Collision with terrain - MD Helicopters Inc.369D, YJ-HEL, Unua Village, Malekula, Vanuatu, on 26 August 2011

Final report

Report release date: 02/10/2012

Safety summary

What happened

On 26 August 2011, the pilot of an MD Helicopter Inc. 369D helicopter, registered YJ‑HEL, was conducting sling load operations near a small village 183 km north‑north‑west of Port Vila, Vanuatu. As the helicopter approached the village, with two passengers onboard, witnesses heard a single, loud bang and watched the helicopter fall 10 to 15 m to the ground before coming to rest on its right side. One of the passengers received minor injuries and was able to exit the helicopter unaided. The other passenger received serious injuries, and the pilot was fatally injured.

What the ATSB found

The ATSB found that as the helicopter approached the village to land, the wire rope attached to the helicopter’s cargo hook contacted a tree. That contact resulted in the rope fouling on the main rotor blades, which in turn led to the detachment of segments of the rotor blades and the tail boom. This rendered the helicopter uncontrollable. It was also found that the occupants of the helicopter were not wearing the installed shoulder harness restraints or using flight helmets during the flight.

What has been done as a result

This investigation was conducted by the ATSB at the request of the Civil Aviation Authority of Vanuatu and no organisational or systemic issues that might adversely affect the future of aviation operations in Vanuatu were identified.

Safety message

The circumstances of this accident serve as a reminder that the severity of contact injuries in survivable helicopter accidents can be significantly reduced by the use of shoulder harnesses and protective flight helmets. As such, pilots and operators should consider the use of such equipment in the interest of enhancing survivability should an accident occur.

Occurrence summary

Investigation number AO-2011-108
Occurrence date 26/08/2011
Location Unua village, Malekula, Vanuatu
State International
Report release date 02/10/2012
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Collision with terrain
Occurrence class Accident
Highest injury level Fatal

Aircraft details

Manufacturer McDonnell Douglas Corp.
Model 369
Registration YJ-HEL
Serial number 80778D
Sector Helicopter
Operation type Aerial Work
Departure point Maleluka Island, Vanuatu
Destination Maleluka Island, Vanuatu
Damage Destroyed

Wirestike - Air Tractor AT-802, VH-NIW, 5 km north of Mogumber, Western Australia, on 26 August 2011

Summary

Report release date: 14/03/2012

What happened

On 26 August 2011, at about 1545 Western Standard Time, an Air Tractor Inc. AT-802, registered VH-NIW, struck power lines and impacted terrain, during agricultural spraying operations.

Earlier that day, the pilot had commenced the first of six agricultural spraying flights. At mid-morning, he was approached by a farmer to carry out an unscheduled spraying operation of wheat paddocks next to a main road. The farmer supplied the pilot with a map of the fields to spray, which included the location of two powerlines.

On reaching the property, the pilot commenced his field inspection and identified the two powerlines and paddocks marked on the farmer's map. At the same time, he noticed vehicle traffic on the main road located next to the spraying area and a third set of powerlines.

The pilot noted a break in the traffic and commenced the spraying operation. When about 300 m into the paddock, the aircraft struck an unseen fourth set of powerlines. The aircraft's engine lost power and impacted terrain in a neighbouring paddock. The aircraft sustained serious damage, and the pilot was not injured.

This accident highlights the vital role hazard identification plays, particularly when operating at low-level, and how distractions can impact operations. It is a reminder that distractions are not unique to any one type of operation and that no pilot is immune.

Occurrence summary

Investigation number AO-2011-107
Occurrence date 26/08/2011
Location 5 km N of Mogumber
State Western Australia
Report release date 14/03/2012
Report status Final
Investigation level Short
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Wirestrike
Occurrence class Accident
Highest injury level None

Aircraft details

Manufacturer Air Tractor Inc
Model AT802
Registration VH-NIW
Serial number 802-0300
Sector Turboprop
Operation type Aerial Work
Departure point Newdale, Western Australia
Destination Newdale, Western Australia
Damage Substantial

Aircraft proximity event - Saab 340B, VH-ZRC, and a Hawker Beechcraft B200, VH-MWH, 87 km east of Broken Hill Airport, New South Wales, on 26 August 2011

Summary

Report release date: 24/05/2012

What happened

On 26 August 2011, a Hawker Beechcraft Corporation B200 aircraft, registered VH-MWH (MWH), departed Ivanhoe for Broken Hill, New South Wales. While maintaining flight level 140, the pilot of MWH received a traffic alert and collision avoidance system (TCAS) traffic advisory (TA) on a Regional Express S.A.A.B. Aircraft Corporation 340B aircraft, registered VH-ZRC (ZRC), which had departed Broken Hill for Sydney and was on climb to flight level 170.

