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Qantas 32

Printed page 150. PDF page 170.

Rolls-Royce in response to the safety recommendation On 2 December 2010 Rolls-Royce issued Revision 1 to NMSB 72-G595. This revision incorporated assessment and engine rejection criteria for the measurement of potential counter bore misalignments, and in particular, a tighten
Open official document at PDF page 170ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010

Qantas 32

Printed page 148. PDF page 168.

relevant module according to an agreed programme. On 18 November 2010, Rolls-Royce issued Revision 2 of NMSB 72-AG590, detailing further Trent 900 engine inspections, including for defects in a number of turbine area oil and air feed pipes. 7.1.3 Airbus
Open 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

Qantas 32

Printed page 149. PDF page 169.

2010 by AD 2010-0242-E that incorporated the contents of Rolls-Royce NMSB 72-AG590 (Revision 2). AD 2010-0242-E is available at: http://ad.easa.europa.eu/ad/2010-0242-E 7.1.5 Australian Transport Safety Bureau On 30 November 2010 the ATSB had, in close consultation wit
Open official document at PDF page 169ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010

Qantas 32

Printed page 283. PDF page 303.

Rolls-Royce Non-modification service bulletins (NMSB) 72-G589, 72-AG590, 72- AG590 (Revision 2), 72-G595 & 73-AG639 Rolls-Royce RB211-Trent 900 Line and Base Maintenance training guide Rolls-Royce Summary Failure Modes, Effects and Criticality Analysis (FMECA) for the
Open official document at PDF page 303ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010