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SAE ARP4402 Rev A

Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure
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SAE ARP4402 Rev A

Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure

PUBLISH DATE 2020
PAGES 23
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This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures.
SDO SAE: SAE International
Document Number ARP4402
Publication Date Sept. 22, 2020
Language en - English
Page Count 23
Revision Level A
Supercedes
Committee
Publish Date Document Id Type View
Sept. 22, 2020 ARP4402A Revision
April 1, 1992 ARP4402 Revision