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SAE AS7452

Revision B, August 2014

Complete Document

Bolts and Screws, Steel, Low Alloy Heat Treated, Roll Threaded



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Product Details:

  • Revision: Revision B, August 2014
  • Published Date: August 2014
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 21
  • ANSI Approved: No
  • DoD Adopted: Yes

Description / Abstract:

Type

This procurement specification covers aircraft quality bolts and screws made from a low alloy steel of the type identified under the Unified Numbering System as UNS G87400, and of a series of room temperature tensile strengths ranging from 125 000 to 185 000 psi. 

Application

Primarily for aerospace propulsion system applications where good strength is required and the part is protected against corrosion. 

Safety - Hazardous Materials

While the materials, methods, applications, and processes 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.
AIA/NAS Aerospace Standards