BS 2S 98:1964

Superseded

View Superseded by

Specification for aircraft material. 2½ per cent nickel-chromium-molybdenum steel (high carbon) (75/85 tonf/sq in: limited ruling section 6 in)

Available format(s)

Hardcopy , PDF

Superseded date

12-31-2014

Language(s)

English

Published date

01-31-1964

Publisher

British Standards Institution

1 Inspection and testing procedure
2 Process of manufacture
3 Chemical composition
4 Surface dressing
5 Condition
6 Final heat treatment
7 Mechanical properties

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 2.5% nickel-chromium-molybdenum steel.

Committee	ACE/61/-/15
DevelopmentNote	Supersedes 86/77453 DC and BS S98(1949). (07/2005) Earlier was withdrawn in error by the publisher, now has been reinstated. Reviewed and confirmed by BSI, April 2013. (03/2013)
DocumentType	Standard
Pages	8
PublisherName	British Standards Institution
Status	Superseded
SupersededBy	BS 3S 98:2014

BS 4S100(1975) : 1975	PROCEDURE FOR INSPECTION AND TESTING OF WROUGHT STEELS (OTHER THAN SHEET, STRIP AND TUBES)
BS 350:2004	Conversion factors for units