Loss of separation

Loss of separation between a Boeing 747-400, 9V-SPE and a Boeing 747-400, GC-IVC, on 16 June 2004

Safety Action

Airservices Australia safety action

Airservices Australia included the following modification to the Brisbane Centre local instructions applicable to international HF radio operators:

Relay of communications between ATC and pilots, or between pilots and ATC must be completed within 5 (five) minutes of the message being passed to the AusFIC for relay. Any communications relayed to and from ATC must be passed verbatim.

In the event that a message cannot be relayed within the 5 minutes advice must be provided to the appropriate ATC sector.

Analysis

Communications

The reason the HF operator was unable to establish two-way communication with the crew of IVC could not be determined. A formal procedure for notifying the controller that the HF radio operator could not pass the instruction to the crew of IVC may not have ensured that a separation standard existed, as an incorrect instruction had been issued. However, it may have prompted a more timely reassessment of the situation by the controller. In other circumstances, a formal procedure may alert the controller in sufficient time for action to be taken before separation standards are infringed.

Air Traffic Controller

A review of the controller's training records indicated that he had an adequate understanding of the concept of lateral separation. However, his misapplication of a lateral separation point may have reflected his lack of proficiency due to inexperience in working the particular sector of airspace.

Summary

On 16 June 2004, a Boeing 747-400, registered GC-IVC (IVC), was en-route from Melbourne to Singapore on airway A576. The aircraft was approaching the boundary between the Brisbane flight information region (FIR) and the Bali FIR at flight level (FL) 340. Concurrently, a second 747, registered 9V-SPE (SPE), was en-route from Sydney to Singapore on airway G326. That aircraft was also approaching the boundary between the Brisbane FIR and the Bali FIR at FL 340.

The controller recognised that he had to resolve a potential confliction between SPE and a third aircraft. In resolving that confliction, the controller created a new confliction between IVC and SPE. In response, the controller instructed the crew of IVC to reach FL320 by waypoint ATMAP (see Annex A). That requirement was intended to achieve vertical separation between the aircraft prior to any loss of lateral separation1. However, the required lateral separation point was 94 NM south-east of waypoint ATMAP on airway A576. The incorrect requirement led to an infringement of separation standards.

Following a scan of the air situation display, the controller realised that he had issued an incorrect requirement. The controller then issued a second requirement, via the high frequency (HF) radio operator, for IVC to descend to reach FL320 by 80 NM to the south-east of waypoint ATMAP. The controller reported that this requirement was based on the application of a required navigation performance (RNP) 10 separation standard2. This standard was not authorised for use within the Bali FIR. Upon issuing the requirement, the controller handed over to another controller and went on a scheduled break.

Over a period of 10 minutes and 37 seconds, the HF radio operator made 12 unsuccessful attempts to contact the crew of IVC. The oncoming controller realised that the HF radio operator had not been able to make contact with the crew of IVC. He also realised that RNP 10 was not an authorised standard. By that time the authorised separation standards had already been infringed. The oncoming controller then successfully instructed the crew of IVC to descend their aircraft immediately to FL320, via a controller pilot data link communication3 (CPDLC) message to the crew of another aircraft.

The controller involved in this occurrence had completed his field training in April 2004. A review of his training records indicated that he had approximately five weeks' experience on that sector of airspace. According to his check and standardisation supervisor, the controller demonstrated a satisfactory level of competency on completion of his sector-specific training.

The controller was rostered to work an afternoon shift, which commenced at approximately 1500 eastern standard time. During the shift the controller had a break of one hour, returning to the console at approximately 1930. The incident occurred at 2038. There was no evidence that fatigue played a part in the incident.

Coordination of high frequency radio communications

The controller issued the requirement to the crew of IVC to reach FL320 by waypoint ATMAP while that aircraft was within reliable very high frequency (VHF) radio range. However, when the controller realised the error in the requirement, that aircraft had passed outside VHF radio range. The controller attempted to issue the amended requirement to the crew of IVC through a HF radio operator, because the crew of IVC had not nominated CPDLC on their flight plan as a means of communication with ATC.

The HF radio operator was unable to establish two-way communication with the crew of IVC, to pass the amended requirement, despite repeated attempts. The controller was not aware that the HF radio operator was unable to issue the instruction to the crew of IVC.

The controller did not confirm with the HF radio operator that the instruction had been passed to the crew of IVC, and there was no published procedure requiring him to do so. Although there was a requirement for the HF radio operator to notify the controller that the instruction was not passed to the crew of IVC, there was no formal procedure to facilitate that notification.

1 Lateral separation is considered to exist when there is at least a 1 NM buffer between the possible positions of two aircraft (ICAO PANS-ATM, Chapter 5 in CASA Manual of Standards Part 172 10.8.1.1).
2 For RNP10, the approval process must show that the total navigation system error in each dimension must not exceed +/- 10 NM for 95 per cent of the flight time on any portion of any single flight:
a) the true position of the aircraft must be within 10 NM of the programmed route centre line; and
b) the true distance to way-points must be within 10 NM of the displayed distance to waypoints.' (International Civil Aviation Organization, 1999, Manual on required navigation performance [RNP], second edition, p. 6).
3 Controller Pilot Data Link Communications (CPDLC): A means of communications between a controller and pilot using text-based messages via an ATC data link (Manual of Air Traffic Services, part 10, effective 10 June 2004).

Occurrence summary

Investigation number 200402228
Occurrence date 16/06/2004
Location 174 km SE Atmap, (IFR)
State International
Report release date 10/03/2005
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 9V-SPE
Sector Jet
Operation type Air Transport High Capacity
Departure point Sydney, NSW
Destination Singapore
Damage Nil

Aircraft details

Manufacturer The Boeing Company
Model 747
Registration GC-IVC
Sector Jet
Operation type Air Transport High Capacity
Departure point Melbourne, VIC
Destination Singapore
Damage Nil

Boeing 767-338ER, VH-OGB

Safety Action

In addition to the previous safety actions reported by the ATSB in occurrence report number 200402411, the operator of OGB has implemented the following procedures to be followed when its aircraft are operating in the Ujung Pandang FIR:

Offset tracks are to be flown during en-route phase of flight in all (radar and non-radar) airspace

Aircraft are to return to on track by the Indonesian FIR boundaries and for climb from, and descent to, airports.

