SAE ARP6459 EDDY CURRENT SURFACE CRACK DETECTION IN AEROSPACE STRUCTURES
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Product Code:SAE ARP6459
Title:EDDY CURRENT SURFACE CRACK DETECTION IN AEROSPACE STRUCTURES
Issuing Committee:Ams K Non Destructive Methods And Processes Committee
Scope: This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current detection of surface cracks in aerospace structures.Procedures for eddy current inspection of open fastener holes in aluminum aircraft structures are contained in SAE ARP4402.
Rationale: This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current detection of surface cracks in aerospace structures.Procedures for eddy current inspection of open fastener holes in aluminum aircraft structures are contained in SAE ARP4402.
Title:EDDY CURRENT SURFACE CRACK DETECTION IN AEROSPACE STRUCTURES
Issuing Committee:Ams K Non Destructive Methods And Processes Committee
Scope: This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current detection of surface cracks in aerospace structures.Procedures for eddy current inspection of open fastener holes in aluminum aircraft structures are contained in SAE ARP4402.
Rationale: This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current detection of surface cracks in aerospace structures.Procedures for eddy current inspection of open fastener holes in aluminum aircraft structures are contained in SAE ARP4402.
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