(a) If certification for flight in icing conditions is sought, in addition to the requirements of § 25.1419, an airplane with a maximum takeoff weight less than 60,000 pounds or with reversible flight controls must be capable of operating in accordance with paragraphs (a)(1), (2), or (3), of this section.
CFR 14-25.1420-2014由US-CFR-file 发布于 2014-11-04,并于 2014-11-04 实施。
CFR 14-25.1420-2014 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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