Name: BS S 126:1964 - Specification for aircraft material. 23/14 chromium-nickel heat-resisting steel (niobium stabilized) (35 tonf/sq in: limiting ruling section 6 in)
Brand: British Standards Institution

Specification for aircraft material. 23/14 chromium-nickel heat-resisting steel (niobium stabilized) (35 tonf/sq in: limiting ruling section 6 in)

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Hardcopy , PDF

Language(s)

English

Published date

01-31-1964

Publisher

British Standards Institution

Withdrawn date

09-27-2012

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US$208.86

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Describes inspection and testing of heat resisting alloys used for aerospace purposes. Covers forgings, plate, strip, tubes, and bars. Gives chemical composition and mechanical properties. Covers 23/14 chromium nickel heat resisting steel.

Committee	ACE/61/-/15
DevelopmentNote	Supersedes BS S108(1949). (08/2005) Inactive for the new design. (12/2007)
DocumentType	Standard
Pages	5
PublisherName	British Standards Institution
Status	Withdrawn
Supersedes	BS S108(1949) : LATEST

BS 4S 100:1975	Procedure for inspection and testing of wrought steels (other than sheet, strip and tubes)
BS 350:2004	Conversion factors for units

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BS S 126:1964

Specification for aircraft material. 23/14 chromium-nickel heat-resisting steel (niobium stabilized) (35 tonf/sq in: limiting ruling section 6 in)

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