At about the same time, while climbing through flight level 130, the crew of ZRC received a TCAS TA, shortly followed by a resolution advisory (RA). As the First Officer (FO) believed they were above MWH, he immediately commenced a climb. Shortly after, the Captain noted that the FO's response was contrary to the RA command to descend and advised the FO, who immediately commenced a descent.

A review of the Airservices Australia radar data indicated that, with both aircraft at flight level 142, lateral separation reduced to 2.2 NM.

This incident highlighted the benefit of TCAS in assisting pilots with traffic awareness and the importance of responding appropriately to a TCAS RA.

Occurrence summary

Investigation number AO-2011-106
Occurrence date 26/08/2011
Location 87 km east of Broken Hill Airport
State New South Wales
Report release date 24/05/2012
Report status Final
Investigation level Short
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Separation issue
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Saab Aircraft Co.
Model 340
Registration VH-ZRC
Serial number 340B-390
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Broken Hill, New South Wales
Destination Sydney, New South Wales
Damage Nil

Aircraft details

Manufacturer Hawker Beechcraft Corporation
Model 200
Registration VH-MWH
Serial number BB-2003
Sector Turboprop
Operation type Medical Transport
Departure point Ivanhoe, New South Wales
Destination Broken Hill, New South Wales
Damage Nil

Collision with terrain - PZL-Mielec M18A Turbine Dromader, VH-FOZ, 23 km west-south-west of Dirranbandi, Queensland, on 19 July 2011

Final report

Report release date: 08/06/2012

Safety summary

What happened

At 1157 on 19 July 2011, a PZL-Mielec M18A Turbine Dromader aircraft, registered VH-FOZ, impacted terrain on a cotton station about 23 km west-south-west of Dirranbandi, Queensland while conducting a spraying flight. The pilot was fatally injured, and the aircraft was destroyed by impact forces.

What the ATSB found

The ATSB found that, for reasons that could not be determined with certainty, the aircraft departed from controlled flight during a turn at low altitude and the pilot was unable to recover before impacting the ground.

The ATSB also identified a significant safety issue affecting the safety of future spraying operations in turbine Dromader aircraft: the potential for the aircraft's centre of gravity to vary significantly depending on the weight in the aircraft's chemical/spray tank and exceed the forward and aft limits during a flight. This safety issue was unlikely to have contributed to the accident as the aircraft was probably within the approved weight and balance limits at the time of the accident.

Moreover, although also not found to have contributed to the accident, there was an increased risk to the flight from the aircraft's operation, at times, in excess of its published airspeed and angle of bank limitations.

What has been done as a result

During the investigation, the Australian Transport Safety Bureau worked with the Civil Aviation Safety Authority (CASA) and the Aerial Agricultural Association of Australia to address the risk to turbine Dromader aircraft of the potential for excessive movement of the aircraft's centre of gravity as the contents of the aircraft's chemical/spray tank are dumped or dispensed.

CASA and the owner/developer of the approval for operations at weights of up to 6,600 kg, which had effect during the flight, took action to improve operator and pilot understanding of the issue. In addition, the owner/developer indicated that the design would be reviewed to address any excessive centre of gravity variations.

Safety message

Although it was not contributory in this instance, the ATSB highlights the importance of pilots maintaining their aircraft's weight and balance within limits throughout a flight, and of understanding the implications of changing weight and balance. Similarly, the ATSB reaffirms the importance of being familiar with and adhering to aircraft operational limitations.

Preliminary report

Report release date: 25/08/2011

What happened

On 19 July 2011 a PZL Warszawa-Okecie M-18 Dromader, registered VH-FOZ, was conducting spraying operations on a cotton station about 22 km west-south-west of Dirranbandi, Queensland. The aircraft failed to return from a spraying flight and workers on the station subsequently located the aircraft's wreckage in a ploughed field at about 1445. The pilot, who was the sole occupant, was fatally injured. The aircraft was destroyed by the impact forces.

Occurrence summary

Investigation number AO-2011-082
Occurrence date 19/07/2011
Location 23 km WSW of Dirranbandi
State Queensland
Report release date 08/06/2012
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Loss of control
Occurrence class Accident
Highest injury level Fatal

Aircraft details

Manufacturer PZL Warszawa-Okecie
Model M18
Registration VH-FOZ
Serial number 1Z014-10
Sector Turboprop
Operation type Aerial Work
Damage Destroyed

Engine power loss - Cessna 206G aircraft, VH-LAN, near William Creek ALA, Lake Eyre, South Australia, on 23 August 2011

Summary

Report release date: 14/03/2012

What happened

On 23 August 2011, at about 1145 CST, a Cessna Aircraft Company model U206G aircraft, registered VH-LAN, was conducting a charter flight from Olympic Dam to William Creek Aircraft Landing Area (ALA) near Lake Eyre, South Australia, with the pilot and five passengers aboard, incurred an engine power loss. As a result, the pilot conducted a forced landing onto a dry lakebed. During the landing, the aircraft nose wheel sunk into the soft ground and the aircraft nosed over with the propeller blades and left-wing tip contacting the ground, then settled onto the landing gear. There were no injuries to the occupants who exited the aircraft without incident. Subsequent examination revealed that one engine cylinder had failed.

