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Printed page 5. PDF page 25.
(No. 2 and 3) engines only. 9 An alternative method of extending the landing gear using gravity. -5-Open official document at PDF page 25ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 32. PDF page 52.
the arrival airport. The FMS data, which included the aircraft's weight and centre of gravity, as well as the ECAM list of any system failures that affected landing performance, were automatically synchronised with the captain's and first officer's OITs. TheOpen official document at PDF page 52ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 165. PDF page 185.
information. This included the external temperature, time, aircraft weight and centre of gravity and fuel on board. The lower section displayed the ‘mailbox', which allowed the crew to communicate with air traffic control (ATC) via controller/pilot data link communicationsOpen official document at PDF page 185ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 170. PDF page 190.
messages multiple fuel system messages, including a fuel jettison fault centre of gravity messages autothrust and autoland inoperative No. 1 engine generator drive disconnected left wing pneumatic bleed leaks avionics system overheat. Manufacturer assessmentOpen official document at PDF page 190ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 225. PDF page 245.
power was not available to extend the landing gear, the crew were required to perform a gravity extension procedure. The depressurisation of the Green hydraulic system necessitated the extension of the landing gear by the flight crew using this procedure.Open official document at PDF page 245ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 228. PDF page 248.
operated to: supply fuel to the engines and APU maintain the aircraft's centre of gravity within limits reduce the structural loads on the aircraft through the load alleviation function control the refuelling and defueling of theOpen official document at PDF page 248ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010