraft had planned to use the same air route between Port Macquarie and Taree. VH-IMA and VH-TQO were arriving at Port Macquarie while VH-IMH and VH-SVV were departing. Due to minor deviations in track-keeping, all four aircraft were to the west of the nominal track.

Weather conditions were such that a layer of cloud existed upwards from approximately 7,000 ft.

Although the flight service officer provided a timely and up-to-date directed traffic information service to all crews, radio communications between the crews of IMA and IMH, and between IMH and SVV were insufficient to ensure self-separation between their aircraft. The high number of radio transmissions on the various frequencies, when combined with the frequency management requirements of each crew, limited the opportunities for adequate radio contact.

The crews of IMA and IMH maintained altitudes in Class "G" airspace without broadcasting their intentions on the flight service frequency. In addition, while both crews were maintaining a listening watch on the flight service frequency for 8 minutes prior to their aircraft passing, neither crew made radio contact with the other.

Analysis of the recorded radar data indicated that the aircraft passed within 1,000 m horizontally and 200 ft vertically while IMA was maintaining 8,000 ft.

None of the aircraft were fitted with an Airborne Collision Avoidance System (ACAS). An ACAS would, most probably, have improved the situational awareness of the crews to the extent that a more effective traffic management plan may have been undertaken.

The lack of adequate situational awareness of the crews of IMA and IMH resulted in two regular public transport aircraft coming into relatively close proximity without either crew carrying out a positive separation plan.

The investigation identified safety deficiencies in respect to timely conflict alerting and self-separation procedures and contains seven recommendations to the Civil Aviation Safety Authority addressing those deficiencies.

Occurrence summary

Investigation number 199901959
Occurrence date 28/04/1999
Location 37 km S Port Macquarie, Aero.
State New South Wales
Report release date 02/05/2001
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Separation issue
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Beech Aircraft Corp
Model 1900
Registration VH-IMH
Serial number UE-230
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Port Macquarie, NSW
Destination Williamtown, NSW
Damage Nil

Aircraft details

Manufacturer Beech Aircraft Corp
Model 1900
Registration VH-IMA
Serial number UE-7
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Sydney, NSW
Destination Port Macquarie, NSW
Damage Nil

Aircraft details

Manufacturer Piper Aircraft Corp
Model PA-31
Registration VH-SVV
Serial number 31-7405175
Sector Piston
Operation type Charter
Departure point Port Macquarie, NSW
Destination Sydney, NSW
Damage Nil

British Aerospace Plc 3107, VH-TQJ

Safety Action

As a result of this incident and other occurrences, the Bureau of Air Safety Investigation undertook a systemic investigation of the Class G airspace demonstration. That investigation was part of the Bureau's normal systems safety investigation role. The Bureau of Air Safety Investigation released interim recommendation IR980253 on 9 December 1998, which recommended that the Civil Aviation Safety Authority (CASA) terminate the demonstration. The demonstration was terminated on 13 December 1998 by CASA. This investigation supported the decision to terminate the demonstration.

Significant Factors

  1. The crew of the Jetstream did not hear the King Air crew's inbound broadcast on the mandatory broadcast zone frequency.
  2. The crew of the King Air did not hear the Jetstream crew's taxi broadcast on the mandatory broadcast zone frequency; nor did they hear the transmissions made on the Brisbane control frequency by the air traffic controller that provided essential traffic information regarding the Jetstream, and instructed them to maintain 6,000 ft.
  3. The air traffic controller had insufficient time to establish communications with both crews and provide them with sufficient information to enable them to take action to prevent a near collision.
  4. The crews had not been alerted to the presence of each other's aircraft.
  5. The procedures used in the Demonstration Class G Airspace Trial, which encompassed the Williamtown MBZ and MTA, did not fully consider the impact of radio congestion.

Analysis

The incident occurred because the crew of the King Air had not been alerted to the possibility of conflicting traffic and continued their descent for Williamtown in the Class G demonstration airspace. The crew had been alerted about another aircraft, a Beech 1900, which was to the north of Williamtown. The air traffic controller believed that the crew of the King Air had been alerted regarding the Jetstream. The controller assumed that he had heard a read back of the level requirement, when in all probability, the controller heard the "two in together" transmission. He also assumed that the King Air would stop descending and maintain 6,000ft. These assumptions were unfounded.

