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Printed page 143. PDF page 163.
experience with other engines in the Trent family, with the result that the IP turbine disc accelerated to a rotational speed in excess of its design capacity whereupon it burst in a hazardous manner. [Safety issue] 6.1.2 Manufacture and releaseOpen official document at PDF page 163ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 151. PDF page 171.
experience with other engines in the Trent family, with the result that the IP turbine disc accelerated to a rotational speed in excess of its design capacity whereupon it burst in a hazardous manner. Action taken by Rolls-Royce On 3Open official document at PDF page 171ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 131. PDF page 151.
The IP turbine disc moved rearwards and the engine surged. Within 4 seconds, the disc accelerated, and while the engine was running down from the surge, the HP system partially recovered, supplying additional energy to the IP turbine disc, allowingOpen official document at PDF page 151ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010