• SAE ARP4402

SAE ARP4402

  • Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure
  • standard by SAE International, 06/11/2013
  • Category: SAE

$81.00 $41.00

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.
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SAE AS1712C

SAE AS1712C

COUPLING SUBASSEMBLY, FLEXIBLE, VARIABLE CAVITY, THREADED, FERRULE TYPE TUBE ENDS..

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SAE AS1713C

SAE AS1713C

HALF COUPLING SUBASSEMBLY, FLEXIBLE, VARIABLE CAVITY, THREADED FERRULE TYPE TUBE ENDS..

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SAE AS1714D

SAE AS1714D

NUT ASSEMBLY, COUPLING, FLEXIBLE, VARIABLE CAVITY, THREADED, FERRULE TYPE TUBE ENDS..

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SAE AS1716D

SAE AS1716D

FERRULE, COUPLING, FLEXIBLE, VARIABLE CAVITY, THREADED, FERRULE TUBE END..

$41.00 $81.00