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Miscellaneous rivet standards from ISO, SAE, ASTM, and others for materials
This procurement specification covers rivets fabricated from an aluminum alloy designated as 2117-T4, solution treated. The following specification designations and their rivet coatings are covered: AS7222 Rivets anodized per AMS 2470, chromic acid process; AS7222-1 Rivets anodized per AMS 2471, sulfuric acid process. Primarily for joining aluminum parts where rivets having 26 ksi minimum ultimate shear strength is adequate.
This procurement specification covers aircraft quality solid rivets and tubular end rivets made from a carbon steel of the type identified under the Unified Numbering System as UNS G10100.
This procurement specification covers aircraft quality solid rivets and tubular end rivets made from a corrosion resistant steel of the type identified under the Unified Numbering System as UNS S30200.
This procurement specification covers aircraft quality solid rivets and tubular end rivets made from a corrosion resistant steel of the type identified under the Unified Numbering System as UNS S34700. Primarily for joining corrosion resistant steel parts requiring corrosion, heat, and oxidation resistance up to approximately 1300 degrees F but not requiring high shear strength.
This procurement specification covers aircraft quality solid rivets and tubular end rivets made from a corrosion and heat resistant nickel base alloy of the type identified under the Unified Numbering System as UNS N06600.
This procurement specification covers aircraft-quality solid rivets made from a corrosion resistant nickel-copper alloy of the type identified under the Unified Numbering System as UNS N04400 and of 46 ksi minimum shear strength. Primarily for use as a fastening device where corrosion resistance up to approximately 800 degrees F is required and where ease of forming full heads are essential during riveting operation. The riveting operation shall be done by squeezing, using steadily applied pneumatic or hydraulic pressure; hand peening is not permitted.
This procurement specification covers tubular, blind rivets fabricated from a corrosion resistant nickel-copper alloy of the type identified under the unified numbering system as UNS N04405, and of 52 ksi minimum shear strength for self-plugging style rivets.
This procurement specification covers solid rivets and hollow end rivets made from a corrosion and heat resistant steel of the type identified under the unified numbering system as UNS S66286 and of 80 ksi single shear strength at room temperature. Primarily for joining corrosion resistant steel parts having high strength up to 1200 degrees F and oxidation resistance up to approximately 1500 degrees F.
This procurement specification covers aircraft quality solid rivets made from a corrosion and heat resistant cobalt alloy of the type identified under the Unified Numbering System as UNS R30605. Primarily for joining parts where a high shear strength is required up to 1500 degrees F and oxidation resistance up to 2000 degrees F.
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.