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SAE AMS6488
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SAE AMS6488 Revision H, January 1, 2008
Steel, Bars and Forgings 5.0Cr - 1.3Mo - 0.5V - (0.38 - 0.43C)
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.
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.
SAE AMS6488 Revision H, January 1, 2008
Steel, Bars and Forgings 5.0Cr - 1.3Mo - 0.5V - (0.38 - 0.43C)