Summary

On 22 March 2004, at about 0435 Coordinated Universal Time (UTC), a Boeing Company 767-338ER, registered VH-OGB, and a Boeing Company 767-319, registered ZK-NCF, were involved in a serious incident in the Ujung Pandang Flight Information Region (FIR).

OGB was southbound and NCF was northbound on air route B473, between waypoint OLENG and waypoint OPABA. The crew of OGB advised Ujung Control that they were at OLENG at 0423 and were level at flight level (FL) 350. The crew later reported that they requested approval from Ujung Control to climb their aircraft to FL370. Ujung Control subsequently approved that request. During that climb, and passing approximately FL355, the crew of OGB received a traffic advisory on their aircraft's traffic alert and collision avoidance system (TCAS), followed by a resolution advisory, about NCF. The resolution advisory instructed the crew of OGB to descend their aircraft. The crew complied with the resolution advisory and descended their aircraft to FL350. The crew later reported that, during the descent manoeuvre, they saw NCF pass 600 ft above their aircraft.

NCF was northbound on air route B473, between waypoint OLENG and waypoint OPABA and was level at FL360. The crew later reported that they received a TCAS resolution advisory on OGB, travelling in the opposite direction. The crew of NCF climbed their aircraft in response to the resolution advisory. The crew later reported that they observed OGB on their TCAS, pass 400 ft below them.

The Australian Transport Safety Bureau (ATSB) was advised of the serious incident and commenced an investigation. The crew of OGB was interviewed and data from that aircraft's quick access recorder was analysed. As the incident occurred within Indonesian territory, the Indonesian National Transportation Safety Committee (NTSC) had the responsibility to conduct an investigation in accordance with Annex 13 to the Convention on International Civil Aviation.

On 26 March 2004, the NTSC informed the ATSB that they had commenced an investigation into the incident and the ATSB appointed an accredited representative to that investigation. The NTSC, being the investigation agency of the country in which the incident occurred, will be preparing the report and has control over the public release of any investigation findings.

As a result of another occurrence within an Indonesian FIR, which involved aircraft from the same Australian operator, that operator implemented new procedures to be followed when its aircraft are operating in Indonesian FIRs (see ATSB occurrence report number 200402411).

The Bureau will publish the NTSC report, when released by the NTSC, on the ATSB website.

Occurrence summary

Investigation number 200401115
Occurrence date 22/03/2004
Location 130 km S Oleng, (IFR)
State International
Report release date 14/03/2005
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-OGB
Serial number 24316
Sector Jet
Operation type Air Transport High Capacity
Departure point Hong Kong
Destination Sydney, NSW
Damage Nil

Aircraft details

Manufacturer The Boeing Company
Model 767
Registration ZK-NCF
Sector Jet
Operation type Air Transport High Capacity
Departure point Auckland, NZ
Destination Hong Kong
Damage Nil

Fairchild SA227-AC, VH-SEF, Brisbane Airport, 9 October 2003

Summary

Preliminary investigation was undertaken into a category 4 occurrence involving a Metroliner aircraft and a Bell 47 helicopter at Brisbane Airport. The ATSB has terminated the investigation based on information from Airservices Australia, following that organisation's investigation into the circumstances of the occurrence.

Status: Downgraded the occurrence to category 5 and investigation discontinued.

Occurrence summary

Investigation number 200304220
Occurrence date 09/10/2003
Location Brisbane airport
Report release date 09/10/2003
Report status Discontinued
Investigation status Discontinued
Mode of transport Aviation
Aviation occurrence category Loss of separation
Occurrence class Serious Incident
Highest injury level None

Aircraft details

Manufacturer Fairchild Industries Inc
Model SA227
Registration VH-SEF
Serial number AC-641
Operation type Air Transport Low Capacity
Damage Nil

Aircraft details

Manufacturer Bell Helicopter Co
Model 47
Registration VH-SON
Serial number 3135
Sector Helicopter
Operation type Aerial Work
Damage Nil

Airbus A330-341, PK-GPE

Safety Action

Local safety action

Airservices Australia safety action

In the January issue of one of its newsletter to controllers, Airservices reminded controllers of the factors that contribute to runway incursions. Those factors included inadequate supervision of the manoeuvring areas of the airport, lack of adequate coordination between controllers in the tower, ambiguous clearances and instructions issued by controllers, incorrect read-back of clearances and instructions by pilots and vehicle drivers, and controllers not detecting the errors in those read-backs.

Airservices is investigating the International Civil Aviation Organization's concept of the Advanced Surface Movement Guidance and Control System for Sydney and other Australian airports. The concept includes consideration of improved surface movement radar, improved Aerodrome Mandatory Instruction Signs and Aerodrome Information Signs and the installation of stop-bar lighting. Stop bar lighting consists of a row of red unidirectional, in-pavement lights installed on the taxiway along the holding position marking the entrance to a runway. These initiatives could improve conflict detection for controllers, reduce the incidence of runway incursions and reduce the risk of a collision as a result of a runway incursion.

Overall, the system has the potential to improve the level of safety for operators at airports and improve controller situational awareness.

Sydney Airport Corporation Limited safety action

Since this occurrence, SACL has:

  • formulated an updated Letter of Agreement with Airservices on the exchange of safety information;
  • nominated single points of contact between SACL and Airservices to act as representatives for the distribution of safety related information;
  • established a Runway Incursion Working Group with participation from Airservices, Qantas, Regional Express, Virgin Blue, Jetstar and Eastern Australia Airlines (involvement from other parties will be sought as required);
  • audited all AIA's in accordance with the AVCH (October 2003, s6.4.1, p.46) and acted to ensure any recommendations made, as a result of those audits, were implemented;
  • developed and issued updated category 2 testing examinations to all ADA issuing authorities which include guidelines for use by Approved Issuing Authorities when conducting the written tests;
  • re-issued the category 2 airside driver's pocketbooks with advice to drivers to stop and wait for assistance if they become lost or disorientated while driving airside; and
  • established an Airside Driving Forum co-facilitated with the NSW WorkCover that includes various airside users.

ATSB safety action

As a result of the investigation the Australian Transport Safety Bureau issues the following recommendations:

Recommendation R20040059

The Australian Transport Safety Bureau recommends that Sydney Airport Corporation Limited review the procedures used to ensure initial and ongoing driver competency and knowledge.

Recommendation R20040060

The Australian Transport Safety Bureau recommends Sydney Airport Corporation Limited ensures that Approved Issuing Authorities' driver training programs at Sydney Airport include a course of action that drivers can take should they find themselves lost or disorientated while driving airside.

