BS 2S 98:1964
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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Specification for aircraft material. 2½ per cent nickel-chromium-molybdenum steel (high carbon) (75/85 tonf/sq in: limited ruling section 6 in)
Hardcopy , PDF
31-12-2014
English
31-01-1964
Important note : Users cannot be edited or removed once added to your Multi user PDF.
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 (07/2005) Earlier was withdrawn in error by the publisher, now has been reinstated.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Superseded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 4S100(1975) : 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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