Examination of the feasibility of the establishment of a single source or database of known powerlines and tall structures

Summary

There were 52 fatalities throughout Australia as a result of wirestrike accidents in the period 1994 to 2006. During that period, there was an average of just under 11 reported wirestrike accidents each year and the average number of fatalities was four per annum.

Despite the application of risk strategies to mitigate the consequences of a wirestrike, those consequences can often be expected to be catastrophic. In that case, a large investment is made by operators, pilots and other parties involved in low-level operations to minimise the likelihood of a wirestrike. That includes by ensuring awareness of all known low-level hazards, including powerlines and tall structures, before commencing, and during the conduct of low-level operations.

During a series of recent ATSB investigations into fatal and other wirestrike accidents, a number of different sources of information on the location of known powerlines and tall structures was identified. However, despite the apparent utility and safety benefits inherent in the availability to pilots, operators and low-level campaign managers of a single source or database of the location of known powerlines and tall structures, initial discussions with aviation authorities on the potential development of such a resource were non-productive.

However, Australian Transport Safety Bureau (ATSB) investigators commenced initial discussions with Geoscience Australia (GA) and the Energy Networks Association (ENA) to examine the feasibility of the establishment of such a database. Those discussions determined that GA was amenable to working with other relevant agencies in order to promulgate that data for use by pilots and other parties. ENA indicated that the proposal to establish a national database would be considered as part of its 2008 priority issues.

The ATSB will advise of further developments in its discussions with GA and ENA on its website at 6-monthly intervals.

Occurrence summary

Investigation number AI-2008-019
Occurrence date 02/04/2008
Location Not applicable
State Other
Report release date 02/04/2008
Report status Final
Investigation level Systemic
Investigation type Safety Issue Investigation
Investigation status Completed
Mode of transport Aviation
Occurrence class Other
Highest injury level None

Collision with terrain, Pitts S-2A, VH-NUK, 7 km north-east of Camden, New South Wales, on 18 March 2008

Preliminary report

Preliminary report released 16 May 2008

On 18 March 2008, at approximately 1115 Eastern Daylight-saving Time (EDT), a Pitts S-2A aircraft struck two trees before impacting the ground beside the Northern Road, 7 km NE of Camden, NSW, fatally injuring the occupant of the rear cockpit.

Summary

On 18 March 2008, at approximately 1115 Eastern Daylight-saving Time, a Pitts S-2A aircraft struck two trees before impacting the ground beside the Northern Road, 7 km north-east of Camden, NSW, fatally injuring the occupant of the rear cockpit.

The occupant of the rear cockpit (the candidate), an experienced aerobatic pilot, was undergoing a routine flight review with an instructor. In the instructor's judgment, the candidate flew well during the flight review until a practice forced landing (PFL) manoeuvre just before the accident.

During the PFL, the candidate stopped responding to instructions and commands, so the instructor took control of the aircraft. A powerful nose-up force began acting on the control column and, despite the instructor's efforts to control the aircraft, it entered an incipient aerodynamic stall. The instructor recovered the aircraft from the stall but, as consequence of the nose-up force, this came too late to prevent a collision with trees.

No evidence of any mechanical problem with the aircraft was found. Postmortem examination of the candidate found he had severe heart disease.

Expert medical opinion considered it likely that the candidate suffered an incapacitating event as a result of his heart disease, and that the incapacitating event probably led to him exerting a force on the control column. The nose-up force prevented complete control by the instructor, delayed recovery from the stall, and led to the impact with trees.

Occurrence summary

Investigation number AO-2008-021
Occurrence date 18/03/2008
Location Camden Airport E/6 km
State New South Wales
Report release date 10/02/2009
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Flight crew incapacitation
Occurrence class Accident
Highest injury level Fatal

Aircraft details

Manufacturer Pitts Aviation Enterprises
Model S-2
Registration VH-NUK
Serial number 2116
Sector Piston
Operation type Private
Departure point Bankstown Airport, NSW
Destination Bankstown Airport, NSW
Damage Destroyed

Collision with terrain, VH-KUZ, Airvan GA8, Kalumburu, Western Australia, on 26 February 2008