1 Civil Aviation Regulation 89 defined the Airport operator as 'in relation to a licensed aerodrome-the licence holder'.
2 In accordance with the Airports Act 1996, s172, Airports (Control of On-Airports Activities) Regulations 1997.
3 Airside Vehicle Control Handbook, June 2003, p1.
4 Airside Vehicle Control Handbook, Sydney Airport, June 2003, p. 42.
5 Airside Vehicle Control Handbook, Sydney Airport, June 2003, p. 44.
6 A 'Runway Strip' is 'a defined area, including the runway (and stopway if provided), intended both to reduce the risk of damage to aircraft running off a runway and to protect aircraft flying over it during take-off, or landing operations. (ICAO) (Manual of Air Traffic Services effective 15 April 2004, Pt. 10, s.1, p. 10-18).
7 Drivers Pocketbook, Category 2, May 2002, p3.

Significant Factors

  1. The driver of the catering vehicle became disorientated and entered runway 34L.



 

Analysis

When the ADC issued the take-off clearance to the crew of the Airbus, the catering vehicle was a significant distance from both the Airbus and runway 34L. In the circumstances the ADC would have had no indication that the vehicle was likely to enter the runway and pose a potential collision threat to the Airbus.

There was little, if any, action that the ADC could have taken to resolve the situation when it became apparent to him that the vehicle would enter the runway because:

  • The catering vehicle was not radio equipped;
  • The Airbus crew was committed to the take-off, if not already airborne; and
  • Any alert provided to the crew of the Airbus by the ADC may have exacerbated the problem, given the relative position of the aircraft to the vehicle at that time.

While a runway incursion by a vehicle driven by the holder of a category 2 ADA may have been reasonably unforeseeable, this occurrence has identified a significant risk to the safety of operations at Sydney airport.

A means of detecting knowledge gaps and evaluating the ongoing proficiency of qualified drivers may have identified a knowledge deficiency in the area of taxiway and runway markings recognition and in other areas of knowledge that may have contributed to this incursion. Such quality assurance would enable SACL, as the authority responsible for the management and control of surface vehicles operating on, or in the vicinity of, the airside area of the airport, to recognise and address systemic deficiencies in driver competence on an ongoing basis. That would give SACL the opportunity to mitigate any resultant risks.

The driver of the catering vehicle was properly licensed, and had been driving on perimeter roads and apron areas of the airport for two years. Despite her training, the driver may not have been operationally familiar with taxiway and runway markings because she had not operated on runways or taxiways since she obtained her ADA.

None of the training programs included advice to drivers about recommended actions they could take that might assist them should they become lost or disorientated while driving airside. Such a procedure may have reduced the risk of a collision with the departing Airbus in these circumstances by:

  • reducing the likelihood of a runway incursion in the first instance; and
  • reducing the time the catering vehicle remained on the runway following the incursion.

Summary

Sequence of events

On 24 August 2003, at about 0935 Eastern Standard Time, a motor vehicle involved in catering duties on the international apron area at Sydney airport entered runway 34 left (34L) at taxiway Golf without the driver having first received a clearance from air traffic control to enter the runway. At that time, an Airbus A330-341(Airbus) aircraft had just become airborne from runway 34L. The aircraft passed directly over the vehicle while it was on the runway. The runway incursion by the vehicle resulted in an infringement of runway separation standards.

The driver of the vehicle was authorised to drive only on the perimeter roads, airside roads and apron areas. The driver was not aware that she had entered the runway and was not authorised, or trained, to drive on taxiways or runways. The driver eventually realised that she had entered an area of the airport with which she was not familiar. She attempted to return to the apron and was subsequently escorted from the movement area by an airport operations officer.

Sydney Airport Corporation Limited (SACL)

SACL was the airport licence holder and operator of Sydney airport at the time of the occurrence. In accordance with the legislation current at the time of the occurrence, SACL was ultimately responsible for the proficiency of drivers operating airside at Sydney Airport.

Under the Airports (Control of On-Airports Activities) Regulations 1997, part 4, division 4, s124, the airport operator was required to publish an Airside Vehicle Control Handbook (AVCH) for the airport over which it had control. The Sydney airport AVCH contained particulars for the management and control of surface vehicles operating on, or in the vicinity of, the airside area of Sydney airport. The stated 'intent of the requirements for airside operation of vehicles set out in the AVCH [was] to ensure the safe and orderly movement of staff, passengers, aircraft and vehicular traffic'.

SACL was responsible for issuing an authority to drive airside (ADA) to a driver who had an employment requirement to operate a vehicle airside. That responsibility could be delegated to an 'Approved Issuing Authority' (AIA).

'An Approved Issuing Authority is a company or organisation to which SACL delegated the responsibility to carry out the training, testing, and issuance of an ADA for the Airport' and was generally delegated to those organisations that employed airside drivers. SACL maintained overall responsibility for the training and testing standards of Approved Issuing Authorities at Sydney airport. The AVCH stated that AIAs 'must:

  • Provide the SACL Manager Safety with reasonable access to its records and premises to enable the SACL Manager Safety to carry out audits to ensure that the AIA is maintaining satisfactory standards in the carrying out of its functions as an AIA; and
  • Train and test its employees and employees of its Subsidiaries to drive Airside to the standard required by the SACL Manager Safety'.

Training

Training for a category 2 ADA included information on the recognition of perimeter roadway markings, apron roadway markings, live taxiway crossing markings, runway and taxiway markings. It did not require the driver to be trained in the use of a radio. The catering vehicle was not equipped, nor was it required to be equipped, with a radio suitable for use on an airport to enable two-way communication with air traffic control.

The driver of the vehicle held a current category 2 ADA, having been trained about 2 years previously. A category 2 ADA authorised the driver of an authorised vehicle to operate the vehicle on perimeter roads, airside roads and apron areas of the airport in accordance with the AVCH.

The AVCH specified the prerequisites for applying for the category 2 ADA. They included a requirement for drivers to hold a current State or Territory driver's licence and complete at least 4 hours of driving airside either as an observer or preferably as the driver under the supervision of another driver with at least a category 2 ADA.

Drivers were also required to demonstrate 12 practical and theoretical competencies to an approved training officer.

Category 2 ADA training did not include recommended actions or guidelines for drivers should they become lost or disorientated while driving airside.

