Visual flight into instrument meteorological conditions – Dorrigo, New South Wales, on 9 December 2009, VH-MJO, Bell Helicopter 206L-1 LongRanger

Preliminary report

Preliminary report released 8 February 2010

On 9 December 2009, the pilot of a Bell Helicopter Co. 206L-1 LongRanger, registered VH-MJO, was conducting a visual flight rules (VFR) flight at Dorrigo NSW, with one passenger on board. Shortly after takeoff, he encountered reduced visibility conditions due to low cloud. Subsequently, all visual reference with the horizon and the ground was lost. The pilot attempted to conduct a landing but the helicopter impacted the ground with a significant vertical force. As a result, the pilot was seriously injured and the passenger was fatally injured. The helicopter was seriously damaged.

Summary

On 9 December 2009, at about 1120 Eastern Daylight-saving Time, the pilot of a Bell Helicopter Company 206L-1 LongRanger, registered VH-MJO, was conducting a visual flight rules fire-fighting support flight in the area of Dorrigo, New South Wales with one passenger on board. Shortly after takeoff, the pilot encountered reduced visibility conditions due to low cloud. Subsequently, all visual reference with the horizon and the ground was lost. The pilot attempted to land, but the helicopter impacted the ground in an uncontrolled state and with significant vertical force. The passenger was fatally injured, and the pilot was seriously injured. The helicopter was seriously damaged.

The investigation found that after the pilot established the hover, the helicopter entered the rapidly fluctuating cloud. The pilot lost visual reference and became spatially disoriented and the helicopter impacted the ground in an uncontrolled state. The at times rapidly-moving fog or low cloud in the vicinity of the helicopter landing area (HLA) increased the risk of visual operations encountering instrument meteorological conditions at the HLA.

Following the accident, a full review of the operational procedures affecting the operation was conducted jointly by the then Department of Environment, Climate Change and Water; the NSW Rural Fire Service; and other NSW fire‑fighting authorities. An action plan was implemented to make several safety enhancements to those operational procedures. In addition, the National Parks and Wildlife Service ceased operations at the Dorrigo helicopter landing site.

Occurrence summary

Investigation number AO-2009-077
Occurrence date 09/12/2009
Location Dorrigo
State New South Wales
Report release date 11/05/2011
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 Bell Helicopter Co
Model 206
Registration VH-MJO
Serial number 45745
Sector Helicopter
Operation type Aerial Work
Damage Substantial

In-flight cargo door separation - Eurocopter AS350D, VH-PIH, 28km north-west of Sunshine Coast Airport, Queensland, on 1 December 2009

Summary

On 1 December 2009 at approximately 0730 EST, the forward, left-side cargo door of a Eurocopter AS350D helicopter (registered VH-PIH) separated from the helicopter fuselage during fire-fighting operations near Maryborough, Queensland. The helicopter subsequently landed safely and there were no injuries.

It was probable that separation of the cargo door occurred as a consequence of replacement of the door seal during a recent overhaul. That replacement resulted in the door sitting proud of the mating surfaces when closed and latched. Elevated air loads acting on the door as a product of its overly proud position would subsequently have led to its fracture.

It was considered that the installation of improved door locks per Service Bulletin SB 52.00.25 and SB 52.00.26 would likely address this safety issue and significantly reduce the likelihood of a future AS350 cargo door separation event.

As a result of this occurrence the operator applied the cargo door lock modifications detailed in SB 52.00.25 and SB 52.00.26 to the new door installed on VH-PIH. In addition, the Australian Transport Safety Bureau has issued a Safety Advisory Notice to all operators of Eurocopter AS350 aircraft to consider the implications of the safety issue and take action where considered appropriate.

