British Aerospace 146 (BAe 146), en route from Norfolk Is. to Sydney, on 18 September 1998

Safety Action

As a result of this occurrence, the Bureau of Air Safety Investigation is investigating a safety deficiency relating to the use of controller-pilot data link communications messages by air traffic controllers and pilots, for the exchange of operational information.

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

Analysis

The controller taking over may not have been fully aware of the potential for conflict due to the recent handover/takeover. Had a more comprehensive handover/takeover briefing been conducted, it is likely that at least one of the controllers would have recognised that an ETP was required before any consideration of the use of the block level was undertaken.

The controllers' understanding of the operation of the CPDLC appeared to be limited and it was this aspect, in conjunction with an inadequate appreciation of the potential conflict, that led to the occurrence. Once the controller recognised that the approval message had not been placed on hold, HF radio should have been utilised to ensure the B747 crew were to maintain FL290, rather than rely on the CPDLC. Any delay to the crew receiving this instruction may have compromised the safety of the two aircraft.

The use of the TCAS by the B747 crew increased their situational awareness and was an active defence in the prevention of the conflict.

Summary

A Boeing 747 (B747) was on an international flight from Sydney to Los Angeles, maintaining flight level (FL) 290. The flight was operating in controlled airspace and was being managed by the Brisbane Sector 8 air traffic controller, using procedural control methods. The flight crew and controller were communicating via controller-pilot data link communications (CPDLC). The crew requested approval to climb to and operate between FL290 and FL330. The controller sent an approval at 0659 on the CPDLC for the crew to climb to the block level. Prior to changing levels, the crew received traffic information on their aircraft traffic alerting and collision avoidance system (TCAS) display. The traffic was approaching from the opposite direction, 2,000 ft above the B747. The B747 crew maintained their aircraft at FL290 and immediately reported via the CPDLC that they were unable to comply due to traffic. This message was sent at 0659 but was not received at the controller's terminal until 0706. The delay was believed to be due to network lag. The traffic was subsequently identified as a British Aerospace 146 (BAe 146), en route from Norfolk Island to Sydney at FL310.

The controller had assumed responsibility for the sector following a handover/takeover a few minutes after the request from the B747 crew, to operate in the block level, had been received. The previous sector controller had coordinated the use of the block level with adjacent sectors in anticipation of approving the request, after establishing that the two aircraft had passed each other. Neither controller had calculated an estimated time of passing (ETP) for the aircraft. An ETP of 0659 was subsequently calculated after the occurrence. Air traffic control standards require that aircraft travelling in the opposite direction on the same route cannot climb or descend through the level of the other aircraft during a specific period before and after the ETP. In this case, the appropriate time standard was 10 minutes. Consequently, the controller should only have approved the use of the block level after 0709.

The controller taking over responsibility for the sector stated that he was aware of the confliction and had prepared the message approving the use of the block level, with the intention of holding it in the CPDLC terminal until after the aircraft had passed each other. The CPDLC did not have a hold function in the "reply" mode in which it was operating. Consequently, the message was ready for dispatch. The "send" function on the terminal was actioned by selecting an icon and activating this via a computer "mouse" button. The controller's response to the initial request should have been either to acknowledge receipt with "standby" or "request deferred". This would have then enabled the controller to respond further to the message after establishing a passing standard. The controller awaited an audio response from the terminal to indicate that the message was being held. When this did not occur, he prepared and sent a message to the crew instructing them to maintain FL290. The crew responded to this instruction with "Wilco". This response was received at the controller's terminal at 0701. The controller could have also used Flight Service high frequency (HF) radio communications as an alternative to the CPDLC, in order to instruct the crew to maintain FL290. Delays of up to 5 minutes were common when using the data link system.

Occurrence summary

Investigation number 199804129
Occurrence date 18/09/1998
Location 93 km SW Lord Howe Island, (NDB)
State New South Wales
Report release date 15/07/1999
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer The Boeing Company
Model 747
Sector Jet
Operation type Air Transport High Capacity
Departure point Sydney, NSW
Destination Los Angeles , USA
Damage Nil

Aircraft details

Manufacturer British Aerospace
Model BAe 146
Registration NJS98
Sector Jet
Operation type Air Transport High Capacity
Departure point Norfolk Island
Destination Sydney, NSW
Damage Nil

Piper PA-32-300, VH-POW

Summary

The Piper Cherokee was being flown from Jamestown SA, to Kilfera Station, NSW where the pilot and passenger were to attend a field day. Witnesses at the property reported seeing the aircraft fly overhead and join the circuit on the downwind leg, for a landing in a westerly direction. The final approach was described by witnesses as being slightly high and fast, with the aircraft touching down approximately one third, to halfway along the 900 m airstrip. After a short ground roll, the engine noise was heard to increase and the aircraft became airborne just before the end of the airstrip. Although the aircraft adopted an unusually nose-high attitude, it did not appear to be gaining height.

