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Printed page 7. PDF page 27.
that the No. 2 engine sustained an uncontained failure in the turbine region and that debris from the engine damaged the airframe and systems. -7-Open official document at PDF page 27ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 10. PDF page 30.
vertical and horizontal stabilisers contained numerous indentations and score marks from debris impacts. Further information on the airframe damage is contained in Appendix B. System effects The debris from the engine failure directly damaged a number of systems and aOpen official document at PDF page 30ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 161. PDF page 181.
the aircraft electrical system (feeder cables) were damaged from the liberated engine debris, the No. 2 generator line contactor (GLC2) physically opened in order to isolate the Primary Electrical Power Distribution Center (PEPDC) from potential damage (that is, from shoOpen official document at PDF page 181ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 199. PDF page 219.
door 2 left to the horizontal stabiliser, had impact damage from engine and airframe debris. Although the debris did not penetrate through the fuselage skin, that damage was considered significant and required repair prior to further flight. Centre fuselage -Open official document at PDF page 219ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 202. PDF page 222.
horizontal stabiliser leading edge (Figure B26) was damaged from engine and airframe debris at five locations along the leading edge (scratches, gouges and dents). Damage at that location required repair prior to flight. Figure B26: Trimmable Horizontal Stabiliser leadiOpen official document at PDF page 222ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 208. PDF page 228.
Aircraft systems System effects - wiring damage The debris from the engine failure directly damaged a number of systems, which in turn affected a number of other systems. Although some systems sustained direct mechanical damage, most ofOpen official document at PDF page 228ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010