Runway excursion - VH-­SBA, Mount Gambier Aerodrome South Australia, on 6 May 2010

Summary

On 9 May 2010 at about 0815 Central Standard Time, a Saab 340B aircraft, registered VH-SBA, landed at Mount Gambier aerodrome, South Australia (SA). The crew reported that following a routine approach and touchdown, light braking was applied. At a speed of between 40 and 50 kts, braking pressure was increased because of the speed of the aircraft in relation to its position on the runway.

When braking pressure was increased, the aircraft pulled to the left. The aircraft continued to veer left, until it came to a stop with the nose and left main wheels bogged, off the left side of the runway, at an estimated angle of 50 degrees off runway heading.

The operator's maintenance personnel determined that the left-seat pilot's right brake pedal was producing less braking force than the left pedal. Following extensive fault finding, the associated brake control cable conduit was inspected with a boroscope. A gouge was found on inside radius. The cable was replaced and the aircraft returned to service.

Occurrence summary

Investigation number AO-2010-028
Occurrence date 06/05/2010
Location Mount Gambier Aerodrome
State South Australia
Report release date 14/10/2010
Report status Final
Investigation level Short
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Runway excursion
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Saab Aircraft Co.
Model 340
Registration VH-SBA
Serial number 340B-311
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Adelaide SA
Destination Mount Gambier SA
Damage Unknown

Operational non-compliances - Airbus A330, 9M-XXB, Gold Coast Airport, Queensland, on 4 and 29 May 2010

Summary

On 4 and 29 May 2010, an Airbus A330-343E aircraft, registered 9M-XXB, was being operated by AirAsia X on scheduled passenger services from Kuala Lumpur, Malaysia to the Gold Coast, Queensland. On both occasions, there was low cloud and reduced visibility on arrival at the Gold Coast. 

During non-precision instrument approaches conducted at Gold Coast Airport on both days, the flight crews descended the aircraft below the segment minimum safe altitudes. As a result, the aircraft descended to an altitude where there was no longer separation assurance from terrain and aircraft operating outside controlled airspace.

While those operational non-compliances occurred prior to the final approach fix for the instrument approaches and not below 1,200 ft above aerodrome height, they were indicators of a minor safety issue regarding the operator's training of its flight crews.

In response to this incident, the aircraft operator made a number of changes to flight crew procedures when conducting instrument approaches. The operator also modified the recurrent simulator training program to include more complex non‑precision instrument approaches.

Occurrence summary

Investigation number AO-2010-027
Occurrence date 04/05/2010
Location Gold Coast Airport
State Queensland
Report release date 10/02/2012
Report status Final
Investigation level Systemic
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 Airbus
Model A330
Registration 9M-XXB
Serial number 974
Aircraft operator AirAsia X
Sector Jet
Operation type Air Transport High Capacity
Departure point Kuala Lumpur, Malaysia
Destination Gold Coast, Qld
Damage Nil

Collision between XPT passenger train WT27 and a track-mounted excavator, near Newbridge, New South Wales, on 5 May 2010

Preliminary report

Preliminary report released 25 September 2014

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 1113 on 5 May 2010, XPT passenger train WT27, travelling from Sydney to Orange, New South Wales collided with a track-mounted excavator on the main line between Bathurst and Newbridge. The XPT was travelling at about 69 km/h at the time of the collision.
The excavator and a utility vehicle were severely damaged; the leading power car of the train received moderate damage.

The operator of the track-mounted excavator was fatally injured, and one train passenger incurred minor injuries.

Final report

Safety summary

What happened

At about 1116 on 5 May 2010 a collision occurred between an XPT passenger train and a track-mounted excavator near Newbridge, New South Wales. The operator of the track-mounted excavator was fatally injured. During the course of the investigation a similar incident occurred near Wards River, New South Wales (17 March 2011), where two work groups had to hurriedly vacate their on-track worksite due to an approaching train (there were no injuries). Both incidents occurred despite the fact that the work groups had been authorised, under a Track Occupancy Authority (TOA), to occupy and work on the track.

