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探讨了民用直升机在持续适航阶段为满足特殊用途而进行的重要改装设计的适航性问题。着重论述了直升机重要改装设计的适航符合性验证方法。
This paper discusses the airworthiness of civil helicopters in the important modification design for special purpose during the continuous airworthiness phase. Emphatically discusses the airworthiness conformity verification method of helicopter important retrofit design.