Occurrence summary

Investigation number AO-2009-073
Occurrence date 01/12/2009
Location 28km NW Sunshine Coast Airport
State Queensland
Report release date 11/04/2011
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Navigation - Other
Occurrence class Accident
Highest injury level None

Aircraft details

Manufacturer Aerospatiale Industries
Model AS350
Registration VH-PIH
Serial number 1341
Sector Helicopter
Operation type Aerial Work
Damage Minor

Fuel planning event, weather-related event and ditching involving Israel Aircraft Industries Westwind 1124A, VH‑NGA, 6.4 km west-south-west of Norfolk Island Airport, on 18 November 2009

Final report

What happened

On 18 November 2009, an Israel Aircraft Industries Westwind 1124A aircraft, registered VH-NGA, was operated on an air ambulance flight from Apia, Samoa to Norfolk Island, Australia. Two flight crew, a doctor, a flight nurse, a patient and a passenger (the patient’s husband) were on board.

On arrival at Norfolk Island at night, there was low cloud and the aircraft had insufficient fuel to divert to another airport. After four unsuccessful approaches, the flight crew ditched the aircraft 6.4 km west-south-west of the airport.

During the ditching, the aircraft encountered significant impact forces, and the flight nurse and first officer were seriously injured. The aircraft cabin rapidly flooded, and all six occupants evacuated from the aircraft, but with only three of the six life jackets on board and neither of the aircraft’s life rafts. The evacuees were rescued 85 minutes later by personnel on a search vessel launched from Norfolk Island.

What the ATSB found

The flight crew were conducting a long-distance flight to a remote island at night. At the time the flight was planned, the aerodrome forecast for Norfolk Island indicated the weather conditions at the time of arrival would be above the alternate minima.

Contrary to the consistent practice of the operator’s Westwind fleet for such flights, the flight departed with full main tanks (or about 7,200 lb of fuel) rather than full main tanks and tip tanks (about 8,700 lb). The reasons why the captain elected to depart without the maximum fuel load on this occasion were not fully determined. However, the ATSB found the captain’s pre-flight planning did not include many of the elements needed to reduce the risk of a long-distance flight to a remote island. These included miscalculating the total fuel required for normal operations, not calculating the additional fuel required for aircraft system failures, not obtaining relevant forecasts for upper-level winds, and not obtaining current information about potential alternate aerodromes. Although there was no requirement for the flight to depart with alternate or holding fuel, the fuel on board was insufficient to meet operator and regulatory requirements for the flight to allow for aircraft system failures.

Although the operator’s Westwind pilots generally used a conservative approach to fuel planning, the operator’s risk controls did not provide assurance there would be sufficient fuel on board flights to remote islands or isolated aerodromes. Limitations included no explicit fuel planning requirements for such flights, no formal training for planning such flights, no formal guidance information about hazards at commonly-used aerodromes, no procedure for a captain’s calculation of the total fuel required to be checked by another pilot, and little if any assessment during proficiency checks of a pilot’s ability to conduct fuel planning.

There were also limitations with Australian regulatory requirements. Other than requirements for fuel planning of passenger-carrying charter flights to remote islands, there were no explicit fuel planning requirements for other passenger-carrying flights to remote islands, and no explicit requirements for planning flights to isolated aerodromes. In addition, air ambulance flights were classified as ‘aerial work’ rather than ‘charter’. Consequently, they were subject to a lower level of requirements than other passenger-transport operations (including requirements for fuel planning).

During the flight, the weather conditions at Norfolk Island deteriorated below the landing minima. Air traffic services in Nadi and Auckland did not provide the flight crew with all the information that should have been provided. In addition, the flight crew did not request sufficient information prior to passing the point of no return (PNR), and the captain did not use an appropriate method for calculating the PNR. Related to these actions, the operator’s risk controls did not provide assurance that its pilots would conduct adequate in-flight fuel management activities during flights to remote islands or isolated aerodromes. The Civil Aviation Safety Authority (CASA) had also published limited guidance material regarding in-flight fuel management.

After the aircraft passed the PNR, there were opportunities to minimise the risk associated with the developing situation. However, the flight crew did not effectively discuss approach options, and they did not effectively review their fuel situation and consider alternate emergency options prior to ditching the aircraft. The flight crew did not refer to the ditching checklist and the final approach was conducted at an airspeed significantly below the reference landing speed (VREF), which increased the descent rate just prior to impact. A range of local conditions influenced the performance of the crew during the latter stages of the flight, including workload, stress, time pressure and dark night conditions.