What the ATSB found

The ATSB established that, for the accident at Newbridge, a TOA was an appropriate method of authorising the work to be performed. However, a combination of individual actions and systemic issues contributed to the collision. When requesting the TOA, neither the Protection Officer (PO) nor the Network Control Officer (NCO) positively identified the location and type of worksite. Their actions were influenced by a deficiency in the TOA form, in that no provision was provided to record this critical information. Consequently, both the PO and NCO incorrectly concluded that the train had already passed beyond the limits of the worksite. In addition, the workers accessed the danger zone before additional site protection measures (detonators and flags) had been put in place. The ATSB also found that the workers were relatively inexperienced and that their training had not specifically discussed the hazards and protections that were relevant when working under a TOA.

The scenario for the Wards River incident was similar in that the track access point for the work was about 16 km into the section defined by the limits of the proposed TOA. In this case, the location of the work (Wards River) was communicated at about 0735 when the TOA was first requested. Due to operational reasons the TOA was not issued until 0840. Similar to the Newbridge event the PO did not clearly identify the location of the worksite and the NCO did not ensure the train had passed beyond the worksite or track access point.

What has been done as a result

As a result of the incident at Newbridge on 5 May 2010, the Australian Rail Track Corporation (ARTC) took action to reinforce the rules and procedures associated with the issuing of TOAs. The ARTC also implemented the use of a revised TOA form that provides for the recording of critical information regarding the location and type of worksite. It is likely that implementation of the new form should reduce the risk of similar incidents.

Safety message

It is essential that information critical to the safe implementation of a TOA be clearly communicated between the Protection Officer and the Network Control Officer.

It is also essential that workers do not access the track until all levels of worksite protection have been fully implemented.

Inquest

Fatal rail accident

On 8 June 2012 a New South Wales Coroner released findings into a 2010 fatal rail accident near Newbridge, NSW. The findings highlight safety concerns that require review by the rail industry in relation to the safety issues raised by the ATSB in its report released on 20 April 2012. During the course of its investigation, where safety issues were identified, these were communicated to interested parties for safety action.

Those issues cover:

  • Deficient TOA form
  • Minimum training levels
  • Inconsistent TOA procedure
  • Use of non-authorised forms
  • Elevated risk due to fatigue

Circumstances of the accident

At about 11116 on 5 May 2010 collision occurred between a scheduled XPT passenger train and a track-mounted excavator near Newbridge, New South Wales. The operator of the excavator was fatally injured. The ATSB Investigation established that collision had occurred even though the work group using the excavator was authorised to be on the track under a Track Occupancy Authority (TOA) and that work had commenced prior to site protection measures being put in place. The ATSB also found that the members of work group were relatively inexperienced and that their training had not specifically discussed the relevant hazards and protections when working under a TOA.

Safety issues

The ATSB found the following safety issues as part of the investigation. The Coroner's findings were broadly consistent with the ATSB's findings:

1. Deficient TOA

During the Investigation the ATSB found that the TOA form in use at the time of the accident was deficient as there was no provision to record critical information regarding the location and type of worksite.

Consequently, the Protection Officer and Network Control Officer incorrectly conclude that the train had passed beyond the limits of the worksite. The Coroner found that 'the TOA form was deficient and that there was a miscommunication between the Protection Officer and the Network Control Officer. The Coroner also found that there was a weak management system within the Network Control Centre.

Prior to the release of the ATSB report the Australian Rail Track Corporation (ARTC) made changes to their rules and procedures which included changes to the TOA to ensure there was provision to record critical information. The ATSB assessed this action as adequately addressing the safety issue.

2. Minimum training levels

During the Investigation the ATSB found that the track workers were not provided with sufficient competency based or structured on the job training in relation the hazards and required protections for working under the TOA at Newbridge.

Prior to the release of the ATSB report the ARTC advised that it had reinforced with Protection Officers its requirements for Work Method Statement TRA-001 (Access to and working on or about track). The ARTC's internal audit program had also been redirected to safeworking with a focus on reviewing safeworking documentation for compliance with ARTC Network Rules and Procedures. The ATSB was satisfied that the ARTC had initiated action to address this safety issue.

The Coroner found that the supervision and training of the track workers was inadequate, and that some work practices had become sloppy and which were not being sufficiently overseen. The Coroner also found that ARTC rules and protocols were not adhered to by the track working crew. In particular two of the work crew commenced work without being instructed to do so and without regulation protection devices being placed.

3. Inconsistent TOA procedure

During the Investigation the ATSB found that ARTC procedure ANPR-701 (Using a Track Occupancy Authority) was inconsistent in that it did not allow for a scenario that would otherwise be permitted, and intended, under rule ANWT-304 (Track Occupancy Authority).