Analysis of the incident highlights problems involving radio communications, attentional focus, workload, and Class G Airspace training and procedures.

Radio communications

The crew of the King Air did not hear the taxi transmission broadcast by the Jetstream crew on the mandatory broadcast zone frequency; nor did they hear the transmissions made on the Brisbane control frequency by the air traffic controller that provided essential traffic information regarding the Jetstream and instructed them to maintain 6,000 ft.

When the crew of the Jetstream made their first "all stations" broadcasts on the national advisory frequency and the mandatory broadcast zone frequency, the King Air was in Class C airspace and its crew were communicating with air traffic control. The crew of the King Air had no reason to be on the national advisory frequency or the mandatory broadcast zone frequency and could not hear the Jetstream's transmissions.

The crew of the Jetstream reported that they were not aware that communication between themselves and the air traffic control agency could be established while on the ground at Williamtown. The establishment of such communication may have alerted the controller to the potential conflict between the two aircraft much earlier than was the case.

Attentional focus

Throughout the sequence of events for this particular occurrence, when monitoring more than one frequency, the crews had to decide upon which frequency to maintain their primary focus in the face of competing cognitive demands.

The crew of the King Air selected and monitored the mandatory broadcast zone frequency at approximately 31 NM south-west of Williamtown, when the aircraft was passing approximately FL 150. This was entirely reasonable, and accorded with the requirements of AIP. (Annex B to AIP Supplement H48/98, paragraph 5.1, and AIP Supplement H66/98 required crews to monitor the mandatory broadcast zone frequency when below the 8,500 ft upper limit of the mandatory transponder area, except when receiving a radar information service.) However, the focus of the crew's attention would have been centred on the transmissions made on the Brisbane Control frequency.

When the crew of the King Air were cleared by Brisbane to leave the control area on descent, their attention would have been focussed on receiving their clearance and providing an accurate readback to air traffic control. Their focus would not have been on monitoring the mandatory broadcast zone frequency. Accordingly, the crew of the King Air did not hear the Jetstream's departure report, which was being broadcast on the mandatory broadcast zone frequency at that time. Moreover, the Brisbane controller's transmission on the control frequency of 126.9 MHz was the only transmission that linked the King Air with the Williamtown mandatory broadcast zone.

The crew of the Jetstream were broadcasting their departure report on the mandatory broadcast zone frequency using their VHF 1 radio. Their attention would have been focussed on their transmission and on handling the aircraft. They had the Brisbane Control frequency of 126.9 MHz selected on their VHF 2 radio, but their focus would have been on their transmission on the mandatory broadcast zone frequency on VHF 1. The crew of the Jetstream did not hear the transmission that "linked" the King Air with the Williamtown mandatory broadcast zone. Such a link may have assisted the crew of the Jetstream to develop a better mental model of the air traffic situation.

Although the crew of the Jetstream were monitoring the Brisbane Control frequency of 126.9 MHz for over 4 minutes prior to their departure from Williamtown, insufficient information was broadcast on that frequency for the crew to develop an accurate picture of the air traffic situation. Notwithstanding the monitoring of the control frequency, the crew's attentional focus during their taxi and departure would have been on any transmissions made on the mandatory broadcast zone frequency.

When the King Air crew confirmed that they were still on the control frequency, the controller gave them traffic information on a Beech 1900. The King Air was passing 8,700 ft on descent when this traffic information was received and focus of their attention was shifting towards the establishment of mutual separation with other aircraft in the mandatory broadcast zone.

The crew of the Jetstream reported their position to Brisbane Centre passing 4,000 ft on climb. During the period of the Jetstream's transmission, the crew of the King Air was making an "all stations" broadcast on the Williamtown MBZ frequency. The crew of the Jetstream did not hear this broadcast because their attention was focussed upon making their report, and reading back the clearance. The crew of the King Air did not hear the Jetstream's transmission because they were concentrating on arranging mutual separation in the mandatory broadcast zone with the Beech 1900.

Weather

The meteorological area forecast for Williamtown and the trend type forecast were not favourable and indicated that an instrument approach would be necessary for aircraft inbound to Williamtown. The actual weather was consistent with the forecast.

