Collision with terrain - Robinson R22, VH-RPN, 257 km east-north-east of Derby, Western Australia, on 13 June 2010

Preliminary report

Preliminary report released 6 August 2010

On 13 June 2010, a Robinson Helicopter Co R22 Beta, registered VH-RPN, was engaged in cattle mustering operations on a station property about 257 km east-north-east of Derby, Western Australia. During those operations the helicopter collided with the ground and caught fire. The pilot, the sole occupant of the helicopter sustained fatal injuries.

Summary

On 13 June 2010, a Robinson Helicopter Co. R22 Beta, registered VH-RPN, was engaged in aerial cattle mustering operations on a station property about 257 km east-north-east of Derby, Western Australia. During those operations, the helicopter collided with the ground and caught fire. The pilot, the sole occupant of the helicopter, sustained fatal injuries.

The investigation found that the helicopter had a high descent rate and some forward speed at impact but, due to the lack of evidence as a function of the type and location of the operation, was unable to positively establish any further contributing factors.

The investigation did not identify any organisational or systemic issues that might adversely affect the future safety of aviation operations. However, the accident provides a reminder of the hazards involved in aerial mustering operations that result in, or add to a number of low‑level risks that require close management. Any pilot distraction, aircraft or systems failure, adverse weather or aircraft performance, or handling inattention can reduce the margins for continued safe flight.

Occurrence summary

Investigation number AO-2010-042
Occurrence date 13/06/2010
Location 257 km ENE of Derby
State Western Australia
Report release date 08/06/2011
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 Robinson Helicopter Co
Model R22
Registration VH-RPN
Serial number 2241
Sector Helicopter
Operation type Aerial Work
Damage Destroyed

Collision with terrain - Piper PA-31P-350, VH-PGW, 6 km north-west of Bankstown Airport, New South Wales, on 15 June 2010

Preliminary report

Preliminary report released 15 July 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.

At about 0807 Eastern Standard Time on 15 June 2010, a Piper PA-31P-350 Mojave aircraft, registered VH-PGW, with a pilot and flight nurse on board, collided with terrain in a suburban area about 6 km north-west of Bankstown Airport, New South Wales. At the time, the pilot was attempting to return to Bankstown following a reported in-flight engine shutdown. Both occupants were fatally injured, and the aircraft was destroyed by the impact forces and an intense post-impact fire.

The Australian Transport Safety Bureau has conducted a series of examinations of the propellers, engines and some associated engine and airframe components that were not destroyed during the impact and subsequent fire. The examination of the propellers indicated that, at the time of impact, the right propeller was in the feathered position and the left propeller was in the full fine position, which was consistent with low engine power. The examination of the engines did not find any evidence of mechanical failure. Impact and fire damage to the cockpit area resulted in most of the instruments and systems being destroyed or extensively damaged. The position of several cockpit switches was determined but an examination of the cockpit instruments was unable to determine any instrument indications at the time of impact.

The investigation is continuing and will include:

  • an ongoing examination of operational issues including pilot training and checking
  • continued analysis of recorded radar data and voice transmissions
  • an ongoing human factors review.

It is anticipated that the final investigation report will be released to the public in the first quarter of calendar year 2012.

Aircraft flight path chart

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Final report

Safety summary

What happened

At about 0806 Eastern Standard Time on 15 June 2010 a Piper PA-31P-350 Mojave aircraft, registered VH-PGW, with a pilot and a flight nurse on board, collided with terrain in a suburban area about 6 km north-west of Bankstown Airport, New South Wales. At the time of the accident, the pilot was attempting to return to Bankstown following a reported in-flight engine shutdown. Both occupants were fatally injured, and the aircraft was destroyed by the impact forces and an intense post-impact fire.

What the ATSB found

The Australian Transport Safety Bureau (ATSB) found that following the shutdown of the right engine, the aircraft’s airspeed and rate of descent were not optimised for one engine inoperative flight. In addition, spectral analysis indicated it was unlikely that the left engine was being operated at maximum continuous power as the aircraft descended. As a result, the aircraft descended to a low altitude over a suburban area and the pilot was then unable to maintain level flight, which led to the collision with terrain.

Examination of the engines, propellers and governors and other aircraft components found no evidence of any pre-impact faults. However, the engine surging identified by the spectral analysis of radio transmissions during the flight was consistent with uneven fuel distribution to the cylinders.

