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Printed page 16. PDF page 24.
resulted in a vibration in the engine that caused deterioration to some air seals, allowing oil to leak directly into the engine. The resulting low oil pressure in the left engine caused the caution light to illuminate. The combustion ofOpen final report at PDF page 24ATR72-600, ZK-MVL Engine fire and evacuation Wellington 1 September 2024
Printed page 30. PDF page 38.
resulted in a vibration in the engine that caused deterioration to some air seals, allowing oil to leak directly into the engine. 4.2. It is virtually certain that the fire was extinguished shortly after the second fire-agent bottle was discharged.Open final report at PDF page 38ATR72-600, ZK-MVL Engine fire and evacuation Wellington 1 September 2024
Printed page 149. PDF page 169.
Branch, established that the occurrence was directly related to the fatigue cracking of an oil feed stub pipe within the No.2 engine's HP/IP bearing support structure. The ATSB identified the following safety issue: Safety issue Misaligned stub pipe counter-boring isOpen 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