As a result of this accident, the operator chose to remove from service all engine cylinders provided by the specific manufacturer.

Occurrence summary

Investigation number AO-2011-104
Occurrence date 23/08/2011
Location Near William Creek ALA, Lake Eyre
State South Australia
Report release date 14/03/2012
Report status Final
Investigation level Short
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Engine failure or malfunction
Occurrence class Accident
Highest injury level None

Aircraft details

Manufacturer Cessna Aircraft Company
Model 206
Registration VH-LAN
Serial number U20606574
Sector Piston
Operation type Charter
Departure point Birdsville, Queensland
Destination William Creek, South Australia
Damage Minor

VFR flight into dark night involving Aérospatiale AS355F2 (Twin Squirrel), VH-NTV, 145 km north of Marree, South Australia, on 18 August 2011

Final report

Report release date: 14/11/2013

Safety summary

What happened

On 18 August 2011, an Aérospatiale  AS355F2 (Twin Squirrel) helicopter, registered VH-NTV, was being operated under the visual flight rules (VFR) in an area east of Lake Eyre, South Australia. At about 1900 Central Standard Time, the pilot departed an island in the Cooper Creek inlet with two film crew on board for a 30-minute flight to a station for a planned overnight stay. It was after last light and, although there was no low cloud or rain, it was a dark night.

The helicopter levelled at 1,500 ft above mean sea level, and shortly after entered a gentle right turn and then began descending. The turn tightened and the descent rate increased until, 38 seconds after the descent began, the helicopter impacted terrain at high speed with a bank angle of about 90°. The pilot and the two passengers were fatally injured, and the helicopter was destroyed.

What the ATSB found

The ATSB found that the pilot probably selected an incorrect destination on one or both of the helicopter's global positioning system (GPS) units prior to departure. The ATSB concluded that, after initiating the right turn at 1,500 ft, the pilot probably became spatially disoriented. Factors contributing to the disorientation included dark night conditions, high pilot workload associated with establishing the helicopter in cruise flight and probably attempting to correct the fly-to point in a GPS unit, the pilot’s limited recent night flying and instrument flying experience, and the helicopter not being equipped with an autopilot.

Although some of the operator’s risk controls for the conduct of night VFR were in excess of the regulatory requirements, the operator did not effectively manage the risk associated with operations in dark night conditions. The ATSB also identified safety issues with the existing regulatory requirements in that flights for some types of operations were permitted under the VFR in dark night conditions that are effectively the same as instrument meteorological conditions, but without the same level of safety assurance that is provided by the requirements for flight under the instrument flight rules (IFR).

What's been done as a result

The Civil Aviation Safety Authority (CASA) has advised of safety actions in progress to clarify the nature of what is meant by the term ‘visibility’ in dark night conditions, provide enhanced guidance on night VFR flight planning, and provide enhanced guidance on other aspects of night VFR operations. The ATSB has issued a recommendation to CASA to prioritise its efforts in this area. In addition, CASA advised that it will require that helicopter air transport operations with passengers at night use either a helicopter fitted with an autopilot or a two-pilot crew.

Safety message

The ATSB advises all operators and pilots considering night flights under the VFR to systematically assess the potential for the flight to encounter dark night conditions by reviewing weather conditions, celestial illumination and available terrain lighting. If there is a likelihood of dark night conditions, the flight should be conducted as an IFR operation, or conducted by a pilot who has an IFR-equivalent level of instrument flying proficiency and in an aircraft that is equipped to a standard similar to that required under the IFR.

Preliminary report

What happened

On 18 August 2011, an Aérospatiale Industries AS355F2 helicopter, registered VH-NTV, was operating in an area east of Lake Eyre, South Australia (SA). On board were the pilot and two passengers. The helicopter landed on an island in the Cooper Creek inlet, about 145 km north of Marree, SA, at about 1715 Central Standard Time.

At about 1900, the helicopter departed the island, and soon after take-off it collided with terrain. The pilot and the two passengers were fatally injured, and the helicopter was destroyed by the impact forces and a fuel-fed fire.

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Updated 19 July 2013

The Australian Transport Safety Bureau (ATSB) received the results of the flight simulations and modelling that were previously advised as being conducted by external specialists in June 2012. The ATSB is now finalising its draft report, which will be sent to directly involved parties and other parties with an interest in July/August 2013. Feedback from those parties on the factual accuracy of the draft report over the 28-day DIP period will be considered for inclusion in the final report, which is anticipated to be released to the public in September/October 2013. 

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Updated 9 July 2013

The Australian Transport Safety Bureau (ATSB) received the results of simulations and modelling conducted by external specialists in June 2012. The ATSB is now finalising its draft report, which will be sent to directly involved parties and other parties with an interest in July/August 2013. The final report will be publicly released in September/October 2013.