Class G airspace

Contributing to the incident was the confusion on the part of aircrew concerning the requirements of the Demonstration Class G Airspace trial. Also contributing, was the fact that the design of the Class G procedures encompassing the Williamtown mandatory broadcast zone and mandatory transponder area did not fully consider the impact of radio congestion.

During the Class G airspace trial, there was some confusion within the aviation community regarding the termination of radar services. The Civil Aviation Safety Authority reviewed the first fortnight of the trial and as a result clarified some of the procedures in "Aiming Higher", vol. 1 no. 8, October-November 1998. In the section "Termination of radar services by Air Traffic Control (ATC)", the article explained that when an aircraft receiving a radar control service leaves controlled airspace and the radar service continued as a radar information service, ATC would advise "Control service terminated". Further, ATC would advise "Radar service terminated" when a radar information service was terminated.

The air traffic controller's transmissions reflected this aircrew confusion. Indeed, his workload was increased because of deficiencies in the education program provided to the aviation community prior to the introduction of the Demonstration Class G airspace. Also, although the crew of the King Air complied with all of the provisions of the AIP, they did not fully understand the procedures to be used when operating in the Demonstration Class G airspace.

The design of the procedures used in the Demonstration Class G airspace did not fully consider the impact of radio congestion. Even though the controller attempted to separate the two aircraft, he was not required to do so in Class G airspace.

Summary

The crew of British Aerospace Jetstream 31, VH-TQJ, had flight-planned from Williamtown to Sydney via Mt McQuoid at flight level (FL) 120. The crew of Beechcraft Super King Air B200, VH-KCH, had flight-planned from East Sale, to Williamtown via Mt McQuoid at FL 250. Both aircraft were equipped with dual very high frequency (VHF) radios and Mode C transponders, which were operating at the time. A transponder is a radio device which, when triggered by a secondary surveillance radar signal, transmits a response that provides, when selected to mode C, altitude and positional data on a radar display for air traffic controller reference.

The routes flown by the two aircraft were within the Class G demonstration airspace detailed in the Aeronautical Information Publication (AIP) Supplement H66/98 of 5 November 1998. The route segment from Williamtown to Mt McQuoid included airspace inside the mandatory broadcast zone for the Williamtown control zone up to and including 5,000 ft. It also included the mandatory transponder area from 5,000 ft to 8,500 ft for a radius of 30 NM centred on Williamtown, and Class C airspace above 8,500 ft to the south-west. The crew of the King Air were descending on air traffic services route Whisky 170 (W170) on track from Mt McQuoid to Williamtown. W170 was a low-level two-way route. The crew of the Jetstream tracked to intercept W170 to Mt McQuoid after departing from Williamtown and were on climb.

Williamtown was listed in paragraph 4.3 of AIP Supplement H66/98, which required aircraft not receiving a radar information service to "monitor and, when required, use the frequency specified", which was 118.3 Megahertz (MHz), the Williamtown mandatory broadcast zone frequency when inside the Williamtown mandatory transponder area. The crews of both aircraft attempted to monitor and use the mandatory broadcast zone frequency while they were inside the mandatory transponder area.

The meteorological area forecast for Williamtown issued at 1800 Eastern Summer Time (ESuT) was for 3 octas of stratus at 1,000 ft, 6 octas of cumulus at 1,800 ft and 6 octas of stratocumulus at 2,500 ft. The trend type forecast included moderate turbulence below 5,000 ft from 1800 to 1900 ESuT, and from 1900 to 2100 ESuT the visibility was expected to reduce to 4,000 m in drizzle with broken cloud at 1,000 ft. The reported weather was a varied cloud base from 1,200 ft to 1,600 ft, with the tops 4,000 ft to 5,000 ft. A higher level cumulo-nimbus cloud cell was reported to the west of Williamtown.

While taxiing at Williamtown, the crew of the Jetstream made "all stations" broadcasts on the national advisory frequency and the mandatory broadcast zone frequency. The crew of the King Air did not hear these transmissions because they had not selected or transferred to those frequencies at that time, nor were they required to. The King Air was established in Class C airspace and the crew was communicating with the air traffic controller located in the Brisbane Area Control Centre.