Prior to the release of the ATSB report the ARTC advised that it had trained its employees in this particular scenario and will review the procedure to ensure that it is consistent with the training and the TOA. The ATSB was satisfied that the ARTC had initiated action to address this safety issue.

4. Use of non-authorised forms

During the Investigation the ATSB found that some ARTC maintenance contractors were using non-authorised reproductions of the ARTC's TOA form.

Prior to the release of the ATSB report the ARTC conducted extensive briefings with all employees and contractors to explain changes to the ARTC TOA that took effect in November 2011. The ARTC made clear that only the new form was to be used and provided books of forms to employees and contractors. The ATSB was satisfied that the action taken would adequately address this safety issue.

5. Elevated risk due to fatigue

During the Investigation the ATSB found that it was possible that at times throughout the Network Control Officer's roster, fatigue levels were conducive to performance degradation.

Prior to the release of the ATSB report the ARTC advised that it is applying continuous improvement processes to fatigue as it does with all safety related matters. Recent activities that ARTC completed in relation to fatigue management included:

  • Revising ARTC's fatigue policy and procedure to include more detailed hours of work guidelines, and information to support managers manage potential fatigue related matters,
  • Scheduling managers to attend a supervisors fatigue management training course. This course trains managers in identifying and controlling possible fatigue related risks. This training supplements existing fatigue management training for all employees, and
  • Rolling out an awareness campaign that has included sending a letter and pamphlet about rest and sleep directly to employee's homes, posters for display at all worksites, and a new safety.

The ATSB noted that ARTC mangers develop rosters in accordance with the ARTC policies and procedures. Considering the ARTC's advice that the fatigue policy and procedure is to be reviewed along with additional training and awareness programs, the ATSB was satisfied that the Australian Rail Track Corporation has initiated action to address this safety issue.

The Coroner concluded that there was insufficient evidence that the miscommunication in relation to the TOA (see Safety Issue 1 above) was the result of fatigue or other work conditions.

The ATSB emphasises that it is essential that information critical to the safe implementation of a TOA be clearly communicated between the PO and the NCO. The ATSB also emphasises that it is also essential that workers do not access the track until all levels or worksite protection have been fully implemented.

ATSB investigations and coronial inquiries

Inquests are separate to ATSB investigations. There are differences in the ATSB's and the Coroner's conclusions with respect to this accident. However, as outlined above The Coroner's findings were broadly consistent with those of the ATSB.

The ATSB's report can be downloaded by clicking on the PDF link to the top right of this page. Feedback can be provided via the link provided.

The Coroner's report can be obtained from the Coroner's Court of New South Wales, contact details are available via the Coroner's Court of NSW website.

Occurrence summary

Investigation number RO-2010-004
Occurrence date 05/05/2010
Location Newbridge
State New South Wales
Report release date 20/04/2012
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Rail
Rail occurrence category Collision
Occurrence class Accident
Highest injury level Fatal

Train details

Train number Train WT27
Type of operation Passenger
Departure point Sydney
Destination Orange

Wirestrike - VH-JHR, Cessna 188 Agwagon, near Ayr, Qld, 10 April 2010

Discontinued report

 

Section 21 (2) of the Transport Safety Investigation Act 2003 (TSI Act) empowers the Australian Transport Safety Bureau (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.

On 10 April 2010, the ATSB commenced an investigation into a wirestrike that occurred at about 1737 Eastern Standard Time that day and involved a Cessna Aircraft Co. A188B/A1 Ag Truck aircraft, registered VH-JHR. The aircraft was being operated on an agricultural weed-spraying flight over a cane field that was located about 13km south-west of Ayr, Queensland. The aircraft was positioned to fly under powerlines that crossed the intended flight path at about 3.25 m above the top of the crop. The aircraft, which is about 3.6 m high, contacted the powerlines and severed the top of the aircraft's fin and rudder horn (Figure 1). Control of the aircraft was lost and it collided with terrain shortly afterwards in a steep, nose-down attitude. The pilot was fatally injured.

Figure 1: Power conductors and detached rudder horn

VH-JHR picture of tail

In the hours prior to the flight, witness, video and other information indicated that the pilot had consumed a quantity of alcohol. A postmortem examination subsequently indicated that the pilot had a high blood alcohol concentration.