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Update 26 November 2012

The Global Positioning System (GPS) data that was recovered from the accident site indicates that the helicopter took off normally, before being established on a heading of 035 °M at 1,500 ft above mean sea level (AMSL). After maintaining 1,500 ft for 17 seconds, the helicopter commenced a gradual turn to the right and started to descend. The descending right turn continued for about 35 seconds until the last GPS plot at an altitude of about 728 ft, or about 725 ft above the elevation of the accident site. The location of the accident site was consistent with a continuation of the recorded flight path.

The Australian Transport Safety Bureau (ATSB) is examining various scenarios to explain the helicopter’s flight path, including spatial disorientation and pilot incapacitation. As part of these activities, the ATSB has arranged for simulations to be conducted of the flight by external agencies. Given the time required to conduct and analyse these simulations, the final report is now not expected to be released until the first quarter of 2013.

Although the reasons for the flight path have not yet been determined, the ATSB is concerned about the conduct of visual flight rules (VFR) flights in dark night conditions – that is, conditions with minimal celestial illumination, terrestrial lighting cues or visible horizon. The ATSB is reviewing the regulatory requirements and guidance for the conduct of night VFR flights, and the training and ongoing assessment of pilot skills to conduct such flights. The ATSB is also preparing an ‘Avoidable Accidents’ educational report focussing on night VFR accidents. 

The information contained in this web update is released in accordance with section 25 of the Transport Safety Investigation Act 2003 and is derived from initial investigation of the occurrence. Readers are cautioned that new evidence will become available as the investigation progresses that will enhance the ATSB’s understanding of the occurrence as outlined in the web update. As such, no analysis or findings are included in this update.

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Update 15 August 2012

Since the Preliminary Report was issued on 16 September 2011, the ATSB investigation has:

  • examined the helicopter's maintenance and airworthiness records
  • examined the helicopter's engines, instruments and other recovered components
  • tested fuel samples from the drums that were used to refuel the helicopter
  • recovered and analysed data from a GPS device on board the helicopter
  • reviewed the pilot's experience and medical status
  • analysed witness statements and conducted further witness interviews as required. 

The download and analysis of the GPS data required an extensive period of time, as well as input from overseas investigation agencies.
 
Overall, the analysis of the circumstances of the accident has been difficult due to the limited evidence available.
 
The ATSB has completed its data collection activities and is preparing its draft final report, which will be issued to Directly Involved Parties for their comments.

Occurrence summary

Investigation number AO-2011-102
Occurrence date 18/08/2011
Location 145 km north of Marree (near Lake Eyre)
State South Australia
Report release date 14/11/2013
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Loss of control
Occurrence class Accident
Highest injury level Fatal

Aircraft details

Manufacturer Aerospatiale Industries
Model AS355
Registration VH-NTV
Serial number 5380
Sector Helicopter
Operation type Aerial Work
Damage Destroyed

Fuel starvation - Cessna 210N, VH-OCM, Kununurra Airport, Western Australia, on 18 August 2011

Summary

Report release date: 14/03/2012

What happened

On 18 August 2011, at 0755 Western Standard Time, a Cessna Aircraft Company 210N aircraft registered VH-OCM, departed Mitchell Plateau, Western Australia, on a charter flight to Kununurra. On board were the pilot and five passengers.

Prior to departure the fuel quantity was physically checked and recorded. The pilot completed a normal take-off and climbed to a cruise altitude of 5,500ft above mean seal level (AMSL).  At about 28 NM from Kununurra aerodrome, the pilot commenced descent for a straight-in approach to runway 12.  At 3 NM from the runway threshold, the pilot reduced engine power and lowered the flaps, then commenced the pre-landing checks. The aircraft started to sink below the approach profile during strong wind gusts. The pilot increased engine power to regain the approach profile, and did not complete the pre-landing checks, including selecting the fullest fuel tank for the landing.

At about 0.6 NM from the runway threshold, and approximately 250ft above ground level (AGL) the engine began to splutter then stopped. The pilot lowered the nose of the aircraft to maintain airspeed and checked the fuel mixture, fuel pumps on and both magnetos on. When the engine failed to start, the pilot broadcast a Mayday call. At about 0928 he conducted a forced landing short of the runway threshold. During the landing, the aircraft impacted an earth bank and was seriously damaged and one passenger sustained a minor injury. The pilot secured the aircraft and disembarked the passengers.

In response to the accident, the operator implemented the following actions to reduce the risk of another occurrence.

  • An operations manual amendment was raised to require all pilots to use a standardised fuel log on all flights.
  • For new engines being run-in, increased block fuel flow figures for flight planning will be used.

