Ground strike involving British Aerospace BAe 146-300, VH-SAJ, at Brisbane Airport, Queensland, on 25 June 2024

Final report

Report release date: 09/09/2025

Investigation summary

What happened

On 25 June 2024, a British Aerospace BAe 146‑300, registered VH‑SAJ, was being operated by ASL Airlines Australia on a freight flight from Sydney, New South Wales, to Brisbane, Queensland. On board the aircraft were the captain and first officer.

While on descent into Brisbane, the meteorological conditions worsened with visibility reducing to about 1,000 m in fog. The crew conducted an instrument approach for runway 19L, using the autopilot, and visually identified the high intensity approach lighting at about 220 ft. The first officer disconnected the autopilot at about 110 ft and made control inputs that resulted in an increasing aircraft pitch attitude with decreasing airspeed. The aircraft touched down with a high pitch angle and a vertical acceleration of about 2.4 g. The tail of the aircraft struck the runway, resulting in damage to the tail strike indicator and surrounding panels.

What the ATSB found

The ATSB’s investigation identified that the first officer likely became disoriented after disconnecting the autopilot and lost situation awareness. Consequently, they did not identify the increasing aircraft pitch attitude, decreasing airspeed, or low power setting and did not correct the resulting sink rate prior to touchdown. The captain prevented further rearward input by the first officer during the flare by placing their hand on the control column, likely reducing the severity of the tail strike.

It was also found that during the approach the captain became preoccupied with the remaining fuel on board and this likely limited their capacity to monitor other factors such as the first officer’s ability to undertake the approach and the undesired state of the aircraft during the flare. The ATSB also identified that the captain’s actions and communications during the approach likely increased the pressure on the first officer to commit to the landing. 

Prior to joining the operator, the captain had predominantly flown single pilot operations in non‑jet aircraft. They had been promoted to the position of captain early, which resulted in a missed opportunity to gain valuable experience within a multi‑crew environment prior to commencing in the role. This limited multi‑crew experience likely reduced the captain’s capacity to include the first officer in the decision-making process during the approach or make an authoritative decision to assume the pilot flying role.

The ATSB identified that both the captain and first officer had been appointed to their respective positions despite not meeting the ASL Airlines Australia minimum experience requirements. This occurred without additional controls in place to manage the risk of lower experienced pilots and resulted in a reduction in the intended experience level on the flight deck for the incident flight. 

What has been done as a result

Following an internal investigation by ASL Airlines Australia the following safety actions have been taken:

  • The upgrade or fleet transfer requirement of a minimum of 500 hours on a company type, or as deemed appropriate by the Director of Flight Operations contained in the operations manual was amended to a minimum of 500 hours on a company type, or similar type in terms of maximum take‑off weight as deemed appropriate by the Director of Flight Operations, Head of Training and Checking and Director of Safety.
  • Inexperienced flight crew that have been checked to line will not have their inexperienced status removed without a review of the candidate’s progress by the Director of Flying Operations or Head of Training and Checking.
  • The Planned Supervised Line Flying sectors for Captains – No Jet Experience listed in the OM‑D – Training and Checking Manual have been increased from 30 to 36 sectors.
  • Supervised Line Flying sectors for First Officers without previous jet experience has been increased from 30 to 36 sectors.
  • The Fleet Training Manager will review a candidate’s experience at the planning stage, and may elect to plan less, or more sectors, dependent upon the candidate’s progress.
  • Additional systems to track pilots with inexperienced status to avoid inadvertent rostering of inexperienced crew together.
  • The operator’s internal review identified an inconsistency between the operator’s standard operating procedures and the manufacturer’s recommendation with regard to which pilot (the pilot flying or the pilot monitoring) was to make an ‘attitude’ call when the aircraft pitch angle approaching landing increased above 5°.
  • The BAe 146 standard operating procedures manual has been updated and aligns with the manufacturer’s recommendation.
  • The operator’s internal review identified there was no policy stipulating that the captain must perform the landing when the weather conditions are below certain weather criteria.
  • A policy has been developed and incorporated into the operations manual that states the captain must conduct the approach and landing with visibility within 1,000 m and cloud within 100 ft of the minima unless the pilot in command is a company approved training or check pilot.

Safety message

Current shortages of aviation professionals, including pilots, have resulted in the need for operators to employ crew with less experience than has previously been expected. Operators are encouraged to review the employment and promotion processes for inexperienced crew, ensuring that additional training programs, or limitations on inexperienced crew and the pairing of less experienced crew during rostering are considered.

 

The occurrence

Overview

On 25 June 2024, a British Aerospace BAe 146‑300, registered VH‑SAJ, was being operated by ASL Airlines Australia on a freight flight[1] from Sydney, New South Wales, to Brisbane, Queensland. There were 2 flight crew on board. The captain was pilot monitoring, and the first officer (FO) was pilot flying. [2]

The aircraft departed Sydney at about 0415 with first light occurring at Brisbane at 0613. The forecast visibility for arrival at Brisbane was 10 km. While on descent to Brisbane, the meteorological conditions worsened with visibility reducing to about 1,000 m in fog. The crew conducted an instrument landing system (ILS) approach for runway 19L,[3] using the autopilot, and visually identified the high intensity approach lighting at about 220 ft. 

The FO disconnected the autopilot at about 110 ft and made control inputs that resulted in an increasing aircraft pitch attitude with decreasing airspeed. The aircraft touched down with a high pitch angle and a vertical acceleration of about 2.4 g. The tail of the aircraft struck the runway, resulting in damage to the tail strike indicator and surrounding panels.

Cruise and descent

At about 0457, while the aircraft was in cruise at flight level[4] (FL) 270 and approximately 350 km to the south of Brisbane, air traffic control (ATC) advised the crew to expect runway 19L for their arrival.

At about 0505, cockpit voice recorder (CVR) data indicated that the captain obtained the automatic terminal information service (ATIS)[5] for Brisbane Airport. The meteorological conditions at that time were reported as a wind from 190° at 8 kt, visibility greater than 10 km with showers in the area, cloud few[6] at 500 ft, scattered[7] at 3,000 ft, and a temperature of 14°C (see Meteorological information). The captain then completed the take‑off and landing data (TOLD) card. This included calculated figures for fuel overhead the destination (Brisbane) of 2,400 kg and a minimum divert fuel of 1,700 kg.

The crew then conducted a briefing for the arrival into Brisbane and the ILS approach for runway 19L (see Airport information).

During the briefing, the FO noted the minima for the approach including a decision altitude (DA)[8] of 220 ft and visibility of 800 m, stating that conditions in Brisbane at the time were ‘showers and wet’.

At 0513, ATC advised the crew that the ATIS had been updated, and the cloud was now few at 200 ft, scattered at 3,000 ft and the temperature was 13°C. At 0519, when the aircraft was about 125 km south of Brisbane, ATC issued the crew with a clearance to descend to FL 130. A short time later, the captain commented on the cloud at 200 ft to the FO. The FO stated that they had 20 minutes of fuel, which was enough for a second approach if needed. The captain replied with ‘yeah, then we’re landing anyway’. The crew then completed the approach checklist.

The captain later advised that they believed their comment was a standard operational comment based on fuel limits.

Figure 1: VH-SAJ flight track for arrival to Brisbane Airport

Good Earth image showing VH-SAJ flight track from 0513. The image shows the location of where the crew received advice on low cloud and reduced visibility.

Source: Google Earth, annotated by the ATSB. *Flight was conducted in darkness

At 0521, the crew commenced the descent to FL 130. At 0525, ATC issued the crew with a further clearance to descend to 9,000 ft. A short time later, the crew were advised by ATC to expect the ILS approach for runway 19L.

At 0526, when the aircraft was about 67 km south-east of Brisbane, ATC advised the crew of low cloud south of the airport that was moving north and that they may be required to delay their arrival. On receipt of the meteorological information from ATC, the captain commented to the FO that they had ‘no fuel’. The FO proposed that they had sufficient fuel to complete 2 approaches, declare minimum fuel, and complete a third approach. The captain commented that they would just land from the second approach as they would ‘rather be on the ground’, expressing concerns about the paperwork involved. 

Over the following 2 minutes, the captain and the FO continued to discuss the options for the approach with the captain stating that, given the fuel state, conducting a go‑around may result in a worse scenario as they expected the meteorological conditions at Brisbane to worsen. The crew did not discuss options for a diversion if they were required to undertake a go‑around due to the meteorological conditions. The closest suitable airport was the Gold Coast (see Gold Coast Airport meteorological conditions during flight). 

At 0529, ATC advised that the visibility had reduced to 1,000 m in fog, with a cloud base of 200 ft and that low visibility procedures were in force with the high-intensity approach and runway lighting operating.

At 0530 the crew discussed the changing meteorological conditions. During this discussion, the captain stated that the conditions would only get worse and if they could see the high‑intensity approach lighting, then they were going to land. The FO agreed and stated that the captain should ‘call it when you see it’.

At about 0531, the aircraft passed through 11,000 ft and, a short time later, the crew initiated the additional approach checks. At 0533, the crew were cleared to continue the descent to 4,000 ft.

There were 3 aircraft ahead of VH-SAJ on approach to land on runway 19L at Brisbane Airport. At about 0532, the first of the 3 preceding aircraft landed and reported becoming visual with the runway at the minima.

Final approach

At 0534, ATC provided a clearance for the crew to undertake the ILS approach for runway 19L.

At 0536, the second aircraft in the sequence ahead of VH‑SAJ conducted a go‑around, later reporting to the ATSB that the combination of reduced visibility and low cloud prevented them from landing. At 0537, the captain of the third aircraft in the sequence declared to ATC, ‘should we, we will require an immediate diversion to the Gold Coast’. However, the third aircraft landed successfully.

The CVR indicated on hearing the transmission from the aircraft advising a go‑around, the captain stated ‘we haven't got the fuel for this’. The captain later stated that their comment was over concern should multiple go‑arounds be required.

At about 0539, VH-SAJ became established on the ILS for runway 19L. At about 0540, approximately 4 minutes prior to landing, the captain stated to the FO that they did not have enough fuel to divert to the Gold Coast. The FO queried if it was possible to recalculate if there was sufficient fuel to conduct the diversion to the Gold Coast, to which the captain responded ‘not now on final, but let's try and get in’. 

The captain later stated that they believed that it was not appropriate on final approach to calculate fuel for a diversion. 

At 0541:28, the crew completed the landing checklist.

Landing

At 0541:45, the crew were provided with a landing clearance from ATC (Figure 2) and were advised that the runway visual range[9] was 1,200 m at the touchdown zone, 1,200 m at the runway mid‑point and 1,800 m at the end point of the runway. 

Figure 2: VH-SAJ final approach to Brisbane Airport

VH-SAJ flight track on final approach and landing at Brisbane.

Source: Google Earth, annotated by the ATSB. *Flight was conducted in darkness

At 0542:05, the captain instructed the FO to leave the autopilot connected until the aircraft reached 220 ft (the BAe 146‑300 minimum autopilot disconnect height is 60 ft). The captain later recalled to the ATSB that they did so to keep the aircraft on an accurate approach to the runway. The FO confirmed they would leave the autopilot engaged but also stated they would disconnect it should they require a go-around. In response, the captain stated ‘we don't want to go around. It’s gonna be a world of hurt’. The FO responded ‘but if we can't see, then we're gonna have to’. 

The captain later responded after reviewing the draft report that their comment was over concern that a go‑around may lead to a more dangerous fuel critical situation and recalled at the time they considered similar occurrences that had occurred to other operators. 

At 0542:40, the aircraft descended through 1,000 ft and was about 7 km from the runway threshold. At the same time, the captain advised the FO that the aircraft was stable, with the missed approach altitude set and armed.

At 0543:05 and about 600 ft, the captain announced they were visual with the high intensity approach lighting, the FO responded that they could also see the lighting, however ‘not super clearly’. At 0543:31 and about 350 ft, the captain instructed the FO to increase engine power.

At 0543:45, the aircraft reached the DA and the FO announced they could see the high intensity approach lighting. Four seconds later, the captain announced ‘there’s the runway’. The captain later recalled to the ATSB that they had more visibility than they had expected.

At 0543:57 the captain instructed the FO to disconnect the autopilot, which occurred at about 110 ft and an airspeed of about 128 kt. The airbrake[10] was extended and fully deployed as the aircraft passed 80 ft. Several pitch adjustments were made by the FO after the autopilot was disconnected. The FO later described that from the DA until landing, their workload increased ‘to a 9 or 10 out of 10’, they became ‘overwhelmed’ and that their scan pattern had broken down. The CVR indicated that neither the FO nor the captain commented on workload during the approach.

At 0544:01, both the captain and the FO announced becoming visual with the PAPI lights.[11] The FO later recalled they could make out the runway edge lighting, however could not see the touchdown point.

Just prior to touchdown, the captain instructed the FO ‘don’t come back too far’. The captain later recalled to the ATSB that the FO had levelled the aircraft shortly after disconnecting the autopilot and began to flare[12] too early. They recalled that the aircraft became high, slowed and then developed a high sink rate. From previous experiences they anticipated that the FO would attempt to pitch the aircraft up to arrest the sink rate. As a result, the captain placed their hand on the control column to prevent the FO from pulling back too far without verbalising their intention (see Operational policy and procedures). The FO also later recalled feeling the captain’s pressure on the control to prevent further rearward input. 

The captain recalled to the ATSB that it was a common reaction for less experienced pilots to pull back and increase the pitch when the aircraft experienced a drop, and that this is discussed during their command training.

At 0544:11 the aircraft main wheels contacted the runway. The onboard flight data recorder captured a vertical acceleration of 2.4 g at initial touchdown, an aircraft pitch attitude of about 5.3°, and an airspeed of 105 kt (see Recorded information). 

The crew were unaware of the tail strike until the damage was discovered on the post‑flight aircraft inspection. The tail contact with the runway damaged the tail strike indicator and surrounding fuselage skin panels (Figure 3). 

Figure 3: VH-SAJ damage to tail strike indicator and surrounding panels

Image shows the underside of VH-SAJ with damage to the tail strike indicator and surrounding panels.

Source: ATSB

Context

Personnel information

Captain
Experience

The captain held an air transport pilot licence (aeroplane), issued in October 2017, and a valid class 1 aviation medical certificate. At the time of the incident, the captain had about 7,500 hours total aeronautical experience, of which about 5,400 hours was multi‑engine command. They had a total of 411 hours on the BAe 146, which included 198 hours as captain. The BAe 146 was the captain’s first jet aircraft rating, having previously flown smaller twin turboprop aircraft mostly in single pilot operations before commencing employment with the operator.

Operator training

The captain joined ASL Airlines Australia in November 2022 as a first officer. They completed their type rating on the BAe 146 aircraft in early 2023 and they were checked to line as a first officer in July 2023. In October 2023, they were assessed and recommended to undertake command training. At that time, their total BAe 146 time was 155 hours.

Their command training commenced in November 2023 and involved simulator training and command checks. During this training, the captain’s initial operator proficiency check (OPC) was assessed as unsatisfactory due to a breakdown in situation awareness during an instrument approach. Additional simulator training was provided, and the captain passed their OPC on 23 November 2023. The captain’s subsequent command simulator training was also assessed as unsatisfactory and was required to be retaken. 

On 4 December 2023, the captain commenced supervised line flying sectors. The captain completed 19 sectors before being recommended to undertake their check to line on 19 December 2023. The captain’s check to line was assessed as unsatisfactory after the first sector. The captain was provided with additional simulator and ground school training support. The captain completed a further 8 supervised line flying sectors before being recommended to retake their line check. The captain successfully completed their line check on 15 February 2024.

The captain’s command training consisted of 31 sectors and 58 hours of flying.

First officer
Experience

The first officer (FO) held a commercial pilot licence (aeroplane), issued in March 2020, and a valid class 1 aviation medical certificate. The FO’s total aeronautical experience was about 1,090 hours, including about 113 hours as an FO on the BAe 146. Prior to their employment with the operator, the FO had flown for a general aviation operator, flying mostly smaller, single-engine aircraft and operating under visual flight rules.  

Operator training

The FO joined ASL Airlines Australia in January 2024. They completed their type rating on the BAe 146 aircraft on 4 March 2024. They undertook 2 simulator sessions before successfully completing their OPC on 28 March 2024. 

The FO commenced supervised line flying sectors in April 2024. The FO was assessed as achieving below the required standard in several areas including situation awareness, approach and landing. The FO undertook a simulator session on 8 May 2024 and an additional 16 supervised line flying sectors. The FO recalled that their simulator training included low visibility operations, but they had not previously landed an aircraft in foggy conditions.  

On 28 May 2024 they were assessed as not proficient during their check to line. The FO was reassessed on 29 May 2024, 28 days prior to the incident and successfully completed their check to line.

The FO’s training consisted of 51 sectors and 90 hours of flying. 

Fatigue

The ATSB considered the role of crew performance due to fatigue and found that, from the available evidence, fatigue was unlikely to have contributed to the incident (see Fatigue).

Aircraft information

General information

The BAe 146 (Figure 4) is a high‑wing cantilever monoplane with a T‑tail. It is powered by 4 Avco Lycoming ALF 502 turbofan engines mounted on pylons underneath the wings and had retractable tricycle landing gear. 

The aircraft, serial number E3150, was a BAe 146‑300 series aircraft manufactured in 1989 and configured for air freight operations. It was first registered in Australia as VH‑SAJ on 24 October 2019. The last periodic inspection was completed on 12 June 2024 and on the day of the occurrence, the aircraft had accumulated 34,746 hours total time in service. 

Figure 4: VH-SAJ BAe 146-300

VH-SAJ image whilst flying on a clear sky day.

Source: Jet photos, Cameron Roberts

Aircraft operator

At the time of the incident, ASL Airlines Australia (previously Pionair) held an air operator’s certificate issued by the Civil Aviation Safety Authority (CASA) on 14 May 2020 and valid until 1 December 2027, that authorised air transport in larger aeroplanes (CASR Part 121). ASL Airlines Australia operated a mixed fleet of aircraft that comprised 6 BAe 146s and 1 Boeing 737 aircraft, conducting mostly domestic air freight operations. 

Airport information

Brisbane Airport

Brisbane Airport has 2 runways oriented 10°/190° magnetic (01L/19R and 01R/19L). At the time of the incident, aircraft departures and arrivals were taking place using runway 19L. The airport has a category 1 instrument landing system (ILS) on both runways. This landing system, combined with a 100% LED[13] category 1 lighting system,[14] including stop bar lighting, enables operations during low visibility events like fog.

Instrument approach

The crew of VH-SAJ were flying an ILS approach for runway 19L. The minima for the approach included a decision altitude8 of 220 ft, visibility of 800 m, and a runway visual range of 550 m (Figure 5).

Figure 5: Brisbane ILS runway 19L approach chart with landing minimums (blue box)

Brisbane ILS runway 19L approach chart with landing minimums (blue box)

Source: Airservices Australia, annotated by the ATSB

Meteorological information

Predeparture briefing

The captain and FO were issued with a flight briefing package at 0057 that morning, which included the current terminal aerodrome forecast (TAF)[15] that was valid between 0000 on 25 June and 0400 on 26 June for Brisbane Airport. 

At the time the flight briefing was issued, the TAF for Brisbane indicated:

  • wind 210° at about 4 kt
  • visibility greater than 10 km
  • cloud few at 2,000 ft and broken[16] at 4,000 ft
  • active INTER[17] from 0000 through till 0400 for visibility of 3,000 m in showers of moderate rain and broken cloud at 1,500 ft. 

Prior to their departure from Sydney, the crew checked the latest weather information for their arrival into Brisbane. The latest TAF had not extended the INTER period for showers beyond 0400.

Brisbane Airport meteorological conditions during flight

The aircraft departed Sydney Airport at 0415, one hour and 15 minutes after the scheduled departure time and had an estimated time of arrival in Brisbane at 0555. Over the period 0500 to 0525 the visibility at Brisbane Airport remained greater than 10 km. From 0525 to 0550 the visibility reduced from greater than 10 km to 660 m due to the formation of advected fog.[18] The recorded visibility at the time VH‑SAJ landed was 912 m (Figure 6). 

Figure 6: Brisbane Airport visibility 0445 to 0615 on 25 June 2024

Graph depicting the reduction in visibility from 0445 through until 0615. Visibility reduced to 912 m during the time VH-SAJ landed.

Source: Bureau of Meteorology, annotated by the ATSB

Closed circuit television (CCTV) recorded from the Brisbane air traffic control tower captured a progressive reduction in visibility that was consistent with the recorded meteorological information (Figure 7). 

Figure 7: CCTV images from Brisbane Airport tower facing south

4 images of the same location at Brisbane airport facing south over a 19 minute period. The images show the decreasing visibility due to fog.

