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研究了CCAR25.683条款的要求和条款制定背景,对CCAR25部、FAR25部和CS25部中25.683条款差异进行了分析,研究了针对25.683条款要求可接受的验证方法,结合电传飞控系统的设计特征提出了为满足25.683条款要求所需采取的验证方法和具体验证工作。
The background and requirements of CCAR25.683 are studied. The differences of 25.683 clauses in CCAR25, FAR25 and CS25 are analyzed. The acceptable verification method for the requirements of Clause 25.683 is studied. Combined with the design of fly-by-wire system, Features The validation methods and validation required to meet the requirements of Section 25.683 are presented.