No fatalities

2015-05-15: Airbus A319-132 (VH-VCJ) — 25 km N Melbourne Airport, Victoria

25 km N Melbourne Airport, Victoria

On May 15, 2015, an Airbus A319-132 (registration VH-VCJ) was involved in an aviation accident near 25 km N Melbourne Airport, Victoria. No fatalities were reported. Investigators recorded the probable cause as: These findings should not be read as apportioning blame or liability to any particular organisation or individual. Safety issues, or system problems, are highlighted in bold to emphasise their importance. This summary draws on records from the Australian Transport Safety Bureau (ATSB).

Sourcesthe Australian Transport Safety Bureau (ATSB)Primary reportUpdated 1779791586Data APIEditorial standards
Aircraft registered VH-VCJ
Aircraft registered VH-VCJ. Photo: Bidgee / CC BY-SA 3.0 au, via Wikimedia Commons

On 15 May 2015, a Skytraders Airbus A319 descended to about 2,200 ft during an arrival procedure, below the ATC-assigned 3,000 ft, triggering TAWS and MSAW alerts and exceeding flap speed limits.

Incident Overview

On 15 May 2015, a Skytraders Airbus A319 was conducting an arrival procedure prior to commencing an approach into Melbourne, Victoria. During the procedure, the aircraft descended to approximately 2,200 ft, which was below the air traffic control (ATC)-assigned altitude of 3,000 ft. The crew subsequently broke off the arrival procedure and climbed to the new ATC-cleared altitude of 5,000 ft before returning to land at Melbourne.

Warning Systems Activation

During the descent below 3,000 ft, the aircraft's Terrain Avoidance and Warning System (TAWS) initiated a number of warning alerts. Additionally, the speed limit for the aircraft flaps was exceeded, and the Minimum Safe Altitude Warning System (MSAW) generated an alert to the ATC controller.

Key Sequence of Events

Critically, during a 26-second period starting from when the pilot flying (PF) pressed the instinctive disconnect pushbutton on the thrust levers to when the aircraft reached its minimum altitude, the aircraft descended just over 1,000 ft and increased speed by approximately 100 kt.

Causal Factors

The event was initiated by an inadvertent switch selection by the PF. This was followed by a combination of errors, rapidly changing events, high workload, and an apparent response to a pitch-up illusion. These factors resulted in the aircraft quickly developing a very high rate of descent and increasing airspeed.