BS-2S-98 › Specification for aircraft material. 2$9H per cent nickel-chromium-molybdenum steel (high carbon) (75/85 tonf/sq in: limited ruling section 6 in)

BS-2S-98 - AMD 5680 - SUPERSEDED -- See the following: BS-3S-98
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Specification for aircraft material. 2$9H per cent nickel-chromium-molybdenum steel (high carbon) (75/85 tonf/sq in: limited ruling section 6 in)

Keywords

Nickel steels, Chromium steels, Molybdenum steels, High-carbon steels, Tensile strength, Bars (materials), Billets, Forgings, Aircraft components, Chemical composition, Designations, Heat treatment, Mechanical properties of materials, Hardness, Steels

To find similar documents by classification:

49.025.10 (Steels)

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Document Number

BS-2S-98

Revision Level

AMD 5680

Status

Superseded

Publication Date

July 1, 1988

Committee Number

ACE/61/-/15