民用飞机设计与研究
民用飛機設計與研究
민용비궤설계여연구
CIVIL AIRCRAFT DESIGN AND RESEARCH
2015年
1期
6-10,71
,共6页
构型偏离清单%飞机性能%适航审定
構型偏離清單%飛機性能%適航審定
구형편리청단%비궤성능%괄항심정
Configuration Deviation List ( CDL)%aircraft performance%airworthiness certification
参考美国FAA咨询通告AC 25-7 C、EASA可接受符合方法AMC 25.1581和某机型的资料，对构型偏离清单相关项目的性能影响计算和验证方法进行研究，以获得既满足适航要求又较合理的性能折算数据。
參攷美國FAA咨詢通告AC 25-7 C、EASA可接受符閤方法AMC 25.1581和某機型的資料，對構型偏離清單相關項目的性能影響計算和驗證方法進行研究，以穫得既滿足適航要求又較閤理的性能摺算數據。
삼고미국FAA자순통고AC 25-7 C、EASA가접수부합방법AMC 25.1581화모궤형적자료，대구형편리청단상관항목적성능영향계산화험증방법진행연구，이획득기만족괄항요구우교합리적성능절산수거。
With reference to FAA AC 25-7C, EASA AMC 25. 1581 and the material of some aircraft,this paper studies the method of calculation and validation for the performance degradation relative to configuration deviation list items. Some examples of analysis procedure to the typical items are presented. Except to be satisfied with the safety requirements of airworthiness rules performance degradation information developed with this method in Config-uration Deviation List ( CDL) should be reasonable and economical.
