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SAE AMS-S-6050
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SAE AMS-S-6050 Revision B, February 1, 2005
Steel, Chrome-Nickel-Molybdenum (8630) Bars and Reforging Stock (Aircraft
Quality)
Description / Abstract:
The material covered by this specification is intended for use
in the manufacture of aircraft parts and components. It may be
welded. The material is not recommended for very heavy sections.
The hardenability and weldability of this material are considered
equivalent to that of material conforming to MIL-S-6758.
SAE AMS-S-6050 Revision B, February 1, 2005
Steel, Chrome-Nickel-Molybdenum (8630) Bars and Reforging Stock (Aircraft
Quality)