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Printed page 16. PDF page 24.
increasing the risk of other similarly faulty turbine blades re-entering service. 3.4. The engine fire warning was initiated by a failure of an LPT blade, which resulted in a vibration in the engine that caused deterioration to some air seals,Open final report at PDF page 24ATR72-600, ZK-MVL Engine fire and evacuation Wellington 1 September 2024
Printed page 20. PDF page 28.
informed the crew when 30 seconds had elapsed. The crew confirmed there was still an engine fire warning light and so discharged the second fire-agent bottle in accordance with the memory checklist. 3.27. The engine fire warning light remained illuminatedOpen final report at PDF page 28ATR72-600, ZK-MVL Engine fire and evacuation Wellington 1 September 2024
Printed page 30. PDF page 38.
4 Findings Ng kitenga 4.1. The engine fire warning was initiated by a failure of a low-pressure turbine blade, which resulted in a vibration in the engine that caused deterioration to some air seals, allowing oil toOpen final report at PDF page 38ATR72-600, ZK-MVL Engine fire and evacuation Wellington 1 September 2024
Printed page 26. PDF page 46.
area (zone 1). It is likely that the rear fire detector in zone 1 triggered the No. 2 engine fire warning. Although the temperature in zone 1 levelled out then slowly decreased when the thrust levers were returned to idle,Open official document at PDF page 46ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010
Printed page 1. PDF page 9.
with four crew and 70 passengers on board. On approach to land at Wellington the left engine caught fire. The crew landed the aeroplane safely, stopping on the runway, and then discharged fire suppressant into the engine area. 1.2. WhileOpen final report at PDF page 9ATR72-600, ZK-MVL Engine fire and evacuation Wellington 1 September 2024
Printed page 41. PDF page 61.
warning and extinguishing systems. Following a UERF event, the fire warning systems of all engines should continue to be operational and the extinguishing systems of the remaining engines should also remain operational. Flammable fluid shut-off valve. The guidance identifieOpen official document at PDF page 61ATSB AO-2010-089: In-flight uncontained engine failure, Airbus A380-842 VH-OQA, overhead Batam Island, 4 November 2010