Source: Brisbane Airport Corporation, annotated by the ATSB

Gold Coast Airport meteorological conditions during flight

The closest alternate to Brisbane Airport was Gold Coast Airport which had a TAF issued at 0306 that contained an active TEMPO[19] for visibility of 4,000 m in showers of rain, with cloud scattered at 1,000 ft and broken at 2,000 ft. 

At 0530, the Gold Coast meteorological aerodrome report (METAR) indicated visibility greater than 10 km and lowest cloud base of few at 6,100 ft. The subsequent METAR, issued at 0600, indicated visibility was still greater than 10 km with the lowest cloud base being scattered at 3,600 ft. 

The Gold Coast Airport forecast was not issued to the crew as part of their flight briefing package and the crew did not obtain the Gold Coast Airport ATIS during the flight.

Recorded information

The aircraft was fitted with an L3[20] F1000 flight data recorder and L3 FA2100 cockpit voice recorder. Both units were transferred to the ATSB technical facilities in Canberra, Australian Capital Territory, for download.

Recorded flight data during the approach phase indicated the aircraft was flown within the ASL Airlines Australia stabilised approach criteria. At a height of about 110 ft, approximately 13.5 seconds before the main gear touchdown, the data indicated the autopilot was disconnected. Immediately following the disconnection of the autopilot, over a period of 5 seconds, the aircraft pitch attitude increased from about −4.3° to about 0° (Figure 8). At the same time the aircraft speed reduced from about 128 kt to about 120 kt. The crew had calculated the aircraft landing reference speed (Vref)[21] to be 115 kt and the aircraft approach speed (Vapp)[22] to be 120 kt (Vref + 5 kt). 

The airbrake was deployed at a height of 100 ft and was fully extended when the aircraft reached 80 ft. ASL Airlines Australia standard operating procedures manual for the BAe 146 advised that the airbrake should be deployed on final approach once the landing was assured.

Figure 8: Recorded flight data

Onboard data recorded from VH-SAJ showing the last 150 ft of descent prior to landing, an increased pitch after auto pilot disconnection. From 50 ft an increased rate of descent is followed by a pitch increase prior to touchdown.

Source: ATSB

At a height of about 65 ft, the aircraft decelerated through 117 kt with a pitch attitude of about −3.6° and an increasing rate of descent. Several further pitch attitude adjustments were recorded as the aircraft continued to descend.

At a height of about 30 ft, the pitch attitude decreased to about −2.3°, airspeed reduced to about 109 kt and the rate of descent increased. Shortly after, the pitch attitude increased to a maximum of about 5.3° coincident with main gear touchdown. The vertical acceleration at main gear touchdown was 2.4 g and the airspeed was 105 kt. The aircraft engine power throughout the landing sequence was about 37% N1[23] and there was no recorded increase in power prior to contact with the runway. About 4 seconds after the initial touchdown the main gear momentarily recorded a weight off wheels followed by a vertical acceleration of 1.7 g, indicating a possible bounce.

The aircraft manufacturer advised that a tail strike in a BAe 146‑300 would occur on a hard landing, when the main gear oleos[24] had fully compressed, at a pitch attitude of 6.9° or higher. The difference between the values provided by the manufacturer and the recorded data were likely due to a combination of the flight data recorder sampling rate for the pitch attitude parameter (4 times a second) and the overall system accuracy (+/− 1.34°).

Operational information

Flight plan

ASL Airlines Australia operations provided the flight plan as part of the flight briefing package. The flight would depart Sydney and climb to FL 270. The track would take the flight overhead Newcastle, Grafton, Lismore and the Gold Coast, before landing at Brisbane. The flight was scheduled to continue from Brisbane with a planned landing in Townsville before the crew would end their duty period in Cairns.

Fuel planning

On departure from Sydney, the onboard fuel load was recorded as 5,800 kg with a planned trip fuel of 3,332 kg, including taxi fuel. ASL Airlines Australia operations had planned the flight with an additional 30 minutes of holding fuel due to the forecast INTER, planned between midnight and 0400 in Brisbane, which was later cancelled. A delay due to an engine vibration warning light resulted in an additional fuel burn, however the crew determined that as the INTER had been removed, that they had sufficient fuel for the sector. After discussion with the engineering team, the warning light was deemed to be a faulty indicator and the aircraft cleared to depart.

The operator’s fuel policy required a fixed final reserve fuel of 30 minutes as well as an additional 15 minutes of holding fuel when no alternate was required. This was a provision for weather, GPS RAIM[25] outage, traffic, or beginning of daylight. A contingency fuel margin of 5% of the trip fuel was also required to compensate for unforeseen factors.

VH-SAJ landed in Brisbane with about 2,300 kg of fuel remaining, which equated to about 72 minutes of flight time that included the use of reserve fuel. The ATSB was advised that ASL Airlines Australia had undertaken an internal review of the flight and that this review determined that the aircraft had sufficient fuel to conduct a missed approach at Brisbane and then divert to the Gold Coast before having to utilise the final reserve fuel margin.

Weight and balance

The operator’s load and trim sheet records indicated the aircraft was within the weight and balance limitations for the intended flight.

Preflight briefing

At the beginning of the duty period, the operator’s policy was for flight crew to conduct a ‘big picture briefing’. This was an opportunity to discuss any significant factors that may affect the planned operation and to focus on underlying threats or unusual factors and to discuss any means of mitigating those threats. 

During the big picture briefing conducted prior to flight, the captain and FO recalled that they discussed that they had not previously flown together, and the captain communicated that they were open to receiving any criticisms or concerns regarding their operating practices. The captain recalled assuming that the FO was new to the position, but they were unaware of the FO’s previous flying experience and were also unaware they had not previously landed in low visibility conditions. 

Operational policy and procedures

Flight crew experience requirements
Legislative requirements to be qualified as pilot in command

Civil Aviation Safety Regulation (CASR) part 121.495 required the following pilot in command experience:

(1) A pilot is qualified as pilot in command for a flight of an aeroplane if:

(a) the pilot meets the minimum flying experience requirements specified, in accordance with subregulation (2), in the aeroplane operator’s exposition for the aeroplane; and 

(b) the pilot has successfully completed command training that complies with regulation 121.565 for the aeroplane operator and an aeroplane; and

(c) the pilot is:

(i) if the aeroplane is an Australian aircraft—authorised to pilot the aeroplane during the flight as pilot in command under Part 61; or

(ii) if the aeroplane is a foreign registered aircraft—authorised to pilot the aeroplane during the flight as pilot in command by the aeroplane’s State of registry.

(2) For the purposes of paragraph (1)(a), the aeroplane operator’s exposition must include minimum flying experience requirements for all aeroplanes operated by the operator for Part 121 operations.

Operator’s documented requirements

The ASL Airlines Australia operations manual (OM-A) version 5.5, which was current when the flight crew were checked to their positions, contained the minimum experience requirements to be met before an FO could be considered for promotion to the position of captain (pilot in command). The stated experience requirements were:

• meet all regulatory requirements

• minimum of 3000 hours aeroplane

• minimum of 500 hours on a company type, or as deemed appropriate by the GMFO [General manager of flying operations]

• minimum of 500 hours multi-engine PIC [pilot in command] or ICUS [in command under supervision]

• Australian ATPL [air transport pilot licence] or CPL [commercial pilot licence] with exam credit in all required examination subjects may be acceptable if the company is able to arrange/conduct an ATPL flight test as part of the upgrade training program.

The OM-A also contained the minimum experience required for the employment of a first officer. The stated experience requirements were:

• minimum total time of 1000 hours

• minimum of 500 hours in multi-engine aircraft

• a current Australian CPL [commercial pilot licence] or ATPL [air transport pilot licence]. 

The OM-A permitted the employment or promotion of crew below the prescribed minimum hours in ‘exceptional circumstances’, with the specific approval of the director of flight operations (DFO). It stated:

All crew seeking positions as pilots with Pionair are to comply with the Australian CASR Part 61 requirements with respect to licencing. Flight crew experience criteria for the various categories are as detailed below. These criteria may be varied, with the specific approval of the Director of Flight Operations to cater for exceptional circumstances.

There was no definition of what would be considered ‘exceptional circumstances’ within the OM-A.

Incident flight crew engagement

Neither the captain nor the FO met the documented minimum requirements to hold their assigned positions at the time of the occurrence.

The FO had about 106 hours of multi-engine experience at the time of their engagement with ASL Airlines Australia and about 219 hours of multi‑engine experience at the time of the incident. The OM-A minimum multi-engine experience requirement for the position was 500 hours.

The captain completed their command check to line in February 2024. At that time, they had accumulated about 213 hours on the BAe 146, of which 155 hours were as FO and an additional 58.7 hours in command under supervision as part of their command training course. At the time of the incident, they had accumulated about 411 hours total flying in the BAe 146 as FO and captain. The minimum company type experience requirement for the position was 500 hours. 

The DFO was interviewed by the ATSB and described the captain as having ‘significant operational experience in night freight operations and the ability to manage fatigue with appropriate rest which was a very important but often overlooked skill for a new captain.

The DFO also recalled that the FO had previously been an airline cadet (for a major carrier) and had performed well in their interview. 

No evidence of the ‘exceptional circumstances’ that led to the promotion of the captain or the employment of the FO was provided or identified by ATSB. There was also no evidence that ASL Airlines Australia had considered and managed the risks associated with the engagement of flight crew that did not meet the stated minimum requirements. 

The DFO explained that during the period after COVID‑19, other airlines were recruiting significant numbers of flight crew and that ASL Airlines Australia had less opportunity to recruit for experienced crew during that time. 

The Australian Government’s Aviation White Paper released in 2024 cited that a shortage of aviation professionals, including flight crew, was worsening, with job vacancies having more than tripled since 2019. The report also identified the effect a pilot shortage has on regional airlines and smaller operators, as crew leave these organisations to progress their careers with larger airlines, resulting in a higher turnover and a pool of less experienced applicants during recruitment.

Rostering of ‘inexperienced’ flight crew

The ASL Aviation Australia OM-A contained a policy to prevent ‘inexperienced’ flight crew being rostered together for a flight. It stated: 

A flight crew member is deemed to be 'inexperienced' following completion of a type rating or command course until achieving the following additional experience on the type in their respective flight crew role after a successful check-to-line: 

a. 100 flying hours and 10 operational sectors, within a consolidation period of 60 days; or 

b. 150 flying hours and 20 operational sectors (with no time limit). 

The policy further stated:

The OCC [Operations Control Centre] must ensure that inexperienced flight crew are not rostered together. In exceptional circumstances on Day of Operations the Director of Flight Operations may approve a crew complement that does not meet the above minimum experience requirements. To ensure compliance with current Regulations the Director of Flight Operations must ensure that, at an absolute minimum, the above minimum hours and sectors have been met when considering a crew member’s total type experience (including line training).

The captain had accumulated 198 hours since their successful check to line in February 2024 and was not considered inexperienced.

The FO had accumulated a total of 113 hours total time on the BAe 146 including their line training. Since their successful check to line on 29 May 2024, they had flown about 25 hours and completed 15 sectors as FO and was still considered ‘inexperienced’ according to the operator’s policy.

The policy did not have a provision for crew members that had been promoted to their position below the operator’s minimum prescribed hours.

Operational restrictions for 'inexperienced' flight crew 

CASA acceptable means of compliance guidance material regarding pilot experience, stated: 

The operator should consider any operational restrictions to be placed on an 'inexperienced' crew member after the completion of the conversion training or post command line check. These considerations may include cross wind limits, aerodrome limits and weather minima limits if the operator assesses these limits as suitable for their operation.

ASL Airlines Australia reported that it did not have a policy that restricted ‘inexperienced’ FOs landing in adverse weather and raised concern that this would reduce the exposure of FOs to less than desirable weather conditions.

The ATSB interviewed the captains of 2 of the 3 aircraft that were on approach to Brisbane ahead of VH‑SAJ. These aircraft were being operated by the same CASR Part 121 operator. Both captains advised that the FO on board was originally the pilot flying for that sector. However, if the visibility was less than 2,000 m or if the cloud was within 200 ft of the minima,[26] their operator’s policy was that the captain was required to conduct the approach and landing. Both captains reported that as the visibility on the ATIS was reported as 1,000 m and the cloud height at 200 ft, both had assumed the pilot flying roles of their respective aircraft prior to landing in accordance with their operator’s captains only approach procedure. 

The ATSB reviewed expositions from 6 CASR Part 121 operators and found that 5 out of 6 operators had restrictions on FO’s conducting take‑offs and landings in adverse weather conditions, including reduced visibility, low cloud and strong winds.

Responsibility for control of the aircraft

The ASL Airlines Australia OM-A stated:

The authority and responsibilities of the captain are crucial for the safe operation of an aircraft. The captain holds ultimate authority over the aircraft, maintains discipline, and is responsible for ensuring the safety of individuals and cargo onboard, as well as the overall safe operation of the aircraft.

During interview with the ATSB, the FO recalled that as the approach continued, they became uncomfortable with the reduced visibility and described feeling overwhelmed by the conditions. However, the cockpit voice recording indicated the FO did not advise the captain of this, and they continued the approach as pilot flying. The FO recalled that, in hindsight, they should have requested control handover to the captain when they started feeling uncomfortable. Additionally, the captain also reported that in hindsight they should have assumed control and landed the aircraft. 

The ASL Airlines Australia OM-A required: 

Handover of control from one pilot to another must always be conducted in a positive manner. To minimise confusion or operational risk, the PF must not relinquish control until the PM has advised that they have taken control of the aircraft. NOTE: The standard phraseology to be used for handover/takeover procedures is: "You have control" and "I have control". 

• In non-normal situations or when required, the Captain must initiate the takeover procedure.

• If corrected responses are not achieved from control inputs, control should be handed over to another flight crew member.

• In critical phases of flight, Captains must be in a position to enable rapid takeover of controls.

Standard calls

ASL Airlines Australia operations manual B (OM-B) for the BAe 146 detailed the required standard calls for flight crew during an approach. Cockpit voice recorder information indicated that the crew missed several required calls (Table 1).

Table 1: Standard calls on descent BAe 146

EventStandard callCall event description
Gear extension

PF : Gear Down

PM : Speeds Checked … Selected … Gear Down, 3 Greens

Speed checked not called
ILS glideslope Alt/distance check

PM : (Position) ___ (Altitude) 

PM : ___ DME ___ (Altitude)

Not called
100 ft above minima

PM : Approaching Minimum

PF: Check

Not called
Minima

PM : Minimum 

PF : Continue; or Go-Around

Continue or go-around not called

In addition to the standard calls, the ASL Airlines Australia OM-B for the BAe 146 stated that during landing the:

PF/PM must monitor the attitude – if the nose up attitude becomes excessive on the ADI the PF should stop the increase in pitch attitude and consider a go-around if necessary. Recommended attitudes at which an “attitude” call should be made by the PF are:

• BAe146-300: 5°

The cockpit voice recording indicated that no attitude call was made by the crew when the aircraft pitch attitude increased above 5° just prior to main gear touchdown.

Fatigue

General

Fatigue affects everyone regardless of skill, knowledge and training and its effects can be particularly dangerous in the transportation sector, including the aviation industry.

The International Civil Aviation Organization (ICAO, 2015) defined fatigue as a physiological state of reduced mental or physical performance capability resulting from sleep loss, extended wakefulness, circadian phase, and/or workload (mental and/or physical activity) that can impair a person’s alertness and ability to perform safety related operational duties. Fatigue can have a range of adverse influences on human performance. These include:

  • slowed reaction time
  • decreased work efficiency
  • increased variability in work performance
  • lapses or errors of omission (Battelle Memorial Institue, 1998).
Duty period and sleep obtained

ASL Airlines Australia exposition stated that when flight crew are rostered to begin a duty period between 0000 and 0459 and scheduled to fly 4 sectors, the maximum duty period is 9.5 hours. If both flight crew agree, the duty may be extended by 1 hour during the duty period.

The captain recalled not being rostered on for the previous 72 hours before they signed on for their duty period in Melbourne at about 0015. They reported that, on the Samn‑Perelli scale of alertness,[27] they felt fully alert, however at the time of the occurrence, reported they felt ‘okay, somewhat fresh’. The captain reported having about 5 hours sleep in the 24 hours prior to their duty period and about 12 hours of sleep in the past 48 hours.

The FO recalled not being rostered on for the previous 72 hours before starting their duty. They reported having about 9 hours sleep in the past 24 hours prior to their duty period and about 17 hours in the past 48 hours and that they felt ‘a little tired, less than fresh’ at the time of the occurrence. 

The ATSB assessed that both crew had sufficient sleep opportunity prior to commencing their duty.

Adequate sleep is an obvious prerequisite for alertness during duty. The concept of adequate sleep however is subject to individual variability with inconsistencies in amount and quality. 

Window of circadian low

The duty period required working through the time in the circadian body clock cycle when self‐rated fatigue and mood are worst (Salas & Maurino, 2010). According to ICAO (2015) there are 2 times of peak sleepiness within a 24‑hour cycle. The main peak is in the early morning between 0300‑0500 known as the window of circadian low (WOCL), another smaller peak is around 1500‑1700 known as the afternoon nap window (International Civil Aviation Organisation, 2015). For each individual this time can vary. The incident occurred at 0544 which was close to the WOCL, which would have had some impact on their alertness levels as seen in their subjective alertness ratings above. 

However, the FO’s alertness was possibly heightened (Causse and others, 2024) due to their unfamiliarity with the unforecast conditions and as a result this would likely have counteracted any effect of fatigue.

Operator's biomathematical model of fatigue

The operator provided the ATSB with a summary of the June 2024 report from their fatigue management software which uses biomathematical modelling to predict fatigue risk from the roster times and duty periods. The results did not identify fatigue risk had occurred with either crew member. However, the model does not account for individual susceptibility or resilience to fatigue. 

Fatigue summary

The ATSB considered the role of crew performance due to fatigue and found that the available evidence indicated that fatigue was unlikely to have contributed to the incident. However, the captain’s self-reported amount of sleep in the 24 hours prior to their duty period is below the guidelines for recommended hours (Hirshkowitz and others, 2015). 

Related occurrences

Tail strike – Brisbane Airport, Queensland, 23 October 2008 (AO‑2008‑74)

On 23 October 2008 at 2357 Eastern Standard Time, a BAe 146‑300 aircraft, registered VH‑NJM, operating a freighter flight, had a tail strike on landing at Brisbane Airport, Queensland. The aircraft and crew had commenced duty earlier that evening at Adelaide, South Australia, and had flown via Sydney, New South Wales, to Brisbane. The aircraft and crew then did the reverse sectors back to Adelaide. It was only after landing at Adelaide that the crew became aware of the tail strike. Damage to the aircraft consisted of abrasion to the tail strike indicator through to the fuselage skin and abrasion to the fuselage skin. There was also damage to the aircraft’s structural frame under the tail strike indicator. The aircraft manufacturer had identified an increase in the number of BAe 146‑300 tail strikes and has recommended a number of procedural changes for flight crew. The aircraft operator has implemented those changes and issued notices to flight crew highlighting the risks and conditions for tail strike.

Tail strikes during landing involving Bombardier DHC-8 402, VH‑QOT and VH‑QOS, Brisbane Airport, Queensland, on 5 November 2013 and Roma Airport, Queensland, on 11 December 2013 (AO-2013-201)

On 5 November 2013 and 11 December 2013, 2 Dash 8‑400 aircraft, registered VH‑QOT and VH‑QOS, were being operated by QantasLink on scheduled passenger flights from Roma to Brisbane and Brisbane to Roma, Queensland, respectively. Both flights were crewed by a training captain, operating as pilot monitoring, and a trainee first officer, operating as pilot flying.

Although the 2 approaches utilised different flap settings, both were conducted using a propeller setting of 1,020 RPM. The early, initial and final stages of the approaches were unremarkable. Both training captains reported that as the aircraft approached the flare, they thought that the respective trainees had handled the approach well.

During landing, both trainees arrested the descent rate by raising the nose of the aircraft. In both cases the maximum pitch attitude was exceeded and the aircraft’s tail contacted the runway. Each aircraft sustained impact and abrasion damage to the fuselage skin and buckling of internal structures in the area of the tail strike sensor.

Safety analysis

Introduction

On 25 June 2024, a British Aerospace BAe 146‑300, registered VH‑SAJ, was being operated by ASL Airlines Australia on a freight flight from Sydney, New South Wales to Brisbane, Queensland. There were 2 flight crew on board. The captain was pilot monitoring (PM), and the first officer (FO) was pilot flying (PF). 

