(a) The landing gear system must be designed so that when it fails due to overloads during takeoff and landing, the failure mode is not likely to cause spillage of enough fuel to constitute a fire hazard. The overloads must be assumed to act in the upward and aft directions in combination with side loads acting inboard and outboard. In the absence of a more rational analysis, the side loads must be assumed to be up to 20 percent of the vertical load or 20 percent of the drag load, whichever is greater.
CFR 14-25.721-2014由US-CFR-file 发布于 2014-10-02,并于 2014-10-02 实施。
CFR 14-25.721-2014 在中国标准分类中归属于: V35 航空器及其附件综合。
非常抱歉,我们暂时无法提供预览,您可以试试: 免费下载 CFR 14-25.721-2014 前三页,或者稍后再访问。
点击下载后,生成下载文件时间比较长,请耐心等待......
Copyright ©2007-2022 ANTPEDIA, All Rights Reserved
京ICP备07018254号 京公网安备1101085018 电信与信息服务业务经营许可证:京ICP证110310号