What has been done as a result

The Civil Aviation Safety Authority has started a project to amend advisory material relating to multi-engine aircraft training and operations to include guidance information about engine problems encountered during the climb and cruise phases of flight. This amended guidance material will include information about aircraft handling, engine management, and decision making during these phases of flight.

Safety message

This accident reinforces the importance when flying twin-engine aircraft with one engine shutdown that the optimal speed be selected, along with maximum continuous power on the operative engine, and that the aircraft’s performance should be verified prior to conducting a descent. Pilots should also use the appropriate PAN or MAYDAY phraseology when advising air traffic control of non-normal or emergency situations.

Inquest

ATSB response to Findings

The Coroner’s Court of New South Wales (NSW) recently made findings and recommendations into a 2010 fatal accident involving a Piper PA-31P-350 Mojave aircraft, registered VH-PGW, which occurred 6 km north-west of Bankstown Airport, NSW.

The ATSB summary explains that on 15 June 2010, the pilot of a Piper PA-31P-350 Mojave aircraft and a flight nurse passenger took off from Bankstown Airport. At about 0806 Eastern Standard Time, the aircraft collided with terrain. At the time of the accident the pilot was attempting to return to Bankstown following a reported in-flight engine shutdown.

The Coroner made two recommendations, the first of which reflects a minor safety issue identified by the ATSB in its report:

Coroner’s Recommendation

That the Civil Aviation Safety Authority (CASA) finalise the guidance material for Civil Aviation Advisory Publication (CAAP) 5.23 Multi-engine Aeroplane Operations and Training such that the guidance material is completed and released as soon as possible. The coroner noted that the guidance material provides for multi‑engine aeroplane operations and training to support the flight standard in Appendix A of s.1.2 of the CAAP. This relates to engine failure in the cruise.

Safety message

This accident reinforces the importance when flying twin-engine aircraft with one engine shutdown that the optimal speed be selected, along with maximum continuous power on the operative engine, and that the aircraft’s performance should be verified prior to conducting a descent. Pilots should also use the appropriate PAN or MAYDAY phraseology when advising air traffic control of non-normal or emergency situations.

What has been done as a result

CASA has started a project to amend advisory material relating to multi-engine aircraft training and operations to include guidance information about engine problems encountered during the climb and cruise phases of flight. This amended guidance material will include information about aircraft handling, engine management, and decision making during these phases of flight. Updates on this work by CASA are available on the ATSB website

Inquests are separate to ATSB 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-PGW.

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

Final report (2.33 MB)

The Coroner's report can be obtained from the Coroner's Court of NSW. Contact details are available at: www.coroners.justice.nsw.gov.au. Queries regarding the Coroner's findings should be directed to the NSW Coroner’s Court.

Occurrence summary

Investigation number AO-2010-043
Occurrence date 15/06/2010
Location 6 km NW of Bankstown Airport
State New South Wales
Report release date 20/12/2012
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 Fatal

Aircraft details

Manufacturer Piper Aircraft Corp
Model PA-31
Registration VH-PGW
Serial number 31P-8414036
Sector Piston
Operation type Aerial Work
Departure point Bankstown, NSW
Destination Archerfield, Qld
Damage Destroyed

Aircraft proximity event - VH-­YHM and VH-­RQZ, 4 km south of Dayboro, Queensland, on 4 June 2010

Summary

On 4 June 2010, at about 1345 Eastern Standard Time, a Diamond Aircraft Industries DA40-D (DA40), registered VH-YHM, was travelling in a westerly direction towards Esk, Queensland (Qld), maintaining 2,500 ft. When passing Dayboro, Qld, the DA40 came into close proximity with a Cessna Aircraft Company 172R (C172), registered VH-RQZ, which was descending through 2,500 ft, heading to the south.

The lateral separation between the aircraft was estimated at 10 m, with the DA40 in front of, and slightly below the C172. While the pilots of both aircraft had sighted each other, there was insufficient time to respond and take any action.

The pilots both reported maintaining a visual lookout, but having been temporarily distracted just prior to the incident.

Flights conducted outside controlled airspace (Class G) are not provided with a traffic separation service from air traffic control (ATC). Consequently, maintaining separation is the pilot's responsibility. It is crucial that pilots employ a number of defences to ensure that separation between aircraft is suitably achieved. Applying unalerted and alerted see-and-avoid principles by maintaining a vigilant lookout, and providing and interpreting radio communications will assist in enhancing situational awareness.