While on descent to Brisbane, the meteorological conditions worsened with visibility reducing to about 1,000 m in fog. The crew conducted an instrument landing system (ILS) approach for runway 19L, using the autopilot, and visually identified the high intensity approach lighting at about 220 ft. The FO disconnected the autopilot at about 110 ft and made control inputs that resulted in an increasing aircraft pitch attitude followed by several corrections and continued decreasing airspeed. The aircraft touched down with a high pitch angle and a vertical acceleration of about 2.4 g. The tail of the aircraft struck the runway, resulting in damage to the tail strike indicator and surrounding panels.

This analysis will explore the operational considerations pertaining to flight crew experience and training, situation awareness, command decision‑making and crew communication.

Loss of situation awareness

The FO was new to their position with ASL Airlines Australia, having been checked to line 28 days prior to the incident. During their line training, the FO required additional simulator and supervised line flying sectors to achieve the required standard associated with situation awareness, approach and landing. At the time of the incident, the FO had accumulated a total of 113 hours of flying on the BAe 146.

The meteorological conditions at Brisbane at the time of the approach included reduced visibility due to the formation of advected fog. At the time the crew reached the ILS decision altitude (DA) for runway 19L, the visibility was recorded as 912 m. Although this exceeded the minimum required for the approach, the FO had only experienced flying in reduced visibility during their BAe 146 simulated training, and they had not previously landed an aircraft in foggy conditions. (The FO’s experience prior to employment with the operator had predominately been flying smaller single engine aircraft in visual meteorological conditions).

The presence of low cloud or fog can create a false visual reference which can result in a pilot orientating the aircraft to the fog layer, rather than the ground references (Federal Aviation Administration). The FO recalled that the low cloud and fog created a sight picture that they had not previously experienced in the aircraft and that following the transition to visual flying, their instrument scan pattern broke down as their attention shifted to outside the aircraft as they attempted to make sense of the landing environment. 

Research by Garland et al, (1999) identified that high mental workload can negatively impact situation awareness, as only a subset of the available information can be processed and acted upon. Situation awareness can be defined as ‘the perception of the elements in the environment within a volume of time and space, the comprehension of their meaning and the projection of their status in the near future’ (Endsley, 1988) . The maintenance of a high level of situation awareness is a critical feature of a pilot’s role (Garland et al, 1999). 

The combination of degraded visibility, potential visual illusion, high workload, and inexperience operating in similar meteorological conditions likely resulted in the FO losing situation awareness of the aircraft state. Consequently, the FO did not effectively manage the aircraft following the disconnection of the autopilot resulting in the aircraft initially becoming high on the approach. 

A short time later, the FO likely became aware of the high profile and attempted to correct the height with several pitch attitude changes. However, the FO’s attention was outside the aircraft at this time and their instrument scan had broken down. 

Consequently, they were likely not monitoring aircraft airspeed and did not command any change to the engine power settings. As a result, the airspeed reduced and the aircraft’s rate of descent increased. The FO likely identified the increased rate of descent as the aircraft neared the runway, as a large pitch attitude increase was recorded just prior to touchdown. However, these actions were not sufficient to arrest the high rate of descent and this, in combination with the high pitch attitude, resulted in the tail of the aircraft striking the runway surface.

Contributing factor

The first officer became disoriented after disconnecting the autopilot on short final and likely lost situation awareness. Consequently, they did not identify the increasing aircraft pitch attitude, decreasing airspeed, or low power setting and did not correct the resulting sink rate prior to touchdown.

Captain’s focus on remaining fuel

As a consequence of the unforecast reduction in visibility, with no original requirement to plan an alternative airport, the captain became increasingly concerned about the fuel state as the aircraft continued on the approach.

It was also an expectation of the captain that the visibility would deteriorate further, commenting to the FO that if they were to conduct a go-around this could potentially leave them in a worse situation. During the approach, the captain also made several remarks about committing to a landing including that if they could see the high-intensity approach lighting, then they were going to land. About 2 minutes prior to landing, the FO expressed concern regarding the autopilot usage stating that they would disconnect it should a go‑around be required. In response, the captain stated ‘we don't want to go around. It’s gonna be a world of hurt’.

Prior to their descent into Brisbane, the crew had calculated the minimum fuel to divert to the Gold Coast was about 1,700 kg. The aircraft landed at Brisbane with about 2,300 kg of fuel on board, indicating there was sufficient fuel to conduct a go-around at Brisbane and safely divert the aircraft to the Gold Coast.

The captain’s preoccupation with the aircraft fuel state, combined with the expectation of worsening conditions, led to an increased desire to land the aircraft on the first approach and avoid conducting a go‑around which they perceived would have resulted in an approach in conditions that would likely deteriorate further.

Contributing factor

The captain became preoccupied with remaining fuel. This combined with an expectation of worsening visibility resulted in a sense of urgency to land off the first approach.

Continued communication regarding fuel

Brisbane air traffic control (ATC) had alerted the crew to the approaching low cloud bank about 18 minutes prior to landing. From the time of the alert until the landing, the CVR recorded continued concern from the captain. 

This concern included that they had ‘no fuel’ and ‘we haven't got the fuel for this’ as well as concern with the conditions stating, ‘the weather will only get worse’ and ‘if we can see the HIAL’s,[28] we’re going to land’. 

About 4 minutes prior to landing, the FO asked if it was possible to calculate the fuel needed to divert to the Gold Coast, to which the captain responded ‘not now, on final, but let's try and get in’. Shortly after the FO discussed the go‑around procedure in preparation for the DA, to which the captain reinforced their intention to land.

Although there was continued communication regarding the fuel state and visibility, no discussion was recorded regarding diversion plans to an alternative airport until established on the final approach. Additionally, the crew did not proactively obtain the weather conditions for alternate aerodromes, in the event that they were required to conduct a go-around without a planned diversion, limiting the crew’s options to return to conduct a second approach in Brisbane, further exacerbating the expectation of landing off the approach.

In contrast, the crew of the preceding aircraft on the approach prior to VH‑SAJ, advised that there was sufficient time during descent to plan for a diversion on receipt of the weather changes. Subsequent ATC recordings indicated that this crew also advised ATC of their intention to divert to the Gold Coast, if a go-around was required.

The FO had no previous experience in a multi‑crew environment and had only recently been checked to line. According to Fabre (2022), when a newly appointed FO is paired with a captain that they consider as experienced, the captain’s opinion strongly influences the FO’s decision‑making and significantly increases the likelihood of the crew attempting a moderate to high-risk landing scenario. The FO’s limited experience in the position and in a multi‑crew environment likely meant they were more susceptible to the captain’s pressure to land and less likely to voice any concerns.

The continued verbal concern over landing off the approach compounded pressure on the FO, which likely compelled them to commit to a landing on reaching the DA.

Contributing factor

Repeated communications from the captain regarding the need to land off the first approach likely increased pressure on the first officer to commit to a landing.

Crew appointments

The ASL Airlines Australia operations manual outlined the minimum experience requirements for the appointment of captains and first officers. However, neither the captain nor the FO met these requirements at the time of their engagement, nor at the time of the incident. 

In ‘exceptional circumstances’, the ASL Airlines Australia operations manual permitted the variance of the experience requirements with the specific approval of the director of flight operations. 

There was no evidence that ASL Airlines Australia had considered the hazards associated with the appointment of pilots that did not hold the required level of experience, nor was any control put in place to manage the risks. Such controls could have included, but were not limited to, operational limitations for low experience crew. The ATSB reviewed expositions from 6 CASR Part 121 operators and found that 5 had restrictions on FOs conducting landings in marginal meteorological conditions, including reduced visibility and low cloud. 

ASL Airlines Australia did not have such a policy, and it reported that having similar limitations could lead to FOs being promoted to captain without having acted as pilot flying in adverse weather conditions. However, the FO’s limited experience in marginal meteorological conditions likely contributed to the tail strike incident. Had a similar limitation been in place, it would likely have resulted in the captain assuming control when the crew were alerted to the low visibility at Brisbane Airport. 

ASL Airlines Australia had a rostering policy that prevented crew who had not accumulated 100 hours in their positions from being rostered together. However, there was no consideration made for crew who had been provided early promotion to their positions. As a result, the captain, promoted early to their position and at the time of the occurrence had not yet attained the minimum experience requirements to hold the position, was paired with an inexperienced FO. Without administrative controls in the rostering policy to prevent unsuitable pairing of crew without requisite experience, the result was a reduction in the intended experience level on the flight deck for the incident flight.

Contributing factor

ASL Airlines Australia employed and promoted pilots earlier than the prescribed minimum experience hours without additional controls in place to manage the risk of lower experienced pilots on the flight deck. (Safety issue)

Captain’s multi-crew experience 

The captain commenced with ASL Airlines Australia in November 2022, initially as a FO, before undertaking command upgrade training after 155 hours. They had held the position since February 2024 and had accrued 198 hours as a captain at the time of the incident. Prior to joining ASL Airlines Australia, the captain had not flown a jet aircraft and had mostly flown in single pilot operations. As discussed above in Crew appointments, the captain had been nominated for command upgrade training below the required 500 hours, and this reduced their opportunity: 

  • to gain valuable exposure operating in a multi-crew environment
  • to model behaviour on experienced captains’ decision making

prior to commencing in the captain role themselves. 

The missed opportunity to gain valuable multi-crew experience likely impacted the captain’s capacity to include the FO in the decision‑making process and limited the effectiveness of the crew during the approach. Although the captain was not the PF during the approach, the ultimate responsibility for the safety of the aircraft lay with themThe cockpit voice recording indicated that, although it was reasonable for the captain to assume the FO was competent in flying the ILS, they did not ask the FO if they were comfortable to continue the approach after being alerted to the low cloud, fog and changing weather conditions. Likewise, while the FO did not advise the captain that they were experiencing difficulties during the approach, the captain did not recognise other cues, such as the FO’s response when requested to disconnect the autopilot at the DA, their ability to clearly see the approach lighting on short final, or their obvious discomfort with the approach. 

It is likely that the captain’s limited command multi-crew experience may also have reduced their ability to establish an appropriate ‘cockpit gradient’ following advice that the meteorological conditions at Brisbane Airport were deteriorating. The term ‘cockpit gradient’ describes the level of authority that exists between the crew members, and the way this authority influences communication and decision‑making. Although the pilot in command has ultimate responsibility in terms of decision‑making, depending on the cockpit gradient, other crew members can be either encouraged or discouraged from influencing these decisions through their own inputs. 

A ‘steep’ cockpit gradient exists when the pilot in command has an overwhelming influence in decision‑making, with little input sought from other crew members. A steep gradient can ‘inhibit communication, coordination and the cross-checking of errors’ (Harris, 2011). The cockpit voice recording indicated a steep cockpit gradient existed during the approach phase, with the captain dismissing the FO’s request to recalculate diversion fuel or plans in the event of a go-around, thereby reducing the effectiveness of the decision‑making process.

The captain provided control input instructions to the FO during the final stages of the approach. Likely due to their limited experience in the captain role, they did not recognise that the approach would have been better handled by a more experienced crew member who had previously encountered comparable conditions. Consequently, no authoritative decision was made by the captain to assume the PF role or to command a go‑around when the aircraft entered an undesired state after autopilot disconnection. 

Contributing factor

The captain’s limited command experience in a multi-crew environment likely reduced their capacity to include the first officer in the decision‑making process, consider the need to assume the pilot flying role or command a go-around when the aircraft entered an undesired state during landing.

Captain’s control input

The captain reported that as the high sink rate developed, they anticipated the FO’s reaction and placed their hand on the control column to prevent any further increase in the aircraft’s pitch during the landing. This likely reduced the severity of airframe damage caused by the tail strike.

ASL Airlines Australia procedures stated that any control handover must be conducted in a positive manner to minimise confusion and operational risk. The FO recalled feeling the captain’s pressure on the control column preventing further rearward input, but the captain did not verbalise their actions at the time. While the control column input from the captain may have prevented further damage to the aircraft, it also risked confusion about who was in control of the aircraft during a critical stage of flight. 

Other finding

The captain prevented further rearward input by the first officer during the flare by placing their hand on the control column. While this action is not usually completed without the required takeover procedure it likely reduced the severity of the tail strike.

Findings

ATSB investigation report findings focus on safety factors (that is, events and conditions that increase risk). Safety factors include ‘contributing factors’ and ‘other factors that increased risk’ (that is, factors that did not meet the definition of a contributing factor for this occurrence but were still considered important to include in the report for the purpose of increasing awareness and enhancing safety). In addition, ‘other findings’ may be included to provide important information about topics other than safety factors. 

These findings should not be read as apportioning blame or liability to any particular organisation or individual.

From the evidence available, the following findings are made with respect to the ground strike involving British Aerospace BAe 146‑300, registered VH‑SAJ on 25 June 2024.

Contributing factors 

  • The first officer became disoriented after disconnecting the autopilot on short final and likely lost situation awareness. Consequently, they did not identify the increasing aircraft pitch attitude, decreasing airspeed, or low power setting and did not correct the resulting sink rate prior to touchdown.
  • The captain became preoccupied with remaining fuel. This combined with an expectation of worsening visibility resulted in a sense of urgency to land off the first approach.
  • Repeated communications from the captain regarding the need to land off the first approach likely increased pressure on the first officer to commit to a landing.
  • ASL Airlines Australia employed and promoted pilots earlier than the prescribed minimum experience hours without additional controls in place to manage the risk of lower experienced pilots on the flight deck. (Safety issue)
  • The captain’s limited command experience in a multi-crew environment likely reduced their capacity to include the first officer in the decision‑making process, consider the need to assume the pilot flying role or command a go-around when the aircraft entered an undesired state during landing

Other findings

  • The captain prevented further rearward input by the first officer during the flare by placing their hand on the control column. While this action is not usually completed without the required takeover procedure it likely reduced the severity of the tail strike.

Safety issues and actions

Central to the ATSB’s investigation of transport safety matters is the early identification of safety issues. The ATSB expects relevant organisations will address all safety issues an investigation identifies. 

Depending on the level of risk of a safety issue, the extent of corrective action taken by the relevant organisation(s), or the desirability of directing a broad safety message to the Aviation industry, the ATSB may issue a formal safety recommendation or safety advisory notice as part of the final report.

All of the directly involved parties are invited to provide submissions to this draft report. As part of that process, each organisation is asked to communicate what safety actions, if any, they have carried out or are planning to carry out in relation to each safety issue relevant to their organisation. 

Descriptions of each safety issue, and any associated safety recommendations, are detailed below. Click the link to read the full safety issue description, including the issue status and any safety action/s taken. Safety issues and actions are updated on this website when safety issue owners provide further information concerning the implementation of safety action.

Employment and promotion of pilots earlier than company minimum hours

Safety issue number: AO-2024-036-SI-01

Safety issue description: ASL Airlines Australia employed and promoted pilots earlier than the prescribed minimum experience hours without additional controls in place to manage the risk of lower experienced pilots on the flight deck.

Additional safety action by ASL Airlines Australia

The operator’s internal review identified an inconsistency between the operator’s standard operating procedures and the manufacturer’s recommendation with regard to which pilot (the pilot flying or the pilot monitoring) was to make an ‘attitude’ call when the aircraft pitch angle approaching landing increased above 5°.

ASL Airlines Australia’s internal investigation of the occurrence will be incorporated into the relevant sections of the ASL Airlines Australia HF/NTS training.

A summary of the internal investigation will also be included in the operator’s internal safety publication.

Glossary

 

ATCAir traffic control
ATISAutomatic terminal information service
CAACivil Aviation Authority (UK)
CASACivil Aviation Safety Authority
CASRCivil Aviation Safety Regulations
CCTVClosed circuit television
CVRCockpit voice recorder
DFODirector of flight operations
DADecision altitude
FOFirst officer
ILSInstrument landing system
LED Light-emitting diode
METARMeteorological aerodrome report
OPCOperator proficiency check
PAPIPrecision approach path indicator
PFPilot flying
PM Pilot monitoring
TAFTerminal area forecast
TEMPOTemporary significant variation to prevailing conditions
WOCLWindow of circadian low 

Sources and submissions

Sources of information

The sources of information during the investigation included:

  • ASL Airline Australia flight records from the occurrence aircraft
  • ASL Airlines Australia Operations Manuals and Standard Operating Procedures for the BAe 146
  • the captain and first officer of the occurrence aircraft
  • the director of flying operations, ASL Airlines Australia
  • Civil Aviation Safety Authority
  • BAE Systems
  • Airservices Australia
  • cockpit voice recorder and flight data recorder
  • Brisbane Airport Corporation CCTV images
  • the captains from the 2 preceding aircraft to VH-SAJ
  • Bureau of Meteorology
  • Flight Radar24
  • Google Earth

References

Australian Transport Safety Bureau. (2009). Tail Strike, Brisbane Airport, Queensland, on 23 October 2008, VH-NJM, British Aerospace BAe 146-300. Retrieved from /publications/investigation_reports/2008/aair/ao-2008-074

Australian Transport Safety Bureau. (2016). Tail strikes during landing involving Bombardier DHC-8 402, VH-QOT and VH-QOS, Brisbane Airport, Queensland, on 5 November 2013 and Roma Airport, Queensland, on 11 December 2013. AO-2013-201.

Causse. (2024). How a pilot's brain copes with a stress and mental load.

Civil Aviation Safety Aurthority. (2024). Civil Aviation Safety Regulations 1998. Retrieved from CASR 121.495: https://www.legislation.gov.au/F1998B00220/latest/text/3

Endsley, M. (1988). Design and evaluation for situation awareness enhancement. Proceedings of the Human Factors Society 32nd Annual Meeting , 97-101.

Fabre, D. E. (2022, June). AXA. Retrieved from Hierarchy in the cockpit: understanding decision making at the time of landing: https://www.axa.com/en/insights/hierarchy-in-the-cockpit-understanding-…

Federal Aviation Administration. (n.d.). Spatial Disorientation Visual Illusion.

Garland, D. W. (1999). Handbook of Aviation Human Factors. Mahwah, NJ.

Harris, D. (2011). Human Performance on the Flight Deck. Ashgate Surrey, England.

Hirshkowitz, M. W.-4. (2015). National Sleep Foundation’s sleep time duration recommendations: methodology and results summary. Sleep health.

Institute, Battelle Memorial. (1998). An Overview of the scientific literature concerning fatigue, sleep and the circadian cycle.

International Civil Aviation Organisation. (2015). ICAO, Fatigue Management Guide for Airline Operators. Retrieved from ICAO:

Roach, G. D. (2004). A model to predict work-related fatigue based on hours of work. Aviation, Space and Environmental Medicine,.

Salas, & Maurino. (2010). Human Factors in Aviation, Second edition. 

United Kingdom Civil Aviation Authority. (2023). Flight-crew human factors handbook. Retrieved from https://www.caa.co.uk/publication/download/14984

Submissions

Under section 26 of the Transport Safety Investigation Act 2003, the ATSB may provide a draft report, on a confidential basis, to any person whom the ATSB considers appropriate. That section allows a person receiving a draft report to make submissions to the ATSB about the draft report. 

A draft of this report was provided to the following directly involved parties:

  • Director of Safety, ASL Airlines Australia
  • the captain
  • the first officer
  • Civil Aviation Safety Authority
  • Air Accidents Investigation Branch, United Kingdom
  • Part 121 aircraft operator (party with involvement)
  • Bureau of Meteorology
  • Airservices Australia.

Submissions were received from:

  • the captain
  • ASL Airlines Australia
  • Civil Aviation Safety Authority
  • Bureau of Meteorology.

The submissions were reviewed and, where considered appropriate, the text of the report was amended accordingly.

Purpose of safety investigations

The objective of a safety investigation is to enhance transport safety. This is done through: 

  • identifying safety issues and facilitating safety action to address those issues
  • providing information about occurrences and their associated safety factors to facilitate learning within the transport industry.

It is not a function of the ATSB to apportion blame or provide a means for determining liability. At the same time, an investigation report must include factual material of sufficient weight to support the analysis and findings. At all times the ATSB endeavours to balance the use of material that could imply adverse comment with the need to properly explain what happened, and why, in a fair and unbiased manner. The ATSB does not investigate for the purpose of taking administrative, regulatory or criminal action.

Terminology

An explanation of terminology used in ATSB investigation reports is available here. This includes terms such as occurrence, contributing factor, other factor that increased risk, and safety issue.

Publishing information

Released in accordance with section 25 of the Transport Safety Investigation Act 2003

Published by: Australian Transport Safety Bureau

© Commonwealth of Australia 2025

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Copyright in material obtained from other agencies, private individuals or organisations, belongs to those agencies, individuals or organisations. Where you wish to use their material, you will need to contact them directly.

[1]     The flight was operated under Civil Aviation Safety Regulations Part 121 (Air transport operations – larger aeroplanes).

