ARP4402A: Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure - Recommended Practice

Features

Issuing Committee: AMS K Non Destructive Methods and Processes Committee

Scope

Content: This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures.

Meta Tags

Topics: Non-destructive tests
Disaster and emergency management
Voltage regulators

Details

DOI: https://doi.org/10.4271/ARP4402A

Pages: 23

Citation: SAE International Recommended Practice, Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure, SAE Standard ARP4402A, Revised September 2020, Reaffirmed June 2013, Issued April 1992, https://doi.org/10.4271/ARP4402A.

Additional Details

Publisher: SAE International

Published: Sep 22, 2020

Product Code: ARP4402A

Content Type: Recommended Practice

Status: Revised

Language: English

Historical

ARP4402A-TEST-REC