摘要
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。
The potential airworthiness limitation items candidates are identified according to the failure impact that could affect the structural integrity necessary for the safety of the aircraft. The airworthiness limitation items selection criterion is established based on the inspection threshold and repeat inspection interval, whose determining approach is derived from the calculated service life of the structural candidates.
出处
《民用飞机设计与研究》
2016年第4期17-19,23,共4页
Civil Aircraft Design & Research
关键词
持续适航
结构适航限制项目
检查门槛值
重复检查间隔
continued airworthiness
structural airworthiness limitation items
inspection threshold
repeat inspection interval