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AS6459 - EDDY CURRENT SURFACE CRACK DETECTION IN AEROSPACE STRUCTURES

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Document Number: AS6459
Project Initiation: 02-17-2011
Project Number:
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Sponsor Name: Tom Dreher
Title
EDDY CURRENT SURFACE CRACK DETECTION IN AEROSPACE STRUCTURES
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 Aerospace Recommended Practice documents procedures to be used for directed inspections of critical areas or areas where visible evidence of damage is detected and is not intended for use as a global inspection method, particularly on parts with complex shapes.
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