摘要
CCAR25中条款CCAR25.963(d)要求机身内的燃油箱不会因受到应急着陆情况下的惯性力作用破裂并导致燃油的泄漏。本文件研究了适航条款CCAR25.963(d)、14CFR25.963(d)和CS25.963(d)之间的要求差异,提出了条款CCAR25.963(d)建议的符合性方法和验证思路,为运输类飞机的符合性验证提供参考。
CCAR25.963 requires fuel tanks within the fuselage contour must be able to resist rupture and to retain fuel, under the inertia forces in emergency landing conditions. This paper studied the differences between CCAR25.963（d）14 CFR25.963（d） and CS25,963（d）, and gave suggestions about the compliance methods and Means of Compliances for CCAR25.963（d）. It provides guidances to transport category airplanes on compliance verification.
出处
《航空科学技术》
2013年第3期21-23,共3页
Aeronautical Science & Technology