The crew of the King Air selected and monitored the mandatory broadcast zone frequency at approximately 31 NM south-west of Williamtown, when the aircraft was passing approximately FL 150. AIP Supplement H66/98 required crews to monitor the mandatory broadcast zone frequency when below 8,500 ft, the upper limit of the mandatory transponder area, except when receiving a radar information service.

At 18:45.41, the crew of the King Air was cleared by Brisbane Centre to leave control area on descent, was given the area QNH, and informed that control services would terminate passing 8,500 ft. They were also advised that Williamtown was operating on mandatory broadcast zone procedures. The crew acknowledged this transmission. During this period, the crew of the Jetstream broadcast their departure on the mandatory broadcast zone frequency on their VHF 1 radio. On their VHF 2 radio, they had the Brisbane Control frequency of 126.9 MHz, selected, which they had been monitoring, together with the MBZ frequency, for four minutes prior to departure. The crew of the King Air reported that they did not hear the Jetstream's departure broadcast.

At 18:46.41, the controller asked if the crew of the King Air was still on the control frequency, and then provided the crew with traffic information regarding a Beech 1900 inbound to Williamtown from the north that was descending through 6,000 ft. The crew of the King Air acknowledged the traffic information. The King Air was passing 8,700 ft on descent when the traffic information was passed.

At 18:47.01, the controller attempted to provide the crew of the King Air with additional information about unidentified traffic (the Jetstream), 3 NM south-west of Williamtown. The transmission was over-transmitted by another aircraft and was unreadable. The crew of the King Air heard only the last few words of the transmission, and did not consider it relevant to their flight. The King Air was passing 8,500ft, which meant that it was leaving Class C controlled airspace and entering the Williamtown mandatory transponder area in the Class G demonstration airspace. During the high workload at that period of the flight, the crew was preparing for an instrument arrival into Williamtown due to the weather conditions. The controller did not follow up this "unacknowledged" transmission, because the crew of the Jetstream reported on the control frequency, its reported position identifying it as the previously unidentified traffic.

The mandatory broadcast zone at Williamtown was established in Class G (uncontrolled airspace). While within the mandatory broadcast zone, pilots were required to maintain a continuous listening watch on the mandatory broadcast zone frequency. They could arrange mutual separation within the mandatory broadcast zone. The frequency was not normally monitored by air traffic services. Pilots of IFR aircraft were required to report "Changing to Williamtown mandatory broadcast zone 118.3 MHz" when they were inbound to the Williamtown mandatory broadcast zone area.

At 18:47.24, the crew of the Jetstream reported their position to Brisbane Centre and that they were passing 4,000 ft on climb. The controller instructed the crew to squawk (transponder) ident, to squawk code 1201, and to maintain 5,000 ft due to inbound traffic. The squawk code and altitude restriction were read back correctly by the Jetstream crew, although the crew then inadvertently selected the wrong code of 1207. During the period of the Jetstream's transmission, the crew of the King Air was making an "all stations" broadcast on the Williamtown mandatory broadcast zone frequency. The Jetstream crew reported that they did not hear the broadcast.

At 18:47.56, the controller again attempted to provide traffic information about the Jetstream to the crew of the King Air, together with an instruction to maintain 6,000 ft. That transmission was over-transmitted by another aircraft and was not heard by the King Air crew. The over-transmission was confirmed by the crew of the Jetstream, who transmitted "two in together". The controller reported that he was "95% sure" that the King Air crew had read back "maintain 6,000 ft", which was not supported by analysis of recorded audio data. The transmission "two in together" was recorded. At the time of the controller's transmission, the Beech 1900 crew initiated communication with the King Air crew on the mandatory broadcast zone frequency and between them they subsequently arranged mutual separation.

