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基于对咨询通告(AC)25.571-1D和可接受的符合性方法(AMC)25.571的对比分析,讨论了美国联邦航空管理局和欧洲航空安全局在结构损伤容限与疲劳评定上适航要求和适航符合性验证方法上的区别,包括条款要求、结构分类、试验要求和检查间隔等问题。
Based on a comparative analysis of Advisory Circular (AC) 25.571-1D and Acceptable Compliance Method (AMC) 25.571, discussions were made on the requirements of the Federal Aviation Administration and the European Aviation Safety Agency for airworthiness requirements for structural damage tolerance and fatigue assessment and Differences in airworthiness conformity verification methods, including requirements for clauses, structural classifications, test requirements and inspection intervals.