The left wing of the aircraft struck a radio mast approximately 8.5 m above ground level. The outboard section of the left wing and aileron were separated 1.25 m from the wingtip. The aircraft rolled to the left and passed through the upper foliage and branches of a large tree. The aircraft continued to roll inverted and collided with the ground. An intense post-impact fire consumed the aircraft wreckage and an adjacent building. The pilot and passenger sustained fatal injuries.

The homestead and property buildings were situated beyond the western end of the airstrip. The radio mast was approximately 104 m beyond the end of the airstrip, 32 m to the left of the extended runway centreline. There was no windsock at the landing area, nor was there a requirement for one. The pilot was experienced in remote area operations and had operated from property airstrips on many previous occasions.

On-site examination of the aircraft wreckage did not reveal any pre-existing defect that may have contributed to the circumstances of the occurrence. Propeller slash marks on the tree were consistent with the engine operation described by witnesses. The flaps were in the fully extended position and the intensity of the post-impact fire indicated that a substantial amount of fuel had been onboard. The aircraft's weight and balance was assessed as being within approved limits at the time of the accident.

The Area 22 forecast issued by the Bureau of Meteorology indicated that the aircraft would have encountered a tailwind on the easterly track to Ivanhoe, with fine conditions enroute. The aerodrome forecast for Ivanhoe predicted a light southeasterly wind of approximately 10 knots. It was not possible to determine whether the pilot had obtained this information prior to departure from Jamestown. No activity had been recorded on the pilot's Avfax briefing account for the day of the accident.

Photographs taken immediately after the accident provided evidence to support witness observations of wind velocity. It was estimated that there was a downwind component of approximately 10 knots at the time of the approach and landing. Although there was no windsock available, the pilot should have been familiar with alternative methods of determining wind velocity. It is possible that the pilot's perception of the wind direction was influenced by the tailwind conditions that he had encountered enroute.

The aircraft's climb performance would have been substantially degraded with full flap extended and the nose-high attitude described by witnesses. In that configuration, the pilot would have experienced difficulty in accelerating the aircraft to a safe flying speed. The aircraft's nose-high attitude during the climb would have obstructed the pilot's forward vision and he may have been unaware that the aircraft had diverged from the extended centreline of the airstrip.

Occurrence summary

Investigation number 199804109
Occurrence date 30/09/1998
Location Kilfera Station, 24 Km SW Ivanhoe
State New South Wales
Report release date 20/08/1999
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Collision with terrain
Occurrence class Accident
Highest injury level Fatal

Aircraft details

Manufacturer Piper Aircraft Corp
Model PA-32
Registration VH-POW
Serial number 32-40062
Sector Piston
Operation type Private
Departure point Jamestown, SA
Destination Kilfera Station, NSW
Damage Destroyed

Fairchild SA227-DC, VH-WBA

Safety Action

As a result of this and other occurrences, the Bureau of Air Safety Investigation is investigating a safety deficiency relating to the use of conditional clearances for runway entry and runway crossings by vehicles and aircraft. An assessment of the procedures used by air traffic controllers to alert themselves that vehicles or aircraft are on an active runway is to be included.

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

Significant Factors

  1. The aerodrome controller did not change the 'runway designator' strip to indicate that Car 23 had entered the runway.
  2. The aerodrome controller did not adequately scan the runway prior to issuing a landing clearance to the crew of WBA.

Analysis

The reduced density and complexity of the traffic may have relaxed the aerodrome controller to the degree that he was less alert than required when clearing WBA to land. The use of the 'runway obstructed' strip and the 'runway designator' strip should have assisted the controller to maintain an adequate awareness of the vehicle activity on the airfield. However, at the time of the occurrence, the 'runway designator' strip provided misleading information on the runway obstruction.

Although he scanned the runway prior to clearing WBA to land, the aerodrome controller did not expect to see a vehicle, as he was aware that the tractors were no longer obstructing the runway. Both strips had been in the bay for some time, which could have served to further diminish possible recall that Car 23 was now on the runway. It is also likely that the white colour of Car 23 made it difficult to see against the background of white runway markings or white gable markers. Consequently, without an effective alert to the presence of the vehicle on the runway, the controller's scan was inadequate to see Car 23.

The reason why the aerodrome controller did not follow his normal practice and change the notation on the 'runway designator' strip to indicate that Car 23 was on runway 21 could not be determined.

