GB/T 38825-2020
ActiveRequirements of riveting connection in civil aircraft of composite parts
民用飞机复合材料制件铆接要求
Application Summary AI generated
This standard specifies the technical requirements, inspection methods, and acceptance criteria for riveting composite parts in civil aircraft structures. It is applied during the manufacturing and assembly of composite fuselage panels, wing skins, and control surfaces to ensure joint integrity and prevent delamination or damage. The standard is used by aircraft manufacturers and maintenance organizations for production quality control and airworthiness certification.
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Transparency note: The application summary and key sentences on this page were automatically generated by AI from the standard's original text. This content has not been human-verified and should not be used for compliance or regulatory purposes. Always refer to the official standard document from the issuing authority.