Occurrence summary

Investigation number AO-2011-101
Occurrence date 18/08/2011
Location Kununurra Airport
State Western Australia
Report release date 14/03/2012
Report status Final
Investigation level Short
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Fuel starvation
Occurrence class Accident
Highest injury level Minor

Aircraft details

Manufacturer Cessna Aircraft Company
Model 210
Registration VH-OCM
Serial number 21064466
Sector Piston
Operation type Charter
Departure point Mitchell Plateau, Western Australia
Destination Kununurra, Western Australia
Damage Substantial

Investigation of rail operations on the interstate rail line between Melbourne and Sydney

Preliminary report

Preliminary report released 29 September 2011

On 16 August 2011, the Hon Anthony Albanese MP, Minister for Infrastructure and Transport, requested that the Australian Transport Safety Bureau (ATSB) undertake a systemic investigation of rail operations on the interstate rail line between Sydney and Melbourne. In accordance with the Minister's request the ATSB commenced a safety issue investigation which will consider:

  • The condition of the interstate rail track and measures that have been put in place to maintain the safety of rail operations where track quality is below acceptable operational standards;
  • Actions taken by the Australian Rail Track Corporation (ARTC) to remediate the track and address the safety of operations;
  • Safeworking practices in relation to the track;
  • A systemic review of safety systems, including signalling and the quality assurance of work undertaken on the track; and,
  • Any other matters considered relevant by the ATSB.

Interim factual

Interim factual report released 8 February 2012

On 16 August 2011, the Hon Anthony Albanese MP, Minister for Infrastructure and Transport, requested that the Australian Transport Safety Bureau (ATSB) undertake a systemic investigation of rail operations on the interstate rail line between Melbourne and Sydney.

A key request from the Minister was for the ATSB to examine and report on the measures taken to maintain the safety of rail operations where track quality is below acceptable operational standards. This interim report provides a summary of factual information that has been obtained during the early stages of the investigation and focuses on the processes put in place to maintain the safety of rail operations.

 

 

 

 

 

Executive summary

In 2007, the Australian Rail Track Corporation (ARTC) embarked on a major investment program to upgrade the rail track between Melbourne and Sydney. Since the program began, there have been a number of incidents and the condition of the line has been subject to significant adverse comment about its safety, largely in relation to rough ride characteristics and the existence and lack of remediation of ‘mud-holes’. On 16 August 2011, the Hon Anthony Albanese MP, Minister for Infrastructure and Transport, requested that the Australian Transport Safety Bureau (ATSB) undertake an investigation to examine (in broad terms) the safety of rail operations on the Melbourne to Sydney line.

In the course of its subsequent investigation, the ATSB found that the track structure between Melbourne and Sydney had historically been particularly vulnerable to degradation in vertical alignment, resulting in poor ride quality and mud-holes. While this was the result of a number of factors, major contributors were the weakness of the track formation (the earthwork foundation on which the track was laid) and ballast fouling (contamination of the aggregate material laid between the formation and the rails and sleepers).

In some locations, this pre-existing vulnerability had been increased by the track upgrade as a result of the process of installing new concrete sleepers. This exacerbated the problems of the pre-existing weak formation and reduced the effectiveness of the ballast. In addition, train forces on a weakened formation, as well as the effects of highly fouled ballast, poor drainage and heavy rainfall during 2010 and 2011, contributed to the development of mud-holes and poor vertical alignment. It is also possible that rail imperfections (localised defects) may have introduced concentrated impact loading that, when transmitted through the sleepers and ballast, may also have overstressed the formation in some locations.

The decisions made by the ARTC about the planning and execution of the upgrade project balanced safety, financial and operational considerations. The ARTC determined that the long term benefits of completely re-sleepering the track between Melbourne and Sydney were high. Safety improvements focused predominantly on controlling track gauge through the installation of concrete sleepers, while financial and operational considerations focused on minimal disruption to rail services and maximum track coverage (sleeper replacement) within financial constraints. The ARTC concluded that this was only possible if the side insertion method of re-sleepering was used and existing ballast was reused as much as possible. The upgrade program proceeded on this basis.

However, the ARTC’s quality assurance process during the project planning phase did not adequately consider foreseeable risks in relation to the track structure’s pre-existing vulnerabilities. It is possible that a more detailed examination of historical information and/or on-site testing may have highlighted any unknown track structure issues and influenced the decisions made prior to the re-sleepering works. Similarly, the ARTC was aware that the existing ballast and track drainage were in poor condition, but appeared not to have adequately considered the potential for higher than normal rainfall following a protracted period of drought. The ARTC believed the drainage problems could be addressed as part of ongoing maintenance programs, but has acknowledged that, following the track upgrade, the rate of track deterioration (including the development of mud-holes) was faster than expected.

During the early stages of the re-sleepering project, the quality control process focused on sleeper spacing, fastening of the rail to new sleepers, clearance of trackside infrastructure and the re-establishment of track geometry, but was inadequate with respect to ballast condition and depth of ballast under the new sleepers. During the course of the project, the procedures were updated based on additional identified risks, including the potential for formation damage due to inadequate ballast depth. The ARTC has since developed more detailed process documentation for side insertion of concrete sleepers. The updated process includes a stronger focus on quality assurance and recording of quality control data. In general, the ARTC appeared to have a quality assurance process in place that provided for identification of deficiencies, systems review and subsequent improvement to work practices.