Summary

The crew of a Metroliner, VH-WBA, had flight-planned from Plutonic Mine in Western Australia to Perth. On first contact with Perth Tower, the crew were instructed to continue the approach for sequencing with VH-EAM, which was to land on the crossing runway 24. After EAM had landed and was clear of runway 03/21, the aerodrome controller noted that his 'runway designator' strip had 'Tractor' written on the runway 03/21 section. He observed the tractor to be clear, scanned the runway and, when WBA was 5-6 NM from touchdown, cleared the aircraft to land on runway 21.

At the time the landing clearance was issued, Car 23 was parked on the runway, approximately 200 m from the southern end. The surface movement controller reacted by instructing Car 23 to 'vacate 21 immediately'. Using binoculars, the controller observed the technician throwing tools and equipment into the back of the vehicle. The controller assessed that Car 23 would not vacate runway 21 prior to WBA crossing the runway threshold, and advised the aerodrome controller. The aerodrome controller then directed that the aircraft go around, advising the crew that a vehicle was on the runway. The pilot in command estimated that WBA was at about 400-500 ft when they were instructed to go around and both pilots looked for, but did not sight, the vehicle on the runway.

The surface movement controller was in radio communication with four vehicles. Car 23, a white vehicle equipped with a flashing yellow light, had been on and off runway 21, conducting instrument landing system checks. Tender 1 was being repositioned across the airfield and two tractors were engaged in mowing near the threshold of runway 21. Shortly before the incident, both tractors were clear of the threshold area and Car 23 requested approval to enter the runway for the fourth time. Once on the runway, Car 23 required a 1-minute recall to allow for the clearing of tools and equipment. The surface movement controller noted that no aircraft were due immediately and checked with the aerodrome controller for a clearance for Car 23 to re-enter runway 21. The aerodrome controller approved the clearance, but did not change the 'runway designator' strip notation to indicate that runway 21 was now obstructed by Car 23. The surface movement controller then cleared Car 23 to enter the runway.

The procedures in use at the time required that an individual clearance be obtained each time a vehicle entered or crossed a runway. As a memory prompt, both the aerodrome controller and the surface movement controller utilised red flight progress strips engraved with the words 'runway obstructed'. The aerodrome controller would place the strip above the 'taxiing aircraft' bay on the console. In addition, the aerodrome controller used a red 'runway designator' strip which was divided into three sections indicating the runways 03/21, 06/24 and 11/29.

When a vehicle was cleared onto the runway, the 'runway designator' strip was moved into the console's 'active runway' bay. The vehicle's callsign would then be written in the section that designated the obstructed runway. The annotation of the 'runway designator' strip with vehicle callsigns was not a requirement of the Local Instructions, but was a normal practice of the aerodrome controller.

The use of the flight progress strip was intended to assist the controller's situational awareness in two ways: (1) the action in placing the strip in the appropriate console bay (setting the memory prompt) should have assisted in consolidating a strong memory trace, and (2) the strip could be checked at any time should the controller be unsure as to the status of the item or condition referred to. The use of the 'runway designator' strip with the vehicle callsign notated provided an additional memory prompt.

Four air traffic controllers were rostered for duty in the control tower at the time of the incident. In addition to the aerodrome controller and the surface movement controller, the team leader was in the Airways Clearance Delivery position and a fourth controller was performing administrative duties. The Coordinator position was not occupied because the team leader considered that the traffic was light. Each controller was appropriately trained and rated in their operating position. All were extensively experienced in tower operations at Perth. The controllers had earlier completed a busy traffic sequence and were in a lull between sequences at the time of the occurrence.

Occurrence summary

Investigation number 199804072
Occurrence date 29/09/1998
Location Perth, Aero.
State Western Australia
Report release date 20/05/1999
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Fairchild Industries Inc
Model SA227
Registration VH-WBA
Serial number DC-883B
Sector Turboprop
Operation type Charter
Departure point Plutonic Mine, WA
Destination Perth, WA
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

Breakdown of co-ordination between a Boeing Co 737-476, VH-TJG and a Pilatus PC-12, VH-FMC, Adelaide Airport, South Australia, on 26 September 1998

Safety Action

Local Action

ATC management has tasked the Adelaide tower team leaders to review procedures to prevent a future recurrence.

BASI Safety Action

As a result of this and other occurrences, the Bureau of Air Safety Investigation is investigating a perceived safety deficiency relating to the use of blanket clearances for runway entry and runway crossings by vehicles and aircraft, and the procedures used by air traffic controllers to alert themselves that vehicles or aircraft are on an active runway.