Occurrence summary

Investigation number 199805078
Occurrence date 16/11/1998
Location 11 km SW Williamtown, Aero.
State New South Wales
Report release date 13/12/1999
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Separation issue
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer British Aerospace
Model 3100
Registration VH-TQJ
Serial number 703
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Williamtown, NSW
Destination Sydney, NSW
Damage Nil

Aircraft details

Manufacturer Beech Aircraft Corp
Model 200
Registration VH-KCH
Serial number BB-1125
Sector Turboprop
Operation type Military
Departure point East Sale, VIC
Destination Williamtown, NSW
Damage Nil

Boeing 767-238, VH-EAL

Safety Action

As a result of this and other occurrences, the Bureau of Air Safety Investigation is investigating two perceived safety deficiencies. The first 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 and aircraft are on an active runway. The second relates to the inappropriate use of paragraph 29 of the Manual of Air Traffic Services 6-2-3 by aerodrome controllers.

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

Significant Factors

  1. A conditional clearance authorising the surface movement controller to clear CZH to cross runway 34 was issued to the surface movement controller by the aerodrome controller.
  2. The aerodrome controller's training officer was not aware that a conditional clearance was active when he instructed the aerodrome controller to clear EAL for take off.
  3. There was no tactile memory marker alerting the controllers that an aircraft had been cleared to cross an active runway.
  4. The aerodrome controller did not scan runway 34 before issuing the take-off clearance.
  5. Neither the aerodrome controller nor the training officer cancelled EAL's take-off clearance when they became aware that CZH was crossing runway 34.

Analysis

The investigation revealed that the local practice for issuing a conditional clearance for a taxiing aircraft to cross an active runway might have been deficient. When a taxiing aircraft needed to cross an active runway, coordination was required between the surface movement controller and the aerodrome controller. If traffic conditions permitted, it may have been possible to issue the taxiing aircraft with an immediate clearance to cross the active runway. However, at other times, a taxiing aircraft may have been issued with a conditional clearance, authorising it, for example to cross the active runway after a landing aircraft had vacated the runway.

When a conditional crossing clearance had been issued, the continued safe operation of the system was dependent on both the surface movement controller and the aerodrome controller remembering that this traffic coordination had been arranged and was still pending. Interviews with controllers and observation of current work practices indicated that the coordination between the surface movement controller and the aerodrome controller for conditional clearances was verbal only. Neither controller used any form of memory aid to record the fact that a conditional clearance had been issued and was still pending. In this occurrence, this led the aerodrome controller, at a time of high workload and possible stress, to forget that a conditional crossing clearance was pending.

In addition, the training officer was not aware that a clearance had been coordinated between the surface movement controller and the aerodrome controller. Because the system did not provide any physical record that a conditional clearance was pending, there was no cue to alert the training officer to the fact that this was the case.

The use of memory markers recording actions by annotation or other means, assists controllers in remembering vital operational information in two ways. Firstly, the associated actions that the controller carries out in setting the memory marker assist in the consolidation of a strong memory trace. Secondly, the marker can be checked at any time by the controllers if they are uncertain of the current status of the item or condition that it refers to.

Summary

After landing on runway 27 at Melbourne during land and hold short operations, VH-CZH, a Boeing 737, vacated the runway via the parallel taxiway Echo which crossed runway 34 at a distance of 2,333 m from the threshold. The surface movement controller instructed the crew to hold short of runway 34 because VH-OGK, a Boeing 767, was landing.

VH-EAL, a Boeing 767, was taxiing for a runway 34 intersection departure at taxiway Juliet, 773 m from the runway 34 threshold. The co-pilot was the flying pilot. OGK had just landed on runway 34 and was vacating at the high-speed taxiway Foxtrot, 1,588 m from the runway 34 threshold. The aerodrome controller instructed the crew of EAL to line up and wait.

EAL's crew had noted VH-NKN, a Beech 1900, on final approach for runway 27. When OGK was clear of runway 34, the aerodrome controller cleared EAL for an immediate take-off. NKN was on a practice instrument landing system approach to runway 27 and was approximately at the outer marker. The aerodrome controller requested the crew of NKN to reduce to minimum approach speed.

The pilot in command of CZH reported that he saw OGK vacate runway 34 at taxiway Foxtrot and then received a clearance to cross runway 34. As CZH began to cross the runway, the crew observed EAL lining up with its landing lights on. At about one-half to two-thirds of the way across runway 34, the co-pilot of CZH commented to the pilot in command that it looked like EAL had started to roll for take-off. The pilot in command confirmed this and both pilots monitored EAL's progress. The forward section of CZH was well clear of the runway but the rear section was believed to be obstructing the runway when the crew noticed that EAL's take-off had been rejected. Both pilots observed the spoilers of the B767 extend.

