Breakdown of separation - Boeing 767-338, VH-OGG and Airbus A320-232, VH-VNC, 74 km north-west of Tamworth Airport, New South Wales, on 1 July 2010

Summary

On 1 July 2010, at 1003 Eastern Standard Time, a breakdown of separation occurred between an Airbus Industrie A320-232 aircraft and Boeing Company 767-338 aircraft, about 40 NM (74 km) to the north-west of Tamworth, New South Wales. The aircraft were operating on crossing tracks, with an angular displacement between the tracks of about 50°. Both aircraft were operating at standard cruising levels. The enroute air traffic controller first identified the confliction about 2 minutes before the separation breakdown occurred, when both aircraft were maintaining FL360 and there was 26.2 NM (48.5 km) between their lateral positions. An instruction to climb to FL370 was issued to the flight crew of the 767. When there was 14.6 NM (27.04 km) between the aircraft, the controller subsequently instructed the flight crew of the 767 to expedite their aircraft's climb. Shortly before a 1,000 ft separation standard between the 767 and A320 was established, the radar data indicated that longitudinal separation had reduced, below the required standard of 5NM (9.26 km), to 3.8 (7.04 km) NM.

This incident highlighted the importance of the provision of timely and appropriate traffic information to flight crew by air traffic control, in that it can significantly enhance pilots' situational awareness.  It also supported the opportunity for flight crew to enhance the situational awareness of air traffic control, such as in providing direct information regarding individual aircraft performance.

Airservices Australia (Airservices) has advised that they are conducting a systemic review into the number of breakdown of separation occurrences. Outcomes from that review will be considered in terms of further safety improvement. In addition, Airservices has implemented a Compromised Separation Recovery training module for enroute air traffic control groups.

Occurrence summary

Investigation number AO-2010-050
Occurrence date 01/07/2010
Location 74 km NW of Tamworth Airport
State New South Wales
Report release date 12/09/2011
Report status Final
Investigation level Short
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Loss of separation
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer The Boeing Company
Model 767
Registration VH-OGG
Serial number 24929
Sector Jet
Operation type Air Transport High Capacity
Departure point Sydney, NSW
Destination Cairns, Qld
Damage Nil

Aircraft details

Manufacturer Airbus
Model A320
Registration VH-VNC
Serial number 3275
Sector Jet
Operation type Air Transport High Capacity
Departure point Brisbane, Qld
Destination Melbourne, Vic.
Damage Nil

Aircraft proximity event - VH-­JXY and VH-­BDP, 4 km west-north-west of Mandurah, Western Australia, on 30 June 2010

Summary

On 30 June 2010, a Grob - Burkhaart Flugzeugbau G-115C2 (Grob) aircraft, registered VH-BDP, and an Avions Pierre Robin R-2160 (Robin) aircraft, registered VH‑JXY, were conducting flying training north-west of Mandurah, Western Australia (WA). On board both aircraft were a flight instructor and student.

At about 1400 Western Standard Time, the Robin was travelling to the south-west, maintaining about 3,500 ft. The instructor in the Robin reported that he had just cleared the area in preparation for conducting a manoeuvre when he saw the Grob on a reciprocal heading, at about the same altitude. The aircraft was sighted too late to take any action. The instructor in the Grob also sighted the Robin, slightly to the left, and immediately initiated a steep turn to the right. It was estimated that the distance between the aircraft was about 50 m horizontally and 150 ft vertically, with the Grob positioned above the Robin.

As a result of this incident, the operator of the Grob has modified their operating procedures so that flying training will only be conducted in the designated training area. The operator of the Robin has implemented a procedure requiring pilots to request traffic information or flight following from air traffic control prior to commencing aerial work.

Occurrence summary

Investigation number AO-2010-049
Occurrence date 30/06/2010
Location 4 km WNW of Mandurah
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 Near collision
Occurrence class Serious Incident
Highest injury level None

Aircraft details

Manufacturer Avions Pierre Robin
Model R-2160
Registration VH-JXY
Serial number C181
Sector Piston
Operation type Flying Training
Departure point Jandakot, WA
Destination Jandakot, WA
Damage Nil

Aircraft details

Manufacturer Grob - Burkhart Flugzeugbau
Model G115
Registration VH-BDP
Serial number 82031/C2
Sector Piston
Operation type Flying Training
Departure point Jandakot WA
Destination Jandakot WA
Damage Nil

Aircraft proximity event - Pilatus PC-12, VH-FDK and Aeronautica Macchi S.P.A. AL60, VH-ELI, 50 km north-west of Mount Gambier Airport, South Australia, on 1 July 2010

Summary

On 1 July 2010, an Aeronautica Macchi S.P.A. AL60 aircraft, registered VH-ELI (ELI), departed Devonport, Tasmania (Tas.) for Portee Station, South Australia (SA) with planned refuelling stops at King Island, Tas. and Hamilton, Victoria (Vic.).

While enroute from King Island to Hamilton, the crew observed low cloud along the track and   diverted to Mount Gambier, SA to refuel. After departing Mount Gambier, the crew observed that the left fuel tank gauge was indicating half full. The crew discussed the situation and elected to continue the flight. Also, the directional gyro had to be aligned twice by the crew due to gyroscopic precession. As a result, the aircraft diverted to the left of the planned track by about 2-4 km. The crew commenced correcting the track when an inbound Pilatus Aircraft Ltd. PC-12/45 aircraft, registered VH‑FDK (FDK), passed to the left in close proximity.