It is unlikely that selecting an alternative method of re-sleepering would have prevented deterioration in track condition or the development of mud-holes, unless ballast, drainage and formation issues were also addressed. It is also likely that the cost associated with addressing the ballast, drainage or formation issues would have precluded completely re-sleepering the Melbourne to Sydney line with the funding available and therefore some residual safety risk associated with poor track gauge would have remained if this path had been chosen.

The track deterioration following the re-sleepering works required both short term management and the development of a longer-term major rectification program to maintain the operational effectiveness of the track. For the short term, an increased inspection and maintenance frequency, especially during periods of wet weather, was adopted. Where rail geometry defects were identified, actions were applied as specified by the ARTC (Track & Civil) Code of Practice. Pending rectification, the safety of train operations were maintained largely through the application of speed restrictions. These speed restrictions, together with increased maintenance activities, have resulted in extended train running times along the corridor.

While the application of temporary speed restrictions may in general control the safety risk, the system still relies on prompt identification of track condition hazards before the control measures can be implemented. If the track is performing in a constantly poor and degraded condition, there is an increased risk that defects compromising safety are not immediately identified. In this case, the ARTC have increased the inspection regime to mitigate this risk. However, if the system was performing well, it is likely to be inherently safer since it would place fewer burdens on the defect identification process.

The rail safety regulators in Victoria and New South Wales have, and continue to, actively monitor, audit and inspect the activities of the ARTC with respect to safety on the rail network. Regulatory intervention has resulted in the modification or development of processes aimed at ensuring the safety of rail operations. With the introduction of the Office of the National Rail Safety Regulator, this involvement has continued, but with a more national perspective.

Considering the combination of actions implemented by the ARTC and by the rail safety regulators, the ATSB is satisfied that safety of operations on the Melbourne to Sydney line has been maintained at an appropriate level, albeit with a requirement for greater vigilance to be applied to the inspection of deteriorating track conditions.

Longer term strategies ARTC implemented to rectify persistent problem areas on the line included a combination of undercutting and sledding to address ballast problems (fouling and depth) and track works targeting the correction of general drainage problems. While the treatments applied to date are likely to correct most ballast and drainage problems, the treatments are unlikely to correct the more deep-seated formation problems. Unless additional treatments are applied to improve the formation, it is possible that water will continue to weaken the structure in some locations, with a corresponding requirement for an increased regime of track maintenance (or some localised formation reconstruction) and the application of new or further speed restrictions.

Since the safety of the Melbourne to Sydney line remains dependent on the application of temporary speed restrictions, the ATSB examined the adequacy of the processes for applying such restrictions. The ATSB identified a number of opportunities where operational rail safety could be improved. This was detailed in an Interim Factual Report released in February 2012. The ARTC advised of their proposed actions in response and the ATSB is satisfied that those actions addressed the issues that were identified.

Both the initial upgrade and the subsequent rectification program led to a significant amount of track work being conducted on the Melbourne to Sydney line. This increased the likelihood of safeworking incidents involving track maintenance activities. The ATSB examined a number of reported safeworking incidents that occurred at various times between 2009 and 2012 and found that, in general, the safeworking rules and procedures were adequate as long as they were complied with. However, some of the incidents highlighted that protection methods for work on track were susceptible to human error, either through mistake or violation. In some cases, the safeworking systems were vulnerable to a ‘single point of failure’ which could increase the risk to rail safety. The ARTC, in consultation with rail safety regulators, has implemented changes to their systems for safely managing work on track and help protect against human error.

During the course of the investigation, rail operators also raised a number of specific concerns about the safety of the Melbourne to Sydney rail line. These related to elements of the signalling system, train parting incidents and quality assurance of track-related work. For signalling, the ATSB found that the principles applied to signalling design and the process for assessing signal sighting issues were consistent with recognised acceptable practice. For train partings, the ATSB found that track condition was a factor but not always the sole issue. Where deficiencies were identified, the ARTC issued additional instructions aimed at ensuring the safety of rail operations.

Taken as a whole, the ATSB is satisfied that the necessary steps have been taken to address any issues that might otherwise compromise the safety of rail operations where track quality is below acceptable operational standards. However, the actions taken to ensure safe operations have come at the expense of operational efficiencies through increased train running times.