[2]     Pilot flying and pilot monitoring: procedurally assigned roles with specifically assigned duties at specific stages of a flight. The PF does most of the flying, except in defined circumstances, such as planning for descent, approach and landing. The PM carries out support duties and monitors the PF’s actions and the aircraft’s flight path.

[3]     Runways are named by a number representing the magnetic heading of the runway. Parallel runways are represented by an L for left and R for right.

[4]     Flight level: at altitudes above 10,000 ft in Australia, an aircraft’s height above mean sea level is referred to as a flight level (FL). 

[5]     ATIS: an automatic service which broadcasts airport specific information on the aviation VHF radio frequencies. 

[6]     Few: 1–2 okta of cloud cover. An Okta is a unit of measurement used to describe the extent of cloud cover (1–8).

[7]     Scattered: 3–4 okta of cloud cover. An Okta is a unit of measurement used to describe the extent of cloud cover (1–8).

[8]     Decision altitude is a specified altitude in the precision approach at which a missed approach must be initiated if the required visual reference to continue the approach has not been established.

[9]     Runway Visual Range: measured using an electronic instrument RVR is the maximum distance at which the runway, or lights or markers delineating it, can be seen from a position above a specified point on its centreline.

[10]    BAe 146 airbrake forms part of the aircraft’s tail cone when in the closed position, two petals extend from the tail cone to provide aerodynamic resistance and slow the aircraft.

[11]    Precision Approach Path Indicator (PAPI): a ground-based system that uses a system of coloured lights used by pilots to identify the correct glide path to the runway when conducting a visual approach. Four white PAPI lights on approach indicate the aircraft is too high.

[12]    Flare: the final nose-up pitch of a landing aeroplane used to reduce the rate of descent to about zero at touchdown.

[13]    Light-emitting Diode: a semiconductor diode which glows when a voltage is applied.

[14]    Category 1 (CAT I) lighting system: a CAT I lighting system normally consists of a row of lights on the extended centre line of the runway extending over a distance of 900 m from the runway threshold.

[15]    TAF: a statement of meteorological conditions expected for a specific period of time in the airspace within a radius of 5 NM (9 km) of the aerodrome reference point.

[16]    Broken: 5–7 okta of cloud cover. An okta is a unit of measurement used to describe the extent of cloud cover (1–8).

[17]    INTER: an intermittent deterioration in the forecast weather conditions, during which a significant variation in prevailing conditions is expected to last for periods of less than 30 minutes duration.

[18]    Advection fog develops when warm moist air moves (advects) over a cooler surface resulting in the cooling of the air to below its dew-point temperature, and subsequent saturation and condensation.

[19]    Tempo: used to indicate significant temporary variations from the prevailing conditions of 30 minutes or more but less than 60 minutes.

[20]    L3: now L3 Harris Technologies, Inc. Melbourne, Florida, USA.

[21]    Vref: reference landing speed calculated on the aircrafts gross weight for landing.

[22]    Vapp: reference approach speed when the flaps are in landing configuration and the landing gear extended.

[23]    N1: presents the rotational speed of the low pressure (low speed) engine spool.

[24]    Oleo: an oleo strut is a pneumatic air–oil hydraulic shock absorber used on the landing gear of most large aircraft

[25]    RAIM: receiver autonomous integrity monitoring – used to assess the integrity of individual signals collected by a GPS receiver.

[26]    Minima: landing minima consist of both visibility and/or RVR, and cloud base elements.

[27]    The self-report instrument utilised the Samn-Perelli Fatigue Checklist, which utilises a 7‑point scale ranging from “1 – Fully Alert, Wide Awake” to “7 – Completely Exhausted, Unable to Function Effectively” (Samn & Perelli, 1982).

[28]    HIAL’s: high intensity approach lighting.

Occurrence summary

Investigation number AO-2024-036
Occurrence date 25/06/2024
Location Brisbane Airport
State Queensland
Report release date 09/09/2025
Report status Final
Investigation level Defined
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Ground strike, Unstable approach
Occurrence class Serious Incident
Highest injury level None

Aircraft details

Manufacturer British Aerospace
Model BAe 146 Series 300
Registration VH-SAJ
Serial number E3150
Aircraft operator ASL Airlines Australia
Sector Jet
Operation type Part 121 Air transport operations - larger aeroplanes
Departure point Sydney Airport, New South Wales
Destination Brisbane Airport, Queensland
Damage Minor

Pilots urged to properly declare all medical information

The ATSB urges pilots to monitor changes in their health and lifestyle and properly declare all medical information during aviation medical examinations, following an investigation into a JetRanger helicopter accident near Maitland.

On 6 October 2022, the pilot of a Bell 206B JetRanger left Casino in northern New South Wales for a solo ferry flight to Warnervale on the Central Coast.

While transiting the Williamtown military restricted area via the inland visual flight rules lane, the helicopter turned around and deviated outside the lane, and the pilot did not respond to radio calls from air traffic control.

The helicopter then flew south, exiting the restricted area about 500 ft above ground level. 

Witnesses then observed the helicopter heading towards the Hunter River, descend slightly and possibly began to turn, before rolling markedly and descending rapidly. The helicopter collided with the riverbank and was destroyed, and the pilot was fatally injured.

The ATSB’s investigation found it was likely the pilot experienced an incapacitating event prior to the accident.

“While it was not possible to forensically determine if the pilot experienced a heart attack, it remained a significant risk factor,” ATSB Director Transport Safety Kerri Hughes said.

A cardiology review undertaken less than 12 months before the accident found only minor coronary artery disease in the pilot. However, the pilot’s post-mortem showed they had severe coronary atherosclerosis within all 3 major coronary arteries, with at least 80% blockage observed within each artery.

“This accident reinforces to pilots the importance of remaining aware of any health and lifestyle changes, and how these may affect your fitness to fly.”

While not determined to have contributed to the accident, the ATSB also found the pilot had not declared a significant surgery during their most recent aviation medical examination, nor the use of numerous prescribed, and non-prescribed drugs.

“Pilots are responsible for declaring their full medical history and medication use at the time of an aviation medical examination, so CASA and your designated aviation medical examiner can assess suitability for flying,” Ms Hughes stressed.

“Don’t fly if feeling unwell and manage chronic conditions in association with your DAME. They are best placed to balance your personal medical risks against those of aviation safety.”

The report also notes at least one of the undeclared non-permitted medications being used by the pilot had an alternative, which would have allowed the pilot to continue flying.

“Alternative medication may be available to medications that are incompatible with flying,” Ms Hughes said.

Read the final report: Collision with terrain involving Bell Helicopter 206B, VH-PHP, 6.5 km east-north-east of Maitland Airport, New South Wales, on 6 October 2022

Flight preparation event involving Hawker Beechcraft Corporation B200, Darwin Airport, Northern Territory, on 8 May 2024

Occurrence Briefs are concise reports that detail the facts surrounding a transport safety occurrence, as received in the initial notification and any follow-up enquiries. They provide an opportunity to share safety messages in the absence of an investigation.

What happened

On 8 May 2024, a Hawker Beechcraft B200 was being prepared for an air transport flight at Darwin Airport.

Prior to departure, the pilot conducted a pre-flight inspection of the aircraft. A critical step in this process was to remove pitot covers from the pitot tubes[1] on both the front left and right side of the aircraft’s fuselage. These covers protect the tube from contamination and are designed to slide on and off the pitot tubes. They consisted of a cover placed over the pitot tube and an attached red flag, which provided a visual reminder to pilots and ground crew that the covers had been applied and needed to be removed prior to departure.

The pilot completed the preflight inspection, confirmed that both red flags were in their possession, and secured these items along with the propeller covers inside the aircraft. However, the pilot did not detect that the flag for the right-side cover had detached from the cover, nor that the cover was still attached to the pitot tube. This went unnoticed by the pilot and ground personnel, and the aircraft subsequently taxied to the runway with the right-side pitot cover still in place.

The pilot commenced the take-off run, but during rotation[2] they detected a speed discrepancy on their cockpit instrumentation. The pilot continued the climb to 3,000 ft before returning via a visual approach to Darwin Airport. 

During the post-flight inspection, the pilot identified that the right-side pitot cover was still in place, covering the pitot tube. This prevented airflow from entering the pitot tube, which subsequently prevented the aircraft’s pitot-static system from operating as designed. 

Safety message

This incident highlights the importance of conducting an airspeed check early in the take‑off run. This allows the take-off to be rejected as soon as an airspeed mismatch is detected.

It also illustrates the importance of maintaining a high level of attention and awareness when doing visual inspections of critical aircraft systems such as the pitot tubes and static ports. It is important that the pitot tubes and static ports are fully uncovered and free from obvious obstructions, contamination, or damage prior to departure. 

Pilots should also remain cognisant of the risk that pitot covers may not be sufficiently conspicuous when installed on the aircraft, and that tags or streamers may not be robust enough to remain attached to the cover when pilots attempt to remove these items during their regular pre-flight inspections. Targeted inspections of specific aircraft components, along with secondary means of accounting for ground-based protective equipment, can provide an extra layer of assurance that these items have been removed from the aircraft and are safely stowed prior to departure. 

About this report

Decisions regarding whether to conduct an investigation, and the scope of an investigation, are based on many factors, including the level of safety benefit likely to be obtained from an investigation. For this occurrence, no investigation has been conducted and the ATSB did not verify the accuracy of the information. A brief description has been written using information supplied in the notification and any follow-up information in order to produce a short summary report, and allow for greater industry awareness of potential safety issues and possible safety actions.

[1]     Pitot tubes are part of the aircraft's pitot-static system and are used to compute the aircraft's indicated airspeed

[2]     Rotation: the positive, nose-up, movement of an aircraft about the lateral (pitch) axis immediately before becoming airborne.

Occurrence summary

Mode of transport Aviation
Occurrence ID AB-2024-025
Occurrence date 08/05/2024
Location Darwin Airport
State Northern Territory
Occurrence class Incident
Aviation occurrence category Flight Preparation / Navigation
Highest injury level None
Brief release date 24/06/2024

Aircraft details

Manufacturer Hawker Beechcraft Corporation
Model B200
Sector Turboprop
Operation type Part 135 Air transport operations - smaller aeroplanes
Departure point Darwin Airport, Northern Territory
Destination Darwin Airport, Northern Territory
Damage Nil

Flight below minimum altitude involving Boeing 737, PK-LDK, 19 km south of Canberra Airport, New South Wales, on 14 June 2024

Final report

Report release date: 17/06/2025

Investigation summary

What happened

On the evening of 13 June 2024, a Batik Air Boeing 737-800, registered PK-LDK, departed I Gusti Ngurah Rai (Denpasar) International Airport, Bali, Indonesia for the inaugural passenger transport flight of a new service to Canberra, Australian Capital Territory. While en route, the flight crew noted that the estimated time of arrival into Canberra was prior to 0600 local time on 14 June, when Canberra Tower and Approach air traffic control began providing services for the day. The crew elected to proceed without any delays and prepared for an arrival without those air traffic control services, using the Canberra Airport common traffic advisory frequency (CTAF).

As the aircraft was descending toward uncontrolled airspace and tracking direct to Canberra along the flight path cleared by air traffic control, the crew deviated from the cleared track by commencing the AVBEG 5A standard arrival route (STAR). The duty air traffic controller intervened and provided altitude instructions to maintain separation from an en route restricted area. This intervention resulted in the aircraft becoming higher than the desired descent profile and the crew decided to use the holding pattern at the approach waypoint of MOMBI to reduce altitude. While flying the holding pattern at MOMBI, the aircraft was descended to 4,700 ft above mean sea level (AMSL), significantly below the holding pattern minimum safe altitude of 5,600 ft AMSL. The aircraft’s recorded radio height subsequently reduced to a minimum of 924 ft above ground level before the approach was recommenced from 4,700 ft AMSL, below the 5,400 ft AMSL minimum altitude for that segment of the approach.

The Canberra Approach controller who took over management of the airspace while the aircraft was in the holding pattern identified that the aircraft was operating below the minimum altitude, contacted the crew to provide a safety alert and advised the crew to contact Canberra Tower. The approach continued using controlled airspace procedures and the aircraft landed shortly after without further incident.

What the ATSB found

The ATSB found that the MOMBI holding pattern was not correctly flown by the crew and resulted in the aircraft descending significantly below the minimum safe altitude. The Canberra CTAF was also not selected by the crew, and the appropriate radio broadcasts were not made. This prevented the crew from receiving the oncoming Canberra tower controller's safety alerts, being able to illuminate the runway lights and increased the risk of conflict with other traffic.

Prior to commencing the approach, when the crew deviated from the cleared track to Canberra by commencing the AVBEG 5A STAR, the air traffic controller did not advise them of the deviation or provide a safety alert. Instead, the controller provided instructions that contributed to the crew becoming confused regarding the airspace classification for the arrival and approach. 

The Melbourne Centre controller providing the flight information service for the aircraft was not, and was not required to be, aware of the holding pattern minimum altitudes. Therefore, the controller did not issue a safety alert when the aircraft descended below the minimum safe altitude.

The ATSB also found that Batik Air's change management processes were not effective at fully identifying and mitigating the risks associated with the commencement of the Denpasar to Canberra route. Batik Air also did not ensure that the crew had completed all CTAF training prior to them operating flights into Australia where the use of these procedures could be required.

The investigation also determined that during a 2022 review of Canberra runway 35 instrument landing system approaches, an obstacle evaluation error led to Airservices Australia increasing the MOMBI holding pattern minimum altitude from 5,100 ft to 5,600 ft. This increase resulted in a transition from the holding pattern to the approach glideslope that increased the risk of unstable approaches and sudden pitch ups. After conducting a revalidation test flight of the holding pattern minimum altitude increase, the Civil Aviation Safety Authority advised Airservices Australia that the increased minimum altitude did not provide an appropriate transition to the approach glideslope and recommended modifications to the holding pattern design. Despite Airservices Australia receiving this advice, no changes were made, and the increased holding pattern minimum altitude was maintained.

What has been done as a result

Following the incident, Batik Air has implemented several proactive safety actions including: 

  • Revising the Canberra Airport Briefing document to include detailed information on Canberra air traffic control hours, CTAF procedures, holding requirements and guidance for adherence to lowest safe altitude requirements.
  • Issuing internal notices to flight crew highlighting the importance of a comprehensive approach briefing, adherence to air traffic control instructions and altitude awareness. These notices also provided information on CTAF and traffic information by aircraft (TIBA) procedures and highlighted the additional risks and absent protections when operating in uncontrolled airspace. Batik Air also disseminated details of the incident to all flight crew and conducted a special flight crew briefing with event details and lessons.
  • Completing practical and theoretical CTAF training for all flight crew assigned to Australian operations and incorporating this training into its annual training program.
  • Issuing an internal notice highlighting the mandatory Risk Management Review (RMR) process for all new routes and other significant operational changes. This notice intends to ensure comprehensive hazard identification, detailed risk assessments and an evaluation of the need for route proving flights or additional crew familiarisation.
  • Adjusting the flight schedule for the Denpasar to Canberra flight to ensure that early arrivals occur during Canberra Tower and Approach air traffic control operating hours.

In December 2024, Airservices Australia reassessed the MOMBI holding pattern and reduced the minimum holding altitude back to 5,100 ft.

Safety message

This incident underlines the need for operators to ensure that they have comprehensive and effective change management processes in place to identify all foreseeable risks relevant to a new route and implement appropriate mitigations to ensure the safe operation of these routes. In this case, the unfamiliar operating environment included the potential for operations using a CTAF, an uncommon operating procedure for non‑Australian operators and crews. Comprehensive and regular crew training is vital in ensuring that crews can effectively manage the risks inherent in the use of unusual procedures.

Additionally, the investigation highlights the importance of suitably designed and appropriate instrument flight procedures for safe air transport operations. In this case, the error made in the holding pattern design was not identified before it was published and while the error did not contribute to this occurrence, it introduced the potential for an unstable approach and/or a sudden pitch up risk to flight crews using the procedure.

The occurrence

On the evening of 13 June 2024, a Batik Air Boeing 737-800, registered PK-LDK, departed I Gusti Ngurah Rai (Denpasar) International Airport, Bali, Indonesia for the inaugural passenger transport flight of a new service to Canberra, Australian Capital Territory. The flight was operating with an enlarged flight crew, the captain was acting as pilot flying, the first officer was acting as pilot monitoring[1] and a second captain was occupying the flight deck jump seat.[2]

As the aircraft climbed to the cruising level of flight level 350,[3] the crew input forecast en route winds, which included strong tailwinds, into the aircraft’s flight management system. The crew noted that the estimated time of arrival into Canberra was prior to 0600 local time on 14 June, when Canberra Tower and Approach air traffic control began providing services for the day (see the section titled Canberra Airport and airspace). The crew elected to continue to Canberra without any en route delays and prepared for an arrival without those air traffic control services, using the Canberra Airport common traffic advisory frequency (CTAF). 

As the aircraft descended towards Canberra in darkness, the flight was cleared by air traffic control (ATC) to track via the waypoint AVBEG direct to Canberra Airport and to descend to FL 120. During the descent, the crew prepared to conduct the AVBEG 5A standard arrival route (STAR) (see the section titled AVBEG 5A standard arrival route and restricted areas)but did not make a request to track via the STAR to the Melbourne Centre air traffic controller managing the airspace.

At 0541 local time, as the aircraft approached AVBEG, ATC cleared the crew to leave controlled airspace descending. The aircraft crossed AVBEG while descending below FL 205 and commenced tracking via the AVBEG 5A STAR. 

At 0543, the controller managing the airspace handed over management of the airspace to a controller commencing work. This oncoming controller identified that the Batik Air flight was deviating from the cleared track (direct to Canberra) presented in the ATC system while still in controlled airspace. The oncoming controller was unsure if the aircraft was deviating from its clearance or if it had been provided the clearance by the outgoing controller and that clearance had not been entered into the ATC system. The controller also noted that the aircraft was descending toward an active restricted area (Figure 1).

The controller did not query the crew’s deviation or provide a safety alert (see the section titled Safety alerts) but instead asked the crew if they were going to remain clear of the restricted area 17 NM to the south of their position. The crew advised the controller that they were tracking via the AVBEG 5A STAR. The controller acknowledged the tracking advice and instructed the crew to maintain 10,000 ft above mean sea level (AMSL) to remain above the restricted area. After receiving this instruction, the crew became uncertain as to whether the aircraft would be operating within, or outside of, controlled airspace during the STAR and approach.

Figure 1: Overview of the descent

A satellite image overlaid with the aircraft's flight path for the descent. The location of the restricted area, AVBEG and Canberra are annotated.

 Source: Google Earth, recorded flight data, Airservices Australia and ATSB

The crew levelled the aircraft at 10,000 ft AMSL with the autopilot engaged and the aircraft passed over the restricted airspace. As was required by ATC procedures, the controller waited until the aircraft was observed to be more than 2.5 NM past the restricted area before instructing the crew to continue the descent to leave controlled airspace. The crew responded by advising that they would descend and continue tracking via the STAR. At about this time, the crew noted that the aircraft was about 1,300 ft above the desired descent profile for the arrival.

At 0551, the crew requested confirmation from ATC that they had clearance to conduct the instrument landing system (ILS) approach to runway 35 at Canberra. The controller responded by advising that the Canberra control tower was closed and that CTAF procedures applied for that airspace. At 0551:38, the aircraft descended below 8,500 ft AMSL, outside controlled airspace (into class G airspace).

As the aircraft was higher than the desired flightpath, the captain decided to conduct a holding pattern at the approach waypoint of MOMBI to reduce altitude and the first officer requested ATC clearance to hold at MOMBI. The controller responded by providing traffic information for the MOMBI holding pattern. At 0552:56, the crew again requested confirmation that they had clearance to conduct the ILS approach and the controller responded by advising that clearance was not required, the crew were now in class G (non-controlled) airspace and that the crew must broadcast their intentions on the Canberra CTAF.

At 0553:10, the aircraft passed the ILS initial approach fix waypoint MENZI (Figure 2) while descending below 6,720 ft AMSL and soon after, made another request to hold at MOMBI. The controller provided traffic information for the hold and requested that the crew make a right‑hand orbit to remain clear of the restricted airspace, now to the west of the aircraft.

Figure 2: Overview of arrival

A satellite image overlaid with the aircraft's flight path for the arrival. The location of the restricted area, the arrival waypoints and ILS approach are annotated.

Source: Google Earth, recorded flight data, Airservices Australia and the ATSB

As the aircraft approached MOMBI, the captain entered 5,400 ft AMSL (the approach’s minimum safe altitude before intercepting the ILS glideslope) into the autopilot mode control panel (MCP) and at 0554:15, the aircraft descended below the minimum holding altitude of 5,600 ft AMSL (see the section titled Instrument landing system approach) before levelling at 5,400 ft AMSL.