In addition to the rapid flooding of the aircraft cabin, the occupants’ evacuation was hampered by there being no formal, specific procedures and limited training regarding on how to secure life rafts in an appropriate, readily accessible location prior to a ditching, and a designated storage location for the stretchered patient’s life jacket. In very difficult circumstances, the nurse and doctor did an excellent job evacuating the patient, and then assisting the injured first officer and the patient in the water, both of whom did not have life jackets.

Due to the inherent limitations of most emergency locator transmitters (ELTs) for a submerged aircraft, and the limited information provided by the flight crew regarding the location of the ditching, search and rescue personnel initially had no reliable information about where to search for the aircraft. It was fortunate that a firefighter made a chance sighting of the captain’s torch, resulting in the search effort being redirected to the appropriate area and the successful rescue of the evacuees.

In addition to issues associated with fuel planning and in-flight fuel management, the ATSB identified safety issues with the operator’s risk controls for emergency procedures and training, fatigue management, crew resource management training and flight crew training for newly-installed systems on the accident aircraft. The ATSB also identified limitations with the operator’s hazard identification processes and the definition of roles and responsibilities of key management personnel, and the processes used for the operator and air ambulance provider for conducting pre-flight risk assessments. Limitations were also identified with the processes used by CASA for planning surveillance, scoping audits and conducting audits.

What's been done as a result

Following the accident, CASA conducted a special audit of the operator, and this audit involved an extensive assessment of the operator’s air ambulance operations. The operator voluntarily ceased its Westwind operations and collaborated with CASA during the audit. During this process, the operator reviewed and substantially enhanced its risk controls and management oversight of flight/fuel planning and in-flight fuel management. It also enhanced its risk controls and management oversight of many other areas of its air ambulance operations.

In 2014, CASA modified the requirements for operations to Australian remote islands, so that all passenger-carrying transport flights, including air ambulance flights, were required to depart with alternate fuel. In addition, in 2012 CASA initiated action to change the regulatory classification of air ambulance (or medical transport) flights from aerial work to air transport. However, although CASA released a Notice of Proposed Rule Making about this issue in 2013, no changes have yet occurred. Accordingly, the ATSB issued a safety recommendation to CASA to continue reviewing the requirements for air ambulance operations and address the limitations associated with the current classification of these flights. The ATSB also issued two other recommendations to CASA for it to continue its activities to address the limitations with the requirements and guidance for fuel planning of flights to isolated aerodromes and the requirements and guidance of in-flight fuel planning.

In addition to these actions, since 2009 there have been improvements in a range of other areas. These include improvements to CASA’s surveillance processes, weather forecasting processes at Norfolk Island, and the publishing of advisory information about the hazards at remote island aerodromes. In addition, there now exists an enhanced capability for satellites to detect the location of ELT signals from aircraft involved in ditchings and similar impacts where the ELTs are unable to emit signals for extended periods.

Safety message

The investigation report contains 36 safety factors that provide lessons to flight crews, operators, regulators and/or other organisations. Overall, the most fundamental lesson for all flight crew, operators and regulators is to recognise that unforecast weather can occur at any aerodrome. Consequently, there is a need for robust and conservative fuel planning and in-flight fuel management procedures for passenger-transport flights to remote islands and isolated aerodromes.

Additional safety messages include:

  • Flight crew should discuss and consider options to manage threats when there is time available to do so.
  • Operators should ensure their flight crew proficiency checks assess the performance of all key tasks required of their flight crew.
  • Operators should not rely on informal risk controls for managing the performance of safety-critical tasks, particularly when there is significant turnover of pilots in a fleet.
  • Operators of air ambulance flights should ensure medical personnel have clearly defined procedures and appropriate practical training for using the emergency equipment on board to ensure they can effectively assist a patient in the event of an emergency.
  • All organisations in safety-critical industries should use proactive and predictive processes to identify hazards in their operations.
  • Organisations that use a bio-mathematical model of fatigue as part of their fatigue risk management system should ensure they have a detailed understanding of the assumptions and limitations associated with such models.
  • Regulators should develop effective methods for obtaining, storing and integrating information about operators and the nature of their operations so that they can develop effective surveillance plans.

