正常类飞机CCAR23.2205符合性验证方法分析OA

To promote the compliance verification work of the airworthiness requirement CCAR23.2205"Interactions between Systems and Structures"for normal category aircraft,a set of compliance verification methods for the"Interactions between Systems and Structures"requirement have been developed based on the domestic aircraft strength design work.The methods include five specific steps:filtering of failure types,evaluation of system performance under normal conditions,evaluation of system performance under failure conditions,indication of system failure and dispatch of aircraft under failure conditions.This method provides a detailed explanation of the compliance verification approach and the necessary computational analysis work to be carried out in each step,which provides some inspiration for the verification of airworthiness clause compliance of normal aircraft structural strength specialty.