SAE ARP4402 PDF

Name:
SAE ARP4402 PDF

Published Date:
06/11/2013

Status:
Active

Description:

Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure

Publisher:
SAE International

Document status:

Active

Format:

Electronic (PDF)

Delivery time:

10 minutes

Delivery time (for Russian version):

200 business days

SKU:

This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures. This process has been used typically by maintenance and overhaul facilities personnel to inspect aluminum aircraft structures for service-induced cracks, but usage is not limited to such applications.

File Size :	1 file , 580 KB
Note :	This product is unavailable in Ukraine, Russia, Belarus
Published :	06/11/2013

History

SAE ARP4402A

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Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure

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Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure

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