Driver reference materials

The airport operator, SACL, produced a pocketbook for use by drivers with a category 2 ADA, and another for use by drivers with either a category 3 or a category 4 ADA. Holders of a category 3 ADA were authorised to operate an authorised vehicle on all movement areas excluding runway strips. Holders of a Category 4 ADA were authorised to operate on all airside areas which included an authorisation to enter a runway strip in accordance with airport procedures. The pocketbooks were intended to be 'a quick reference guide to explain the main rules which apply to all drivers operating airside'. The driver involved in this runway incursion had been provided with a copy of the category 2 driver's pocketbook.

The Category 2 pocketbook did not include recommended actions or guidelines for drivers should they become lost or disorientated while driving airside.

Air traffic control (ATC)

Air Traffic Controllers provided an Air Traffic Service to aircraft on that part of the Sydney aerodrome used for take-off, landing and taxying, excluding the apron areas, for the purpose of preventing collisions between aircraft and obstructions. The aerodrome controller (ADC) was responsible for authorising aircraft, personnel and vehicles to cross a runway or to operate on a runway strip.

The Manual of Air Traffic Services required ADCs to visually scan the length of the runway prior to issuing a take-off clearance and immediately before the take-off is commenced to confirm that the runway was free from obstacles including vehicles and other aircraft. Vehicle operators and pilots were also required to obtain a clearance from ATC prior to entering an active runway, and air traffic controllers operating from the control tower maintained a routine visual surveillance of the manoeuvring area of the airport.

A review of the recorded radar data showed that, when the controller issued a clearance to the crew of the Airbus to enter the runway, the vehicle was in the vicinity of bay 59 on the international apron. That was approximately 2.78 km from the Airbus and approximately 0.83 km from the intersection of taxiway Golf and runway 34L. When the Airbus commenced its take-off roll, the vehicle was near the intersection of taxiway Golf and taxiway Yankee. That was approximately 2.77 km from the Airbus and 0.5 km from the intersection of taxiway Golf and runway 34L.

Occurrence summary

Investigation number 200303726
Occurrence date 24/08/2003
Location Sydney, Aero.
State New South Wales
Report release date 05/11/2004
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 Airbus
Model A330
Registration PK-GPE
Sector Jet
Operation type Air Transport High Capacity
Departure point Sydney, NSW
Destination Denpasar, Indonesia
Damage Nil

Boeing 747-4H6, VH-OED, 2 km west-south-west of Los Angeles Airport, on 24 August 2002

Summary

The following text has been reproduced from NTSB Report OPS02SA003 into this incident:

History of Flight

At 0703:50 [UTC], the flight crew of ROK17 contacted the LAX local controller (LC1) and advised they were on a visual approach to runway 6R. Radar data indicated the airplane's radar track was approximately 7 miles west of the airport on a southerly heading. The LC1 controller issued the flight crew a landing clearance for runway 6R and advised that opposite direction traffic was departing the south complex turning southbound at the shoreline. The flight crew acknowledged the transmission.

At 0704:14, the LC1 controller issued the flight crew of QAF108 a take off clearance for runway 25R and advised of opposite direction traffic landing the north complex. The flight crew acknowledged the transmission.

At this point the LC1 controller began assisting the flight crew of Aero Mexico 460, the previous arrival to runway 6R that required assistance exiting the runway. According to the FAA, the LC1 controller walked to the north side of the tower cab (opposite side from the LC1 position) to view the situation. The controller returned to the LC1 position and noticed ROK17 was south of course heading northeast bound and at 0704:55, transmitted to the flight crew, "confirm turning back to six right." The flight crew responded, "affirmative." Radar data indicated the airplane's radar track began a left turn.

The LC1 controller then assisted the flight crew of Aero Mexico 460, who needed additional instructions to exit runway 6R. According to the FAA, the LC1 controller walked to the north side of the tower cab again to view the situation. The controller returned to the LC1 position and noticed ROK17 appeared to be aligned for runway 7L and at 0705:31, instructed the flight crew to "turn immediately north you are lined up for runway seven there's a seven forty seven opposite direction." The flight crew acknowledged the instructions. Radar data indicated the target separation was 4.05 miles and 1,300 feet.

The LC1 controller then instructed the flight crew of QAF108 to turn left heading 210 degrees and advised, "the Boeing seven five seven is moving out of your way." The flight crew of QAF108 responded, "that was close." Radar data indicated the closest proximity between the 2 targets was 1.17 miles and 600 feet.

The LC1 controller reissued the landing clearance to the flight crew of ROK17 and advised QAF108 to change to departure control frequency.

Approximately 2 minutes later the flight crew of ROK17 apologized to the LC1 controller on the frequency and stated that they had made a mistake and were not aligned properly for runway 6R.

ATC Environment

a. Airport Information

The Los Angeles International Airport is located in the northwest suburbs of Los Angeles, California adjacent to the Pacific coastline. The terrain is largely flat to coastal with large expanses of urban areas.

The airport has dual parallel runways. Runways 6L/24R and 6R/24L are referred to as the north complex and runways 7L/25R and 7R/25L comprise the south complex.Runway 6R is 10,285 feet long and 150 feet wide with a displaced threshold of 331 feet. The runway is equipped with high intensity runway lights, runway centerline lighting and medium-intensity approach lighting system with runway alignment indicator lights. According to the FAA, at the time of the incident the appropriate lighting systems for runway 6R were on and operating normally.

b. Tower and ATC Operations

The Los Angeles Air Traffic Control Tower is a Level 12 ATC facility, and is classified as a tower with radar. The tower is centrally located on the airport between the north and south complexes. The tower operation can accommodate 2 local control positions, Local 1 (LC1) and Local 2 (LC2). The LC1 workstation is located on the south side of the tower cab and is typically responsible for arrival and departure operations at the south complex. The LC2 workstation is located on the north side of the tower cab and typically responsible for the arrival and departure operations at the north complex.