Summary

On 26 February 2008, at about 1655 Western Daylight-saving Time, the pilot of a Gippsland Aeronautics Pty Ltd GA-8 Airvan, registered VH-KUZ, with two passengers on board, commenced take-off at Kalumburu Aerodrome, WA. Witnesses reported that the aircraft started to drift to the left of the runway prior to becoming briefly airborne. The aircraft settled back onto the runway strip, veering further left across the runway strip. The aircraft subsequently ran up an embankment, through low scrub, and then through small trees beyond the runway strip. The impact with the trees flipped the aircraft onto its back, where it came to rest, facing the opposite way to the direction of take-off. The aircraft was seriously damaged, and the pilot and two passengers received minor injuries.

Occurrence summary

Investigation number AO-2008-015
Occurrence date 26/02/2008
Location Kalumburu Aerodrome
State Western Australia
Report release date 23/06/2009
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Collision with terrain
Occurrence class Accident
Highest injury level Minor

Aircraft details

Manufacturer Gippsland Aeronautics Pty Ltd
Model GA8
Registration VH-KUZ
Serial number GA8-07-110
Sector Piston
Operation type Charter
Departure point Kalumburu, WA
Destination Kununurra, WA
Damage Substantial

Procedures-related event, Launceston Airport, Tasmania, on 12 March 2008, VH-VQY, Airbus A320-200

Summary

On 12 March 2008, an Airbus A320-200 aircraft, registered VH-VQY, was being operated on a scheduled passenger service from Launceston, Tas. to Sydney, NSW. While the crew were preparing for the flight, the control tower closed, and the airport lighting switched over to a pilot activated lighting system. The aircraft subsequently departed without the airport lighting being turned on. A number of situational factors were probably associated with the crew not activating the airport lights before the departure. Several similar incidents have previously occurred in Australia and overseas.

Occurrence summary

Investigation number AO-2008-020
Occurrence date 12/03/2008
Location Launceston Airport
State Tasmania
Report release date 25/06/2009
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Airbus
Model A320
Registration VH-VQY
Serial number 2299
Sector Jet
Operation type Air Transport High Capacity
Departure point Launceston, Tas.
Destination Sydney, NSW
Damage Nil

Collision with terrain – 7 km north-north-west of Hornsby, New South Wales, on 1 March 2008

Summary

On 1 March 2008, at about 1300 Eastern Daylight-saving Time the pilot of a Bell Helicopter 206B Jetranger III was flying over a property on a private flight with four passengers. Witnesses reported seeing the helicopter flying over the property at about 100 ft above ground level. At the completion of one pass, the helicopter was observed by witnesses on the ground to bank steeply to the left, roll out and descend into surrounding trees. The helicopter impacted the trees and was seriously damaged. One of the occupants was discovered outside the helicopter and all sustained serious injuries.

Examination of the wreckage did not indicate any mechanical defects that would have affected the safe operation of the helicopter.

Occurrence summary

Investigation number AO-2008-017
Occurrence date 01/03/2008
Location 7 km NNW, Hornsby
State New South Wales
Report release date 03/10/2008
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 Serious

Aircraft details

Manufacturer Bell Helicopter Co
Model 206
Registration VH-NBP
Serial number 4185
Sector Helicopter
Operation type Private
Damage Destroyed

Fumes Event, VH-EBY, 275 km west-south-west of Sydney, New South Wales, on 25 February 2008

Summary

On 25 February 2008, at about 2128 Eastern Daylight-saving Time, the flight crew of a Boeing Company 747-338 (747) aircraft, registered VH-EBY, detected a smell that slowly increased in intensity. At that time, the aircraft was cruising at 37,000 ft and was about 275 km west south-west of Sydney, NSW.

The flight crew donned their emergency oxygen equipment and transmitted a PAN call to air traffic control. The aircraft was cleared direct to Sydney for landing and was escorted to the terminal by the airport fire services for disembarkation.

An inspection by the operator determined that loose terminal connections to the left windshield heat element resulted in electrical arcing and fumes on the flight deck.

