Accident Piper PA-31 Navajo VH-UFO,
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ASN Wikibase Occurrence # 697
 
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Date:Tuesday 20 July 1993
Time:15:46
Type:Silhouette image of generic PA31 model; specific model in this crash may look slightly different    
Piper PA-31 Navajo
Owner/operator:Private
Registration: VH-UFO
MSN: 31-7712060
Fatalities:Fatalities: 1 / Occupants: 1
Aircraft damage: Destroyed
Category:Accident
Location:18 km NW Brisbane, QLD -   Australia
Phase: Initial climb
Nature:Private
Departure airport:Archerfield, Brisbane, Queensland (BNE/YBAF)
Destination airport:Caboolture, Queensland (YCAB)
Investigating agency: BASI
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The aircraft, with only the pilot on board, was being flown on July 20 1993 from Archerfield to Caboolture, via the light aircraft lane to the west of Brisbane, in company with another aircraft.

About five minutes after departing Archerfield, the pilot radioed that he was experiencing problems with both engines and that he was in an emergency situation. The pilot of the other aircraft advised him that there were suitable forced landing areas in and around a nearby golf course.

However, the aircraft continued and slowly lost altitude before rolling inverted and diving steeply into the ground 18 Km north-west of Brisbane. Ground witnesses reported hearing loud backfiring and fluctuating engine RPM from the aircraft. These sounds were accompanied by erratic rolling and yawing of the aircraft before it rolled to the left and inverted.

The right wing was severed outboard of the engine as the aircraft impacted a large tree before crashing onto a road. Wreckage examination revealed that the fuel selectors for both engines were set at the auxiliary tank positions, causing fuel for each engine to be drawn from the corresponding auxiliary tank in each wing.

It was established that the aircraft had been refuelled to full main tanks prior to the flight. Further, the pilot had advised in a telephone conversation with an engineer before the flight that the contents of both auxiliary tanks was 60 litres or less. All fuel tanks except the left auxiliary tank were ruptured during the impact sequence. About one litre of fuel was recovered from this
tank.

Examination of the aircraft engines indicated that the right engine was under power at impact while the left engine was not. The mechanical condition of the engines indicated that they were capable of normal operation

ATSB Conclusions:
1. The pilot did not use a written checklist.
2. The pilot operated the aircraft with the auxiliary tanks selected when the fuel contents of these tanks was low.
3. The pilot failed to conduct a forced landing

Accident investigation:
cover
  
Investigating agency: BASI
Report number: 
Status: Investigation completed
Duration:
Download report: Final report

Sources:

1. http://www.atsb.gov.au/publications/investigation_reports/1993/aair/aair199302151.aspx
2. http://www.atsb.gov.au/media/24235/ASOR199302151.PDF

Revision history:

Date/timeContributorUpdates
21-Jan-2008 10:00 ASN archive Added
06-May-2014 03:46 Dr. John Smith Updated [Time, Cn, Operator, Total fatalities, Total occupants, Other fatalities, Location, Phase, Nature, Departure airport, Destination airport, Source, Damage, Narrative]

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