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Printed page 1. PDF page 21.
retracted the landing gear and flaps and changed the thrust setting to climb. At about 02:01, while maintaining 250 kt in the climb and passing 7,000 ft above mean sea level (AMSL), the crew heard two, almost coincident ‘loud bangs'.Open official document at PDF page 21ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 24. PDF page 44.
engine fire detectors were in zone 1 (the fan casing). The recorded data showed that at 02:01:52 the No. 2 engine thrust lever was advanced (Figure 21). There were increases in the zone 1 temperature that followed further thrust leverOpen official document at PDF page 44ATSB 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.
Actual time Time sequence Comment (UTC) hh:mm:ss 02:01:01 -6 sec No. 2 engine HP turbine vibrations peak in 76 amplitude and the N1 and N2 drop by about 1%. N3 in the No. 2 engine increases by about 3% andOpen 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 75. PDF page 95.
Figure 54: Graphical representation of engine data from 02:00:00 to 02:01:30 - 75 -Open official document at PDF page 95ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 76. PDF page 96.
Figure 55: Graphical representation of engine data from 02:00:00 to 02:01:30 - 76 -Open official document at PDF page 96ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 77. PDF page 97.
Figure 56: Graphical representation of engine data from 02:01:00 to 02:04:00 - 77 -Open official document at PDF page 97ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010