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按破坏是否对飞机安全必需的结构完整性产生影响,对潜在的适航限制项目候选项进行分类。给出通过计算候选项目的寿命得到检查门槛值和重复检查间隔的方法,以及基于检查门槛值、重复检查间隔确定结构适航限制项目的原则。
Depending on whether the damage affects the structural integrity necessary for the safety of the aircraft, potential airworthiness constraints candidates are classified. The method of obtaining inspection thresholds and repeated inspection intervals by calculating the lifetimes of candidate items and the principle of determining the structural airworthiness restriction items based on inspection thresholds and repeated inspection intervals are given.