The consumption of alcohol by pilots is regulated by Civil Aviation Regulation 256, which mandates that a person shall not:

  • while in a state of intoxication, enter any aircraft
  • act as, or perform any functions in preparation to act as a member of the operating crew of an aircraft within 8 hours of consuming alcohol
  • operate an aircraft if, by reason of having consumed alcohol (or other prescribed substances), that person's ability to operate the aircraft is impaired.

 

The ATSB safety research report titled Alcohol and Human Performance from an Aviation Perspective: A review' found that alcohol use by pilots was a major potential risk to flight safety. Of particular relevance, alcohol:

  • affects almost all forms of cognitive function, such as information processing, attention, vigilance, perception and reasoning
  • impairs registration, recall and the organisation of information, which leads to increased reaction times and increased errors
  • significantly impairs attention, especially in terms of tasks requiring sustained, selective or divided attention
  • adversely affects psychomotor performance, particularly on tracking tasks. Performance was found to suffer most when an unexpected or unanticipated event occurred.

The ATSB's primary focus is on enhancing safety with respect to fare-paying passengers and, in particular, those transport safety matters that may present a significant threat to public safety and are the subject of widespread public interest. The ATSB therefore needs to direct significant attention to identifying systemic failures in aviation, marine and rail mass public transport systems.

Many accidents involve the repetition of past occurrences, where the contributing factors are similar and the safety issues are well known. The ATSB has investigated a number of accidents in which the operating crew were affected by alcohol and the cognitive impairment likely as a result of alcohol consumption, and its effects on tasks such as flying and driving, are well known. Given that existing knowledge, and the pilot's decision to carry out the flight after consuming alcohol, the ATSB considered there was limited potential to enhance transport safety by continuing this investigation.

On that basis, the ATSB has elected to discontinue the investigation. However, 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-2010-026
Occurrence date 10/04/2010
Location near Ayr
State Queensland
Report release date 16/07/2010
Report status Discontinued
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Discontinued
Mode of transport Aviation
Aviation occurrence category Wirestrike
Occurrence class Accident
Highest injury level Fatal

Aircraft details

Manufacturer Cessna Aircraft Company
Model 188
Registration VH-JHR
Serial number 188-02366T
Operation type Aerial Work
Departure point Home Hill aerodrome
Destination Home Hill aerodrome

Independent investigation into the grounding of the Chinese registered bulk carrier Shen Neng 1, at Douglas Shoal, Queensland, on 3 April 2010

Preliminary report

Preliminary report released 15 April 2010

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.

Abstract

At 1705 on 3 April 2010, Shen Neng 1 grounded at Douglas Shoal, about 50 miles north of the entrance to the port of Gladstone, Queensland.

The ship had departed Gladstone at 1054 that day after loading a full cargo of coal destined for Bayuquan, China. The ship's hull was seriously damaged by the grounding and a number of water ballast tanks and at least one fuel oil tank were breached resulting in pollution. Sea water also entered the engine room. Salvors boarded the ship on 4 April. The ship was refloated on 12 April and towed to a location off Great Keppel Island.

Final report

Executive summary

At 1705 on 3 April 2010, the Chinese registered bulk carrier Shen Neng 1 grounded on Douglas Shoal, about 50 miles north of the entrance to the port of Gladstone, Queensland. The ship's hull was seriously damaged by the grounding, with the engine room and six water ballast and fuel oil tanks being breached, resulting in a small amount of pollution.

The ATSB investigation found that the grounding occurred because the chief mate did not alter the ship's course at the designated course alteration position. His monitoring of the ship's position was ineffective and his actions were affected by fatigue.

The ATSB identified four safety issues during the investigation: there was no effective fatigue management system in place to ensure that the bridge watchkeepers were fit to stand a navigational watch after they had supervised the loading of a cargo of coal in Gladstone; there was insufficient guidance in relation to the proper use of passage plans, including electronic route plans, in the ship's safety management system; there were no visual cues to warn either the chief mate or the seaman on lookout duty, as to the underwater dangers directly ahead of the ship; and, at the time of the grounding, the protections afforded by the requirement for compulsory pilotage and active monitoring of ships by REEFVTS, were not in place in the sea area off Gladstone.