Occurrence summary

Investigation number AO-2009-072
Occurrence date 18/11/2009
Location 6.4 km WSW of Norfolk Island Airport
State External Territory
Report release date 23/11/2017
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Low fuel
Occurrence class Accident
Highest injury level Serious

Aircraft details

Manufacturer Israel Aircraft Industries Ltd
Model Westwind 1124A
Registration VH-NGA
Serial number 387
Sector Jet
Operation type Medical Transport
Departure point Apia, Samoa
Destination Norfolk Island
Damage Destroyed

Cessna 210N, Lake Neale, Northern Territory

Summary

The pilot was conducting a night freight operation, carrying newspapers from Darwin to Alice Springs via Tindal and Tennant Creek. The flight from Darwin to Tindal was uneventful and the aircraft subsequently departed Tindal at 0219 am local time.

On departure, the pilot reported that he mistakenly established the aircraft on a track 30 degrees right of the correct track. After the pilot had levelled the aircraft at the intended cruising altitude, he fell asleep. As the flight progressed, the pilot occasionally woke up and made slight corrections to the heading, but he did not identify the 30 degree error. When the pilot realised that he should be on descent to Tennant Creek, he selected the appropriate frequencies, however the aircraft's navigation instruments did not provide any directional information. Believing that the aircraft was west of Tennant Creek, the pilot turned the aircraft and flew east, climbing to 14000 ft in an attempt to improve the range of the aircraft's navigation instruments. The instruments still did not show where Tennant Creek was, so the pilot decided to continue to Alice Springs at his flight planned altitude. At the time that the aircraft should have been approaching Alice Springs, the pilot selected the appropriate frequencies for the Alice Springs navigation aids. The aircraft's navigation instruments did not indicate the direction of Alice Springs, even though the pilot again climbed the aircraft to 14000 ft. The pilot reported that as the aircraft was now running low on fuel, the pilot decided to conduct a precautionary search and landing. The pilot advised Adelaide Flight Service on high frequency radio that he intended to land the aircraft on a dry salt lake.

The aircraft sustained minor damage during the landing however the pilot was not injured. He then activated the Emergency Locater Transmitter, and the aircraft was subsequently located 370 km WSW of Alice Springs. The company reported that its roster for night freight pilots has operated satisfactorily for around four years, with no reported serious fatigue problems. The pilots usually operate a one night shift every eight days, and the three days before the night shift are either days off or standby days. The pilot involved in this incident had done no flying on his rostered standby day, and therefore had had three full days off prior to signing on late in the evening of the day before the accident. He stated that he normally tried to sleep in on the morning before the night shift, and then get a couple of hours sleep in the afternoon. However, on the morning before he signed on for the night flight he was unable to sleep in and was then also unable to sleep in the afternoon. Consequently, by the time he signed on for the flight, the pilot had been awake for approximately 13.5 hours. The aircraft was not equipped with GPS. It is probable that the pilot's lack of sleep prior to signing on for the flight resulted in an increased level of fatigue. The increased fatigue may have contributed to the pilot selecting the incorrect heading on departure from Tindal and his subsequent lapses into sleep. Once the aircraft was out of range of the Tennant Creek and Alice Springs navigation aids and because of the lack of terrain features visible at night, there was no information available to the pilot to help him identify his position. The company is currently ensuring that flight crews have access to GPS equipment. The company is also drafting detailed standard operating procedures regarding sleep management, and these procedures will be included in the operations manual.

