If you wish to contribute or participate in the discussions about articles you are invited to join SKYbrary as a registered user



Semantic search

  • DH8C, vicinity Sydney Australia, 2008 (Synopsis: On 26 December 2008, a DHC8-300 being operated by Eastern Australia Airlines from Moree to Sydney made an auto ILS approach in which became de-stabilised and was continued as such until a stick shaker activation occurred.)
  • DH8D / B772, vicinity Sydney Australia, 2016 (Synopsis: On 9 December 2016, a Bombardier DHC8-400 departing Sydney lost prescribed separation against an inbound Boeing 777-200 after its crew failed to ensure that the aircraft levelled as cleared at 5,000 feet and this was exceeded by 600 feet. The Investigation found that the First Officer, as Pilot Flying, had disconnected the autopilot prior to routinely changing the selected airspeed because it tended to disconnect when this was done with altitude capture mode active but had then failed to re-engage it. The Captain's lack of effective monitoring was attributed to distraction as he sought to visually acquire the conflicting traffic.)
  • SF34, vicinity Sydney Australia, 2008 (Synopsis: On 3 November 2008, a Saab 340B being operated on a domestic passenger flight by Regional Express AL was tracking in daylight to join a 7nm final for Runway 34R at destination Sydney, when a passenger sustained minor injuries as the result of a transient encounter with turbulence that had led to a momentary loss of control of the aircraft and which was suspected as being of wake vortex origin.)
  • SF34, vicinity Sydney Australia, 2017 (Synopsis: On 17 March 2017, uncommanded engine indications on a Saab 340B en route to Sydney were followed by vibration of the right engine after which, as the crew commenced right engine shutdown, its propeller assembly separated from the engine. A PAN was declared and the flight subsequently reached Sydney without further event. The Investigation found that the propeller gearbox shaft had fractured because of undetected internal fatigue cracking in the shaft. Applicable in-service shaft inspection procedures were found to be inadequate and mandatory enhancements to these procedures have since been introduced.)