The captain then used the heading select function to make a right turn to a heading of 170°[4] and the aircraft commenced turning prior to crossing MOMBI. At 0554:30, the aircraft passed MOMBI at a speed of 172 kt (2 kt above the maximum speed for the 5,600 ft AMSL minimum holding altitude).

The captain then asked the first officer to enter a holding pattern into the aircraft’s flight management system (FMS) at MOMBI. As the aircraft had already passed MOMBI, the waypoint had dropped off the FMS track and the first officer was required to manually re‑enter the waypoint into the FMS planned track. As the turn continued, the speed reduced below 170 kt, the captain selected 4,700 ft AMSL (the crew’s intended MOMBI crossing altitude) on the autopilot MCP and the aircraft commenced descending to that altitude. During this time, the Melbourne Centre controller did not identify that the aircraft was operating below the minimum holding altitude of 5,600 ft AMSL.

The aircraft turned to a heading of 170° and continued descending until levelling at 4,700 ft AMSL at 0555:59. As the aircraft tracked south, the oncoming Canberra Approach air traffic controller prepared to take control of the Approach airspace (see the section titled Canberra Tower and Approach) and commenced a handover with the Melbourne Centre controller.

The aircraft continued south and at 0556:25, proceeded beyond the 14 distance measuring equipment (DME) limit for the 5,600 ft AMSL minimum holding altitude. At or before that DME limit, an inbound turn back to MOMBI needed to be commenced, or the minimum holding altitude had to be increased to 6,000 ft AMSL to maintain clearance from higher terrain further to the south. By that time, the first officer had completed re‑entering MOMBI into the FMS and the captain then used the lateral navigation autopilot mode to commence a right turn toward the waypoint.

As the aircraft was turning back toward MOMBI, at 0556:58, the incoming Canberra Approach controller completed their handover with the Melbourne Centre controller and took over the airspace as well as the Melbourne Centre radio frequency that the aircraft was using (this frequency then became a Canberra Approach frequency).

At the same time, the Canberra Tower air traffic controller preparing to commence the tower service observed that the aircraft was operating below the minimum holding altitude and made multiple attempts to contact the crew on the Canberra CTAF. At that time, the crew had not selected the Canberra CTAF and did not receive these broadcasts. As the Tower controller did not have a direct means of communication with the Melbourne Centre controller, the Tower controller contacted a Melbourne Approach air traffic controller to relay their concerns to the Melbourne Centre controller.

The aircraft continued turning toward MOMBI (Figure 3) and as it crossed over the eastern slopes of Mount Campbell at 0557:46, the recorded radio height reduced to a minimum of 924 ft above ground level. The aircraft did not penetrate the ground proximity warning system activation envelope and no alert was generated. At 0558:21, the aircraft rejoined the ILS approach.

Figure 3: Overview of MOMBI hold

A satellite image overlaid with the aircraft's flight path for the MOMBI HOLD. The location of the descent below the minimum safe latitude, the approach waypoints of KATIA and MOMBI, the position of the minimum recorded height and the safety alert are all annotated.

Source: Google Earth, recorded flight data, Airservices Australia and the ATSB

The Melbourne Approach controller contacted the Melbourne Centre controller to relay the Canberra Tower controller’s concerns about the aircraft’s altitude and the Melbourne Centre controller responded by advising that the airspace was now being controlled by Canberra Approach.

At about the same time, the Canberra Approach controller also identified that the aircraft was operating below the minimum altitude. The controller contacted the crew and provided a safety alert, querying whether the crew were ‘visual’. The crew responded advising that they were ‘visual with the runway’ and continued the approach. The Approach controller then advised the crew to contact Canberra Tower and the approach continued using controlled airspace procedures. The aircraft landed at 0602 without further incident.

Context

Canberra Airport and airspace

Canberra Tower and Approach

On the day of the incident, the operating hours of controlled airspace associated with Canberra Airport were 0600 to 2300 local time. During these hours, Canberra Airport was within class C airspace, with airspace bases that increased as the airspace fanned out at increasing distances from the airport (Figure 4). The Canberra Tower and Approach air traffic control (ATC) services controlled the class C airspace within 30 DME of Canberra and below 8,500 ft above mean sea level (AMSL). Control services for the airspace above 8,500 ft AMSL were provided by a Melbourne Centre controller at all times during the flight’s descent and approach.

Figure 4: Canberra airspace when Tower and Approach were operating

A profile view of Canberra airspace when Approach and Tower ATC services are operating. The figure shows that the base of the class C airspace reduces as it gets closer to Canberra. Also shown is the area controlled by Approach and Tower, below 8,500 ft.

All altitudes and elevations are above mean sea level. Source: ATSB

Outside of the Canberra Tower and Approach operating hours, the base of the Class C airspace was 8,500 ft AMSL. Below this was class G, non‑controlled airspace (Figure 5). Within class G airspace, flight crews could manoeuvre aircraft as required to position for an approach and were responsible for maintaining adequate terrain clearance. ATC was unable to issue STARs or approach clearances within class G airspace. 

Figure 5: Canberra airspace when Tower and Approach were not operating

A profile view of Canberra airspace when Approach and Tower ATC services are not operating. The area otherwise controlled by Approach and Tower, below 8,500 ft when they are operating is shown to be class G airspace.

All altitudes and elevations are above mean sea level. Source: ATSB

Common traffic advisory frequency

When the Canberra Approach and Tower services were not operating, flight crew used a common traffic advisory frequency (CTAF) to make positional radio broadcasts and coordinate self‑separation with other traffic. The CTAF used the same frequency as Canberra Tower (when it was operational). 

Pilot‑activated lighting

When Canberra Tower services were not available, the runway and movement area lighting was activated using a pilot-activated lighting system. The lighting was activated by a series of timed transmissions on the CTAF and remained active for 30 minutes.

Aviation rescue firefighting service

Canberra Airport aviation rescue and firefighting services operated only during times advised by NOTAM.[5] On the day of the incident, category 7 rescue and firefighting services[6] were provided from 0540 until 2225. Outside of these hours, no rescue or firefighting service was provided at the airport.

Air traffic control procedures

Manual of air traffic standards
Safety alerts

Airservices Australia’s manual of air traffic standards stated that an air traffic controller must issue a safety alert as soon it is recognised that an aircraft has deviated from an air traffic control clearance and will enter an active restricted area or is operating in unsafe proximity to terrain.[7] Additionally, if possible, a controller was required to provide an alternative clearance.

Track deviation

When observed, air traffic controllers were required to advise flight crews of flight path deviations.[8]

Controller knowledge

When the aircraft descended below the MOMBI holding pattern minimum altitude, the aircraft was operating in non‑controlled airspace. Within that airspace, aircraft operating under the instrument flight rules, such as the incident flight, were only provided with a flight information service.

The Melbourne Centre controller providing the flight information service for this airspace held an area radar control rating. This rating did not require a controller to have knowledge of STAR altitude restrictions and minimum holding altitudes associated with instrument approaches to airports located in non‑controlled airspace, nor did it require controllers be trained to provide specific instructions or corrections to pilots conducting instrument arrivals. The appropriate instrument flight procedure charts were available to the controllers using electronic displays at the control console, but area radar‑rated controllers were not required to know the details of the charts and only required to have awareness of broader lowest safe altitudes within that airspace.

Controllers providing an approach service within controlled airspace (such as the airspace that became active as the aircraft rejoined the approach) were trained to have more detailed knowledge of instrument approach procedures within the airspace. In addition, automated minimum safe altitude warning alerts were generated by the air traffic control system within that airspace.

When the aircraft descended below the minimum safe altitude of the MOMBI holding pattern, the Melbourne Centre controller providing the flight information service was not aware that this had occurred and therefore did not provide a safety alert. The oncoming Canberra Approach and Tower controllers both identified the aircraft operating below the minimum safe altitude. The Tower controller tried several times to contact the crew, but the crew did not have that frequency selected. The Approach controller issued a safety alert to the crew at the earliest available opportunity.

Canberra instrument flight procedures

AVBEG 5A standard arrival route and restricted areas

South‑west of Canberra Airport, restricted areas of airspace (R430 A‑C) encompassed the Canberra Deep Space Communication Complex at Tidbinbilla. The uppermost of these restricted areas (R430C) had a radius of 10 NM and a ceiling of 10,000 ft AMSL. The AVBEG 5A standard arrival route (STAR) (Figure 6) passed over this restricted area and had a 10,000 ft AMSL descent restriction at the waypoint LANYO which prevented aircraft descending via the STAR from entering the restricted area.

Figure 6: AVBEG 5A standard arrival route

The AVBEG 5A STAR chart. The location of the restricted areas, beneath the STAR flight path and the LANYO altitude restriction are annotated.

Source: Batik Air and Navblue, annotated by the ATSB

Instrument landing system approach

An instrument landing system (ILS) is an instrument approach procedure that provides lateral (localiser) and vertical (glideslope) position information using angular deviation signals from the localiser antennas (located past the upwind end of the runway) and the glideslope antennas (located approximately 1,000 ft from the runway threshold).

The AVBEG 5A STAR connected with the Canberra runway 35 ILS Y approach at the initial approach fix waypoint MENZI. The minimum crossing height for MENZI was 5,400 ft AMSL. The ILS approach from MENZI included a 3° glidepath to the runway which crossed MENZI at 6,040 ft and the approach waypoint of MOMBI at 4,760 ft AMSL.

The approach included a right turn, 1-minute holding pattern at the approach waypoint MOMBI (Figure 7) available for use if required. The minimum holding altitude at MOMBI was 5,600 ft AMSL. To use that minimum altitude, the crew was required to adhere to a maximum speed of 170 kt and a 14 DME limit from the Canberra DME for commencing the inbound turn back to MOMBI. A higher minimum holding altitude of 6,000 ft AMSL could also be used which allowed for a higher maximum speed of 210 kt with no DME limit.

Figure 7: Canberra runway 35 instrument landing system approach

The Canberra runway 35 ILS Y approach chart. The holding information and MOMBI glidepath crossing height are annotated.

Source: Airservices Australia, annotated by the ATSB

Increase to MOMBI holding pattern minimum altitude
Incorrect assessment area

In March 2022, Airservices Australia undertook a required 3-yearly review of Canberra instrument flight procedures. During this review, the reference file for the MOMBI holding pattern could not be retrieved within the procedure design software. To conduct the review, the reviewing designer imported a new procedure template and assessed the relevant terrain and obstacles for the holding pattern. This assessment unintentionally omitted the area reduction associated with the 14 DME limit for the outbound leg of the holding pattern. Therefore, the assessed area was larger than necessary and included higher obstacles that necessitated an increase from the existing 170 kt speed‑limited minimum holding altitude of 5,100 ft to 5,600 ft. The minimum altitude for the 210 kt speed‑limited pattern remained 6,000 ft. These 170 kt and 210 kt speed‑limited minimum altitudes were respectively 840 ft and 1,240 ft above the unchanged 4,760 ft glidepath crossing height at MOMBI. The assessment and increased holding altitudes underwent an internal review, but the error was not identified. Airservices Australia then published the increase in the MOMBI holding pattern minimum altitude (Figure 8) via NOTAM.

Figure 8: Approach charts showing the increase to the MOMBI minimum holding altitude

The Canberra runway 35 ILS Y approach chart. The holding information and MOMBI glidepath crossing height are annotated.

The 23 March 2023 version of the approach chart was the last version to include the 5,100 ft minimum altitude, but from May 2022, the minimum altitude had been increased to 5,600 ft by NOTAM. Source: Airservices Australia, annotated by the ATSB

Glideslope intercept

Intercepting an ILS glideslope is normally accomplished from below as intercepting the glideslope from above requires high descent rates, increasing the risk of an unstable approach. Furthermore, the ILS ground equipment can also emit false glideslopes at steeper than normal glideslope angles. The Airservices Australia Aeronautical Information Publication cautioned that these false glideslopes could lead to a severe and sudden pitch up when intercepting a glideslope from above and that caution should be exercised in such situations, particularly for autopilot coupled approaches.[9]

The lowest of these false glideslopes typically occurs at an angle of about 9° to 12°, well above the flightpath of PK‑LDK during the incident approach.

Flight revalidation

In April 2022, the instrument flight procedure underwent a periodic revalidation flight by the Civil Aviation Safety Authority (CASA). For this revalidation, Airservices Australia provided CASA with the results of the 3‑yearly review including the increased minimum holding altitudes. On 19 May 2022, following the revalidation flight, CASA provided the flight report to Airservices Australia. The report’s findings stated that: 

  • the suitability of the holding procedure design was unsatisfactory
  • the holding altitude at MOMBI did not allow for an appropriate transition to the ILS glidepath
  • the flyability of the ILS approach procedure was satisfactory
  • modification of the procedure was desirable.

The report also recommended moving the holding point to the waypoint KATIA (if design requirements allowed).

Following receipt of the report, the findings were not incorporated into the associated instrument flight procedures and, on 30 November 2023, updated instrument flight procedures were published without modification, with the increased minimum holding altitude.

The Airservices Australia procedure design manual stated that upon receipt of an instrument flight procedure revalidation report, the chief designer would assign the report to the designer who compiled the relevant revalidation pack. Any issues identified by the report were required to be addressed and advice of any action taken needed to be provided to the chief designer. Airservices Australia advised that for the MOMBI holding pattern flight revalidation report, internal records of correspondence regarding the possible relocation of the holding pattern were located, but the record of the outcome could not be found.

CASA surveillance of instrument flight procedure design

CASA conducts regular surveillance of instrument flight procedures, including approach design. The surveillance included a review of the incorporation into flight procedures of relevant revalidation flight findings and recommendations. However, the surveillance was conducted on a sampling basis and therefore did not include every revalidation report finding. CASA surveillance activities did not include the MOMBI holding pattern findings and therefore it was not identified that these had not been incorporated into the published instrument approach procedure.

Action following Batik Air incident

In December 2024, following ATSB enquiries into the MOMBI holding pattern design, Airservices Australia conducted a review of the 2022 design changes. This review found that when the 14 DME limit was correctly incorporated into the terrain and obstacle assessment area, the higher terrain that caused the minimum altitude increase from 5,100 ft to 5,600 ft was excluded. This assessment also determined that the minimum altitude for the 210 kt speed limit could be reduced and, on 20 December 2024, Airservices Australia published a NOTAM reducing the MOMBI minimum holding altitudes to 5,100 ft for the 14 DME‑limited and 170 kt speed‑limited holding pattern and 5,600 ft (from 6,000 ft) for the 210 kt speed‑limited holding pattern.

Pilot details 

The captain was an instructor pilot with Batik Air and held an Indonesian air transport pilot licence (aeroplane) and the required aviation medical certificates and operational ratings to undertake the flight. The captain had a total flying experience of 10,508 hours of which 7,772 were on the Boeing 737 aircraft type. In the previous 90 days, they had flown 164 hours, all in the Boeing 737.

The first officer held an Indonesian commercial pilot licence (aeroplane) and the required aviation medical certificates and operational ratings to undertake the flight. The first officer had a total flying experience of 6,843 hours of which 6,688 were on the Boeing 737 aircraft type. In the previous 90 days, they had flown 159 hours, all in the Boeing 737.

The second captain held an Indonesian air transport pilot licence (aeroplane) and the required aviation medical certificates and operational ratings to undertake the flight. The second captain had a total flying experience of 11,295 hours of which 11,018 were on the Boeing 737 aircraft type. In the previous 90 days, they had flown 191 hours, all in the Boeing 737.

From 1998 to 2010, the captain was a pilot in the Indonesian military and, in that role, had conducted operations in non‑controlled airspace. In 2010, the captain commenced employment with Batik Air’s parent company Lion Air and moved to Batik Air in 2013. From 2010, the captain had not undertaken any flights within non‑controlled airspace. The first officer and second captain reported having no experience operating in non‑controlled airspace. All crewmembers had previously operated flights to Australian destinations, but not to Canberra.

Batik Air

Batik Air began operations in 2013 as a subsidiary of Lion Air and commenced flights to Australia in 2016. At the time of the incident, Batik Air operated to 2 Australian destinations: Perth, Western Australia, and Canberra, Australian Capital Territory. The airline operated 46 Airbus A320 series aircraft, 22 Boeing 737‑800s and 1 Airbus A330‑300. All of Batik Air’s scheduled flights were undertaken in controlled airspace, except for any early Canberra arrivals (before 0600) and potential diversions from Perth Airport to the operator‑nominated diversion destination of Kalgoorlie, which operated using a CTAF at all times.

In October 2024, unrelated to this occurrence, Batik Air ceased operating the Denpasar to Canberra route.

Denpasar to Canberra route preparation

Prior to commencing the Denpasar to Canberra route, Batik Air conducted the required process to risk assess and obtain approval to commence the new route. This included conducting a risk management review and publishing a company airport briefing document.

Risk Management Review

The risk management review identified several risks and associated mitigations that were relevant to the incident including the items shown in Table 1 below:

Table 1: Relevant risk management review items

Identified riskMitigation
Unfamiliarity with new route and new airport

During the initial flight of any new route, provide the crew with all data available.

If available, the initial flight is to be flown by a pilot who has previously had experience on the route. If such pilot is unavailable, an instructor captain shall operate the initial flight.

High obstacle standard instrument departure

Create a specific one engine inoperative standard instrument departure procedure.

Ensure the one engine inoperative standard instrument departure procedure is included in the company airport briefing document.

CTAF operations in non-controlled airspace/airports

Ensure the crew is familiar with and understands CTAF operations.

Ensure guidance of CTAF operations is included in the company airport briefing.

Airport area surrounded by obstacles.Publish a company airport briefing and train crew for special airports.

The risk management review did not identify that Canberra Airport aviation rescue and firefighting services operated only during times advised by NOTAM. Batik Air’s minimum permissible category of rescue and firefighting (RFF) services for 737‑800 operations was RFF category 7. On the day of the incident, this category of service began 13 minutes before the aircraft commenced the approach. Before that time, the available category of RFF was less than that permitted by Batik Air’s operations manual.

Company airport briefing

The company airport briefing document provided to the crew for the inaugural flight was incomplete. Specifically, in the airport information section the: 

  • radio frequency for company operations was listed as ‘TBA’ (to be advised)
  • airport operating hours were listed as ‘24’, but the operational hours of air traffic control services were not provided
  • aviation rescue and firefighting information provided did not state that services were only provided during hours advised by NOTAM, nor was it advised that outside of these hours, the available level of rescue and firefighting was less than that required for the 737‑800 by Batik Air.

The CTAF information and high obstacle standard instrument departure risk mitigations required by the risk management review were also not included in the briefing. 

Common traffic advisory frequency procedures and training
Operations manual

Batik Air’s operations manual noted that Australian routes may require the use of non‑controlled aerodromes as alternate airports and that these airports did not provide 24‑hour air traffic control services. The manual did not provide information advising that Canberra, a destination airport, could also be non‑controlled at times. The manual provided adequate procedures for an arrival to a non‑controlled airport (destination or alternate), including the use of pilot‑activated lighting and guidance for appropriate CTAF procedures and radio broadcasts.

CTAF training

Prior to commencing operations into Australia, Batik Air flight crew were required to complete a module of online training for CTAF operations. All flight crew had completed this training prior to operating the incident flight.

Batik Air also incorporated CTAF use into one simulator session (session 15) of its recurrent training program. This session simulated a flight from Denpasar to Perth, Western Australia and included a diversion from Perth to Kalgoorlie, where pilots were trained in the use of CTAF procedures for the arrival into Kalgoorlie.

Session 15 had last been incorporated into Batik Air’s training program in 2020, 4 years prior to the incident flight. The captain last undertook this training in May of 2020 and the second captain in March of 2020. The first officer commenced employment with Batik Air in 2021 and had therefore not undertaken session 15.

Crew training before route commencement

Prior to commencing the Canberra route, Batik Air reviewed the route and associated operational requirements. Batik Air assessed that a proving flight on the route or simulator training were not required as the new destination did not involve any significant operational complexities, and the aircraft type had demonstrated the required performance capabilities when operating similar routes.

To prepare the crew for the new route, the chief pilot had provided an in-person briefing to the operating crew on the day of the flight.

CASA route approval process

In March 2023, Batik Air applied to CASA to extend its Australian services beyond Perth to 3 additional airports – Adelaide, Brisbane and Canberra.

CASA conducted a desktop review of the application that included examination of Batik Air’s organisational structure, operational certificates and manuals, infrastructure and operational approvals to ensure that the required items were in place. This included an assessment of Batik Air’s CTAF procedures and guidance. CASA did not review Batik Air’s risk management review or the company airport briefing for Canberra, nor was it required to.