At the time of the incident the local control positions were combined at LC1. In this type of configuration the LC1 controller was responsible for operations at both the north and south complexes. LAX was conducting over ocean operations, which consisted of airplanes arriving runway 6R (north complex) and departing runway 25R (south complex). According to the facility's Standard Operating Procedures Manual, LAXT 7110.1B, the operation is used primarily during 0000 and 0630 (Pacific Time) to mitigate noise. During these hours the facility's runway selection program requires the use of the inboard runways (6R and 25R) to the maximum extent possible.

c. Meteorological Information

The LAX surface weather observation at 2350 PDT indicated wind conditions from 240 degrees at 6 knots, visibility 6 statute miles, sky condition clear, temperature 17 degrees Celsius, dew point 16 degrees Celsius, altimeter 29.98 (inches of mercury).

d. Applicable ATC Procedures

I. Visual separation is a means employed by ATC to separate aircraft within airport traffic areas. Tower controllers base separation on observed or known traffic and airport conditions. Visual separation procedures are outlined in FAA Order 7110.65, "Air Traffic Control", paragraph 7-2-1 and states in part:

e. TERMINAL

Visual separation may be applied between aircraft under the control of the same facility within the terminal area up to but not including FL 180, provided:

1. Communication is maintained with at least one of the aircraft involved or the capability to communicate immediately as prescribed in 3-9-3, Departure Control Instructions, subparagraph a2 is available, and:

2. The aircraft are visually observed by the tower and visual separation is maintained between the aircraft by the tower. The tower shall not provide visual separation between aircraft when wake turbulence separation is required or when the lead aircraft is a B757.

II. FAA Order 7110.65, paragraph 2-1-6, Safety Alert states in part:

Issue a safety alert to an aircraft if you are aware the aircraft is in a position/altitude, which in your judgment places it in unsafe proximity to terrain, obstructions, or other aircraft.

Occurrence summary

Investigation number 200204016
Occurrence date 24/08/2002
Location 2 km WSW Los Angeles, Airport
State International
Report release date 06/03/2003
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Loss of separation
Occurrence class Serious Incident
Highest injury level None

Aircraft details

Manufacturer The Boeing Company
Model 747
Registration VH-OED
Serial number 25126
Sector Jet
Operation type Air Transport High Capacity
Departure point Los Angeles, USA
Destination Sydney, NSW
Damage Nil

Aircraft details

Manufacturer The Boeing Company
Model 757
Sector Jet
Departure point Unknown
Destination Los Angeles, USA
Damage Nil

Boeing 737-476, VH-TJL

Summary

A Boeing 737-400 (737) registered VH-TJL was en route from Brisbane to Townsville at FL340. Another 737 registered VH-TJF was en route from Cairns to Brisbane at FL330. Both aircraft were in the area of responsibility of the Brisbane Air Traffic Centre. TJL was operating on the Tabletop Sector radio frequency (120.55 Mhz) and TJF was operating on the Swampy Sector radio frequency (133.2 Mhz). The two sectors are adjacent to each other with the Swampy Sector located south of the Tabletop Sector.

The Tabletop Sector controller issued instructions to the crew of TJL to descend 'when ready' and shortly afterward, that crew reported receiving a traffic alert and collision avoidance system (TCAS) resolution advisory (RA), instructing them to climb. The controller issued traffic information on TJF to the crew of TJL. Shortly after, the controller received a short-term conflict alert on The Australian Advanced Air Traffic System display.

The crew of TJF then advised the Swampy controller that they had received a TCAS RA instructing them to descend. The controller issued traffic information on TJL to that crew.

The horizontal distance between the aircraft reduced to 0.4 NM while the vertical distance was 400 ft. The required radar or vertical separation standard was respectively 5 NM or 1,000 ft. There was an infringement of separation standards.

An Airservices Australia investigation found that:

  1. the Tabletop and Swampy sectors had been de-combined about 4 minutes before the occurrence;
  2. the crews of both aircraft had been given direct tracking;
  3. the crews were operating on different VHF radio frequencies; and
  4. there were supervisory and operational control deficiencies during the period leading to the occurrence.

With regard to the use of direct tracking, the Airservices investigation noted that the route structure was designed to segregate traffic where conflicts may occur and that to some extent direct tracking could reduce the separation assurance provided by the route structure. Had the two aircraft operated on their respective planned routes it was estimated that they would have crossed about 50 NM south of Townsville and that their descent profiles would have resulted in a vertical distance of 16,000 ft between them. The investigation also estimated that the difference in track length between the planned and actual routes was 1 NM. Thus, the efficiencies achieved by the provision of direct tracking were minimal compared with the increased risk to aircraft associated with the reduction in separation assurance.

As a result of this and other occurrences, Brisbane Centre implemented a trial of Aisle Supervisors that commenced 9 September 2002. Aisle Supervisor duties include operational command authority for a group or groups in the aisle plus administration and operational responsibilities.

Occurrence summary

Investigation number 200203940
Occurrence date 30/08/2002
Location 204 km SE Townsville, (VOR)
State Queensland
Report release date 13/05/2003
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-TJL
Serial number 24437
Sector Jet
Operation type Air Transport High Capacity
Departure point Brisbane, QLD
Destination Townsville, QLD
Damage Nil

Aircraft details

Manufacturer The Boeing Company
Model 737
Registration VH-TJF
Serial number 24431
Sector Jet
Operation type Air Transport High Capacity
Departure point Cairns, QLD
Destination Brisbane, QLD
Damage Nil

Loss of separation between a Piper 601B, VH-IGN and a Pacific CT4B, VH-YCS, 13 km south-east of Tamworth, (VOR), on 24 June 2002

Summary

The pilot of a Piper Aircraft Corporation Aerostar (Aerostar) had been issued with a clearance by the Tamworth aerodrome controller (ADC) to 'track east of the New England Highway until intercepting final runway 30R' at Tamworth and, subsequently, to 'report established east of the highway'. The voice recording of the occurrence confirmed that the clearance issued by the ADC to the pilot of the Aerostar clearly stated the route to be flown by that pilot. The pilot correctly read back the clearance and reported established east of the highway but did not remain east of the highway. The readback of the clearance, and confirmation from the pilot that the Aerostar was east of the New England Highway, enabled the ADC to clear the pilot of the Aerostar to descend below 4,000ft.

Tamworth Air Traffic Control (ATC) provided a non-radar, or procedural control, service to aircraft operating within the Tamworth control area and control zone. Controllers used non-radar information to establish and maintain procedural separation standards. The ADC intended to establish a lateral separation standard (between the Aerostar and a Pacific Aerospace CT4B (CT4) that was departing the Tamworth southern circuit). The standard used a '1 NM buffer to the track or position of an aircraft determined relative to a prominent topographical feature' in accordance with the Manual of Air Traffic Services. In this case the prominent topographical feature was the New England Highway that runs approximately south from Tamworth township and which crossed underneath the inbound track of the Aerostar approximately 12 NM southeast of the airport.

