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Qantas 32

Printed page 5. PDF page 25.

for a progressive descent to 4,000 ft. The captain set engines No. 1 and 4 to provide symmetrical thrust, and controlled the aircraft's speed with thrust from No. 3 engine. Following the engine failure and subsequent system damage, the autopilot

Open 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