Occurrence summary

Investigation number AO-2010-041
Occurrence date 04/06/2010
Location 4 km south of Dayboro
State Queensland
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 Near collision
Occurrence class Serious Incident
Highest injury level None

Aircraft details

Manufacturer Diamond Aircraft Industries
Model DA40
Registration VH-YHM
Serial number D4.308
Sector Piston
Operation type Flying Training
Departure point Gold Coast, Qld
Destination Gold Coast, Qld
Damage Nil

Aircraft details

Manufacturer Cessna Aircraft Company
Model 172
Registration VH-RQZ
Serial number 17280980
Sector Piston
Operation type Flying Training
Departure point Wondai, Qld
Destination Archerfield, Qld
Damage Nil

Loss of separation assurance - VH-­IVT and VH-­IMV, Moorabbin Aerodrome, Victoria, on 2 June 2010

Summary

On 2 June 2010, a Cessna Aircraft Company 172R aircraft (C172), registered VH-IMV, was cleared to line up and hold on runway 17R at Moorabbin aerodrome, Victoria. On board the aircraft were an instructor and student, with the intention of conducting a training flight to Essendon aerodrome.

After processing a number of other aircraft, the controller cleared a Cessna Aircraft Company 152 aircraft (C152), registered VH-IVT, for a touch and go on runway 17R. The C172 continued to line up and hold at the end of the runway without making any further transmissions.

A Beech Aircraft Corporation 58 then reported ready for runway 17R at taxiway Alpha 1. The controller noticed the C172 lined up and instructed the C152 on final to go around. When the C152 was upwind, the C172 was cleared for takeoff.

Although Moorabbin was a General Aviation Aerodrome Procedures (GAAP) aerodrome at the time of the occurrence, runway separation standards were required to be applied. There was a loss of separation assurance.

Airservices advised that they would introduce the use of flight progress strips for Moorabbin control tower during the second half of 2010. They also advised that they planned to conduct an ergonomic study of the Moorabbin control tower layout.

Occurrence summary

Investigation number AO-2010-040
Occurrence date 02/06/2010
Location Moorabbin aerodrome
State Victoria
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 Loss of separation assurance
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Cessna Aircraft Company
Model 172
Registration VH-IMV
Serial number 17280270
Sector Piston
Operation type Flying Training
Departure point Moorabbin Aerodrome Vic
Destination Moorabbin Aerodrome Vic
Damage Nil

Aircraft details

Manufacturer Cessna Aircraft Company
Model 152
Registration VH-IVT
Serial number 15280246
Sector Piston
Operation type Flying Training
Departure point Moorabbin Aerodrome Vic
Destination Moorabbin Aerodrome Vic
Damage Nil

Weather related event - VH-NGX, Southern Cross (ALA), Western Australia, on 1 June 2010

Summary

On 1 June 2010, a Fairchild Industries Inc. SA226-TC (Metro II) aircraft, registered VH-NGX, was being prepared for a charter passenger service from Perth to the Southern Cross aeroplane landing area (ALA), Western Australia (WA).

Prior to departing, the crew obtained the weather forecasts for the flight. The area forecast (ARFOR), which covered a large area, forecast fog, while the aerodrome forecast (TAF), which covered a particular location, forecast conditions as clear. The crew contacted the Bureau of Meteorology (BoM) to confirm the conditions. The crew received an amended forecast for Southern Cross indicating fog, and visibility reducing to 300 m until 0800 Western Standard Time; after this time conditions were forecast to improve.

Due to the payload requirements of the flight, additional fuel for an alternate aerodrome could not be carried as required if the weather conditions at Southern Cross were unfavourable. Consequently, the crew elected to delay the departure from Perth until 0800.

While en route, the crew observed a band of cloud between Perth and Southern Cross. On arrival at Southern Cross, the conditions were not as expected by the crew, with overcast low cloud and fog present. The crew tracked to the north of the airstrip, where the fog had cleared, and commenced the approach. In order to remain clear of cloud and maintain visual sight with the runway, the aircraft was descended to 337 ft above ground level (AGL). From this point, the crew determined that a straight-in-approach could not be conducted and a low level circling approach to position the aircraft on final for runway 14 was performed. The aircraft landed at about 0915 without further incident.

The BoM conducted a review of this incident and made a number of recommendations, including making forecasters aware of the synoptic conditions behind this incident and its consequential effect on users; and as part of a national review, establishing the minimum observation requirements needed in order to issue and maintain a weather watch on a TAF.

