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SAE AMS-S-18728
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SAE AMS-S-18728 Revision B, June 1, 2006
Steel Plate, Sheet and Strip, Alloy 8630, Aircraft Quality
Description / Abstract:
This specification covers chrome-nickel-molybdenum steel, 8620, plate, sheet, and strip of thicknesses to and including 1.50 inches.
Classification:
Materials covered by this specification shall be of the following physical conditions, as specified (see 6.2)
A Annealed.
MA Modified annealed.
NORM Normalized or otherwise heat-treated by the producer.
Classification:
Materials covered by this specification shall be of the following physical conditions, as specified (see 6.2)
A Annealed.
MA Modified annealed.
NORM Normalized or otherwise heat-treated by the producer.
SAE AMS-S-18728 Revision B, June 1, 2006
Steel Plate, Sheet and Strip, Alloy 8630, Aircraft Quality