The vertical separation standard applicable between the CT4 and the Aerostar was 500 ft. However, the ADC applied a vertical distance of 1,000 ft between the Aerostar and the CT4 until the pilot of the Aerostar reported established east of the New England Highway. The ADC was then able to clear the pilot of the Aerostar for further descent because the ADC believed, based on the information provided by the pilot of the Aerostar, that a procedural lateral separation standard had been established between the Aerostar and the CT4, and between the Aerostar and other traffic operating in the southern circuit. However, the lateral separation standard was infringed when the Aerostar crossed to the west of the New England Highway, and the vertical separation standard was infringed when the Aerostar left 4,000 ft on descent, because no other separation standard had been established.

The pilot of the Aerostar was operating under the instrument flight rules (IFR) and later reported that he would have preferred to track with reference to his instruments, via IFR tracking points. The applicable Civil Aviation Regulation stated that the pilot shall 'ensure that maps and charts applicable to the route to be flown are carried and are readily accessible to the crew'. The pilot of the Aerostar carried a current world aeronautical chart that covered the Tamworth area but reported that he did not have time to refer to that chart after the clearance to track via the New England Highway had been issued. He was not carrying a visual terminal chart for Tamworth. He also reported that his workload at the time of the occurrence was high due to the combined effects of the sun in his eyes, the visual tracking instructions issued by the ADC and because he was unfamiliar with the airport.

The pilot of the Aerostar had a responsibility to advise the ADC that he was either uncertain about the clearance he had been issued, or that he was unable to proceed in accordance with the clearance issued. The ADC could then have issued an alternative clearance. Such timely notification is particularly important in a procedural environment where controllers rely on the integrity of the information provided by pilots to ensure the safe, orderly and expeditious flow of air traffic.

Occurrence summary

Investigation number 200202896
Occurrence date 24/06/2002
Location 13 km SE Tamworth, (VOR)
State New South Wales
Report release date 20/02/2003
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 Piper Aircraft Corp
Model PA-60
Registration VH-IGN
Serial number 61-0682-7962142
Sector Piston
Operation type Aerial Work
Departure point Sydney, NSW
Destination Tamworth, NSW
Damage Nil

Aircraft details

Manufacturer Pacific Aerospace Corporation
Model CT/4
Registration VH-YCS
Sector Piston
Operation type Flying Training
Departure point Tamworth, NSW
Destination Tamworth, NSW
Damage Nil

de Havilland Canada DHC-8-314, VH-TQC

Summary

A de Havilland Canada DHC-8-314 (Dash 8) was on initial descent to flight level (FL) 140 and was being radar vectored for a right circuit to land on runway 35. At the same time a Boeing 737-376 (B737) had departed from runway 35 and had made a right turn to avoid weather on climb to FL200. The approach controller had issued radar heading instructions to the crew of the Dash 8 to provide track shortening and to maintain separation with the B737.

The approach controller expected that the radar heading issued to the crew of the Dash 8 would have ensured that a radar separation standard of 3 NM would continue to exist between the B737 and the Dash 8 while the vertical separation standard of 1,000 ft did not exist between the two aircraft. During the occurrence, radar separation reduced to 1.9 NM when there was 600 ft vertical separation between the two aircraft. There was an infringement of separation standards.

At the time of the infringement of separation standards, both aircraft were above `approach' airspace, within the vertical limits of an overlying sector, but under the control of the approach controller. Transfer of control of aircraft in these circumstances was permitted in accordance with the provisions detailed in the Manual of Air Traffic Services. The minimum radar separation standard in that overlying sector of airspace was 5 NM. The minimum radar separation standard within the airspace under the control of the approach controller was 3 NM.

The radar heading issued to the crew of the Dash 8 resulted in that aircraft taking up a track that was approximately 15 degrees different from that which the approach controller had expected. He reported that the radar heading assigned to the crew of the Dash 8 may not have correctly accounted for the prevailing wind speed and direction, and also that the B737 did not track as he anticipated. The crew of the B737 later reported that they had proceeded in accordance with their airways clearance and that the time taken to execute the turn onto their track was normal.

During the occurrence the approach controller had developed an incorrect mindset that the required radar separation standard was 3 NM instead of 5 NM. He later reported that the need to apply a 5 NM radar separation standard in that overlying airspace was rare due to the natural disposition of traffic.

A combination of the approach controller's incorrect assessment of the effects of the prevailing weather conditions on the radar heading of the Dash 8, the expectation of the B737 track, and the use of an inappropriate radar standard compromised the planned horizontal separation standard while a vertical separation standard did not exist.

Had the approach controller assessed the effectiveness of the assigned heading before issuing instructions to the crews that cancelled the provision of a vertical separation standard, it is likely that the infringement would not have occurred. Application of an effective separation assurance strategy in accordance with the Manual of Air Traffic Services would have ensured that the prescribed radar separation standard was maintained.

Occurrence summary

Investigation number 200202709
Occurrence date 13/06/2002
Location 22 km E Canberra, (VOR)
State Australian Capital Territory
Report release date 25/02/2003
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-TQC
Sector Turboprop
Operation type Air Transport High Capacity
Departure point Sydney, NSW
Destination Canberra, ACT
Damage Nil

Aircraft details

Manufacturer The Boeing Company
Model 737
Registration VH-TAH
Serial number 23479
Sector Jet
Operation type Air Transport High Capacity
Departure point Canberra, ACT
Destination Melbourne, VIC
Damage Nil

Cessna 172, VH-JER

Safety Action

Local safety action

As of 28 May 2002, Airservices Australia had removed all references to the 'southern shores' from Cairns local air traffic control instructions.

Summary

On 25 May 2002, at 1157 hours Eastern Standard Time, a Cessna 172 (Cessna) came within approximately 600 m of a departing Boeing 747-300 (B747) while the B747 was climbing through the altitude of the Cessna. The pilot of the Cessna was tracking in accordance with what he believed to be the visual clearance issued by Cairns air traffic control at 1,000 ft AMSL. The B747 crew was tracking via a standard instrument departure (SID) which specified a left turn after take-off.