Occurrence summary

Investigation number 199901850
Occurrence date 20/04/1999
Location Lakr Neale
State Northern Territory
Report release date 01/05/2000
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Lost/unsure of position
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Cessna Aircraft Company
Model 210
Registration VH-NQP
Sector Piston
Operation type Charter
Departure point Tindal NT
Destination Tennant Creek NT
Damage Nil

Collision with terrain - VH-ZRR, 21 km south-east of Kojonup (ALA), Western Australia, on 17 November 2009

Preliminary report

Preliminary report released 25 January 2010

At about 0800 Western Standard Time on 17 November 2009, the pilot of a Cessna Aircraft Company A188B Agwagon was fatally injured when his aircraft impacted terrain while conducting spraying operations near Kojonup, WA. The aircraft was destroyed.

Summary

At about 0800 Western Standard Time on 17 November 2009, the pilot of a Cessna Aircraft Company A188B Agwagon, registered VH-ZRR was fatally injured when his aircraft impacted terrain during spraying operations near Kojonup, Western Australia. The aircraft sustained serious damage.

The investigation determined that the aircraft stalled at an altitude from which the pilot was unable to recover before the aircraft impacted terrain.

The investigation identified two safety issues in regards to the supervision of agricultural pilots. The first related to confusion within the aerial application industry concerning the required regulatory authorisation for a pilot that is the supervisor of a pilot holding an Agricultural Pilot (Aeroplane) Rating Grade 2 (Ag 2 pilot). In response to this issue, CASA provided an explanation of the relevant legislative material, which has been reproduced in this report, as well as an undertaking to provide education to industry on this matter. The second safety issue concerned the lack of guidance on the supervision of pilots with an Ag 2 rating. In response CASA has agreed to provide Advisory Circular guidance to industry on how to supervise Ag 2 pilots.

Occurrence summary

Investigation number AO-2009-070
Occurrence date 17/11/2009
Location 21 km SE of Kojonup ALA
State Western Australia
Report release date 26/11/2010
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 188
Registration VH-ZRR
Serial number 18802103T
Sector Piston
Operation type Aerial Work
Departure point Crossburn Farm Strip
Destination Crossburn Farm Strip
Damage Substantial

Boeing 737-8FE, VH-VON, Darwin Aerodrome NT, 9 November 2009

Summary

Section 21 (2) of the Transport Safety Investigation Act 2003 (TSI Act) empowers the ATSB to discontinue an investigation at any time. Section 21 (3) of the TSI Act requires the ATSB to publish a statement setting out the reasons for discontinuing an investigation.

The ATSB had commenced an investigation into the triggering of GPWS alerts in a Boeing Company 737 during its approach to land at Darwin Airport, NT on 9 November 2009. Information obtained from the aircraft operator and the aircraft manufacturer indicated that the alerts signalled a minor problem with flap settings that the crew rectified without difficulty. The ATSB has assessed that the occurrence was unlikely to have any significant implications for transport safety and has elected to discontinue the investigation.

The data collected in the course of the investigation may be used by the ATSB for future statistical analysis and safety research purposes.

 

Occurrence summary

Investigation number AO-2009-071
Occurrence date 09/11/2009
Location Darwin Aerodrome
State Northern Territory
Report release date 12/02/2010
Report status Discontinued
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Discontinued
Mode of transport Aviation
Aviation occurrence category E/GPWS warning
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer The Boeing Company
Model 737
Registration VH-VON
Serial number 33795
Operation type Air Transport High Capacity
Departure point Brisbane, Qld
Destination Darwin, NT
Damage Nil

Wirestrike - McDonnell Douglas 369D, VH-PLJ, 13 km north of Murray Bridge, South Australia, on 19 November 2008

Preliminary report

Preliminary report released 5 January 2009

At about 1115 Central Daylight-saving Time on 19 November 2008, a pilot and two linesmen were operating a McDonnell Douglas 369D helicopter, registered VH-PLJ, to test a high-voltage powerline between Mannum and Mobilong, SA. While manoeuvring to test a conductor joint, the helicopter's main rotors struck a conductor and impacted the ground. One linesman was fatally injured and the other sustained minor injuries, while the pilot sustained serious injuries.

