摘要
本文基于已完成适航取证的正常类旋翼航空器,通过研究高度—温度范围补充验证的适航符合性方法,梳理受影响的适航条款,提炼出条款的核心要求,对高度—温度范围补充验证符合性方法进行总结,以期为正常类旋翼航空器高度—温度范围补充验证适航取证提供有益指导。
Based on the completed airworthiness certification of normal category rotorcraf,the airworthiness compliance method for supplementing the altitude temperature range is studied.Sorted out the affected airworthiness clauses and submitted the core requirements of the clauses.Summary of suplementary compliance methods for height temperature rang.Provide some useful guidance for expanding the altitude and temperature range of normal category wing aircraft for airworthiness certification.
作者
门亮
MEN liang(Aviation Industry Helicopter Design and Research Institute,Jingdezhen Jiangxi 333001)
出处
《中国科技纵横》
2025年第2期56-58,共3页
China Science & Technology Overview
关键词
正常类旋翼航空器
高度温度
符合性方法
normal category rotorcraft
height-tmperature
compliance method
