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Full Description

This specification provides the general welding requirements for welding aircraft and space hardware. It includes but is not limited to the fusion welding of aluminum-based, nickel-based, iron-based, cobalt-based, magnesium-based, and titanium-based alloys using electric arc and high energy beam processes. There are requirements for welding design, personnel and procedure qualification, inspection, and acceptance criteria for aerospace, support and non-flight hardware. Additional requirements cover repair welding of existing hardware. A commentary for the specification is included.
 

Document History

  1. AWS D17.1/D17.1M:2010-AMD1


    Specification for Fusion Welding for Aerospace Applications, 2nd Edition (Third Printing, Includes 2012 Amendment)

    • Most Recent
  2. AWS D17.1 / D17.1M:2010

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    Specification for Fusion Welding for Aerospace Applications, 2nd Edition

    • Historical Version
  3. AWS D17.1:2001


    Specification for Fusion Welding for Aerospace Applications, Includes Errata

    • Historical Version
  4. MIL MIL-STD-1595A


    QUALIFICATION OF AIRCRAFT, MISSILE & AEROSPACE FUSION WELDERS (SUPERSEDING MIL-STD-1595) (S/S BY SAE-AMS-STD-1595A)

    • Historical Version
  5. MIL MIL-STD-1595


    QUALIFICATION OF AIRCRAFT, MISSILE & AEROSPACE FUSION WELDERS (S/S BY MIL-STD-1595A)

    • Historical Version