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作 者:陈惠蓉[1] CHEN Huirong(Shenzhen Airlines LTD.,Shenzhen 518000,Guangdong,China)
出 处:《民航学报》2024年第1期38-41,共4页Journal of Civil Aviation
摘 要:本文阐述了影响飞机起飞性能的因素以及制作起飞一发失效应急程序的意义和目的,简述了起飞一发失效应急程序总体设计方案和思路,分析了起飞一发失效应急程序设计过程中的重点和难点,包括决策点的选取、转弯航迹控制以及越障评估的要求等。指出了行业内起飞一发失效应急程序应用方式,包括机组手动打点或者导入机载导航数据库方式,以及使用两种应用方式所需关注的问题。最后,提出了着陆过程中一发失效复飞路径超障评估的必要性和评估思路,针对进近图中的复飞梯度,提出梳理机型着陆复飞爬升梯度,与进近图中复飞梯度比对的方法,以验证飞机着陆复飞性能是否满足进近图复飞梯度的要求。In this paper,the factors that affect aircraft take-off performance are elaborated as well as the significance and purpose of engine-out standard instrument departure procedure(EOSID).The overall design scheme and ideas of EOSID are sketched,and the key points and difficulties in the process of the EOSID design are analyzed,including the selection of decision points,turning track control and obstacle clearance requirements.The application methods of EOSID in the civil aviation industry,including manual input to MCDU by flight crew and importing to the navigation database of aircraft,are mentioned as well as the problems that need to be concerned about for the two application methods.Finally,the necessity and evaluation ideas of obstacle clearance assessment for one engine-out go around during landing are elaborated.In view of the go-around gradient in the approach chart,it is proposed to verify whether an aircraft's landing climb performance meets the requirements of the go-around gradient in the approach chart by obtaining the landing climb gradient of the aircraft and comparing it with the go-around gradient in the approach chart.
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