Occurrence summary

Investigation number AO-2010-039
Occurrence date 01/06/2010
Location Southern Cross (ALA)
State Western 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 Weather - Other
Occurrence class Serious Incident
Highest injury level None

Aircraft details

Manufacturer Fairchild Industries Inc
Model SA226
Registration VH-NGX
Serial number TC-287
Sector Turboprop
Operation type Charter
Departure point Perth, WA
Destination Southern Cross, WA
Damage Nil

Ground handling event - VH-­VQL, Sydney Aerodrome, New South Wales, on 1 June 2010

Summary

On 1 June 2010, an Airbus A320-232 aircraft, registered VH-VQL, was being operated on a scheduled passenger service from the Gold Coast, Queensland (Qld) to Sydney, New South Wales (NSW). On arrival at Sydney the passengers commenced disembarking through the aircraft's forward and rear doors. During this time, a ground handler drove a cargo loader towards the rear cargo door of the aircraft in preparation for unloading baggage and cargo.

When the loader was about 3 m away from the aircraft, the ground handler stopped the loader, completed the relevant safety checks and then commenced moving towards the aircraft. After moving forward about 0.3 m the loader unexpectedly accelerated towards the aircraft. The ground handler reported he was unable to stop the loader or turn it away from the aircraft prior to it impacting the aircraft just forward of the rear cargo door. The aircraft, cargo loader and rear passenger stairs sustained serious damage. No one was injured in the incident.

A subsequent inspection by the operator identified that when the throttle pedal was depressed to the full open position, the pedal would intermittently become caught on the throttle stop due to a missing striker plate on the back of the pedal assembly.

As a result of this incident, the operator inspected all their cargo loaders of the same model to ensure they were not missing the striker plate. One loader was found to be missing a striker plate and this has since been repaired.

Occurrence summary

Investigation number AO-2010-038
Occurrence date 01/06/2010
Location Sydney aerodrome
State New South Wales
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 Ground handling
Occurrence class Serious Incident
Highest injury level None

Aircraft details

Manufacturer Airbus
Model A320
Registration VH-VQL
Serial number 2642
Sector Jet
Operation type Air Transport High Capacity
Departure point Gold Coast, Qld
Destination Sydney, NSW

Operational event - VH-­VQZ, Gold Coast Aerodrome, Queensland, on 30 May 2010

Summary

On 30 May 2010, an Airbus Industrie A320-232 aircraft, registered VH-VQZ, departed Sydney, New South Wales (NSW) on a scheduled passenger service to the Gold Coast, Queensland (Qld). The copilot, who was under training, was designated as the pilot flying for the flight.

The aircraft arrived at the Gold Coast and an instrument approach was commenced. During the landing, the flare was initiated early and the aircraft floated along the runway. The pilot in command (PIC) instructed the copilot to lower the nose of the aircraft; however, the aircraft appeared to maintain a level pitch attitude. The PIC determined that the landing could not be achieved and assumed control of the aircraft. The PIC initiated a go around, during which time the aircraft's main landing gear momentarily contacted the runway. The missed approach procedure was commenced, and a second approach was made without further incident.

The failure to identify or execute a go around/missed approach procedure has been cited by the Flight Safety Foundation as one of the major causes of approach-and-landing accidents. This incident highlights the importance of recognising when a go around should be initiated and supports the safety benefits of being 'go-around-prepared' and 'go-around-minded'.

Occurrence summary

Investigation number AO-2010-037
Occurrence date 30/05/2010
Location Gold Coast aerodrome
State Queensland
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 Control - Other
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Airbus
Model A320
Registration VH-VQZ
Serial number 2292
Sector Jet
Operation type Air Transport High Capacity
Departure point Sydney NSW
Destination Gold Coast Qld
Damage Nil

Aircraft loading issue - VH-­ZPF, Adelaide Aerodrome, South Australia, on 16 May 2010

Summary

On 16 May 2010, an Embraer ERJ 190 aircraft, registered VH-ZPF, was being operated on a positioning flight from Adelaide, South Australia (SA) to Brisbane, Queensland (Qld). After arriving in Brisbane, the pilot in command (PIC) reported that the load and trim sheet for the aircraft was inaccurate due to certain items being counted twice in the aircraft's load and trim calculations.

It was found that an error occurred when the Adelaide airport movements coordinator (AMCO), during a period of high workload, inadvertently selected the incorrect aircraft configuration in the company's computerised load and trim system.

The aircraft was not operated outside its weight and balance limitations; however, there were implications for how the pitch trim was set prior to takeoff.