The ATSB has issued two safety recommendations to Shen Neng 1's management company regarding the safety issues associated with fatigue management and passage planning and acknowledges the safety action taken by the Australian Maritime Safety Authority in relation to the extension of REEFVTS coverage to include the waters off Gladstone.

Occurrence summary

Investigation number 274-MO-2010-003
Occurrence date 03/04/2010
Location Douglas Shoal
State Queensland
Report release date 14/04/2011
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Marine
Marine occurrence category Foundered
Occurrence class Serious Incident
Highest injury level None

Ship details

Name Shen Neng 1
IMO number 9040871
Ship type Bulk Carrier
Flag China
Departure point Gladstone, Qld
Destination Bayuquan, China

Loss of control - Piper PA-30-160B Twin Comanche, VH-KDS, 43 km east of Perth Airport, Western Australia, on 28 March 2010

Preliminary report

Preliminary report released 20 May 2010

On 28 March 2010, a Piper Aircraft Corp PA-30 Twin Comanche, registered VH-KDS, departed from Jandakot Aerodrome, Western Australia for a private flight under the visual flight rules. On board were two qualified pilots, both of whom were endorsed on the aircraft type. Following the failure of the aircraft to return to Jandakot later that day, a search was initiated to locate the aircraft and occupants. The following morning, the seriously-damaged aircraft was located and both occupants were found to have received fatal injuries.

Examination of onboard GPS information indicated that, while tracking towards Jandakot Aerodrome, the aircraft commenced a steep descent from about 3,500 ft above mean sea level that continued to ground level.

Summary

At 0826 Western Standard Time on 28 March 2010, a Piper Aircraft Corp. PA‑30 Twin Comanche aircraft, registered VH‑KDS, departed Jandakot Airport, Western Australia for a private flight under the visual flight rules (VFR). On board were two qualified pilots, both of whom were endorsed on the aircraft type. No details of the flight were submitted to Air Traffic Services nor left with any other person. At 1815, following the failure of the aircraft to return to Jandakot, the Australian Rescue Coordination Centre was notified, and a search was initiated to locate the aircraft.

Following examination of radar data, the aircraft was located the following morning by the crew of a search and rescue (SAR) helicopter. Upon landing, the helicopter crew established that the two occupants had sustained fatal injuries.

Analysis of data recorded by onboard Global Positioning System equipment identified that while maintaining about 3,500 ft above mean sea level, the speed of the aircraft steadily decreased followed by a steep descent that continued to ground level.

Examination of the aircraft identified that the propeller of the left engine was feathered prior to impact; however, no evidence of a defect or other circumstance that would have necessitated feathering of the propeller was identified.

The investigation identified that the circumstances of the accident were consistent with a loss of control due to sufficient airspeed not being maintained. In addition, the investigation found that the lack of flight details available for the search and rescue authorities and the non-activation of the portable emergency locator transmitter hampered the SAR response.

Occurrence summary

Investigation number AO-2010-023
Occurrence date 28/03/2010
Location 43 km east of Perth Airport
State Western Australia
Report release date 02/06/2011
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 Piper Aircraft Corp
Model PA-30
Registration VH-KDS
Serial number 30-952
Sector Piston
Operation type Private
Departure point Jandakot, WA
Destination Jandakot, WA
Damage Substantial

Total power loss - Victa Airtourer, VH-MTC, Hobart, Tasmania, on 4 April 2010

Summary

On 4 April 2010, the pilot of a Victa Airtourer 115 aircraft, registered VH-MTC was conducting a private visual rules return flight from Cambridge Aerodrome, Tasmania. The flight consisted of some aerobatics, followed by some sight-seeing over Hobart.

At about 1020, after the pilot commenced the return to Cambridge, the engine suddenly lost all power. The pilot conducted a forced landing onto a nearby road, seriously damaging the aircraft. The pilot, who was the sole occupant, was uninjured.

The investigation found that the power loss was due to exhaustion of the aircraft's fuel supply.

A number of safety issues were identified concerning the measurement of the quantity of fuel on board, and consumed before and during the flight. Those issues contributed to the pilot's belief that there was more fuel on board the aircraft than was actually the case.

As a result of this accident the aircraft's type certificate holder, aircraft owner's association and the aircraft's operator have undertaken a number of safety actions. Those actions include a number of pilot education initiatives and the amendment of the operator's maintenance processes to ensure compliance with all airworthiness directives.