Occurrence summary

Investigation number RI-2011-015
Occurrence date 16/08/2011
Location Melbourne, Vic to Sydney, NSW
State Victoria
Report release date 22/08/2013
Report status Final
Investigation level Systemic
Investigation type Research Investigation
Investigation status Completed
Mode of transport Rail
Occurrence class Technical Analysis
Highest injury level None

VFR flight into dark night conditions and loss of control involving Piper PA-28-180, VH-POJ, 31 km north of Horsham Airport, Victoria, on 15 August 2011

Final report

Report release date: 03/12/2013

Safety summary

What happened

On 15 August 2011, the pilot of a Piper PA‑28‑180 Cherokee aircraft, registered VH-POJ, was conducting a private flight transporting two passengers from Essendon to Nhill, Victoria under the visual flight rules (VFR). The flight was arranged by the charity Angel Flight to return the passengers to their home location after medical treatment in Melbourne. Global Positioning System data recovered from the aircraft indicated that when about 52 km from Nhill, the aircraft conducted a series of manoeuvres followed by a descending right turn. The aircraft subsequently impacted the ground at 1820 Eastern Standard Time, fatally injuring the pilot and one of the passengers. The second passenger later died in hospital as a result of complications from injuries sustained in the accident.

What the ATSB found

The ATSB found that the pilot landed at Bendigo and accessed a weather forecast before continuing towards Nhill. After recommencing the flight, the pilot probably encountered reduced visibility conditions approaching Nhill due to low cloud, rain and diminishing daylight, leading to disorientation, loss of control and impact with terrain. One of the passengers was probably not wearing a seatbelt at the time of the accident.

The ATSB also established that flights are permitted under the visual flight rules at night (night VFR) in conditions where there are no external visual cues for pilots. In addition, pilots conducting such operations are not required to maintain or periodically demonstrate their ability to maintain aircraft control with reference solely to flight instruments.

What's been done as a result

As a result of previous ATSB investigations the Civil Aviation Safety Authority (CASA) has drafted new legislation, effective 4 December 2013, requiring a biennial review for night VFR‑rated pilots. In addition, CASA has indicated that it will clarify the nature of what is meant by the term ‘visibility’ in dark night conditions, provide enhanced guidance on night VFR flight planning, and provide enhanced guidance on other aspects of night VFR operations. The ATSB issued a safety recommendation as a result of investigation AO-2011-102 for CASA to prioritise this initiative.

The ATSB is also producing an educational booklet in its Avoidable Accident Series related to visual flight at night. When released, this safety education booklet will highlight a number of the risks associated with night VFR flight and discuss strategies for their management.

Safety message

All operators and pilots considering night VFR flights should assess the likelihood of dark night conditions by reviewing the weather conditions, celestial illumination and available terrain lighting affecting their planned flight. A VFR flight in dark night conditions should only be conducted by a pilot with high instrument flying proficiency as there is a significant risk of losing control if attempting to fly visually in such conditions. Application by pilots of the recommendations in CASA advisory publication CAAP 5.13-2(0) will reduce the risks associated with visual flight at night.

Additionally, wearing seatbelts will reduce the likelihood and severity of injuries in an aircraft accident.

Preliminary report

Report release date: 20/09/2011

What happened

On 15 August 2011, a Piper Aircraft Inc. PA‑28‑180 aircraft, registered VH-POJ, was conducting a private flight between Essendon Airport, Victoria and Nhill Aerodrome, Victoria under the visual flight rules (VFR). On board were the pilot and two passengers. The purpose of the flight was to transport one of the passengers, who had been in Melbourne, Victoria for non-emergency medical reasons, back to Nhill.

VH-POJ departed Essendon at 1600 and the pilot made an unplanned landing at Bendigo, Victoria at 1649. The aircraft departed Bendigo for Nhill at 1711.

The weather in the area around the accident was reported by other pilots not to have been suitable for VFR flight in the late afternoon.

Witnesses in, and to the south west of, Warracknabeal, Victoria reported hearing and/or seeing a low-flying light aircraft from approximately 1800 onwards. At approximately 1820, a loud bang was heard.

The aircraft's emergency locator transmitter did not activate. Witnesses raised the alarm immediately, but the crash site was not found until two hours after the accident occurred; the police and emergency services arrived at the scene a further thirty minutes after that.

Although classified as a private operation, the flight had been organised as an 'Angel Flight' by the charity, Angel Flight™ Australia.

The draft investigation report was finalised and released to directly involved parties (DIPs) on 19 September 2013 for comment by 17 October. Feedback from those parties on the factual accuracy of the draft report will be considered for inclusion in the final report, which is anticipated to be released to the public in early December 2013.

Inquest

ATSB response to the Coroner

The ATSB notes that the Victorian Coroner, Jacinta Heffey has recently released a finding into a fatal accident without holding an inquest. The Coroner agreed with the conclusion in the ATSB report published on 3 December 2013 regarding the likely cause of the accident and was satisfied that the safety issue identified by the ATSB investigation into the accident was appropriate. The Coroner also noted that the ATSB had made a recommendation to the Civil Aviation Safety Authority (CASA) in relation to that safety issue.