It was estimated that the distance between the two aircraft was between 5 and 15 m horizontally and about 20 ft vertically.

While the operator of FDK determined that their pilot had complied with the required procedures, they advised the Australian Transport Safety Bureau (ATSB) that they will be conducting an internal education to remind pilots that maintaining a lookout and the use of radio telephony procedures are the primary tools used for traffic separation, supported by the traffic alert and collision avoidance system (TCAS).

Occurrence summary

Investigation number AO-2010-048
Occurrence date 01/07/2010
Location 50 km NW of Mount Gambier aerodrome
State South Australia
Report release date 28/01/2011
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 Pilatus Aircraft Ltd
Model PC-12
Registration VH-FDK
Serial number 466
Sector Turboprop
Operation type Medical Transport
Departure point Adelaide, SA
Destination Mount Gambier, SA
Damage Nil

Aircraft details

Manufacturer Aeronautica Macchi S.p.A
Model AL60/A1
Registration VH-ELI
Serial number 11-6156
Sector Piston
Operation type Private
Departure point Devonport, Tas.
Destination Portee Station, SA
Damage Nil

Crew incapacitation - VH-­KDQ, Cowell Aerodrome, 200 degrees M 41 km, on 22 June 2010

Summary

On 22 June 2010, a Saab 340B aircraft, registered VH-KDQ, was conducting a passenger charter flight from Adelaide to Ceduna, South Australia (SA). After departure, the copilot notified the pilot in command (PIC) that he was feeling unwell. The copilot's condition deteriorated to the point where he was unable to continue the flight to Ceduna. Shortly after reaching the top of climb, the pilot in command (PIC) decided to return the aircraft to Adelaide due to the copilot's deteriorating condition.

During the event, air traffic control (ATC) was not made aware of the reasons for the aircraft returning to Adelaide. Had the wellbeing of the copilot deteriorated further during the return to Adelaide, there may have been unnecessary delays in medical help being available.

Occurrence summary

Investigation number AO-2010-046
Occurrence date 22/06/2010
Location Cowell Aerodrome, 200° M 41 km
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 Flight crew incapacitation
Occurrence class Serious Incident
Highest injury level None

Aircraft details

Manufacturer Saab Aircraft Co.
Model 340
Registration VH-KDQ
Serial number 340B-325
Sector Turboprop
Operation type Charter
Departure point Adelaide, SA
Destination Ceduna, SA
Damage Nil

Loss of control - Cessna 172H, VH-RZV, near Cunnamulla Aerodrome, Queensland, on 30 June 2010

Summary

On 30 June 2010, a Cessna Aircraft Company 172H (C172), registered VH-RZV, with one pilot on board, was engaged in cattle spotting, about 21 km NNW of Cunnamulla, Queensland (Qld.).

While orbiting a water trough at about 500 ft, the pilot lost control of the aircraft. Damage to the aircraft was consistent with the right-wing colliding with a tree branch, followed by the aircraft impacting the ground inverted, with a steep nose-down attitude

The pilot sustained serious injuries, and the aircraft was severely damaged. The pilot reported that the most likely reason for the accident was an inadvertent stall. This probably occurred while the pilot was performing a steep turn, with his attention divided between flying the aircraft and looking for cattle.

Most stall/spin accidents occur when a pilot is momentarily distracted from the primary task of flying the aircraft. This accident highlights that even an experienced pilot performing a familiar task can be momentarily distracted, resulting in the loss of control of the aircraft.

Occurrence summary

Investigation number AO-2010-047
Occurrence date 30/06/2010
Location near Cunnamulla Aerodrome
State Queensland
Report release date 28/01/2011
Report status Final
Investigation level Short
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Loss of control
Occurrence class Accident
Highest injury level Serious

Aircraft details

Manufacturer Cessna Aircraft Company
Model 172
Registration VH-RZV
Serial number 17255652
Sector Piston
Operation type Private
Departure point Unknown
Destination Baroona Station Qld
Damage Substantial

Collision with water - Cessna 172N, VH-UFN, Woolcunda Lake, New South Wales, on 21 June 2010

Summary

On the morning of 21 June 2010, the owner/pilot of a Cessna Aircraft 172N, registered VH‑UFN, departed from a private airstrip near Woolcunda Lake, New South Wales for a flight over the pilot's property. The aircraft did not return and was reported missing that afternoon. A search was initiated and, 2 days later, the aircraft was located in Woolcunda Lake.

The investigation identified that the aircraft impacted the lake in a left banking turn. Irrespective of the reason for being at low level, it is probable that the pilot misjudged the height of the aircraft above the lake's surface or was distracted at a height from which the pilot was unable to recover before impacting the water.

Australian Transport Safety Bureau report AR‑2009-041 Avoidable Accidents No. 1: Low‑level flying addressed the dangers associated with low-level flight and in particular, the reduced time available to recover from any loss of control. This investigation provides a timely reminder of the effect on that risk of flight over expanses of flat, featureless terrain or water.

Occurrence summary

Investigation number AO-2010-045
Occurrence date 21/06/2010
Location Woolcunda Lake
State New South Wales
Report release date 19/08/2011
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 Cessna Aircraft Company
Model 172
Registration VH-UFN
Serial number 17270963
Sector Piston
Operation type Private
Departure point Woolcunda Station, NSW
Destination Woolcunda Station, NSW
Damage Substantial

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

ao2010043_plot1.jpg

ao2010043_plot1.jpg

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