The aircraft manufacturer has a programme to replace the windshields in the 747 with an enhanced windshield heater wiring connection that should address the risk of electrical arcing in that component.

Occurrence summary

Investigation number AO-2008-013
Occurrence date 25/02/2008
Location CULIN NSW, 270 degrees/93 km
State New South Wales
Report release date 29/05/2009
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Fumes
Occurrence class Serious Incident
Highest injury level None

Aircraft details

Manufacturer The Boeing Company
Model 747
Registration VH-EBY
Serial number 23823
Sector Jet
Operation type Air Transport High Capacity
Departure point Perth, WA
Destination Sydney, NSW
Damage Nil

Mid-air collision - 10 km north-east of Wee Waa, New South Wales, on 26 February 2008

Preliminary report

Preliminary report released 11 June 2008

At 0930 Eastern Daylight-saving Time on 26 February 2008, Air Tractor Inc. 502 registered VH-CJK (CJK), whose pilot was engaged in the aerial spraying of a field approximately 10 km NE of Wee Waa township, NSW, and Air Tractor Inc. 502B registered VH-ATB (ATB), that had just departed from an airstrip approximately 13 km north-east of Wee Waa, collided. The pilot of CJK was fatally injured and the aircraft destroyed by collision forces with the other aircraft and by ground impact. It did not catch fire. The pilot of ATB was seriously injured and the aircraft destroyed by collision forces with the other aircraft, ground impact, and a post impact fire.

Summary

At about 0930 Eastern Daylight-saving Time on 26 February 2008, an Air Tractor Inc. 502, registered VH-CJK (CJK) that was aerial spraying 10 km north-east of Wee Waa, New South Wales and an Air Tractor Inc. 502B, registered VH-ATB (ATB) that had just departed from a nearby airstrip, collided at about 200 ft above ground level. The pilot of CJK was fatally injured and the pilot of ATB was seriously injured. Both aircraft were seriously damaged. Neither pilot was aware of the other aircraft and, although visibility at the time of the accident was reported as 'good', either one or both pilots did not see the other aircraft in sufficient time to avoid a collision.

The limitations of an unalerted visual traffic scan could explain why both pilots may not have seen the other aircraft but, without the knowledge of one another's intended operations they lacked situational awareness. Generally, agricultural pilots relied on visual separation and vertical segregation to avoid collisions. In this instance, the proximity of the field being sprayed to the airstrip from which ATB took off and the aircraft's climb gradient from that airstrip, brought the two aircraft into conflict.

Occurrence summary

Investigation number AO-2008-014
Occurrence date 26/02/2008
Location Wee Waa
State New South Wales
Report release date 26/07/2010
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Airborne collision
Occurrence class Accident
Highest injury level Fatal

Aircraft details

Manufacturer Air Tractor Inc
Model AT502
Registration VH-CJK
Serial number 502-0057
Sector Turboprop
Operation type Aerial Work
Departure point ALA 4.5 km SW Wee Waa NSW
Destination ALA 4.5 km SW Wee Waa NSW
Damage Destroyed

Aircraft details

Manufacturer Air Tractor Inc
Model AT502
Registration VH-ATB
Serial number 502B-0287
Sector Turboprop
Operation type Aerial Work
Departure point ALA 13 km NE Wee Waa NSW
Destination ALA 13 km NE Wee Waa NSW
Damage Destroyed

Runway excursion, VH-UZD, Thangool Aerodrome, Queensland, on 12 February 2008

Summary

On 12 February 2008, a Fairchild Industries SA227-AC (Metro III) aircraft, registered VH-UZD, was being operated on a freight service between Emerald and Thangool, Queensland with two pilots. The approach and landing into Thangool were conducted after last light in conditions of scattered low cloud and rain showers. At a speed of about 40 kts after touchdown, the aircraft suddenly veered uncontrollably to the right, departed the runway and became bogged in wet grass.

There was no damage to the aircraft or injuries to the flight crew.

The investigation determined that the runway excursion was probably a result of a directional upset at a time when the nosewheel was in castor mode. The reason for the nosewheel being in the castor mode could not be determined with certainty and may have been the result of an intermittent fault or the inadvertent failure by the flight crew to arm the system.

