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Printed page 26. PDF page 34.
3.56. Despite this, over half the passengers took their baggage with them. The Commission 3.57. identified a number of possible reasons for this, including: � not recalling the before-take-off safety briefOpen final report at PDF page 34ATR72-600, ZK-MVL Engine fire and evacuation Wellington 1 September 2024
Printed page 11. PDF page 19.
technical analyst, acting on behalf of the Commission's TSB Accredited Representative, oversaw the teardown examination by P&WC. A representative from the operator was also present. 2.38. The examination found the No. 6 and No. 7 engine centreline bearing housings wereOpen final report at PDF page 19ATR72-600, ZK-MVL Engine fire and evacuation Wellington 1 September 2024
Printed page 22. PDF page 30.
States and Europe have shown that in a post-crash fire, conditions are conducive to flashover34 after 90 s. The likelihood of survival reduces significantly after this time. Use of only half of the exits simulates the potential for failed evacuationOpen final report at PDF page 30ATR72-600, ZK-MVL Engine fire and evacuation Wellington 1 September 2024
Printed page 233. PDF page 253.
air. Recorded data showed that after the failure, the aircraft levelled at 7,400 ft. Over a 70-minute period, it completed nine orbits over the ocean before commencing a descent into Singapore. During the descent, the flaps extended at half theOpen official document at PDF page 253ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010