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Printed page 2. PDF page 22.
second monitoring period. As part of the turbine overheat procedure, the crew elected to shut down the No. 2 engine. During the shutdown procedure, the ECAM displayed a message indicating that the No. 2 engine had failed. A damage assessmentOpen official document at PDF page 22ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 84. PDF page 104.
to increase, until at 02:02:20 the engine surged again. At 02:03:21, the flight crew shut down the No. 2 engine. - 84 -Open official document at PDF page 104ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page xii. PDF page 14.
large quantities of water and foam below the left wing while the aircraft's engines were shut down. The No. 1 (outer left) engine continued to run following the normal shut-down procedure. Because of the still-running engine and leaking fuel onOpen official document at PDF page 14ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 73. PDF page 93.
engine thrust lever reduced to idle. 02:03:21 +2 min 14 sec No. 2 engine high pressure shut-off valve closed and engine shutdown. 76 The vibrations were below the triggering threshold for ECAM notification. - 73 -Open official document at PDF page 93ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 218. PDF page 238.
Centralised Aircraft Monitoring (ECAM) system displayed messages that required the crew to shut down the Green hydraulic system by disconnecting the No. 1 and 2 engine-driven hydraulic pumps. However, the wiring damage prevented the No. 2 engine hydraulic pumps fromOpen official document at PDF page 238ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 231. PDF page 251.
as commanded when the crew attempted to shut down that engine. The investigation was unable to determine why that fire bottle did not function. Table B7: Fire extinguishing system - bottle discharge status and the electricalOpen official document at PDF page 251ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010