The aerodrome controller issued the pilot of the Cessna with a clearance to track via the 'southern shores'. The term 'southern shores' was referred to in the Cairns local air traffic control instructions as the 'southern shores of Trinity Inlet'. The aerodrome controller understood that the clearance referred to the shoreline between the Cairns inlet and False Cape along the southern shore of the Cairns harbour. The pilot of the Cessna was not familiar with the term 'southern shores' and thought the controller meant the shoreline on the southern side of Cairns airport (which was the northern shore of the Cairns harbour). The term 'southern shores' was not specified in any document available to the pilot.

The pilot correctly read back the clearance to the aerodrome controller. That correct readback indicated to the aerodrome controller that the pilot could comply with the clearance.

The Cairns local air traffic control instructions stated that a clearance to aircraft to track via the 'southern shores' was meant to provide wake turbulence separation between an aircraft departing Cairns via a runway 15 SID and an aircraft over the southern shore of the Cairns inlet.

The aerodrome controller reported that he had kept both the B747 and the Cessna in sight and that visual separation was maintained between the two aircraft throughout the occurrence. The ADC provided the Cessna pilot with turn instructions, to enable him to avoid the B747, and traffic information about the B747 and a wake turbulence advisory. The B747 crew received a resolution advisory from their traffic alert and collision avoidance system about the Cessna.

The controller issued a clearance to the pilot of the Cessna that was, to the aerodrome controller, a specified route but one that was not known to the pilot. The aerodrome controller was not aware that the pilot's understanding of the 'southern shores' differed from his own. The meaning of the term 'southern shores' was not available to the pilot of the Cessna and therefore the potential existed for the misunderstanding between the pilot and the aerodrome controller that resulted in this occurrence.

Occurrence summary

Investigation number 200202385
Occurrence date 25/05/2002
Location Cairns, Aero.
State Queensland
Report release date 29/01/2003
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Loss of separation
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Cessna Aircraft Company
Model 172
Registration VH-JER
Sector Piston
Operation type Flying Training
Departure point Cairns, QLD
Destination Cairns, QLD
Damage Nil

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

Boeing 737-376, VH-TAF

Analysis

As the 737 descended towards FL220, the crew was faced with the apparently conflicting demands of an ATC clearance and a TCAS resolution advisory. Given that the 737 was above the Brasilia, it would be normal for the initial TCAS advisory to have been a `reduce descent' or a climb advisory. Although no evidence of a TCAS or transponder malfunction was found, the investigation could not exclude the possibility of an equipment failure contributing to this incident.

It is possible that the crew may have misidentified the TCAS aural warning. Prompt action was required to resolve the apparent ambiguity, and the crew may have been guided more by the aural warning than by the IVSI display. That may have been, at least in part, due to the limitations of the IVSI display, where a pilot may initially rely more on the aural alert. Compared with a TCAS IVSI display, traffic information that is displayed on an EFIS screen increases the crew's situational awareness. However, pilots are trained to use all the information at their disposal and an aural alert would be the trigger to look at the IVSI display immediately. Therefore, if the green band of the IVSI was indicating a required rate of descent of 1200-1500 ft/min, then the correct procedure would be to disengage the autopilot and smoothly adjust the pitch to attain that rate of descent.

The probability that the crew of the 737 would receive a TCAS RA on the Brasilia could have been reduced had the Brisbane sector controller provided some indication to the crew of the 737 that there was another aircraft restricting further descent. That would have enabled the crew of the 737 to adjust their rate of descent in lieu of possibly maintaining a level and would have provided additional information that the crew could have then used to improve their situational awareness and optimise their decision making.

Summary

An infringement of separation standards occurred 70 NM east of Darwin, NT, between a descending Boeing 737-376 (737) and an Embraer EMB-120 (Brasilia) that was maintaining level flight. The event took place during the hours of darkness and in visual meteorological conditions. The crew of the 737 intentionally flew the aircraft through its assigned level in response to a traffic alert and collision avoidance system (TCAS) warning. The Brisbane sector controller also received a short-term conflict alert (STCA) between the two aircraft from the Australian Advanced Air Traffic System (TAAATS). The STCA alerted controllers when the radar trajectories of two aircraft indicated that separation standards might be infringed. The 737 and the Brasilia passed within 1.6 NM horizontally and 600 ft vertically. The required separation standard was either 3 NM or at least 1,000 ft.

TCAS is an airborne device that functions independently from the ground based air traffic control system and provides collision avoidance protection for a broad range of aircraft. The system fitted to the 737, TCAS II version 6.04, provided recommended escape manoeuvres in the vertical dimension, to either increase or maintain the existing vertical separation between the aircraft. The escape solution was communicated directly to the flight crew via a cockpit display and a synthesised voice attention getter. The TCAS alerts in the 737 used a liquid crystal display (LCD) instantaneous vertical speed indicator (IVSI) with red and green markings to indicate the vertical speeds to be avoided (red), and the desired vertical speed to be flown (green). The display was 70 mm square and had a fixed range of 6.5 NM. Aircraft were depicted using geometric symbols, depending on their threat status. A partial aircraft symbol was displayed at the extremity of the screen for aircraft detected beyond the display range. TCAS information could, in principle, have been incorporated in the electronic flight instrument system display (EFIS) of that aircraft but wiring and space available in the electronics racks of the aircraft would have required a major modification programme. TCAS information that is incorporated in the EFIS display allows the pilot to show traffic at longer ranges.

TCAS equipment interrogates the transponders of other aircraft to determine their range, bearing and altitude. Accordingly, the TCAS does not provide protection against aircraft that do not have an operating transponder. The Brasilia was fitted with an operating mode C transponder (altitude encoding) but was not TCAS equipped and the crew was not immediately aware of the infringement of separation standards. The Brasilia, which had 30 passenger seats and had a maximum take-off weight of 11,990 kg, was not required to be TCAS equipped by the Australian legislation current at the time. That legislation mandated the carriage of TCAS for all turbine-powered aircraft with more than 30 passenger seats or a maximum take-off weight greater than 15,000 kg. When both potentially conflicting aircraft are fitted with TCAS, both TCAS units co-ordinate their intentions to provide appropriate co-coordinated avoidance manoeuvres.

TCAS II can issue two types of alerts:

  • Traffic Advisory (TA) to assist the pilot in the visual search for the intruder aircraft and to prepare the pilot for a potential RA; and
  • Resolution Advisory (RA) to recommend manoeuvres that will either increase or maintain the existing vertical separation from an intruder aircraft.

Once the risk is over, the TCAS issues a synthesised voice `clear of conflict' message.