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

Significant Factors

  1. The ADC did not conduct an effective scan of runway 30 or the flight progress strip display prior to clearing the Pilatus to take off.
  2. The presentation of the yellow flight progress strip did not alert the ADC that a runway 12/30 blanket clearance was in place.
  3. The ADC did not hear the SMC issue a clearance for the crew of the B737 to cross runway 30, nor did the SMC hear the ADC issue a take-off clearance to the Pilatus.
  4. The ADC did not observe the B737 moving towards runway 30.
  5. The SMC was distracted from a surveillance role by other tasks.
  6. The absence of the Tower Coordinator reduced the potential for recognising the development of a safety occurrence.

Summary

The crew of a Boeing 737 (B737) was cleared by the Adelaide surface movement controller (SMC) to taxi to the Foxtrot 5 holding point for runway 05, and to cross runway 30. Earlier, the SMC had been issued with a blanket clearance by the aerodrome controller (ADC) that allowed aircraft to occupy or cross runway 30 without a specific clearance from the ADC. The use of a blanket clearance reduced the need for segmented taxi clearances.

There were three personnel rostered for duty in the control tower; an ADC, a SMC and a tower coordinator. At the time of this occurrence the tower coordinator was absent from the tower cabin, reducing the monitoring potential of tower staff. All staff were appropriately trained and rated.

While the SMC was issuing the taxi clearance to the crew of the B737, the ADC was arranging departure instructions for a Pilatus PC12 from runway 30. The ADC subsequently cleared the Pilatus to take off from runway 30, without first cancelling the blanket taxi clearance and resuming control of the runway. Shortly after issuing the take-off clearance, the ADC became involved in communications with the approach controller regarding other inbound aircraft. The SMC was occupied with other data processing duties.

The crew of the B737 had sighted the Pilatus in the lined-up position on runway 30, but was unaware that a take-off clearance had been issued to that aircraft. As the B737 approached the crossing point of runway 30 on taxiway Foxtrot 2, the crew saw the Pilatus commence to take-off. They applied heavy braking and stopped their aircraft with the nosewheel 1-2 m beyond the runway holding point. The Pilatus continued its take-off run. The crew of the B737 subsequently confirmed with the SMC that they had been cleared to cross runway 30.

The local procedures in the Adelaide tower for a blanket clearance of a runway release required the use of a bright yellow coloured flight progress strip with the words "RUNWAY 12/30 OCCUPIED". Although a strip was correctly placed in each of the strip presentation bays in front of both the SMC and the ADC to indicate that a blanket clearance was issued, that procedure failed to attract the attention of the ADC.

The investigation of this occurrence was carried out by Airservices Australia, monitored by a Bureau investigator. A number of significant factors were identified.

Occurrence summary

Investigation number 199804069
Occurrence date 26/09/1998
Location Adelaide Airport
State South Australia
Report release date 30/09/1999
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Breakdown of co-ordination
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer The Boeing Company
Model 737
Registration VH-TJG
Serial number 24432
Sector Jet
Operation type Air Transport High Capacity
Departure point Adelaide, SA
Destination Melbourne, VIC
Damage Nil

Aircraft details

Manufacturer Pilatus Aircraft Ltd
Model PC-12
Registration VH-FMC
Serial number 109
Sector Turboprop
Operation type Aerial Work
Departure point Adelaide, SA
Destination Unknown
Damage Nil

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

Safety Action

Local Safety Action

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

BASI Safety Action

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

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

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

Summary

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

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

Occurrence summary

Investigation number 199803921
Occurrence date 21/09/1998
Location 9 km S Bindook
State New South Wales
Report release date 17/08/1999
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Loss of separation
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer The Boeing Company
Model 767
Registration N601EV
Sector Jet
Operation type Air Transport High Capacity
Departure point Taipei, TAIWAN
Destination Sydney, NSW
Damage Nil

Aircraft details

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

Fairchild SA227-DC, VH-WAI

Safety Action

Local Action

ATC Management at Perth has made the following recommendations:

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

BASI Safety Action

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

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

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

Significant Factors

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

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

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

The airfield layout increased the potential for a runway incident.

