Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure
ARP4402
This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures.
Rationale: ARP4402 has been reaffirmed to comply with the SAE five-year review policy.
Related Topics:
Maintenance, repair, and service operationsMaintainability and supportabilityAluminumFastenersTests and TestingNon-destructive testsInspectionsX-ray inspections
Also known as: SAE ARP 4402
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