The operator has raised an amendment to its flight operations manual to clarify the correct configuration to use when compiling a load and trim sheet for a positioning flight. The operator has also implemented changes to its load control system software to prevent the inadvertent selection of the incorrect configuration while preparing a load and trim sheet.

Occurrence summary

Investigation number AO-2010-034
Occurrence date 16/05/2010
Location Adelaide 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 Loading related
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Embraer-Empresa Brasileira De Aeronautica
Model ERJ 190
Registration VH-ZPF
Serial number 19000193
Sector Jet
Operation type Air Transport High Capacity
Departure point Adelaide SA
Destination Brisbane Qld
Damage Nil

Wirestrike – Bell Helicopter 206L LongRanger III, VH-OSU, 37 km south-south-west of Latrobe Valley Airport, Victoria, on 20 May 2010

Summary

At about 1253 Eastern Standard Time on 20 May 2010, a Bell Helicopter 206L LongRanger III helicopter, registered VH-OSU, commenced forestry spraying operations about 37 km south-south-west of Latrobe Valley Airport, Victoria. At about 1354 the pilot commenced a final spray run that resulted in the helicopter's flightpath crossing a powerline that was known to the pilot. The helicopter contacted the wire, seriously damaging the helicopter's flight control system and main rotor mast, which likely rendered it uncontrollable. The helicopter subsequently impacted the ground. The pilot was fatally injured.

The investigation found that it was likely that the pilot failed to recall the existence of the wire. The inherent difficulty of visually detecting the wire, combined with the operating groundspeed, meant that the pilot would not have had sufficient time to avoid the wire after seeing it. An examination of the wreckage of the helicopter did not find any mechanical abnormalities that might have contributed to the accident.

No permanent or temporary high visibility devices were attached to the powerlines, nor were they required to be. The helicopter was not fitted with wirestrike protection system (WSPS) equipment, nor was it required to be by aviation regulation. The investigation was unable to determine if a WSPS might have altered the outcome of the wirestrike.

As a result of this accident, Energy Safe Victoria issued a wire safety alert to aerial work operators and infrastructure providers. The Australian Transport Safety Bureau (ATSB) issued a Safety Advisory Notice to Energy Networks Australia and operators and pilots that are involved in low-level operations. The notice suggested that, where wires exist in areas where low-level activity occurs, operators and pilots consider the need for any powerlines to be marked in accordance with AS 3891.2, 2008, Part 2: Marking of overhead cables for planned low level flying operations. In addition, the ATSB has published an educational report aimed at increasing awareness among low-level operators and those agencies organising such activities. The ATSB has also commenced a research investigation that seeks to more fully understand the wirestrike risk in Australia.

Occurrence summary

Investigation number AO-2010-033
Occurrence date 20/05/2010
Location 37 km SSW of Latrobe Valley Airport
State Victoria
Report release date 23/06/2011
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 Bell Helicopter Co
Model 206
Registration VH-OSU
Serial number 51226
Sector Helicopter
Operation type Aerial Work
Damage Destroyed

Incorrect aircraft configuration - Airbus A321-231, VH-VWW, Changi International Airport, Singapore, on 27 May 2010

Summary

At 1845 Singapore Time on 27 May 2010, an Airbus A321-231, registered VH-VWW and operating as Jetstar flight JQ57, was undertaking a landing at Singapore Changi International Airport. The aircraft was not in the correct landing configuration by 500 ft height above the aerodrome and, as required by the operator's procedures in the case of an unstable approach, the crew carried out a missed approach.

The investigation identified several events on the flight deck during the approach that distracted the crew to the point where their situation awareness was lost, decision making was affected and inter‑crew communication degraded. In addition, it was established that the first officer's performance was probably adversely affected by fatigue.

The investigation did not identify any organisational or systemic issues that might adversely impact the future safety of aviation operations. However, following this occurrence, the aircraft operator proactively reviewed its procedures and made a number of amendments to its training regime and other enhancements to its operation.

Occurrence summary

Investigation number AO-2010-035
Occurrence date 27/05/2010
Location Singapore Changi International
State International
Report release date 19/04/2012
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Incorrect configuration
Occurrence class Serious Incident
Highest injury level None

Aircraft details

Manufacturer Airbus
Model A321
Registration VH-VWW
Serial number 3916
Aircraft operator Jetstar
Sector Jet
Operation type Air Transport High Capacity
Departure point Darwin, NT
Destination Singapore
Damage Nil