It was also determined that the aircraft's rate of descent during the latter stages of the approach was significantly higher than for a normal stabilised approach. In addition, the aircraft operator's stabilised approach criteria did not provide flight crew with information on maximum permitted rates of descent. The aircraft operator has advised that, as a result of the investigation, it has redefined its stabilised approach criteria.

Occurrence summary

Investigation number AO-2008-009
Occurrence date 12/02/2008
Location Thangool
State Queensland
Report release date 25/06/2010
Report status Final
Investigation level Systemic
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 Fairchild Industries Inc
Model SA227
Registration VH-UZD
Serial number AC-490
Sector Turboprop
Operation type Charter
Departure point Emerald Qld
Destination Thangool Qld
Damage Nil

Mid-air collision - involving Piper PA-18 Super Cub, VH-OUS and Robinson R44 Raven, VH-ZDP, 54 km north-north-west of Gascoyne Junction, Western Australia, on 13 February 2008

Interim report

Interim factual report released 11 November 2008

On 13 February 2008, a Piper Aircraft Corporation Super Cub aeroplane and a Robinson Helicopter Company R44 Raven helicopter collided in midair during feral goat culling operations. The aeroplane impacted the ground at a steep angle, fatally injuring the two occupants. The helicopter, though damaged, was safely landed.

Preliminary report

Preliminary report released 20 March 2008

On 13 February 2008, a Piper Aircraft Corporation Super Cub aeroplane and a Robinson Helicopter Company R44 Raven helicopter collided in midair during feral goat culling operations. The aeroplane impacted the ground at a steep angle, fatally injuring the two occupants. The helicopter, though damaged, was safely landed.

Summary

On 13 February 2008, a Piper Aircraft Corporation PA-18 Super Cub aircraft and a Robinson Helicopter Company R44 Raven helicopter were engaged in feral goat culling operations in the Kennedy Range National Park, WA.

The two aircraft collided in mid-air as the pilot of the helicopter executed a climbing left turn that brought the two aircraft into close proximity. The pilot and shooter occupants of the R44 were aware that the Super Cub was approaching them at the same height, and the helicopter pilot was aware of the position of the aeroplane during the helicopter's climbing turn, but it appeared probable that the pilot and spotter occupants of the Super Cub did not see the helicopter.

The helicopter's main rotor blades struck the Super Cub's right wing, severing the lift struts. The right wing detached in flight, and the Super Cub fell to the ground. The pilot and spotter were fatally injured. The helicopter was able to land safely.

The investigation determined that the occupants of the Super Cub were probably unaware of the proximity of the R44, and that the R44 pilot did not recognise the collision hazard until there was insufficient time to prevent contact with the Super Cub.

The investigation also identified that there were no formalised operating procedures detailing the conduct of culling operations involving multiple aircraft that may have assisted in the maintenance of aircraft separation.

In response to this accident, a number of safety actions were undertaken by the R44 and Super Cub operators. In addition, extensive safety action was carried out by the WA Government departments that were involved in the operation. That included in the areas of risk management, the review and amendment of guidelines and procedures affecting multiple aircraft operations, the adoption of Safety Management Systems, and the provision of training for departmental personnel.

Inquest

Response to Gascoyne Junction Inquest Findings

On Friday 5 July 2013 the Western Australian (WA) State Coroner released the findings of his investigation into a 2008 fatal Piper Super Cub mid-air collision with a Robinson R44 helicopter 53km north-north-west of Gascoyne Junction. The Australian Transport Safety Bureau (ATSB) has reviewed the Coroner’s findings and reaffirms the safety factors identified by its own investigation. The ATSB’s report was released on 26 June 2009.

ATSB Report

Circumstances of the Accident:

On 13 February 2008, a Piper Aircraft Corporation PA-18 Super Cub aircraft and a Robinson Helicopter Company R44 Raven helicopter were engaged in feral goat culling operations in the Kennedy Range National Park, WA. The operation was initiated by the WA Department of Environment and Conservation (DEC) who contracted the Department of Agriculture and Food, WA (DAF) to assist.