International Civil Aviation Organization guidance

The International Civil Aviation Organization (ICAO) publication Annex 6 to the convention on international civil aviation, Operation of Aircraft provided guidance for appropriate flight crew qualification and training standards for international air transport operations.[10] This stated that an operator shall not utilise a pilot as pilot‑in‑command of an aeroplane on a route for which that pilot was not qualified until the pilot has demonstrated adequate knowledge of relevant operational details for the route including: 

  • terrain and minimum safe altitudes
  • communication and air traffic facilities, services and procedures
  • rescue procedures
  • arrival, departure, holding and instrument approach procedures
  • applicable operating minima.

This demonstration relating to arrival, departure, holding and instrument approach procedures could be accomplished in an appropriate training device, such as a simulator.

The guidance also stated that a pilot shall have made an actual approach into each aerodrome of landing on the route accompanied by a pilot who is qualified for the aerodrome unless: 

• the approach to the aerodrome is not over difficult terrain and the instrument approach procedures and aids available are similar to those with which the pilot is familiar, and a margin to be approved by the State of the Operator is added to the normal operating minima, or there is reasonable certainty that approach and landing can be made in visual meteorological conditions; or

• the descent from the initial approach altitude can be made by day in visual meteorological conditions; or

• the operator qualifies the pilot-in-command to land at the aerodrome concerned by means of an adequate pictorial presentation; or

• the aerodrome concerned is adjacent to another aerodrome at which the pilot-in-command is currently qualified to land.

It was also recommended that a pilot be requalified if more than 12 months had elapsed and the pilot ‘had not made a trip on the route or a route in close proximity and over similar terrain and had not practised such procedures in a training device’.

The ICAO publication Guidance on the Preparation of an Operations Manual provided further guidance for these operations.[11] This document noted that it was common practice for operators to apply similar requirements to all pilots (not just the pilot in command). Depending on the complexity of the area or route and aerodrome, this may require in‑flight familiarisation or familiarisation using a training device. This document also stated that it was normal practice to give each pilot a general route or line check at least every 12 months.

Collision avoidance at non‑controlled aerodromes

Non‑controlled aerodromes cater for flights conducted by a broad mix of aircraft under both the instrument flight rules and the visual flight rules, including:

  • larger turboprop, jet and powered lift aircraft
  • smaller aircraft operated both commercially and privately
  • agricultural aircraft
  • military aircraft
  • various sport and recreational aircraft.

This presents many challenges to pilots operating into, out of, or in the vicinity of these aerodromes including collision avoidance. The Civil Aviation Safety Authority advisory circular AC91-14 pilots’ responsibility for collision avoidance describes the 2 methods of collision avoidance for aircraft operating in the vicinity of non‑controlled aerodromes.

Unalerted see‑and‑avoid:

Unalerted see-and-avoid relies totally on the crew – with no other assistance – to visually detect other aircraft that are on a conflicting flight path. Unalerted see-and-avoid is only viable in a minority of circumstances when all the following factors are present to defend against a mid-air [collision]: 

• horizontal closure rates are slow enough for human reaction

• vertical closure rates are slow enough for human reaction

• aircraft are of sufficient profile to be seen with the available ambient light, or are made sufficiently conspicuous using artificial lighting

• aircraft and/or the ground are sufficiently well lit or ambient light provides sufficient contrast

• the aircraft structure is such that the pilot’s visibility is unhindered in all directions (a near practical impossibility)

Alerted see‑and‑avoid:

As aviation developed, with increasing aircraft performance, traffic density and flight in non-visual conditions, it became apparent that unalerted see-and-avoid had significant limitations. The need to enhance a pilot’s situational awareness led to the principle of ‘alerted see-and-avoid’. The primary tool of alerted see-and-avoid is radio communication. Radio allows for the communication of information to the pilot from the ground or from other aircraft.

Other tools of alerted see‑and‑avoid include airborne collision avoidance systems, but the equipment required for these systems to provide effective alerting were not required for all aircraft types using non‑controlled aerodromes.

The advisory circular describes accurate provision and interpretation of traffic information for the purposes of separation to or from another aircraft as an essential pilot skill and stated that effective training in the use of radio procedures is vital to ensure crews can effectively operate at non‑controlled aerodromes using common traffic advisory frequencies. Without understanding and confirming the transmitted information, the potential for alerted see‑and‑avoid is reduced to the less safe situation of unalerted see‑and‑avoid.

Light and meteorology

The approach was conducted in clear night conditions. On the morning of 14 June 2024, first light[12] was at 0641, 39 minutes after the aircraft landed. The moon was below the horizon. At 0554, when the aircraft descended below the minimum holding altitude, the Bureau of Meteorology (BoM) automatic weather station at Canberra Airport recorded the wind as 1 kt from 141° magnetic. The station recorded that there was no cloud cover, and visibility was greater than 10 km.

Recorded data

Quick access recorder

The aircraft’s quick access recorder data was provided to the ATSB by Batik Air. This data captured the aircraft’s descent commencing from 10,000 ft AMSL at 0550:20, 2.3 NM after passing LANYO. It then continued descending past the waypoints of HONEY at 9,184 ft AMSL, DALEY at 7,104 ft and MENZI at 6,720 ft (680 ft above the ILS glideslope).

At 0554:15, while approaching MOMBI at a speed of 171 kt, the aircraft descended below 5,600 ft AMSL and 2 seconds later, 0.6 NM before crossing MOMBI, the aircraft commenced a right turn from the approach track into the holding pattern at a speed of 172 kt. At 0554:24, the aircraft levelled at 5,400 ft AMSL and 6 seconds later passed MOMBI at a speed of 169 kt while continuing the right turn.

At 0554:51, the aircraft commenced descending from 5,400 ft AMSL and 4 seconds later, airspeed increased to 172 kt, before reducing to 170 kt, 4 seconds later. Speed remained at or below 170 kt for the remainder of the flight.

At 0555:44, the aircraft turned to and maintained a heading of 170° and 15 seconds later levelled at 4,700 ft AMSL (Figure 9). At 0556:25, the aircraft proceeded beyond 14 DME from the Canberra DME before commencing the right turn toward MOMBI 4 seconds later. During this turn, the lowest recorded radio height was 924 ft above ground level (AGL). No ground proximity alerts were recorded.

The aircraft passed KATIA at 0557:53 at an altitude of 4,700 ft AMSL (700 ft below the ILS approach minimum altitude at that waypoint) while tracking back toward MOMBI and rejoined the approach about 12 NM from the Canberra DME at 0558:19. 

At 0558:48, the aircraft began descending from 4,700 ft along the runway 35 glidepath (Figure 9).

Figure 9: Recorded quick access data

The Canberra runway 35 ILS Y approach chart. The holding information and MOMBI glidepath crossing height are annotated.

All times are coordinated universal time (UTC). Local time was Australian Eastern Standard Time (EST), which was (UTC) +10 hours. Source: Quick access recorder from PK-LDK, annotated by the ATSB

Air traffic control 

Recorded air traffic control surveillance and communications audio data was provided by Airservices Australia. The recorded audio showed that:

  • the crew did not request, and were not provided with, a clearance to track via the AVBEG 5A STAR
  • no safety alert was provided by the Melbourne Centre controller
  • no broadcasts were made by the crew on the Canberra CTAF
  • at 0547, and again at 0555, the Canberra runway lighting system was activated using the pilot‑activated lighting. The Batik Air crew did not have the CTAF selected at that time and the only other recorded transmissions on the CTAF at around those times were from a ground vehicle and another aircraft preparing to taxi for departure
  • at 0558, the Canberra Approach controller established communication with the Batik Air crew and provided a safety alert.

Safety analysis

Deviation from clearance and controller response

While en route to Canberra, the flight crew were provided with a tracking clearance from the waypoint AVBEG direct to Canberra Airport and instructed to leave controlled airspace by descending below the 8,500 ft above mean sea level (AMSL) controlled airspace base along that track. 

The crew’s normal practice for arrivals was to use a standard arrival route (STAR), and they prepared for the arrival at Canberra using the AVBEG 5A STAR. However, the crew did not request or receive a clearance to descend via the STAR and with Canberra Approach air traffic control (ATC) services not yet active, this clearance could not have been provided. Therefore, when the aircraft crossed AVBEG and commenced tracking via the STAR, it deviated from the provided clearance.

From AVBEG, this STAR deviated from the aircraft’s cleared track by turning south and crossed restricted areas R430A, B and C. The AVBEG 5A STAR included a 10,000 ft AMSL descent limitation until past the waypoint LANYO to ensure that crew using the STAR did not enter the uppermost of these restricted areas. The descent clearance for the direct track provided to the crew did not have a descent restriction and the controller was unaware that the AVBEG 5A STAR included a descent restriction to prevent the aircraft entering the restricted areas. Therefore, the controller was required to issue a safety alert as it appeared to them that the aircraft’s deviation would take the aircraft into the active restricted areas. However, at that time, the controller had only recently taken over management of the airspace and was unsure if the crew were deviating from the cleared route, or if a clearance had been provided which hadn’t been correctly entered in the air traffic control system and was therefore not visible to the controller. Additionally, the controller noted that the aircraft was still 17 NM from the restricted area and therefore, instead of advising the crew of the clearance deviation and issuing a safety alert, the controller intervened by issuing a descent altitude restriction. 

The crew believed that they were correctly following the AVBEG 5A STAR into non‑controlled airspace and when they received the descent restriction from the controller, they became confused as to whether the approach would be conducted within, or outside of, controlled airspace. Despite the controller stating that the approach would take place outside of controlled airspace and that clearances were not required for the manoeuvring associated with the approach, the crew remained confused and made several clearance requests when operating in non‑controlled airspace. This confusion was only resolved when Canberra Approach and Tower services commenced, and the approach continued using those services. 

A ‘safety alert’ is designed to alert crews to safety critical information to ensure a response is prioritised. The controller’s decision not to issue the safety alert and not to alert the crew to the deviation were missed opportunities to draw the crew’s attention to the situation and may have helped avoid the later confusion about the airspace classification.

Furthermore, the controller needed to wait until the aircraft was observed to be 2.5 NM beyond the restricted area before further descent clearances could be provided and by the time this clearance was issued, the aircraft was about 1,300 ft above the desired STAR profile.

Contributing factor

While descending and tracking direct toward Canberra in controlled airspace, the flight crew were provided with a clearance to leave the controlled airspace by continuing to descend on that track. The flight crew then deviated from the cleared track by commencing the AVBEG 5A standard arrival route (STAR).

Contributing factor

The air traffic controller did not advise the flight crew of the track deviation or provide a safety alert but provided altitude instructions to maintain separation from a restricted area (a separation built into the AVBEG 5A STAR). This intervention resulted in the aircraft becoming higher than the desired descent profile and the crew becoming confused regarding the airspace classification for the arrival and approach.

Descent below minimum altitude

Incorrectly flown holding pattern

Following the controller’s descent clearance after crossing the restricted area, the crew did not re‑establish the desired descent profile prior to commencing the approach. Consequently, the aircraft passed the instrument landing system approach’s initial approach fix waypoint MENZI about 680 ft higher than the glideslope and the captain decided to use the approach holding pattern at MOMBI to descend to the desired descent profile. This decision was made late during the arrival and the crew did not identify that the holding pattern minimum altitude (5,600 ft) was unusual in being significantly higher than the waypoint glideslope crossing altitude (4,760 ft). As a result, the captain referenced the 4,760 ft AMSL glideslope crossing altitude for MOMBI and selected 4,700 ft for the holding altitude.

The crew also did not begin to enter the pattern into the flight management system until after MOMBI had already dropped from the programmed track. As a result, the first officer had to manually enter the holding waypoint. When entering the holding waypoint, the first officer did not enter minimum altitude constraints associated with the holding pattern.

While the first officer entered the holding waypoint, the captain used the heading select function and altitude window to enter the holding pattern. In doing so, the captain did not adhere to several holding pattern requirements. The turn to enter the pattern commenced prior to the aircraft crossing MOMBI resulting in less distance being available to complete the outbound leg of the holding pattern. The maximum speed for the 5,600 ft minimum altitude was marginally exceeded and the aircraft then descended below the 5,600 ft minimum altitude to the commanded altitude of 4,700 ft. As the pattern continued, the inbound turn to MOMBI then did not commence until after the aircraft had proceeded beyond the 14 DME limit. As the aircraft was operating below both the 6,000 ft minimum altitude of the non‑distance restricted holding pattern and the 7,500 ft 25 NM minimum safe altitude, obstacle and terrain clearance was not assured.

As the aircraft turned toward back toward MOMBI at an altitude 900 ft below the minimum safe altitude, it crossed over terrain at a height of 924 ft above ground level. The aircraft did not penetrate the enhanced ground proximity warning system envelope and no alert was generated. Furthermore, as the aircraft then turned to rejoin the approach, it was now positioned about 700 ft below the minimum altitude for that segment of the approach, which also reduced obstacle clearance assurance during this part of the flight.

Contributing factor

The aircraft passed the initial approach fix for the instrument landing system approach about 680 ft higher than the glideslope and the crew intended to use the holding pattern at the approach waypoint of MOMBI to reduce altitude. However, the holding pattern was not correctly flown, and the aircraft was manoeuvred significantly below the minimum safe altitude. The approach was then recommenced from an altitude about 700 ft below the minimum altitude.

Low altitude safety alerts

Unlike approach controllers, area radar controllers providing the flight information service for the non‑controlled airspace were not required to know the details of instrument flight procedures for airports in that airspace. Therefore, the controller providing the flight information service was not aware of the minimum holding altitudes associated with the MOMBI holding pattern. 

Air traffic control procedures required the controller to issue a safety alert as soon as they became aware that the aircraft was in unsafe proximity to terrain. However, the controller was unaware of the minimum holding altitudes and descending below the broader lowest safe altitudes was inherent to the progress of a flight following an instrument approach. Therefore, the controller did not become aware that the aircraft was operating below the minimum safe altitudes and did not issue a safety alert. Had an alert been provided when the aircraft first descended below the minimum altitude, this would have occurred prior to the aircraft turning toward the high terrain, reducing the risk of collision with terrain.

The Canberra Tower and Approach controllers both recognised that the aircraft was operating below the minimum safe altitude. The Tower controller attempted to contact the crew however, as the crew had not selected the CTAF, these broadcasts were not received. After the aircraft rejoined the approach, the Approach controller took over the airspace and immediately provided a safety alert to the crew, but by this time the aircraft was re‑established on the approach and within the associated protected area.

Other factor that increased risk

The Melbourne Centre air traffic controller providing the flight information service for the aircraft was not, and was not required to be, aware of the holding pattern minimum altitudes. Therefore, the controller did not issue a safety alert when the aircraft descended below the minimum safe altitude.

Common traffic advisory frequency use and training

Non-use of Canberra common traffic advisory frequency

During the arrival and approach, the crew were confused about the airspace classification and despite attempts by the controller to clarify this, the confusion was not resolved. As the aircraft approached Canberra Airport the crew did not select the Canberra common traffic advisory frequency (CTAF) but remained on the Melbourne Centre frequency.

As a result, the crew could not have activated the runway lights, nor could they make the required radio broadcasts to ensure separation with other traffic using the airspace. However, at the time the aircraft approached Canberra, another CTAF user had illuminated the runway lights and there was no conflicting traffic using the CTAF.

More importantly however, as the crew had not selected the CTAF, they did not receive the oncoming Canberra Tower controller’s broadcasts attempting to alert them to their low altitude.

Contributing factor

The Canberra common traffic advisory frequency was not selected by the crew, and the appropriate radio broadcasts were not made. This prevented the crew from receiving the oncoming Canberra tower air traffic controller's safety alerts, being able to illuminate the runway lights and increased the risk of conflict with other traffic.

Batik Air common traffic advisory frequency training

Batik Air’s operations manual included guidance on CTAF operations. While this guidance was focused on a Kalgoorlie diversion scenario, this guidance was also suitable for an early morning Canberra arrival.

Australian flights are the only flights in Batik Air’s route network where CTAF operations may have been required and Batik Air required that crew complete online CTAF training before operating to Australia. A simulator training session had also been developed that included CTAF operations, but this had last been incorporated into Batik Air’s recurrent training program 4 years prior to the incident, in 2020. The captain and deadheading captain had completed this session over 4 years before the incident, but the first officer had joined Batik Air after this date and had not undergone the training. None of the crew had previously operated into a non‑controlled airport as an operating crew of an air transport flight.

International Civil Aviation Organization (ICAO) guidance recommended that a pilot acting as pilot‑in‑command undergo training and demonstrate the required knowledge relevant to an intended operation within 12 months of undertaking that operation. Furthermore, this guidance stated that it was commonplace to ensure that all flight crew (not just the pilot‑in‑command) were trained and demonstrated similar operation knowledge.

Operating to a non‑controlled airport in an air transport aircraft while using CTAF procedures is a complex task. The crews of these aircraft may be faced with managing separation with smaller commercial and private aircraft as well as agricultural, military or sport and recreational aircraft. In addition, these aircraft may be operating to either the visual or instrument flight rules and many of these aircraft are not required to be fitted with the equipment required to enable effective alerting using airborne collision avoidance systems. Furthermore, these crews may be required to manage additional tasks like activating the runway lighting when arriving at night.

Effective training in the use of CTAF procedures is vital to ensure crews can effectively and safely operate using these procedures, in particular for crews who may not have previously used them or seldom used them. Batik Air had identified this risk for its Australian operations and developed training to mitigate the risk. However, this training was not conducted regularly, and Batik Air processes did not ensure that all flight crew members had completed the training before undertaking operations to Australia. This was inconsistent with the standards set out by ICAO guidance and increased the risk that crews would be inadequately prepared to manage this task.

After the crew deviated from the airways clearance, the controller’s intervention resulted in the crew becoming confused as to the classification of the airspace for the arrival and approach. This may have contributed to the crew’s non‑use of the CTAF. However, as the non‑use of CTAF procedures did not lead to the descent below minimum altitude, the inadequate CTAF training was not considered contributory to the incident.

Other factor that increased risk

Batik Air did not ensure that flight crew completed all common traffic advisory frequency (CTAF) training prior to them operating flights into Australia where the use of these procedures could be required. (Safety issue)

Route commencement process

Prior to commencing the Denpasar to Canberra route, Batik Air completed the required process to receive approval to commence flights on the route. This included a risk management review for the intended operation which identified a number of risks and associated mitigation actions that were relevant to the operation. However, a number of mitigations were not implemented such as the absence of CTAF guidance and a one engine inoperative standard instrument departure in the company airport briefing document. Other mitigations that were implemented, such as the inclusion of an instructor pilot on the flight and the publication of an (incomplete) company airport briefing document were ineffective at mitigating the risk of operating to an unfamiliar airport. Furthermore, the risk presented by airport fire and firefighting services being unavailable at times was not identified and therefore, no mitigating action was implemented.

ICAO guidance stated that an operator should not utilise a pilot as pilot‑in‑command of an aeroplane on a route for which that pilot was not qualified until the pilot had demonstrated adequate knowledge of relevant operational details. This could be conducted in a number of ways including self‑briefing, operator briefing, undertaking a route proving flight or by using an adequate training device. 

Batik Air assessed that a proving flight or simulator training for the route were not required as the new destination did not involve any significant operational complexities and the aircraft type had demonstrated the required performance capabilities when operating similar routes. Instead, the crew were briefed on the operation by the Chief Pilot on the day of the flight. 

However, the route did involve several significant operation complexities. The scheduled arrival time for the flight was during night hours; Canberra is surrounded by mountainous terrain and may have required the use of CTAF procedures. Furthermore, the runway 35 instrument landing system approach included significant and unusual complexities as demonstrated by the MOMBI holding pattern glideslope transition. 

Recognising that a briefing was provided by the Chief Pilot to the crew prior to the flight, it did not achieve its aim of adequately preparing them for the route. A route proving flight, or the use of a suitable training device, would likely have provided more effective crew preparation in accordance with ICAO guidance, giving them greater awareness of the terrain, airspace and instrument flight procedure complexities of Canberra and may have avoided the descent below the minimum safe altitude.

