BS S 127:1964
Withdrawn
Specification for aircraft material. 24/17 chromium-nickel heat-resisting steel (titanium stabilized) (35 tonf/sq in: limiting ruling section 6 in)
Hardcopy , PDF
English
01-31-1964
03-15-1999
NO CONTENTS SECTION
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 24/17 chromium nickel heat resisting steel.
| Committee |
ACE/61/-/15
|
| DevelopmentNote |
OBSOLESCENT - CURRENT FOR EXISTING EQUIPMENT, NOT FOR USE WITH NEW DESIGNS. REPLACES S 109:1949.
|
| DocumentType |
Standard
|
| Pages |
5
|
| PublisherName |
British Standards Institution
|
| Status |
Withdrawn
|
| Supersedes |
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