At the time EAL was cleared for immediate take-off, its crew was not aware that CZH was crossing 34 at taxiway Echo. As they started to roll, the pilot in command saw that CZH had crossed about two-thirds of the width of the runway and estimated it would be well clear and so continued with the take-off. When the aircraft was at about 90 kts, the pilot-in-command heard the instruction "stop immediately" transmitted twice, took control from the co-pilot, applied reverse thrust and slowed the aircraft before exiting runway 34 at taxiway Foxtrot.

The controllers

The aerodrome controller was undergoing re-familiarisation training under the supervision of a rated training officer. Both controllers had extensive aerodrome control experience. The surface movement controller had worked at Melbourne tower since April 1998 and was a rated surface movement controller. He was not trained in aerodrome control at Melbourne.

The traffic management plan and outcome

The aerodrome controller had planned for CZH to cross runway 34 after OGK had turned to exit runway 34 via taxiway Foxtrot. A conditional clearance was issued to the surface movement controller to this effect. The conditional clearance was "after Qantas 33 has vacated the runway, cross runway 34", which was acknowledged by the surface movement controller. The training officer said that he was not aware of the interchange. The aerodrome controller's plan, which was endorsed by the training officer was to hold EAL in the lined-up position on runway 34 while CZH crossed the runway and while NKN landed on runway 27.

Although the training officer had endorsed the plan, the speed of NKN on final for runway 27 was erratic and as a result, his mental model changed. He perceived that there was an opportunity for EAL to take off before NKN landed. The training officer considered that the new plan was desirable because another aircraft was on long final for runway 34 and there was a possibility that it would have to go-around behind, or over EAL. The training officer reported that he did not think that the aerodrome controller had noticed the performance of NKN on final, which meant that the opportunity for it to land and the plan to work was diminishing.

The training officer conveyed the new plan to the aerodrome controller, who then cleared EAL for an immediate take-off. The aerodrome controller scanned the runway and noticed CZH crossing at taxiway Echo. The training officer reported that he was not aware that CZH had been cleared to cross runway 34 until after the take-off clearance was issued to the crew of EAL. The controllers both reported that they did not immediately cancel the take-off clearance issued to EAL because they assessed that CZH would be clear of the runway before EAL commenced the take-off roll. The rationale for this decision was based on their interpretation of Chapter 6 of the Manual of Air Traffic Services.

The aerodrome controller monitored the position of NKN, which was "getting close". He did not feel comfortable with the developing situation and instructed EAL to cancel departure. This transmission was made 21 seconds after clearing EAL to take-off. EAL started to roll and the aerodrome controller transmitted "EAL, stop immediately". When EAL continued to accelerate, the aerodrome controller transmitted again "EAL, stop immediately, stop immediately." The crew acknowledged this transmission, applied reverse thrust and slowed before exiting the runway at taxiway Foxtrot. The controllers both reported that the motivator for the cancellation of the take-off clearance was the potential for EAL to conflict with NKN on final to runway 27, rather than the potential for EAL to conflict with CZH, which was crossing on runway 34.

ATS procedures

The Manual of Air Traffic Services includes instructions for the control of departing and arriving aircraft within the traffic circuit and on the movement area of an aerodrome. Chapters 6 and 12 were relevant to this occurrence scenario.

Occurrence summary

Investigation number 199803972
Occurrence date 23/09/1998
Location Melbourne, Aero.
State Victoria
Report release date 10/12/1999
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Separation issue
Occurrence class Incident
Highest injury level None

Aircraft details

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

Aircraft details

Manufacturer The Boeing Company
Model 737
Registration VH-CZH
Serial number 23660
Sector Jet
Operation type Air Transport High Capacity
Departure point Adelaide, SA
Destination Melbourne, VIC
Damage Nil

Beech Aircraft Corp B200C, VH-AMB

Safety Action

As a result of this and other occurrences, together with a systemic investigation of the Class G Airspace demonstration, the Bureau of Air Safety Investigation issued interim recommendation IR980253 to the Civil Aviation Safety Authority on 8 December 1998:

"The Bureau of Air Safety Investigation believes that the Class G Airspace Demonstration has served its purpose. In the light of the safety concerns identified by this investigation, BASI recommends that the Civil Aviation Safety Authority should now terminate the demonstration. The results of the demonstration should be subject to a comprehensive evaluation that specifically addresses the safety concerns identified by BASI.