In addition, the aircraft's type certificate holder is undertaking a number of enhancements in response to an unrelated Civil Aviation Safety Authority-initiated review of aspects of the aircraft's fuel system and concerns about the aircraft's original fuel system certification process.

Occurrence summary

Investigation number AO-2010-025
Occurrence date 04/04/2010
Location Cambridge
State Tasmania
Report release date 14/12/2010
Report status Final
Investigation level Systemic
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 Victa Ltd
Model 115
Registration VH-MTC
Serial number 112
Sector Piston
Operation type Private
Departure point Cambridge, Tas.
Destination Cambridge, Tas.
Damage Substantial

Independent investigation into the stevedore fatality on board the Antigua and Barbuda registered container ship Vega Gotland, at Port Botany, New South Wales, on 28 March 2010

Final report

Executive summary

At about 1918 on 28 March 2010, a stevedore was crushed between two containers during loading operations on board the container ship Vega Gotland, while it was berthed at the Patrick Terminals' Port Botany terminal. The stevedore, who was the lashing team leader, died instantly from the injuries he received in the accident.

The ATSB investigation found that the lashing team leader had placed himself in a position of danger and that when a twist lock foundation unexpectedly failed during the repositioning of the container, he was unable to get clear of the swinging container.

The investigation also found that the failure of the twist lock foundation was brought about by an attempt to reposition the container and was consistent with its exposure to gross overstress conditions as a result of the leverage forces applied to it by the container and the unsecured hatch cover.

The investigation identified that while the dangers of working between a moving container and a fixed object were taught to Patrick Terminals' new employees during their induction training, the issue was not specifically covered or reinforced in the company's safe work instructions, the hazard identification and associated risk control processes nor, in some instances, followed in practice by stevedores on board the ships in the terminal.

The ATSB identified seven safety issues during the investigation. The safety issues related to: the absence of policies or procedures concerning safety zones near container operations; that Patrick Terminals' safety management system contained deficiencies; the discontinuity between what was taught to new employees and the contents of the safe work instructions and hence the practices on the work site; hazard identification and associated risk controls for lashing and unlashing; review and compliance auditing of safe work instructions and reporting risk-related events; and that the recognised safe practices of not working under or near a container being loaded were not well reflected in national and international guidance.

The ATSB acknowledges the safety action taken by Patrick Terminals and is satisfied that it adequately addresses the safety issues. The ATSB has issued one safety advisory notice concerning national and international guidance not reflecting the recognised safe practices of not working under or near a container being loaded onto a ship.

Occurrence summary

Investigation number 273-MO-2010-002
Occurrence date 28/03/2010
Location Port Botany
State New South Wales
Report release date 19/12/2011
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Marine
Marine occurrence category Fatality
Occurrence class Accident
Highest injury level Fatal

Ship details

Name Vega Gotland
IMO number 9336347
Ship type Container ship
Flag Antigua and Barbuda
Departure point At berth

Aircraft proximity event - VH-WZJ and VH-WRR, 37 km north-east of Horn Island Aerodrome, Queensland, on 24 March 2010

Summary

On 24 March 2010, at about 1235 Eastern Standard Time, a Cessna Aircraft Company 208B (Caravan), registered VH-WZJ, was descending through cloud inbound to Horn Island aerodrome, Queensland (Qld), when the pilot received an aural traffic warning on the Caravan's traffic advisory system. The system indicated that an aircraft was 200 ft below and 3 NM (5.6 km) ahead of the Caravan. Communications were established with the pilot of a Pilatus Britten-Norman BN2A-26 (Islander), registered VH-WRR, who was transiting the area, and was confirmed as the conflicting aircraft.

In response, the pilot of the Caravan reported commencing a climb, and at this point observed the Islander pass to the right of the aircraft. The pilot of the Islander also reported sighting the Caravan pass above and to the right of his aircraft. It was estimated that the distance between the two aircraft was about 50 m. As a result of this incident, the following safety actions are being considered:

  • The operator of the Islander is considering changing its procedures so that all flights conducted within the Torres Strait, in marginal weather conditions, are carried out under instrument flight rules (IFR).
  • The Civil Aviation Safety Authority (CASA) is reviewing the two discrete frequencies currently assigned to the Horn Island and Northern Peninsula aerodrome Common Traffic Advisory Frequencies (Radio) ((CTAF(R)).