Circumstances of the accident

On 15 August 2011, the pilot of a Piper PA‑28‑180 Cherokee aircraft, registered VH-POJ, was conducting a private flight transporting two passengers from Essendon to Nhill, Victoria under the visual flight rules (VFR).

Global Positioning System data recovered from the aircraft indicated that when about 52 km from Nhill, the aircraft conducted a series of manoeuvres followed by a descending right turn. The aircraft subsequently impacted the ground at 1820 Eastern Standard Time, fatally injuring the pilot and one of the passengers. The second passenger later died in hospital as a result of complications from injuries sustained in the accident.

ATSB Findings

The ATSB found that the pilot landed at Bendigo and accessed a weather forecast before continuing towards Nhill. After recommencing the flight, the pilot probably encountered reduced visibility conditions approaching Nhill due to low cloud, rain and diminishing daylight, leading to disorientation, loss of control and impact with terrain. One of the passengers was probably not wearing a seatbelt at the time of the accident.

The ATSB also established that flights are permitted under the VFR at night (night VFR) in conditions where there are no external visual cues for pilots. In addition, pilots conducting such operations are not required to maintain or periodically demonstrate their ability to maintain aircraft control with reference solely to flight instruments.

Contributing factors

The pilot departed Bendigo for Nhill under the VFR with a high risk of encountering forecast cloud and dark night conditions and of subsequent loss of control due to loss of visual reference and probable spatial disorientation.

Aerial work and private flights were permitted under the VFR in dark night conditions, which are effectively the same as instrument meteorological conditions, but without sufficient requirements for proficiency checks and recent experience to enable flight solely by reference to the flight instruments.

Other factors that increased risk

One of the passengers probably did not use the installed seatbelt, resulting in a greater risk of injury during the collision with terrain.

Safety issue - recommendation

The ATSB issued a safety recommendation to CASA that it prioritise its efforts to address the safety risk associated with aerial work and private flights as permitted under the VFR in dark night conditions, which are effectively the same as instrument meteorological conditions, but without sufficient requirements for proficiency checks and recent experience to enable flight solely by reference to the flight instruments.

CASA’s response to the safety issue may be found at Safety Issue

ATSB investigations and coronial investigations

Coronial investigations are separate to ATSB investigations. In this matter the respective authorities are largely in accord as to the factors that contributed to the development of the accident involving VH-POJ.

The ATSB's report can be downloaded by clicking on the link: 

Final Report (1.48 MB)

The Coroner's report can be obtained from the Coroner's Court of Victoria. Contact details are available at: www.coronerscourt.vic.gov.au/home. Queries regarding the Coroner's findings should be directed to the Coroner's Court of Victoria.

Occurrence summary

Investigation number AO-2011-100
Occurrence date 15/08/2011
Location 31 km north Horsham
State Victoria
Report release date 03/12/2013
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category VFR into IMC
Occurrence class Accident
Highest injury level Fatal

Aircraft details

Manufacturer Piper Aircraft Corp
Model PA-28
Registration VH-POJ
Serial number 28-2593
Sector Piston
Operation type Private
Damage Destroyed

Total power loss - Cessna 177, VH-DSA, South Grafton Airport, New South Wales, on 15 August 2011

Summary

Report release date: 12/12/2011

What happened

On 15 August 2011, a Cessna Aircraft 177 aircraft, registered VH-DSA, departed Ballina, New South Wales, for a private flight to South Grafton, New South Wales. The pilot was the sole occupant. When the aircraft was about 12 minutes from South Grafton and cruising at 2,500 ft above mean sea level (AMSL), the pilot observed traffic below him at 1,500 ft AMSL. The pilot elected to remain at his cruising altitude until closer to the South Grafton aerodrome. When about 5 NM from the aerodrome, he made a right turn into downwind while approaching the runway from the west. He then reduced engine power and quickly descended.

At 1,000 ft, the pilot stated that when he advanced the engine throttle, there was no response from the engine. He then completed the normal recovery procedures for an engine failure, including activation of carburettor heat. He advanced the throttle again but there was still no response from the engine. The aircraft descended at 500 ft/min with flaps extended, and the pilot attempted to reduce speed from 80 kts to 70 kts. At 300 ft with full flap extension and the stall warning sounding, he selected the master switch to OFF and prepared to land into wind. The aircraft landed about 70 m short of the runway threshold and continued along the ground for a short distance before impacting a shallow earth drain, seriously damaging the aircraft.

Occurrence summary

Investigation number AO-2011-098
Occurrence date 15/08/2011
Location South of Grafton
State New South Wales
Report release date 12/12/2011
Report status Final
Investigation level Short
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Engine failure or malfunction
Occurrence class Accident
Highest injury level None

Aircraft details

Manufacturer Cessna Aircraft Company
Model 177
Registration VH-DSA
Serial number 17700460
Sector Piston
Operation type Private
Departure point Ballina, New South Wales
Destination South Grafton Airport, New South Wales
Damage Substantial