The 737 crew were on their fourth consecutive day of duty and completing the last sector of a four-sector day when the incident occurred. It took place at the transfer of control point between Brisbane Centre and Darwin Approach. The 737 was en-route from Cairns to Darwin and was on descent to FL220. The Brasilia was enroute to Groote Island, under the control of Brisbane Centre, with instructions to maintain flight level (FL) 210. Those routes placed the two aircraft on almost reciprocal tracks. As the 737 was passing FL235, the crew were instructed by the Brisbane sector controller to contact Darwin approach control for further descent, but were not advised of the opposite direction traffic.

The Manual of Air Traffic Services (MATS) gave guidance to controllers on how best to manage the situation and advised:

`6.6.5.5 Frequency change management in relation to the transit of an aircraft across airspace boundaries shall be arranged in a manner that normally enables pilot communication with the unit responsible for the airspace within which the aircraft is operating. A lateral tolerance of 10 NM either side of the boundary is permitted, except that when entering controlled airspace, the frequency change shall be within the 10 NM prior to the boundary.

6.6.5.10 Aircraft should normally remain on the frequency appropriate to the airspace in which it is operating. However, aircraft may be transferred to another ATS frequency provided that:

  1. significant operational advantage will be gained;
  2. workload, communications and equipment capabilities will permit the responsible controller to take such action as is necessary to preserve the separation without delay;
  3. the actual separation is in excess of the minimum;
  4. there is no possibility of separation being reduced to the minimum with the normal operation of the aircraft.'

MATS does not require controllers to provide traffic information to either crew in these circumstances.

In order to comply with MATS 6.6.5.10, the Brisbane sector controller could have either:

  • Initially assigned the crew of the 737, FL230 on descent, instead of FL220, then assigned the responsibility for separation to the Darwin approach controller, coordinating the terms of the transfer of the 737 with him, before transferring the aircraft to the Darwin approach frequency; or
  • Assumed the separation responsibility, coordinated the terms of the transfer of the 737 with the Darwin approach controller, and transferred the aircraft once the 737 had passed the Brasilia and a horizontal separation standard existed.

Airservices Australia believed that MATS section 6.6.5.10 did not apply to a change of frequency in these circumstances. According to Airservices Australia the action of the Brisbane sector controller, in assigning the crew of the 737 FL220, was consistent with MATS in that the controller applied a 1,000 ft separation standard between the two aircraft and the 737 crew was transferred to the Darwin approach controller within 10 NM of the lateral boundary between the Brisbane sector and Darwin airspace.

Shortly after acknowledging the instruction to change frequency, the 737 crew received an aural `traffic, traffic' warning and a display indication of an aircraft 5 NM ahead. The pilot in command stated that the TA quickly changed to a RA with a `descend, descend, descend' aural alert. As the aircraft was approaching its assigned level he disconnected the autopilot and pitched the aircraft nose down with the intention of following the RA commands. He stated that the required rate of descent shown on the IVSI was 1,200-1,500 ft/min. On passing FL220 the TCAS command abruptly reversed to a climb RA (aural `climb, climb now') which was followed positively. The climb annunciation continued until the aircraft was at FL225. No more commands were issued and there was no TCAS `clear of conflict', which is normally generated once a RA is removed.

Analysis of recorded data indicated that as the 737 descended through FL230, its rate of descent was approximately 2,900 ft/min. At FL227, the automatic flight system commenced a transition manoeuvre to achieve level flight at FL220. At approximately FL225 the autopilot was disengaged and the descent was continued manually at a rate of descent in excess of 3,200 ft/min to FL215. That was followed by a climb to FL225 at 2,900 ft/min as the pilot responded to the RA reversal (`climb now' advisory).

Maintenance files from the TCAS computer were examined and no indication of TCAS failure was found. Technical expertise was requested from the manufacturer of the TCAS equipment. Their evaluation of the event presented two possible scenarios.

`Explanation 1. The reported `descend' advisory was actually a `reduce descent' advisory that was misunderstood by the crew. A `reduce descent' would be consistent with the expected TCAS response per the reported geometry of the aircraft. Because the advisory was misinterpreted, the rate of descent was increased rather than decreased until the aircraft was below the TCAS required 700 feet vertical separation. Thus, the TCAS was required to issue a `climb now' advisory. The lack of a `clear of conflict' annunciation is explained in the following paragraph.

`Explanation 2. There is a possibility that the intruder aircraft's (equipped with mode C transponder) altitude report was not correctly received by the TCAS. There have been instances when a Mode C reply will not contain all the appropriate pulses in the message or it transmits pulses that are too narrow for the TCAS to detect. This could cause differing altitude reports and could result in multiple unstable tracks at different altitudes for the same intruder aircraft. This being the case, the TCAS could have issued a `descend' advisory for the intruder because it appeared (due to erroneous altitude report) that it was actually above its own aircraft. If subsequent replies had the correct altitude, the erroneous track would be dropped by the TCAS and the TCAS would issue a `climb now' advisory on the track with the correct altitude.

`The reason that `clear of conflict' was not annunciated can be attributed to low track firmness of the intruder aircraft. Mode C equipped aircraft are typically only equipped with a single antenna mounted on the lower hull. Since the intruder aircraft was below the 737 aircraft, it is likely that the TCAS was not able to receive regular replies at close proximity. The TCAS computer unit will `coast' the track of a previously established intruder file if it does not receive a valid or reasonable interrogation response. If the track of the intruder that generated the RA is coasted during the time of the associated RA, then the `clear of conflict' is not announced.'

Since the incident, the operator's TCAS software has been updated to Version 7. The objectives of the Version 7 update were to further increase the safety benefits of TCAS, make TCAS more compatible with the procedures used by ATC and to address operational concerns identified by pilots operating the older versions of TCAS. Improvements to the aural annunciations included a change from `reduce descent, reduce descent' to `adjust vertical speed, adjust'.

Occurrence summary

Investigation number 200201725
Occurrence date 24/04/2002
Location 130 km ESE Darwin, (VOR)
State Northern Territory
Report release date 25/11/2003
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Loss of separation
Occurrence class Incident
Highest injury level None

Aircraft details

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

Aircraft details

Manufacturer Embraer-Empresa Brasileira De Aeronautica
Model EMB-120
Registration VH-ASN
Serial number 120-056
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Darwin, NT
Destination Groote Island, NT
Damage Nil