The two aircraft collided in midair as the pilot of the helicopter executed a climbing left turn that brought the two aircraft into close proximity. The pilot and shooter occupants of the R44 were aware that the Super Cub was approaching them at the same height, and the helicopter pilot was aware of the position of the aeroplane during the helicopter's climbing turn, but it appeared probable that the pilot and spotter occupants of the Super Cub did not see the helicopter.

The ATSB found that the Super Cub climbed up and through the disk formed by the helicopter’s rotor blades. The helicopter's main rotor blades struck the Super Cub's right wing, severing the lift struts. The right wing detached in flight, and the Super Cub fell to the ground. The pilot and spotter were fatally injured. The helicopter was able to land safely.

Safety Factors and Key Findings:

In its Final Report the ATSB found the following contributing safety factors:

  • At about the time the two aircraft passed each other, the R44 pilot initiated a climbing left turn that resulted in the two aircraft coming into close proximity;
  • The Super Cub occupants were probably unable to see the R44 during the period beginning at or about the time the helicopter commenced the climbing left turn until the collision;
  • There was no alerting radio call to advise the Super Cub occupants of the R44 position and intentions;
  • Only the R44 pilot was aware of the relative position of the two aircraft;
  • The Super Cub pilot’s manoeuvre resulted in the two aircraft converging;
  • The R44 pilot did not recognise the collision risk until there was insufficient time to prevent contact with the Super Cub;
  • There were no formalised operating procedures detailing the conduct of multiple aircraft culling operations, including the assurance of aircraft separation that would have assisted the pilots maintain separation from each other [safety issue]. 

The ATSB also made a key finding that:

  • The R44 pilot’s work schedule was unlikely to have resulted in work-induced fatigue leading to a significant performance decrement in his ability to operate the helicopter.

Coroner’s Findings

How the accident occurred:

The coroner found that at impact the R44 was rising up into the Super Cub.

The Coroner based this finding on the recollection of the shooter in evidence. In his evidence, the shooter stated that the Super Cub was higher than the R44 as the aircraft passed each other prior to the collision. The Coroner did not consider the ATSB scenario of events likely.

ATSB response:

The ATSB acknowledges the grounds for the Coroner’s finding while reaffirming its assessment that the wing of the Super cub climbed up and passed through the main rotor blade disk of the R44. The ATSB’s assessment was based on the following grounds:

  • The account of the circumstances prior to the collision given by the R44 pilot to the ATSB following the accident. The shooter did not assert that the Super Cub passed higher than the R44. He advised the ATSB that he “recalled last seeing the Super Cub pass to his left at a lower altitude before his attention was diverted inside the helicopter by the movement of the ammunition container” (see ATSB Final Report p.3);
  • The relative bank and pitch between the two aircraft at impact were derived from physical evidence of the contact. The ATSB maintains that the Supercub and the R44 were aligned on a very similar plane at the time of the collision.

Fatigue

The Coroner found that ‘fatigue must have played a significant role’ in both the R44 and Super Cub pilots decision making to allow the aircraft to come into close proximity.

ATSB response

The ATSB reaffirms its finding that:

The R44 pilot’s work schedule was unlikely to have resulted in work-induced fatigue leading to a significant performance decrement in his ability to operate the helicopter.

As part of its investigation the ATSB undertook a fatigue analysis of the R44 pilot. That involved analysing the R44 pilot’s hours worked and his reported rest over the fortnight preceding the accident and on the day of the accident flight. The analysis included examining the pilot’s work and rest periods on the day of the accident using two separate, internationally-accepted bio-mathematical fatigue modelling software programs (FAID and FAST).1

The ATSB was not able to conduct a similar assessment on the Super Cub pilot but it was reported that his workload in the period leading up to the accident was similar to that of the R44 pilot.

Coroner Recommendations: 

The Coroner did not make any recommendations directed toward the ATSB; however the ATSB notes the following recommendations by the Coroner:

  1. That both DEC and DAF put in place guidelines in respect of aerial work which would specifically cover feral animal culling, to ensure that there is at least a 500 foot vertical buffer between spotter and shooter aircraft in addition to any horizontal buffer.
  2. DEC and DAF take action to ensure that ongoing consideration is given to possible use of available anti-collision systems and particularly the FLARM system.

