SAE AS7237

Rivets, Nickel Alloy, Corrosion and Heat Resistant 47.5ni 22cr 1.5co 9.0mo 0.60w 18.5fe Solution Heat Treated Procurement Specification For.

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Standard:
  • AS7237
Reaffirmed:
  • 2012-11-19
Issued:
  • 1992-10-01
Issuing:
  • E-25 General Standards For Aerospace And Propulsion Systems
Scope:

This procurement specification covers aircraft quality solid rivets and tubular end rivets made from a corrosion and heat resistant nickel alloy of the type identified under the Unified Numbering System as UNS N06002. Primarily for joining parts requiring a combination of corrosion resistance, heat and oxidation resistance up to 2200 degrees F, and relatively high shear strength above 1500 degrees F.

History:
StandardPublishedRevisionStatus
AS72371992-10-01LatestReaffirmed
AKA:
  • SAE AS 7237
Sector:
  • Aerospace
Topic:
  • Nickel
  • Parts
  • Gas turbines
  • Hybrid engines
  • Jet engines

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