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Printed page 5. PDF page 25.
aircraft's angle of attack. When the autopilot disconnected for the second time (at about 800 ft) the captain elected to leave it disconnected and manually fly the aircraft for the remainder of the approach. The aircraft touched down at 03:46:47Open 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 122. PDF page 142.
discovery of a manufacturing quality issue in the B-standard support struts, a 14,800 cycle life limit was applied to the B-standard assembly. The C-standard assembly had been in production since 20 March 2009 and was the current production standard atOpen official document at PDF page 142ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 148. PDF page 168.
Airbus SAS (Airbus), in response to this occurrence, released All Operators Telex A380-728002 that required all operators of A380 aircraft to comply with the engine inspection requirements of Rolls-Royce NMSB 72-G589. Airbus also issued a number of Accident Investigation TeOpen official document at PDF page 168ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 237. PDF page 257.
digital ACMS recorder The wireless digital ACMS recorder (WDAR) was a Teledyne P/N 2243800-81 unit (Figure C5) that stored a continuous record of over 1,000 different aircraft and engine system parameters. These parameters were stored in a customised format thatOpen official document at PDF page 257ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010