(a) It must be shown by operation tests that when portions of the control system subject to pilot effort loads are loaded to 80 percent of the limit load specified for the system and the powered portions of the control system are loaded to the maximum load expected
CFR 14-25.683-2014由US-CFR-file 发布于 2014-10-02,并于 2014-10-02 实施。
CFR 14-25.683-2014 在中国标准分类中归属于: V35 航空器及其附件综合。
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