SAE AS7470D-2019 PDF

Scope: Type This procurement specification covers aircraft quality bolts and screws made from a corrosion and moderate heat-resistant martensitic iron base alloy of the type identified under the Unified Numbering System as UNS S41800 and of 140000 psi and 152000 psi tensile strengths at room temperature. Application Primarily for aerospace propulsion system applications where corrosion and moderate heat resistance is required. Safety - Hazardous Materials While the materials@ methods@ applications@ and process described or referenced in this specification may involve the use of hazardous materials@ this specification does not address the hazards which may be involved in such use. It is the sole responsibility of the user to ensure familiarity with the safe and proper use of any hazardous materials and to take necessary precautionary measures to ensure the health and safety of all personnel involved. Usage of Existing Manufactured Stock Unless otherwise specified@ part inventory manufactured to previous revisions of this specification may be procured and used until stock is depleted.

SAE AS7470D-2019 history

2019 SAE AS7470D-2019 Bolts and Screws@ Steel@ Corrosion and Moderate Heat Resistant Heat Treated@ Roll Threaded
2012 SAE AS7470C-2012 Bolts and Screws, Steel, Corrosion and Moderate Heat Resistant Heat Treated, Roll Threaded
2008 SAE AS7470C-2008 Bolts and Screws, Steel, Corrosion and Moderate Heat Resistant Heat Treated, Roll Threaded
2005 SAE AS7470B-2005 Bolts and Screws@ Steel@ Corrosion and Moderate Heat Resistant Heat Treated@ Roll Threaded
2003 SAE AS7470A-2003 Bolts and Screws@ Steel@ Corrosion and Moderate Heat Resistant Heat Treated@ Roll Threaded (FSC 5306)
2001 SAE AS7470-2001 Bolts and Screws, Steel, Corrosion and Moderate Heat Resistant Heat Treated, Roll Threaded
1991 SAE AS7470-1991 Bolts and Screws@ Steel@ Corrosion and Moderate Heat Resistant Heat Treated@ Roll Threaded