Abstract
In order to demonstrate the aircraft continued safe flight and landing after fan blade out (FBO), Sustained Engine Imbalance Particular Risk Analysis, as part of the civil aircraft safety assessment, is seriously required to implement. Under the guidance of AC25-24 “Sustained Engine Imbalance”, the specific analysis model are given, combined with engineering application experience on civil aircraft development and certification. The model and methods presented herein provide a valid approach and guidance for safety design requirements capturing in aircraft design and certification demonstration regarding Sustained Engine Imbalance.
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