运输类飞机适航标准25.785(b)(d)要求及符合性验证研究
Study of the requirements and compliance verification of 25.785(b)(d)
毛文懿 1李琪 1李杰1
作者信息
- 1. 上海飞机设计研究院,上海 201210
- 折叠
摘要
CCAR25.785(b)(d)条款要求运输类飞机的设计能够保护乘员在遭受应急着陆惯性力等情况时不受到严重伤害.通过对FAA相关咨询通告和审定政策备忘录的研究,结合符合性验证工作实践,完成了对条款 25.785(b)(d)要求的解析和对条款符合性验证考虑的梳理,形成了对条款 25.785(b)(d)的符合性验证方法建议,可为运输类飞机针对条款 25.785(b)(d)的适航性设计和符合性验证提供参考.
Abstract
25.785(b)(d)requires that transport category aircraft be designed to protect occupants from serious in-jury when subjected to emergency landing inertial forces.Based on the study of the relevant advisory circular and certification policy memorandum of FAA,combined with the compliance verification practice,this paper has com-pleted the analysis of the requirements of 25.785(b)(d)and sorted out of the consideration of compliance verifica-tion of 25.785(b)(d),and formed the means of compliance of 25.785(b)(d).It can be used as a reference for the design and compliance verification of transport category aircraft with respect to 25.785(b)(d).
关键词
CCAR/25.785(b)(d)/适航/符合性方法Key words
25.785(b)(d)/airworthiness/means of compliance引用本文复制引用
出版年
2024
NETL
NSTL
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