The evaluation process should take into account the time required to:

  1. review and analyse the demonstration;
  2. refine the model where required and conduct a proper safety analysis; and
  3. provide a comprehensive and effective education and training program for any subsequent changes to Class G Airspace.

If this is not achieved, the deficiencies identified in this investigation are likely to be repeated, thereby seriously compromising the successful introduction of future changes to airspace including reintroduction of Class G Airspace incorporating Radar Information Service and National Advisory Frequency".

The Bureau of Air Safety Investigation simultaneously issued the following related interim recommendations to the Civil Aviation Safety Authority:

"IR980260

The Bureau of Air Safety Investigation recommends that the Civil Aviation Safety Authority review program management policies and procedures for current and proposed changes to the aviation system, in the light of experience gained from the present Class G Airspace Demonstration.

IR980261

The Bureau of Air Safety Investigation recommends that the Civil Aviation Safety Authority, the Department of Transport and Regional Services and Airservices Australia review and clarify the roles and responsibilities of the respective organisations in relation to the regulation, design and management of airspace to ensure the safety integrity of the aviation system".

The Bureau of Air Safety Investigation simultaneously issued IR980261 to the Department of Transport and Regional Services and Airservices Australia as IR980256 and IR980257 respectively.

Subsequently, the Minister for Transport and Regional Services announced in Parliament on 9 December 1998 that the demonstration would cease on 13 December 1998.

Significant Factors

  1. The Beech pilot and the Saab crew did not hear the taxi or departure transmissions from each other on the MBZ frequency.
  2. The air traffic control radar was unable to detect aircraft at an altitude that would have enabled the controller to provide pilots with timely traffic information.

Analysis

The pilots of both aircraft were reliant on mandatory radio broadcasts to gain an awareness of other traffic operating within the confines of the MBZ. It is possible that they had simultaneously broadcast their respective taxi reports, thus blocking each other's transmissions. However, it is more likely that radio transmissions were inhibited by terrain shielding, resulting in neither crew being aware of the other aircraft while they taxied and departed. The demonstration procedures created a situation where pilots had one opportunity to become aware of other traffic. If they missed an MBZ broadcast, there was no other formal procedure to provide that information.

If a directed traffic information service had been in place at the time of this occurrence, a potential confliction would have been recognised by a third party. Traffic information would have been provided to the Beech pilot and the Saab crew, even if the MBZ reporting procedures had failed. In the past, the directed traffic information service provided a level of redundancy to the aviation system that was not available during the Class G airspace demonstration.

The radar information service was limited by the inability of the radar to detect aircraft at relatively low altitudes in that area. Despite attempts to obtain a radar advisory service as soon as possible after departing Lismore, the Beech pilot was unable to obtain traffic information from the radar controller. Supplementation of the radar information service with a directed traffic information service in such an area of limited radar coverage, would have enhanced the situational awareness of the respective flight crews. Alternatively, the provision of radar coverage from ground level to the lower limit of controlled airspace, together with a radar information service for taxiing aircraft, would have also minimised the potential for confliction.

A conflict was ultimately avoided because the pilots were using the air traffic control frequency. This was despite the fact that both aircraft were still operating within the MBZ and monitoring the MBZ frequency.

Summary

A Beech 200 was conducting an instrument flight rules (IFR) flight from Lismore to Glen Innes. The pilot gave a departure report to the Brisbane Sector 2 radar controller, and reported climbing through 3,500 ft. The controller advised that there were no other aircraft observed on the radar display. That departure report was also heard by the crew of an IFR Saab SF-340 that had just departed Casino on a flight to Williamtown, via Point Lookout. The Saab was climbing through 2,700 ft when the crew became aware that both aircraft were approximately 5 NM south-west of Lismore. The Saab crew descended to 2,500 ft, in order to establish 1,000 ft vertical separation from the Beech. The Saab crew subsequently saw the Beech pass from left to right, about 1 NM in front of their aircraft, as the Beech climbed through patches of cloud just under the main cloud base of 4,000 ft. The Beech pilot also saw the Saab pass below his aircraft.