Contributing factor

Batik Air's change management processes were not effective at fully identifying and mitigating the risks associated with the commencement of the Denpasar to Canberra route. (Safety issue)

Holding pattern to glideslope transition design

During a required, periodic review of the Canberra runway 35 ILS approach procedure by Airservices Australia, a new procedure template was imported to assess the approach including the MOMBI holding pattern as the existing design could not be uploaded to the procedure design software. The lower of the existing holding pattern’s 2 minimum altitudes (5,100 ft AMSL) required a crew to turn inbound from the outbound course before reaching 14 DME from Canberra. This distance limitation reduced the size of the pattern’s terrain and obstacle consideration area. When conducting the review, this 14 DME distance limitation was not included when determining the assessment area and therefore an area larger than required was assessed. This larger area included higher terrain and obstacles that required a 500 ft increase to the minimum altitude, raising it to 5,600 ft AMSL. The error in this assessment was not identified during internal reviews by Airservices Australia and the increased holding altitude was then published via NOTAM.

The approach glideslope crossed MOMBI at 4,760 ft AMSL, 840 ft below the minimum holding altitude. Consequently, to rejoin the approach from the holding pattern, crews could be required to intercept the glideslope from significantly above it, increasing the risk of sudden pitch ups. To achieve this could also require significant descent rates, increasing the risk of unstable approaches.

This was identified when the Civil Aviation Safety Authority (CASA) conducted a revalidation flight of the holding pattern and determined that the transition from the pattern to the glideslope was not appropriate and the design was unsatisfactory. This feedback was provided to Airservices Australia and despite Airservices Australia’s internal processes requiring this feedback to be addressed, the approach procedure with the increased altitude was published without any further modification.

The erroneous minimum altitude remained in place for over 2 years until a review following the Batik Air incident. This review identified the assessment area error and resulted in the minimum altitude being lowered back to 5,100 ft AMSL. While this minimum altitude remains above the MOMBI glideslope crossing altitude, the 500 ft reduction allows crews to appropriately transition to the glideslope while on the inbound leg of the holding pattern.

While the transition increased the risk of unstable and sudden pitch ups approaches, it did not contribute to the incident as the captain had manually selected a holding altitude of 4,700 ft AMSL on the flight management system, which in turn descended the aircraft below the lower and more appropriate 5,100 ft AMSL minimum altitude.

Other factor that increased risk

During a 2022 review of Canberra runway 35 instrument landing system approaches, an obstacle evaluation error led to Airservices Australia increasing the MOMBI holding pattern minimum altitude from 5,100 ft to 5,600 ft. This increase resulted in a transition from the holding pattern to the approach glideslope that increased risk of unstable approaches and sudden pitch ups.

Other factor that increased risk

After conducting a revalidation test flight of the holding pattern minimum altitude increase, the Civil Aviation Safety Authority advised Airservices Australia that the increased minimum altitude did not provide an appropriate transition to the approach glideslope and recommended moving the holding location to the waypoint KATIA. Despite Airservices Australia receiving this advice, the holding waypoint remained at MOMBI and the increased minimum holding altitude was maintained.

Findings

ATSB investigation report findings focus on safety factors (that is, events and conditions that increase risk). Safety factors include ‘contributing factors’ and ‘other factors that increased risk’ (that is, factors that did not meet the definition of a contributing factor for this occurrence but were still considered important to include in the report for the purpose of increasing awareness and enhancing safety). In addition ‘other findings’ may be included to provide important information about topics other than safety factors. 

Safety issues are highlighted in bold to emphasise their importance. A safety issue is a safety factor that (a) can reasonably be regarded as having the potential to adversely affect the safety of future operations, and (b) is a characteristic of an organisation or a system, rather than a characteristic of a specific individual, or characteristic of an operating environment at a specific point in time.

These findings should not be read as apportioning blame or liability to any particular organisation or individual.

From the evidence available, the following findings are made with respect to the flight below minimum altitude involving Boeing 737‑800, PK-LDK, 19 km south of Canberra Airport, New South Wales on 14 June 2024.

Contributing factors

  • While descending and tracking direct toward Canberra in controlled airspace, the flight crew were provided with a clearance to leave the controlled airspace by continuing to descend on that track. The flight crew then deviated from the cleared track by commencing the AVBEG 5A standard arrival route (STAR).
  • The air traffic controller did not advise the flight crew of the track deviation or provide a safety alert but provided altitude instructions to maintain separation from a restricted area (a separation built into the AVBEG 5A STAR). This intervention resulted in the aircraft becoming higher than the desired descent profile and the crew becoming confused regarding the airspace classification for the arrival and approach.
  • The aircraft passed the initial approach fix for the instrument landing system approach about 680 ft higher than the glideslope and the flight crew intended to use the holding pattern at the approach waypoint of MOMBI to reduce altitude. However, the holding pattern was not correctly flown, and the aircraft was manoeuvred significantly below the minimum safe altitude. The approach was then recommenced from an altitude about 700 ft below the minimum altitude.
  • The Canberra common traffic advisory frequency was not selected by the flight crew, and the appropriate radio broadcasts were not made. This prevented the crew from receiving the oncoming Canberra tower air traffic controller's safety alerts, being able to illuminate the runway lights and increased the risk of conflict with other traffic.
  • Batik Air's change management processes were not effective at fully identifying and mitigating the risks associated with the commencement of the Denpasar to Canberra route. (Safety issue)

Other factors that increased risk

  • Batik Air did not ensure that flight crew completed all common traffic advisory frequency (CTAF) training prior to them operating flights into Australia where the use of these procedures could be required. (Safety issue)
  • During a 2022 review of Canberra runway 35 instrument landing system approaches, an obstacle evaluation error led to Airservices Australia increasing the MOMBI holding pattern minimum altitude from 5,100 ft to 5,600 ft. This increase resulted in a transition from the holding pattern to the approach glideslope that increased risk of unstable approaches and sudden pitch ups.
  • After conducting a revalidation test flight of the holding pattern minimum altitude increase, the Civil Aviation Safety Authority advised Airservices Australia that the increased minimum altitude did not provide an appropriate transition to the approach glideslope and recommended modifications to the holding pattern design. Despite Airservices Australia receiving this advice, no changes were made and the increased minimum holding altitude was maintained.
  • The Melbourne Centre air traffic controller providing the flight information service for the aircraft was not, and was not required to be, aware of the holding pattern minimum altitudes. Therefore, the controller did not issue a safety alert when the aircraft descended below the minimum safe altitude.

Safety issues and actions

Central to the ATSB’s investigation of transport safety matters is the early identification of safety issues. The ATSB expects relevant organisations will address all safety issues an investigation identifies. 

Depending on the level of risk of a safety issue, the extent of corrective action taken by the relevant organisation(s), or the desirability of directing a broad safety message to the Aviation industry, the ATSB may issue a formal safety recommendation or safety advisory notice as part of the final report.

All of the directly involved parties are invited to provide submissions to this draft report. As part of that process, each organisation is asked to communicate what safety actions, if any, they have carried out or are planning to carry out in relation to each safety issue relevant to their organisation. 

Descriptions of each safety issue, and any associated safety recommendations, are detailed below. Click the link to read the full safety issue description, including the issue status and any safety action/s taken. Safety issues and actions are updated on this website when safety issue owners provide further information concerning the implementation of safety action.

Batik Air common traffic advisory frequency training

Safety issue number: AO-2024-035-SI-01

Safety issue description: Batik Air did not ensure that flight crew completed all common traffic advisory frequency (CTAF) training prior to them operating flights into Australia where the use of these procedures could be required.

Batik Air change management process

Safety issue number: AO-2024-035-SI-02

Safety issue description: Batik Air's change management processes were not effective at fully identifying and mitigating the risks associated with the commencement of the Denpasar to Canberra route.

Proactive safety action not associated with a safety issue
Action number:AO-2024-035-PSA-03
Action organisation:Batik Air
Action status:Closed

Batik Air adjusted the flight schedule for the Denpasar to Canberra flight (6015) to ensure that all Canberra arrivals occur during Canberra Tower and Approach air traffic control operating hours.

Glossary

AGLAbove ground level
AMSLAbove mean sea level
ATCAir traffic control
CASACivil Aviation Safety Authority
CTAFCommon traffic advisory frequency
DMEDistance measuring equipment
FLFlight level
FMSFlight management system
ICAOInternational Civil Aviation Organization
ILSInstrument landing system
MCPMode control panel
NOTAMNotice to airmen
PFPilot flying
PMPilot monitoring
STARStandard arrival route
TIBATraffic information by aircraft

Sources and submissions

Sources of information

The sources of information during the investigation included:

  • Batik Air
  • the flight crew
  • the air traffic controller
  • Civil Aviation Safety Authority
  • Airservices Australia
  • recorded flight data from PK-LDK
  • Bureau of Meteorology.

References

International Civil Aviation Organization 2018, Annex 6 to the Convention on International Civil Aviation, Operation of Aircraft, Part 1 International Commercial Air Transport — Aeroplanes Eleventh Edition.

International Civil Aviation Organization 2023, Doc 10153, Guidance on the Preparation of an Operations Manual.

Civil Aviation Safety Authority 2025, Advisory Circular AC91-14 Pilots’ responsibility for collision avoidance.

Submissions

Under section 26 of the Transport Safety Investigation Act 2003, the ATSB may provide a draft report, on a confidential basis, to any person whom the ATSB considers appropriate. That section allows a person receiving a draft report to make submissions to the ATSB about the draft report. 

A draft of this report was provided to the following directly involved parties:

  • Batik Air
  • the flight crew
  • the air traffic controller
  • Civil Aviation Safety Authority
  • Airservices Australia
  • National Transportation Safety Committee of Indonesia.

Submissions were received from:

  • Batik Air
  • Civil Aviation Safety Authority
  • Airservices Australia
  • National Transportation Safety Committee of Indonesia.

The submissions were reviewed and, where considered appropriate, the text of the report was amended accordingly.

Purpose of safety investigations

The objective of a safety investigation is to enhance transport safety. This is done through: 

  • identifying safety issues and facilitating safety action to address those issues
  • providing information about occurrences and their associated safety factors to facilitate learning within the transport industry.

It is not a function of the ATSB to apportion blame or provide a means for determining liability. At the same time, an investigation report must include factual material of sufficient weight to support the analysis and findings. At all times the ATSB endeavours to balance the use of material that could imply adverse comment with the need to properly explain what happened, and why, in a fair and unbiased manner. The ATSB does not investigate for the purpose of taking administrative, regulatory or criminal action.

Terminology

An explanation of terminology used in ATSB investigation reports is available here. This includes terms such as occurrence, contributing factor, other factor that increased risk, and safety issue.

Publishing information

Released in accordance with section 25 of the Transport Safety Investigation Act 2003

Published by: Australian Transport Safety Bureau

© Commonwealth of Australia 2025

Title: Creative Commons BY - Description: Creative Commons BY

Ownership of intellectual property rights in this publication

Unless otherwise noted, copyright (and any other intellectual property rights, if any) in this report publication is owned by the Commonwealth of Australia.

Creative Commons licence

With the exception of the Commonwealth Coat of Arms, ATSB logo, and photos and graphics in which a third party holds copyright, this report is licensed under a Creative Commons Attribution 4.0 International licence.

The CC BY 4.0 licence enables you to distribute, remix, adapt, and build upon our material in any medium or format, so long as attribution is given to the Australian Transport Safety Bureau. 

Copyright in material obtained from other agencies, private individuals or organisations, belongs to those agencies, individuals or organisations. Where you wish to use their material, you will need to contact them directly.

[1]      Pilot flying (PF) and Pilot monitoring (PM): procedurally assigned roles with specifically assigned duties at specific stages of a flight. The PF does most of the flying, except in defined circumstances such as planning for descent, approach and landing. The PM carries out support duties and monitors the PF’s actions and the aircraft’s flight path.

[2]      Jump seat: an auxiliary seat on the aircraft flight deck.

[3]      Flight level: at altitudes above 10,000 ft in Australia, an aircraft’s height above mean sea level is referred to as a flight level (FL). FL 350 equates to 35,000 ft.

[4]      All headings used in the report are magnetic.

[5]      NOTAM: a notice distributed by means of telecommunication containing information concerning the establishment, condition or change in any aeronautical facility, service, procedure or hazard, the timely knowledge of which is essential to personnel concerned with flight operations.

[6]      Airservices Australia’s levels of aviation rescue firefighting services available at Australia’s 26 busiest airports range from category 6 to category 10 services with the categories dictating number of response personnel, response times, water discharge rates and the required amount of water and foam that is needed to be carried. The category of service provided was determined by the size (length and width) of the largest aircraft serving an airport.

[7]      Manual of air traffic standards, 4.2.21.1 Entering an active Restricted/Military Operating Area and 9.1.4.3 Issuing a safety alert.

[8]      Manual of air traffic standards, 9.7.12.4 Flight path deviation.

[9]      Aeronautical Information Publication En Route section 7 - Precision Approach Operations, paragraph 7.1.3.

[10]    Annex 6, Operation of Aircraft, 9.4.3 Qualifications.

[11]    ICAO document 10153, Guidance for the preparation of an operations manual, 4.6 Route and aerodrome qualifications.

[12]    First light: when the centre of the sun is at an angle of 6° below the horizon before sunrise. At this time the horizon is clearly defined but the brightest stars are still visible under clear atmospheric conditions.

Preliminary report

Report release date: 04/09/2024

This preliminary report details factual information established in the investigation’s early evidence collection phase, and has been prepared to provide timely information to the industry and public. Preliminary reports contain no analysis or findings, which will be detailed in the investigation’s final report. The information contained in this preliminary report is released in accordance with section 25 of the Transport Safety Investigation Act 2003

The occurrence

On the evening of 13 June 2024, a Batik Air Boeing 737-800, registered PK-LDK, departed Denpasar International Airport, Indonesia for the inaugural passenger transport flight of a new service to Canberra, Australian Capital Territory. The captain was acting as pilot flying, and the first officer was acting as pilot monitoring.[1] A second captain was also on board, acting as a relief crewmember, occupying the flight deck jump seat located behind the flight crew during the arrival and approach.

As the aircraft climbed to the cruising level of flight level 350,[2] the crew input forecast winds, which included strong tailwinds, into the aircraft’s flight management computer. The crew noted that the estimated time of arrival into Canberra was prior to 0600 local time on 14 June, when Canberra Tower and Approach air traffic control began providing services for the day (see the section titled Canberra Tower and Approach). The crew elected to continue to Canberra without any en route delays and prepared for an arrival without those air traffic control services, using the Canberra Airport common traffic advisory frequency (CTAF).

As the aircraft descended towards Canberra in darkness, the flight was cleared by air traffic control (ATC) to track via the waypoint AVBEG direct to Canberra Airport and to descend to FL120. During the descent, the flight crew prepared to conduct the AVBEG 5A standard arrival route (STAR) but did not make a request to track via the STAR to the Melbourne Centre air traffic controller managing the airspace.

At 0541 local time, as the aircraft approached AVBEG, ATC cleared the crew to leave controlled airspace descending. The aircraft crossed AVBEG while descending below FL205 and commenced tracking via the AVBEG 5A STAR. The Melbourne Centre air traffic controller identified that the Batik flight was deviating from the cleared track (direct to Canberra) and noted that the aircraft was descending toward a restricted area (Figure 1).

The controller did not query the flight crew’s deviation, but asked the crew if they were going to remain clear of the restricted area. The crew advised the controller that they were tracking via the AVBEG 5A STAR (see the section titled AVBEG 5A standard arrival route and restricted areas). The controller acknowledged the tracking advice and instructed the crew to maintain 10,000 ft above mean sea level (AMSL) to remain above the restricted area. After receiving this instruction, the flight crew became uncertain as to whether the aircraft would be operating within, or outside of, controlled airspace during the STAR and approach.

Figure 1: Overview of the descent

Figure 1: Overview of the descent

Source: Google Earth, recorded flight data, Airservices Australia and ATSB

The crew levelled the aircraft at 10,000 ft AMSL with the autopilot engaged and the aircraft passed over the restricted airspace. As was required by ATC procedures, the controller waited until the aircraft was observed to be more than 2.5 NM past the restricted area before instructing the crew to continue the descent to leave controlled airspace. The crew responded by advising that they would descend and continue tracking via the STAR. At about this time, the crew noted that the aircraft was about 1,300 ft above the desired descent profile for the arrival.

At 0551, the crew requested ATC clearance to conduct the instrument landing system (ILS) approach to runway 35 at Canberra. The controller responded by advising that the Canberra control tower was closed and that CTAF procedures applied for that airspace. At 0551:38, the aircraft descended below 8,500 ft AMSL, outside controlled airspace (class G).

As the aircraft was higher than the desired flightpath, the captain decided to conduct a holding pattern at the approach waypoint of MOMBI to reduce altitude and the first officer requested ATC clearance to hold at MOMBI. The controller responded by providing traffic information for the MOMBI holding pattern. The crew then again requested clearance for the ILS approach and the controller responded by advising that clearance was not required and that the crew must broadcast their intentions on the Canberra CTAF.

At 0553:10, the aircraft passed the arrival waypoint MENZI (Figure 2) while descending below 6,720 ft AMSL and soon after made another request to hold at MOMBI. The controller provided traffic information for the hold and requested that the crew make a right-hand orbit to remain clear of the restricted airspace, now to the west of the aircraft.

Figure 2: Overview of arrival

Figure 2: Overview of arrival

Source: Google Earth, recorded flight data, Airservices Australia and ATSB

As the aircraft approached MOMBI, the captain entered 5,400 ft AMSL (the approach’s minimum safe altitude before intercepting the ILS glideslope) into the autopilot mode control panel (MCP) and at 0554:15, the aircraft descended below the minimum holding altitude of 5,600 ft AMSL (see the section titled Instrument landing system approach) before levelling at 5,400 ft AMSL.

The captain then used the heading select function to make a right turn to a heading of 170°[3] and the aircraft commenced turning prior to crossing MOMBI. At 0554:30, the aircraft passed MOMBI at a speed of 172 kt (2 kt above the maximum speed for the 5,600 ft AMSL minimum holding altitude).

The captain then asked the first officer to enter a holding pattern into the aircraft’s flight management system (FMS) at MOMBI. As the aircraft had already passed MOMBI, the waypoint had dropped off the FMS track and the first officer was required to manually re-enter the waypoint into the FMS planned track. As the turn continued, the speed reduced below 170 kt, the captain selected 4,700 ft AMSL (the crew’s intended MOMBI crossing altitude) on the autopilot MCP and the aircraft commenced descending to that altitude. During this time, the Melbourne Centre controller did not identify that the aircraft was operating below the minimum holding altitude of 5,600 ft AMSL.

The aircraft turned to a heading of 170° and continued descending until levelling at 4,700 ft AMSL at 0555:59. As the aircraft tracked south, the incoming Canberra Approach air traffic controller prepared to take control of the Approach airspace (see the section titled Canberra airspace) and commenced a handover with the Melbourne Centre controller.

The aircraft continued south and at 0556:25, proceeded beyond the 14 distance measuring equipment (DME) limit for the 5,600 ft AMSL minimum holding altitude. At or before that DME limit, an inbound turn back to MOMBI needed to be commenced, or the minimum holding altitude increased to 6,000 ft AMSL. By that time, the first officer had completed re-entering MOMBI into the FMS and the captain then used the lateral navigation autopilot mode to commence a right turn toward the waypoint.

As the aircraft was turning back toward MOMBI, at 0556:58, the incoming Canberra Approach controller completed their handover with the Melbourne Centre controller and took over the airspace and the Melbourne Centre radio frequency that the aircraft was using (this frequency then became a Canberra Approach frequency).

At the same time, the Canberra Tower air traffic controller preparing to commence the tower service observed that the aircraft was operating below the minimum holding altitude and made multiple unsuccessful attempts to contact the crew on the Canberra CTAF frequency. As the Canberra Tower controller did not have a direct means of communication with the Melbourne Centre controller, the Tower controller contacted a Melbourne Approach controller to relay their concerns to the Melbourne Centre controller.

The aircraft continued turning toward MOMBI (Figure 3) and as it crossed over the eastern slopes of Mount Campbell at 0557:46, the recorded radio height reduced to a minimum of 924 ft above ground level. At 0558:21, the aircraft rejoined the ILS approach.

Figure 3: Overview of MOMBI hold

Figure 3: Overview of MOMBI hold

Source: Google Earth, recorded flight data, Airservices Australia and ATSB

The Melbourne Approach controller contacted the Melbourne Centre controller to relay the Tower controller’s concerns about the aircraft’s altitude and the Melbourne Centre controller responded by advising that the airspace was now being controlled by Canberra Approach.

At about the same time, the Canberra Approach controller also identified that the aircraft was operating below the minimum altitude. The controller contacted the crew to provide a safety alert and asked the crew if they were ‘visual’. The crew responded advising that they were ‘visual with the runway’ and continued the approach. The aircraft landed at 0602 without further incident.

Context

Pilot details

The captain was an instructor pilot with Batik Air and held an Indonesian air transport pilot licence (aeroplane) and the required medical certificates and operational ratings to undertake the flight. The captain had a total flying experience of 10,508 hours of which 7,772 were on the Boeing 737 aircraft type. In the previous 90 days, they had flown 164 hours, all in the Boeing 737.

