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SAE AMS-S-8690
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SAE AMS-S-8690 Revision A, September 1, 2002
Steel, Chrome-Nickel-Molybdenum, 8620, Bars Aircraft Quality
Description / Abstract:
Steel covered by this specification is intended for use in the
manufacture of aircraft parts and components. It is suitable for
reforging and for carburizing. The prime application of this
material is for critical carburized parts and components which
require a high core hardness even in thin sections. The core may or
may not be machinable after hardening.
SAE AMS-S-8690 Revision A, September 1, 2002
Steel, Chrome-Nickel-Molybdenum, 8620, Bars Aircraft Quality