Due to their proximity to each other, Lismore, Ballina and Casino aerodromes were encompassed by a non-standard Mandatory Broadcast Zone (MBZ), and used a common radio frequency of 124.2 MHz. The MBZ was approximately 60 NM long and 30 NM wide, and extended from the ground to 5,000 ft above ground level. The intent of the common frequency was to enable pilots operating at any of those aerodromes to hear transmissions from other pilots, so that they could coordinate operations in order to minimise the risk of conflict. Pilots were required to monitor the MBZ frequency when operating within the MBZ. They were also required to broadcast flight details when inbound to, taxiing at, and departing from an aerodrome within the MBZ.

The pilots of both aircraft had made the required broadcasts; however, neither received a response from any other aircraft. While taxiing at Lismore, the Beech pilot had monitored a transmission on the MBZ frequency from another pilot, but disregarded it as that aircraft was operating in the Ballina area. A recording device was installed at Lismore aerodrome to monitor aircraft using that facility. The majority of recorded transmissions from aircraft operating at Lismore were clear. Transmissions recorded from aircraft operating at Ballina and Casino were generally clipped or garbled, and more difficult to understand. The Saab crew later reported that pilots of aircraft on the ground at Lismore were unlikely to hear radio transmissions from aircraft on the ground at Casino, and vice versa.

At the time of the occurrence, both aircraft were operating in non-controlled Class G demonstration airspace. As part of that demonstration, modified procedures had been introduced, including the removal of the directed traffic information service previously provided by flight service, and the introduction of a radar information service provided by air traffic control. The provision of that service to pilots was dependent upon their aircraft being radar-identified. The secondary surveillance radar code from the Beech was not detected by the air traffic control radar system until it had climbed through an altitude of 3,300 ft. The Saab was not detected until it had climbed through approximately 3,000 ft.

Prior to the commencement of the demonstration, pilots of IFR aircraft were provided with traffic information on other IFR aircraft, in accordance with guidelines detailed in the Manual of Air Traffic Services and the Aeronautical Information Publication. Pilots operating an IFR flight from a non-controlled aerodrome were required to contact flight service by radio when taxiing. A flight service officer would then provide traffic information to pilots of conflicting aircraft that were not on the MBZ frequency. Based on that procedure, the Saab crew and Beech pilot would not have been provided with mutual traffic information, as they were both operating on the MBZ frequency at about the same time. However, traffic information was required to be passed to pilots of IFR aircraft climbing or descending through the level of another conflicting IFR aircraft. The overriding intent of the traffic information service was to issue such information if there was any doubt regarding the possibility of a confliction.

The Beech pilot had requested radar service information from air traffic control while taxiing at Lismore. The controller issued the pilot with a secondary surveillance code for the flight and advised that a radar information service would be provided when the aircraft was identified on radar, and that there were no other aircraft observed in the area.

Both aircraft were fitted with dual very high frequency (VHF) radio transmitters and receivers. The pilots were monitoring the MBZ frequency on one receiver while also monitoring the air traffic control frequency on the second receiver, in preparation for requesting a clearance to enter Class E controlled airspace at 8,500 ft. The Beech pilot stated that he normally would not have monitored the air traffic control frequency until passing 4,000 ft, but decided to contact the controller early to request the radar information service. Prior to the commencement of the demonstration period, pilots would normally have simultaneously monitored the MBZ and flight service area frequencies to assist in maintaining their situational awareness during the departure phase.

Occurrence summary

Investigation number 199804984
Occurrence date 10/11/1998
Location 9 km SW Lismore, (NDB)
State New South Wales
Report release date 22/07/1999
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Separation issue
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Beech Aircraft Corp
Model 200
Registration VH-AMB
Serial number BL-131
Sector Turboprop
Operation type Aerial Work
Departure point Lismmore, NSW
Destination Glen Innes, NSW
Damage Nil

Aircraft details

Manufacturer Saab Aircraft Co.
Model 340
Registration VH-SBA
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Casino, NSW
Destination Williamtown, NSW
Damage Nil