Summary

On the morning of 19 November 2008, the pilot of a McDonnell Douglas 369D helicopter, registered VH-PLJ, and two lineworkers were conducting airborne joint-testing operations on an electricity transmission line between Mannum and Mobilong, South Australia. Joint testing involves closely approaching the transmission line to check joints in transmission wires. At about 1150 Central Daylight-saving Time, when about 13 km north of Murray Bridge, the helicopter's main rotor blades contacted a transmission line conductor. The pilot lost control and the helicopter impacted the ground. One lineworker was fatally injured, the other lineworker received minor injuries and the pilot received serious injuries. The helicopter was seriously damaged.

The investigation found that the crew was not aware before the flight that there were transpositions (changes in the relative positions of individual wires) in the line and that they did not detect such a transposition during the approach for the joint test that led to the accident.

Following the occurrence, the helicopter operator amended the guidance for conducting joint-testing and expanded training and supervision of new crews. The powerline owner reviewed the risk profile of its airborne operations and revised a number of hazard treatment options. The powerline maintenance provider made a number of operational changes and contracted an external auditor to examine its operation. All of the recommendations from that audit were adopted by the maintenance provider.

In response to the failure of the recording lineworker's shoulder harness, the shoulder harness repair facility has upgraded relevant repair equipment and provided a replacement program for any incorrectly stitched harness in the operator's helicopter fleet. In addition, the Civil Aviation Safety Authority took action to have a number of seat belt harnesses recalled and examined. No issues were found with any of the seat belts that were examined, and they were able to be re-released without further rework.

Occurrence summary

Investigation number AO-2008-078
Occurrence date 19/11/2008
Location 13 km north of Murray Bridge
State South Australia
Report release date 09/12/2010
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Wirestrike
Occurrence class Accident
Highest injury level Fatal

Aircraft details

Manufacturer McDonnell Douglas Corp.
Model 369
Registration VH-PLJ
Serial number 1280445D
Sector Helicopter
Operation type Aerial Work
Damage Substantial

Reported signal irregularity at Cootamundra, New South Wales, involving trains ST22 and 4MB7

Preliminary report

Preliminary report released 4 December 2009

The information contained in this Preliminary report is released in accordance with section 25 of the Transport Safety Investigation Act 2003 and is derived from the ongoing 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 accident as outlined in this Preliminary report. As such, no analysis or findings are included in this report.

Abstract

At about 0217 on Thursday 12 November 2009, train ST22, an XPT passenger service, was being pathed into the 'Platform Road' at Cootamundra, NSW. The driver of the XPT received a 'PROCEED' indication on signal CA74, signifying that the line into the Platform Road was clear. Shortly after passing over 136B points set reverse, the driver of the XPT observed the last wagon  of freight train 4MB7 to be obstructing the path of his train. He made an emergency brake application and stopped his train just short of train 4MB7.

The driver of the XPT immediately contacted the ARTC Network Controller and advised of the problem. Shortly thereafter, the freight train was moved forward to clear a path for the XPT into the Platform Road.

Preliminary investigation of the event has determined that a signalling design irregularity affecting the 'Up Main Line' at Cootamundra allowed signal CA74 to be cleared for the passage of the XPT even though the route was obstructed by the last wagon of train 4MB7.

Final report

Executive summary

At about 0217 on Thursday 12 November 2009, train ST22, an XPT passenger service, was being routed into No.1 Platform Road at Cootamundra, New South Wales. The driver of the XPT received a Medium Turnout indication on signal CA74 signifying that the route into No.1 Platform Road was set and unobstructed. Shortly after passing over the Gundagai Road level crossing and traversing 136 points set into No.1 Platform Road, the driver of the XPT observed the last wagon of freight train 4MB7, located on the Up Main line, was obstructing the path of his train. He applied the train brakes and stopped just short of train 4MB7.

The driver of the XPT immediately contacted the network controller and advised him of the problem. Shortly thereafter the freight train was moved forward, at the request of the network controller, to clear a path for the XPT into No.1 Platform Road.

The investigation determined that a signalling system design error allowed signal CA74 to be cleared for the passage of the XPT even though the route into No.1 Platform Road was obstructed by the last vehicle of freight train 4MB7 which was stationary on the adjacent Up Main line.