The first officer held an Indonesian commercial pilot licence (aeroplane) and the required medical certificates and operational ratings to undertake the flight. The first officer had a total flying experience of 6,843 hours of which 6,688 were on the Boeing 737 aircraft type. In the previous 90 days, they had flown 159 hours, all in the Boeing 737.

The relief captain held an Indonesian air transport pilot licence (aeroplane) and the required medical certificates and operational ratings to undertake the flight. The relief captain had a total flying experience of 11,295 hours of which 11,018 were on the Boeing 737 aircraft type. In the previous 90 days, they had flown 191 hours, all in the Boeing 737.

From 1998 to 2010, the captain was a pilot in the Indonesian military and, in that role, had conducted operations in uncontrolled airspace. In 2010, the captain commenced employment with Batik Air’s parent company Lion Air and moved to Batik Air in 2013. From 2010, the captain had not undertaken any flights within uncontrolled airspace. The first officer and relief captain reported having no experience operating in uncontrolled airspace. All crewmembers had previously operated flights to Australian destinations.

Operator details

Batik Air was a subsidiary of Lion Air and commenced operations in 2013 and operated to 2 Australian destinations: Perth, Western Australia, and Canberra. The airline operated 46 Airbus A320 series aircraft, 22 Boeing 737-800s and 1 Airbus A330-300. All of Batik Air’s scheduled flights were undertaken in controlled airspace, with the exception of any early Canberra arrivals (before 0600) and potential diversions from Perth Airport to the operator nominated diversion destination of Kalgoorlie, which operated as a CTAF at all times.

Light and meteorology

The approach was conducted in night conditions. On the morning of 14 June 2024, first light[4] was at 0641, 39 minutes after the aircraft landed. The moon was below the horizon.

At 0554, when the aircraft descended below the minimum holding altitude, the Bureau of Meteorology (BoM) automatic weather station at Canberra Airport recorded the wind as 1 kt from 141° magnetic. The station recorded that there was no cloud cover, and visibility was greater than 10 km.

Canberra airspace

Canberra Tower and Approach

On the day of the incident, the operating hours of Canberra Tower and Approach controlled airspace were 0600 to 2300. During these hours, Canberra Airport was within class C airspace, with airspace bases that increased as the airspace fanned out at increasing distances from the airport (Figure 4). The Canberra Tower and Approach air traffic control (ATC) services controlled the class C airspace within 30 DME of Canberra and below 8,500 ft above mean sea level (AMSL). Control services for the airspace above 8,500 ft AMSL were provided by a Melbourne Centre controller at all times during the flight’s descent and approach.

Figure 4: Canberra airspace when tower and approach were operating

Figure 4: Canberra airspace when tower and approach were operating

All altitudes and elevations are above mean sea level.

Source: ATSB

Outside of the Canberra Tower and Approach operating hours, the base of the Class C airspace was 8,500 ft AMSL. Below this was class G, non‑controlled airspace (Figure 5). Within class G airspace, aircraft crews could manoeuvre as required to position for an approach and were responsible for maintaining adequate terrain clearance. ATC was unable to issue STARs or approach clearances for the class G airspace. 

Figure 5: Canberra airspace when tower and approach were not operating

Figure 5: Canberra airspace when tower and approach were not operating

All altitudes and elevations are above mean sea level.

Source: ATSB

When the tower was not operating, Canberra Airport operated using a common traffic advisory frequency (CTAF). When operating using a CTAF, pilots make positional radio broadcasts to coordinate self-separation with other traffic.

AVBEG 5A standard arrival route and restricted areas

South‑west of Canberra Airport, restricted areas of airspace (R430 A-C) encompassed the Canberra Deep Space Communications Complex at Tidbinbilla. The uppermost of these restricted areas (R430C) had a radius of 10 NM and a ceiling of 10,000 ft AMSL. The AVBEG 5A STAR (Figure 6) passed over this restricted area and had a 10,000 ft AMSL descent restriction at the waypoint LANYO which prevented aircraft descending via the STAR from entering that area.

Figure 6: AVBEG 5A standard arrival route

Figure 6: AVBEG 5A standard arrival route

Source: Batik Air and Navblue, annotated by the ATSB

Instrument landing system approach

An instrument landing system (ILS) is an instrument approach procedure that provides lateral (localiser) and vertical (glideslope) position information using angular deviation signals from the localiser antennas (located past the upwind end of the runway) and the glideslope antennas (located approximately 1,000 ft from the runway threshold).

The AVBEG 5A STAR connected with the Canberra runway 35 ILS Y approach at the initial approach fix waypoint MENZI. The minimum crossing height for MENZI was 5,400 ft AMSL. The approach included a 3° glidepath to the runway which crossed the approach waypoint of MOMBI at 4,760 ft AMSL.

The approach included a right turn, 1 minute holding pattern at the approach waypoint MOMBI (Figure 7). The minimum holding altitude at MOMBI was 5,600 ft AMSL. To use that minimum altitude, the crew was required to adhere to a maximum speed of 170 kt and a 14 DME limit from the Canberra DME for commencing the inbound turn back to MOMBI. A higher minimum holding altitude of 6,000 ft AMSL could also be used which allowed for a higher maximum speed of 210 kt with no DME limit.

Figure 7: Canberra runway 35 instrument landing system approach

Figure 7: Canberra runway 35 instrument landing system approach

Source: Airservices Australia, annotated by the ATSB

Recorded data

Air traffic control 

Recorded air traffic control surveillance and communications audio data was provided by Airservices Australia. The recorded audio showed that:

  • the crew did not request, and were not provided with, a clearance to track via the AVBEG 5A STAR
  • no broadcasts were made by the crew on the Canberra CTAF
  • no safety alert was provided by the Melbourne Centre controller.
Quick access recorder

The aircraft’s quick access recorder data was provided by Batik Air. This data captured the aircraft’s descent commencing from 10,000 ft AMSL at 0550:20, 2.3 NM after passing LANYO. It then continued descending past the waypoints of HONEY at 9,184 ft AMSL, DALEY at 8,608 ft and MENZI at 6,688 ft.

At 0554:15, while approaching MOMBI at a speed of 171 kt, the aircraft descended below 5,600 ft AMSL and 2 seconds later, 0.6 NM before crossing MOMBI, the aircraft commenced a right turn from the approach track into the holding pattern at a speed of 172 kt. At 0554:24, the aircraft levelled at 5,400 ft AMSL and 6 seconds later passed MOMBI at a speed of 169 kt while continuing the right turn.

At 0554:51, the aircraft commenced descending from 5,400 ft AMSL and 4 seconds later, airspeed increased to 172 kt, before reducing to 170 kt, 4 seconds later. Speed remained at or below 170 kt for the remainder of the flight.

At 0555:44, the aircraft turned to and maintained a heading of 170° and 15 seconds later levelled at 4,700 ft AMSL (Figure 8). At 0556:25, the aircraft proceeded beyond 14 DME from Canberra DME before commencing the right turn toward MOMBI 4 seconds later. During this turn, the lowest recorded radio height was 924 ft above ground level (AGL). No ground proximity alerts were recorded.

The aircraft passed KATIA at 0557:53 at an altitude of 4,700 ft AMSL while tracking back toward MOMBI and rejoined the approach about 12 NM from the Canberra DME at 0558:19. 

At 0558:48, the aircraft began descending from 4,700 ft along the runway 35 glidepath.

Figure 8: Recorded quick access data

Figure 8: Recorded quick access data

All times are coordinated universal time (UTC). Local time was Australian Eastern Standard Time (EST), which was (UTC) +10 hours.

Source: Quick access recorder from PK-LDK, annotated by the ATSB

Safety actions

Following the occurrence, Batik Air implemented several safety actions:

  • The Canberra Airport flight crew briefing document was revised to include more detailed information on Canberra air traffic control hours, common traffic advisory frequency (CTAF) procedures, holding requirements and guidance for adherence to lowest safe altitude requirements.
  • Internal flight crew notices were also issued to highlight the importance of a comprehensive approach briefing, adherence to air traffic control instructions and altitude awareness. These notices also provided information on CTAF and traffic information by aircraft (TIBA) procedures and highlighted the additional risks and absent protections when operating in non‑controlled airspace. Details of this incident were also disseminated to all flight crew and Batik Air conducted a special flight crew briefing with event details and lessons.
  • Batik Air also adjusted the flight schedule for the Denpasar to Canberra flight (ID6015) to ensure that arrivals occur during Canberra Tower and Approach air traffic control operating hours.

Further investigation

To date, the ATSB has:

  • examined recorded flight and air traffic control data
  • interviewed the flight crew and air traffic controller
  • obtained Batik Air operational procedures and route implementation processes
  • collected operational and airport information.

The investigation is continuing and will include further review and examination of:

  • recorded flight and air traffic control data
  • Batik Air operational procedures and training
  • Batik Air route implementation processes
  • air traffic control procedures and training.

A final report will be released at the conclusion of the investigation. Should a critical safety issue be identified during the course of the investigation, the ATSB will immediately notify relevant parties so appropriate and timely safety action can be taken. 

The ATSB SafetyWatch highlights the broad safety concerns that come out of our investigation findings and from the occurrence data reported to us by industry. One of the safety concerns is improving risk management associated with change.

 

Purpose of safety investigations

The objective of a safety investigation is to enhance transport safety. This is done through: 

  • identifying safety issues and facilitating safety action to address those issues
  • providing information about occurrences and their associated safety factors to facilitate learning within the transport industry.

It is not a function of the ATSB to apportion blame or provide a means for determining liability. At the same time, an investigation report must include factual material of sufficient weight to support the analysis and findings. At all times the ATSB endeavours to balance the use of material that could imply adverse comment with the need to properly explain what happened, and why, in a fair and unbiased manner. The ATSB does not investigate for the purpose of taking administrative, regulatory or criminal action.

Terminology

An explanation of terminology used in ATSB investigation reports is available here. This includes terms such as occurrence, contributing factor, other factor that increased risk, and safety issue.

Publishing information

Released in accordance with section 25 of the Transport Safety Investigation Act 2003

Published by: Australian Transport Safety Bureau

© Commonwealth of Australia 2024

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Copyright in material obtained from other agencies, private individuals or organisations, belongs to those agencies, individuals or organisations. Where you wish to use their material, you will need to contact them directly.

[1]     Pilot flying (PF) and Pilot monitoring (PM): procedurally assigned roles with specifically assigned duties at specific stages of a flight. The PF does most of the flying, except in defined circumstances such as planning for descent, approach and landing. The PM carries out support duties and monitors the PF’s actions and the aircraft’s flight path.

[2]     Flight level: at altitudes above 10,000 ft in Australia, an aircraft’s height above mean sea level is referred to as a flight level (FL). FL 350 equates to 35,000 ft.

[3]     All headings used in the report are magnetic.

[4]     First light: when the centre of the sun is at an angle of 6° below the horizon before sunrise. At this time the horizon is clearly defined but the brightest stars are still visible under clear atmospheric conditions.

Occurrence summary

Investigation number AO-2024-035
Occurrence date 14/06/2024
Location 19 km south of Canberra Airport
State New South Wales
Report release date 17/06/2025
Report status Final
Investigation level Defined
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Flight below minimum altitude
Occurrence class Serious Incident
Highest injury level None

Aircraft details

Manufacturer The Boeing Company
Model 737-8GP
Registration PK-LDK
Serial number 39875
Aircraft operator Batik Air
Sector Jet
Operation type Part 129 Foreign air transport operators
Departure point Denpasar International Airport, Bali, Indonesia
Destination Canberra Airport, Australian Capital Territory
Damage Nil

Loss of control and collision with terrain involving a Bell 47G-3B1, at Nyngan Aerodrome, New South Wales, on 15 March 2024

Occurrence Briefs are concise reports that detail the facts surrounding a transport safety occurrence, as received in the initial notification and any follow-up enquiries. They provide an opportunity to share safety messages in the absence of an investigation.

What happened

On 15 March 2024, a Bell 47G helicopter was conducting a post-purchase familiarisation flight at Nyngan, New South Wales. At 1200 local time, while hovering, the pilot commenced a practice left pedal clearing turn through the 180-degree position. The helicopter experienced weathercocking[1] followed by an unanticipated yaw. The wind was gusting 15‑20 knots. 

The pilot detected that the yaw rate was increasing and climbed the helicopter to 30 ft, attempting to control the increased rate of rotation through the application of the opposite anti-torque pedal. The pilot then experienced a loss of control resulting in a hard landing. The left skid subsequently detached from the airframe and the main rotor blades contacted the ground resulting in damage to the tail rotor guard tube and a tail rotor frame crack. 

The pilot detected leaking fuel from the fuel vents on top of the left fuel tank and a subsequent fire commenced at the base of the helicopter engine. The helicopter was destroyed by fire. 

Figure 1: Helicopter damage – looking at the base of the helicopter 

Figure 1: Helicopter damage – looking at the base of the helicopter

Source: Operator

Figure 2: Helicopter tail rotor damage  

Figure 2: Helicopter tail rotor damage

Source: Operator 

Pilot’s comments

Based on the pilot’s account of the accident and assessment of the recovered aircraft, mechanical malfunctions were ruled out as a contributing factor. 

The pilot advised that they may not have held an effective amount of pedal in an attempt to regain control. A better outcome could have been achieved by transitioning to forward flight allowing them to arrest the rotation speed through the use of the pedals in a controlled manner to improve directional stability. 

Safety message 

Unanticipated yaw is described by the European Union Aviation Safety Agency (EASA) as ‘an unanticipated or unintended rotation of the helicopter about the yaw axis. It occurs when the pedal input is not appropriate, and the helicopter suffers a sudden and unexpected yaw’.

A situational awareness of flight characteristics, weather conditions and recovery procedures are required when conducting low speed flight. The various wind directions can result in significantly differing rates of turn for a given pedal position. The most important principle for the pilot to remember is that the tail rotor is not stalled. The corrective action is to apply pedal opposite to the direction of the turn. Avoiding a loss of control may best be accomplished by pilots avoiding conditions which are conducive to unanticipated yaw. Appropriate and timely response is essential and critical. By maintaining an acute awareness of wind and its effect upon the helicopter, the pilot can significantly reduce exposure to an unanticipated yaw.

About this report

Decisions regarding whether to conduct an investigation, and the scope of an investigation, are based on many factors, including the level of safety benefit likely to be obtained from an investigation. For this occurrence, no investigation has been conducted and the ATSB did not verify the accuracy of the information. A brief description has been written using information supplied in the notification and any follow-up information in order to produce a short summary report, and allow for greater industry awareness of potential safety issues and possible safety actions.

[1]     Weathercocking - a helicopter with its tail into wind is in an unstable position. The wind acts on the vertical fin and continuous and variable yaw control inputs are required to achieve precise control and counteract the tendency of the helicopter to turn into wind. 

Occurrence summary

Mode of transport Aviation
Occurrence ID AB-2024-006
Occurrence date 15/03/2024
Location Nyngan Aerodrome, NSW
State New South Wales
Occurrence class Accident
Aviation occurrence category Collision with terrain
Highest injury level None
Brief release date 19/06/2024

Aircraft details

Manufacturer Bell Helicopter Co
Model 47G-3B1
Sector Helicopter
Operation type Part 91 General operating and flight rules
Departure point Nyngan Aerodrome, New South Wales
Destination Nyngan Aerodrome, New South Wales
Damage Destroyed

Accredited Representative to the Papua New Guinea Accident Investigation Commission – Runway excursion involving de Havilland Canada DHC-6 Twin Otter, P2-BBM, at Kikori Airstrip, Papua New Guinea, on 8 June 2024

Summary

On 8 June 2024, a de Havilland Canada DHC-6 Twin Otter, registered P2-BBM, had a runway excursion at Kikori Airstrip, Papua New Guinea.

The Papua New Guinea Accident Investigation Commission (AIC) is investigating the occurrence. AIC has requested assistance from the ATSB to decompress recovered flight data. 

To facilitate this support and to provide the appropriate protections for the information, the ATSB appointed an accredited representative in accordance with paragraph 5.23 of the International Civil Aviation Organization Annex 13 and commenced an investigation under the Australian Transport Safety Investigation Act 2003

The ATSB provided the decompressed file to the AIC on 19 June 2024.

Any enquiries relating to the investigation should be directed to AIC.

Occurrence summary

Investigation number AA-2024-007
Occurrence date 08/06/2024
Location Kikori Airstrip, Papua New Guinea
State International
Investigation type Accredited Representative
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Runway excursion

Aircraft details

Manufacturer De Havilland Canada/De Havilland Aircraft of Canada
Model DHC-6 Twin Otter
Registration P2-BBM
Sector Turboprop

Obstacles limited climb performance during go-around

An accident at a private airstrip on Queensland’s Sunshine Coast demonstrates the importance of pilots being prepared to conduct a missed approach, and of being aware of factors that affect climb performance.

On 12 November 2023, a Stoddard Hamilton Glastar light aircraft was being used for a private flight from a grass airstrip on a property near Boreen Point, north-east of Noosa, with a pilot and passenger on board.

An ATSB final report notes during the approach to land, the aircraft crossed a tree line in the runway undershoot and the pilot reported that the aircraft encountered sink.

The pilot advised they twice increased engine power in response, but the aircraft touched down firmly and was simultaneously struck by a gust of crosswind, which picked up the left wing and turned the aircraft to the right towards the house on the property.

In response the pilot initiated a go-around and the aircraft became airborne again, cleared a property fence and a building, and then struck the top of a palm tree before impacting the ground.

The aircraft was substantially damaged, the passenger sustained significant injuries, and the pilot sustained minor injuries.

Flight data examined by the ATSB indicated the aircraft had a 49 kt groundspeed as it crossed the threshold on final approach.

While weather data recorded at the nearest airport – Sunshine Coast – indicated some headwind, which would have raised the airspeed, airspeed was still probably below the 65–60 kt recommended by the aircraft’s pilot operating handbook (POH).

“The unexpected sink on final approach would also be consistent with the POH, which advises of increased sink at reduced airspeed,” ATSB Director Transport Safety Stuart Macleod explained.

Once the decision was made to go around, the ATSB report notes, the aircraft was not realigned with the airstrip and instead headed towards the house.

“Obstacles prevented the aircraft from being flown at the optimal, shallow climb profile to increase airspeed,” Mr Macleod said.

“Consequently, the aircraft’s speed and height remained low, resulting in it striking the top of a tree close to the stall speed, before impacting the ground.”

The accident is a reminder for pilots to be prepared to conduct a missed approach, and to be aware of the factors which could affect subsequent climb performance.

“A preparedness to conduct a missed approach and being aware of aircraft climb performance mitigates against slow reaction times to a surprising or startling event, and ensures a safe go-around,” Mr Macleod said.

Read the final report: Collision with terrain involving a Stoddard Hamilton Aircraft Glastar, VH-BAQ, about 18 km north-west of Noosa, Queensland, on 12 November 2023

Accredited Representative to the Indonesian National Transportation Safety Committee – Collision with terrain involving Tecnam P2600T, PK-IFP, 11 km north-west of Pondok Cable Airport, Jakarta, Indonesia, on 19 May 2024

Summary

On 19 May 2024, a Tecnam P2600T aircraft was being operated on a flight from Salakanagara Tanjung Lesung airfield, Banten, Indonesia to Pondok Cabe Airport, Jakarta, Indonesia, with 3 people on board. At 1344 local time, on approach to Pondok Cable Airport at an altitude of 1,000 ft, the pilot declared a MAYDAY. Shortly after, the aircraft collided with terrain near a main road. All occupants were fatally injured. 

The Indonesian National Transportation Safety Committee (NTSC) is investigating this occurrence. 

NTSC has requested assistance from the ATSB to recover data from a damaged GPS unit. To facilitate this support and to provide the appropriate protections for the information, the ATSB appointed an accredited representative in accordance with paragraph 5.23 of the International Civil Aviation Organization Annex 13 and commenced an investigation under the Australian Transport Safety Investigation Act 2003.

The ATSB has completed its work recovering the GPS data. A copy of the data and a report detailing the work undertaken by the ATSB was provided to the NTSC on 19 July 2024.

Any enquiries relating to the investigation should be directed to NTSC.

Occurrence summary

Investigation number AA-2024-006
Occurrence date 19/05/2024
Location 11 km north-west of Pondok Cable Airport, Jakarta
State International
Investigation type Accredited Representative
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Collision with terrain
Occurrence class Accident
Highest injury level Fatal

Aircraft details

Manufacturer Tecnam - C. Aeronautiche SRL
Model P2600T
Sector Piston