Civil aircraft type certification procedure requires the type applicant to submit correct, complete and traceable airworthiness compliance evidences to the certification authority, following the systematic planning and implementation of type development processes. Such evidences show the development assurance on products againstairworthiness regulation requirements. Based on the Vee model theory of the system engineering, this paper chooses the development planning and assurance loop and development process loop as two core routines to identifythe interfaces of evidence system with the configuration management, system development and type certification processes. Using the configuration item type classification under the aircraft, system and equipment levels as a framework, a compliance evidence system consisted by five dimensions of plan assurance, requirement definition, logical/physical solution, validation data and verification data is proposed, which specifies the transferring relationship between the data links.