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SAE AMS6488

Revision H, January 1, 2008

Complete Document

Steel, Bars and Forgings 5.0Cr - 1.3Mo - 0.5V - (0.38 - 0.43C)

Includes all amendments and changes through Cancellation Notice , January 2008


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Product Details:

  • Revision: Revision H, January 1, 2008
  • Published Date: January 2008
  • Status: Not Active, See comments below
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 9
  • ANSI Approved: No
  • DoD Adopted: No

Description / Abstract:

Form:

This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.

Application:

These products have been used typically for parts requiring through hardening to a minimum hardness of 50 HRC in section thicknesses up to 12 inches (305 mm) with a combination of high strength, fatigue resistance, ductility, and thermal stability for operation in the range of -100 to +1000 °F (-73 to +538 °C), but usage is not limited to such applications.

Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking after heat treatment; ARP1110 recommends practices to minimize such conditions.
AIA/NAS Aerospace Standards