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SAE ARP4402

92nd Edition, April 1, 1992

Complete Document

Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure

Includes all amendments and changes through Reaffirmation Notice , June 2013


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Product Details:

  • Revision: 92nd Edition, April 1, 1992
  • Published Date: June 2013
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 16
  • ANSI Approved: No
  • DoD Adopted: No

Description / Abstract:

Purpose:

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

Application:

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.
AIA/NAS Aerospace Standards