Occurrence summary

Investigation number AO-2010-022
Occurrence date 24/03/2010
Location 37 km NE of Horn Island aerodrome
State Queensland
Report release date 29/06/2010
Report status Final
Investigation level Short
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Near collision
Occurrence class Serious Incident
Highest injury level None

Aircraft details

Manufacturer Cessna Aircraft Company
Model 208
Registration VH-WZJ
Serial number 208B1108
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Warraber Island, Qld
Destination Horn Island, Qld
Damage Nil

Aircraft details

Manufacturer Pilatus Britten-Norman Ltd
Model BN2
Registration VH-WRR
Serial number 882
Sector Piston
Operation type Charter
Departure point Northern Penninsula aerodrome, Qld
Destination Saibai Island, Qld
Damage Nil

Loss of control - Embraer S.A. EMB-120ER Brasilia, VH-ANB, Darwin Airport, Northern Territory, on 22 March 2010

Preliminary report

Preliminary report released 19 May 2010

On 22 March 2010, at 1009 Central Standard Time, an Embraer - Empresa Brasileira de Aeronautica EMB-120ER Brasilia with two crew, prepared to take off on a training flight from runway 29 at Darwin Aerodrome, Northern Territory. The crew were the only occupants. The training captain advised the aerodrome controller that the departure would incorporate asymmetric flight (simulated engine failure) and was approved by the controller to perform the manoeuvre.

After becoming airborne, witnesses reported seeing the aircraft roll and diverge left from its take-off path. They watched as the aircraft continued rolling left and entered a steep nose-down attitude. It disappeared into trees, south of the runway threshold from where a column of black smoke was seen shortly afterwards.

Aerodrome rescue and firefighting services were in attendance very shortly thereafter and extinguished the fire. Both pilots were fatally injured, and the aircraft was seriously damaged due to impact forces and an intense post-impact fire.

Summary

On 22 March 2010, an Air North Embraer S.A. EMB-120ER Brasilia aircraft (EMB-120), registration VH-ANB, crashed moments after take-off from runway 29 at Darwin Airport, Northern Territory, fatally injuring both pilots. The flight was for the purpose of revalidating the command instrument rating of the pilot under check and was under the command of a training and checking captain, who occupied the copilot's seat. The take-off included a simulated engine failure.

Data from the aircraft's flight recorders was used to establish the circumstances leading to the accident and showed that the pilot in command (PIC) retarded the left power lever to flight idle to simulate an engine failure. That introduced a simultaneous failure of the left engine and propeller autofeathering system.

The increased drag from the 'windmilling' propeller increased the control forces required to maintain the aircraft's flightpath. The pilot under check allowed the speed to decrease and the aircraft to bank toward the inoperative engine. Additionally, he increased power on the right engine, and engaged the yaw damper in an attempt to stabilise the aircraft's flight. Those actions increased his workload and made control of the aircraft more difficult. The PIC did not restore power to the left engine to discontinue the manoeuvre. The few seconds available before the aircraft became uncontrollable were insufficient to allow 'trouble shooting' and deliberation before resolving the situation.

Shortly after the accident, an EMB-120 simulator and its staff were approved to undertake the operator's training requirements. In response, the operator transitioned the majority of its EMB-120 proficiency checking, including asymmetric flight sequences, to ground‑based training at that facility.

No organisational or systemic issues that might adversely affect the future safety of aviation operations were identified. However, the occurrence provides a timely reminder of the risks associated with in-flight asymmetric training and the importance of the work being carried out by the Civil Aviation Safety Authority to mandate the use of simulators for non-normal flying training and proficiency checks in larger aircraft. In addition, the importance of appropriate operator procedures, and pilot awareness of the potential hazards were reinforced as risk mitigators where the only option was in-flight asymmetric training and checking.

Animation

A computer graphics animation of the Flight Data Recorder data was produced.  The animation covered a 2-minute period commencing with the aircraft taxiing onto the runway and continuing until the end of recording.

Occurrence summary

Investigation number AO-2010-019
Occurrence date 22/03/2010
Location Darwin Airport
State Northern Territory
Report release date 23/02/2012
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 Embraer-Empresa Brasileira De Aeronautica
Model EMB-120
Registration VH-ANB
Serial number 120116
Aircraft operator Air North
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Darwin, NT
Destination Darwin, NT
Damage Substantial