It is not a matter for the ATSB to provide a response to these recommendations. The ATSB considered that the safety issue arising out of this accident that needed to be addressed was the lack of formalised operating procedures detailing the conduct of multiple aircraft culling operations, including the assurance of aircraft separation that would have assisted the pilots maintain separation from each other.

The ATSB report at pp. 29 to 30 details the actions taken or that were planned to be taken in relation to this issue by the:

  • R44 Operator;
  • Super Cub Operator;
  • WA DEC; and
  • DAF WA.

ATSB Investigations and Coronial Inquiries

Inquests are separate to ATSB investigations. The Coroner formulated his findings and recommendations independently of the ATSB. The ATSB cannot speak for the Coroner’s findings. However, the ATSB supports the coronial process and in the interests of ensuring that safety information is made available to the broadest audience the ATSB is making this publication.

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

__________________

1 See www.faidsafe.com and  www.fatiguescience.com 

Occurrence summary

Investigation number AO-2008-010
Occurrence date 13/02/2008
Location Kennedy Range National Park
State Western Australia
Report release date 26/06/2009
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Airborne collision
Occurrence class Accident
Highest injury level Fatal

Aircraft details

Manufacturer Robinson Helicopter Co
Model R-44
Registration VH-ZDP
Serial number 1246
Sector Helicopter
Operation type Aerial Work
Departure point Gascoyne Junction (ALA)
Destination Gascoyne Junction (ALA)
Damage Substantial

Aircraft details

Manufacturer Piper Aircraft Corp
Model PA-18-150
Registration VH-OUS
Serial number 18-7881
Sector Piston
Operation type Aerial Work
Departure point Gascoyne Junction (ALA)
Destination Gascoyne Junction (ALA)
Damage Destroyed

Engine failure – Jabiru, Northern Territory, on 11 February 2008, VH-VAZ, Beech Aircraft 1900

Interim report

Interim Factual report released 22 August 2008

On 11 February 2008 at about 0720 Central Standard Time, following take-off from runway 27 at Jabiru Airport, NT, a Beech Aircraft Corporation 1900D, registered VH-VAZ, sustained an auto-feather of the left propeller and subsequent left engine failure.

The aircraft was being operated on a charter flight to Darwin with two pilots and a passenger on board. The pilots reported that, following the engine failure, they completed a single-engine circuit and landing at Jabiru. Subsequent examination of the left engine revealed catastrophic internal damage to the power section of the engine.

Summary

On 11 February 2008, at about 0720 Central Standard Time, following take-off from runway 27 at Jabiru Airport, NT, a Beech Aircraft Corporation 1900D, registered VH-VAZ, sustained an auto-feather of the left propeller and subsequent left engine failure.

The aircraft was being operated on a charter flight to Darwin with two pilots and a passenger on board. The pilots reported that, following the engine failure, they completed a single-engine circuit and landing at Jabiru. Subsequent examination of the left engine revealed catastrophic internal damage to the power section of the engine. The initiator of the damage was the release of a power turbine second-stage blade. Metallurgical examination determined that the failure of the second-stage turbine blade had occurred as a consequence of the initiation and growth of a high-cycle fatigue cracking mechanism from the downstream trailing corner of the blade fir-tree root post. At the time of blade fracture, approximately 25% of the root cross-section had been compromised by fatigue cracking.

The investigation found that during the most recent overhaul of the engine, the overhaul facility did not comply with the engine manufacturer's service bulletin regarding second-stage turbine blade replacement. Consequently, outdated blades were installed.

Occurrence summary

Investigation number AO-2008-008
Occurrence date 11/02/2008
Location Jabiru Airport
State Northern Territory
Report release date 15/07/2009
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 Incident
Highest injury level None

Aircraft details

Manufacturer Beech Aircraft Corp
Model 1900
Registration VH-VAZ
Serial number UE-115
Sector Turboprop
Operation type Charter
Departure point Jabiru, NT
Destination Darwin, NT
Damage Nil