Summary

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

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

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

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

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

Occurrence summary

Investigation number 199803910
Occurrence date 14/09/1998
Location Perth, Aero.
State Western Australia
Report release date 10/07/2000
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Loss of separation
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Fairchild Industries Inc
Model SA227
Registration VH-WAI
Serial number DC-874B
Sector Turboprop
Operation type Charter
Departure point Perth, WA
Destination Sunrise Dam, WA
Damage Nil

Aircraft details

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

Beech Aircraft Corp F33A , VH-SIO

Summary

The student pilot was flying the Beechcraft Bonanza on a solo navigation exercise from Jandakot to Narrogin and Merredin before returning to Jandakot via Perth. The aircraft departed at about 1300 WST and was due to land at Jandakot about 2 hours later. The pilot reported that during the approach to Jandakot, he levelled the aircraft at 1,000 ft and set power to maintain the altitude. He then completed the pre-landing checks and lowered the flaps to slow the aircraft. Soon after lowering the flaps, he noted that the engine rpm was rapidly dropping. He reported that he opened the throttle and conducted the appropriate checks but the engine did not respond. The pilot transmitted a Mayday and decided to attempt a forced landing in an open patch of ground in the Canning Vale area. He then turned off the aircraft's fuel and electrical systems.

Avoiding parked trucks and buildings, the pilot landed the aircraft in a parking area of the Caning Vale Markets. The aircraft slid 15 m before hitting an unoccupied temporary building and coming to rest. The building was destroyed, the aircraft was substantially damaged and the pilot received minor injuries.

The post-accident inspection of the aircraft revealed that there was a substantial amount of fuel in both wing tanks but no fuel could be found in lines beyond the fuel selector valve. No fault was found with the aircraft's fuel system or engine.

Evidence was consistent with the engine sustaining fuel starvation and losing power but the investigation could not determine the reason for the fuel starvation.

Occurrence summary

Investigation number 199803888
Occurrence date 19/09/1998
Location Canning Vale
State Western Australia
Report release date 04/08/1999
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Forced/precautionary landing
Occurrence class Accident
Highest injury level Minor

Aircraft details

Manufacturer Beech Aircraft Corp
Model 33
Registration VH-SIO
Serial number CE-1329
Sector Piston
Operation type Flying Training
Departure point Jandakot, WA
Destination Jandakot, WA
Damage Substantial

Bell 47G-5, 25031

Summary

Witnesses reported that pilot of the Bell 47 was conducting cattle mustering operations. He departed on a short flight to check for stray cattle on the side of a hill, opposite to where the main mob was located. A short time after the helicopter disappeared from view, the sound of an impact was heard. A search revealed that the helicopter had struck a single wire earth return (SWER) power line which was suspended between a post on top of the hill and another post well left of the probable flight path. One of the landing gear skids had caught the wire, upsetting the helicopter, and causing it to enter uncontrolled flight. It was not determined whether the pilot was aware that there was a wire in the area.

This accident was not the subject of an on-site investigation.

Occurrence summary

Investigation number 199803878
Occurrence date 19/09/1998
Location 2 km W Kajabbi
State Queensland
Report release date 03/08/1999
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Collision with terrain
Occurrence class Accident
Highest injury level Fatal

Aircraft details

Manufacturer Bell Helicopter Co
Model 47
Registration VH-JGO
Serial number VH-JGO
Sector Helicopter
Operation type Aerial Work
Departure point 10 NM SW Kajabbi
Destination 10 NM SW Kajabbi
Damage Destroyed

Robinson R22 Beta, VH-HMR

Summary

This occurrence was investigated in 1998, and a summary report was released. The ATSB received new and significant information about this occurrence in 2004 and initiated further investigation. As a result, the ATSB has revised the summary and reissued the report as follows:

The pilot reported that he disembarked from the helicopter, leaving the engine running and the rotors turning, to converse with a stockman. He was returning to the helicopter when he heard the helicopter's engine and main rotor RPM increasing. The pilot attempted to reach the throttle control and was at the right skid before being forced to dive away as the helicopter became airborne. The helicopter flew into the ground about 5 m from its lift off point and was destroyed. There were no injuries. The wind conditions were reported by the pilot as being light and variable.

The pilot reported that he had set the engine throttle to 75%, selected the governor off, and used the cyclic and collective friction to secure the flying controls. The collective was also fitted with a strap to help secure its position but the pilot could not recall if it was deployed. The operator reported that photos taken after the occurrence indicate that the governor was selected on and the collective strap was not deployed. The circumstances of the occurrence are consistent with inadvertent raising of the collective control.

Occurrence summary

Investigation number 199803826
Occurrence date 14/09/1998
Location Myroodah Station, (ALA)
State Western Australia
Report release date 28/06/2004
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Collision with terrain
Occurrence class Accident
Highest injury level None

Aircraft details

Manufacturer Robinson Helicopter Co
Model R22
Registration VH-HMR
Serial number 1022
Sector Helicopter
Operation type Aerial Work
Departure point Myroodah Station, WA
Destination Myroodah Station, WA
Damage Destroyed