Critical Design Configuration Control Limitations (CDCCL)
Critical Design Configuration Control Limitations (CDCCL) : An AL that preserves a critical feature of the airplane needed for the FRM or IMM to perform their intended function and prevent the occurrence of an unsafe condition. The purpose of the CDCCL is to provide instructions to ensure these critical features are present throughout the life of the airplane, e.g., when alterations, repairs, or maintenance actions occur
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