The Australian Transport Safety Bureau has determined that actions taken by the Australian Rail Track Corporation (ARTC) should mitigate the risk of a similar occurrence but has identified further issues relating to signal design, installation and commissioning where further action may enhance the strategies already put in place by the ARTC.

Occurrence summary

Investigation number RO-2009-009
Occurrence date 12/11/2009
Location Cootamundra
State New South Wales
Report release date 20/01/2011
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Rail
Rail occurrence category Signal Irregularity
Occurrence class Incident
Highest injury level None

Train details

Train number Train ST22
Type of operation Passenger Train
Departure point Melbourne, Vic
Destination Sydney, NSW
Train damage Nil

Train details

Train number 4MB7
Type of operation Freight train
Departure point Melbourne, Vic
Destination Brisbane, Qld
Train damage Nil

In-flight engine malfunction and air turn-back - Boeing 737-476, VH-TJY, 120 km south-west of Brisbane Airport, Queensland, on 10 November 2009

Summary

On 10 November 2009 at around 1900 EST, a Boeing Company 737-467 aircraft, registered VH-TJY, departed Brisbane Airport, Queensland for Melbourne, Victoria. As the aircraft was climbing through 24,000 ft, the flight crew observed abnormal indications associated with the right engine. The aircraft was returned to Brisbane where it landed without further incident.

Engine disassembly and inspection revealed significant damage to the stage-1 low-pressure turbine (LPT). Analysis of the stage-1 LPT blades showed that some blades had sustained levels of thermally-induced microstructural degradation, which may have affected the creep resistance of the alloy and resulted in the blades being susceptible to failure by creep rupture.

Creep rupture was identified as the likely failure mechanism in previous stage-1 LPT blade failures in this engine type investigated by the Australian Transport Safety Bureau and the engine manufacturer. As a result of this occurrence and at the time of writing this report, the engine manufacturer is revising service bulletin SB 72-1113 to expand the range of blade manufacturing batch numbers that had previously been identified as being predisposed to creep-related failure. Blades in the identified batches are to be withdrawn from service as soon as they are next removed from the engine.

Occurrence summary

Investigation number AO-2009-069
Occurrence date 10/11/2009
Location 120 km SW of Brisbane Airport
State Queensland
Report release date 20/07/2011
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Abnormal engine indications
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer The Boeing Company
Model 737
Registration VH-TJY
Serial number 28151
Aircraft operator Qantas
Sector Jet
Operation type Air Transport High Capacity
Departure point Brisbane, Qld
Destination Melbourne, Vic.
Damage Minor

Technical assistance to RA-Aus regarding the accident involving a 'Boorabee' ultralight aircraft, registered 19-1418, on 12 October 2009

Summary

On 12 October 2009, a 'Boorabee' ultralight aircraft, registered 19-1418, being operated on a private flight from Renmark, Vic. to Casino, NSW, impacted the ground approximately 37 km west-south-west of Hay, NSW. The pilot, who was the sole occupant of the aircraft, was fatally injured. In assisting the NSW Police in their investigation of this accident, Recreational Aviation Australia Inc (RA-Aus) requested assistance from the Australian Transport Safety Bureau (ATSB) in the recovery of information from a portable Global Positioning System (GPS) unit recovered from the accident site.

To protect the information supplied by RA-Aus to the ATSB and investigative work undertaken to assist RA-Aus, the ATSB initiated an investigation under the Transport Safety Investigation Act 2003 (TSI Act). The ATSB completed its recovery of data from the Garmin® GPS72 portable GPS receiver (serial No: 82377157) and provided the data to RA-Aus in the interests of transport safety, under the provisions of section 61 of the TSI Act.

Contact details for RA-Aus are at Website: www.raa.asn.au

 

______________

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

 

Occurrence summary

Investigation number AE-2009-067
Occurrence date 12/10/2009
Location 37 Km WSW of Hay, NSW
State New South Wales
Report release date 15/12/2009
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 TL Ultralight
Model Boorabee
Registration 19-1418
Serial number -
Operation type Sports Aviation
Departure point Renmark, Vic
Destination Casino, NSW