Specification for chromium-nickel-copper-molybdenum corrosion-resisting steel (precipitation hardening) billets, bars, forgings and parts (930-1080 MPa)

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

30-11-2001

Publisher

British Standards Institution

NO CONTENTS SECTION

Describes manufacture, inspection and testing of heat resisting alloys for aerospace purposes. Gives chemical composition and mechanical properties. This covers chromium nickel copper molybdenum steel billets.

Committee	ACE/61/-/15
DevelopmentNote	Supersedes 00/709816 DC, 75/74997 DC, 91/70677 DC and 94/701798 DC. Supersedes BS S 143(1969). (12/2001) Reviewed and confirmed by BSI, December 2009. (11/2009)
DocumentType	Standard
Pages	6
PublisherName	British Standards Institution
Status	Current
Supersedes	94/701798 DC : FEB 94 00/709816 DC : JUNE 2000 91/70677 DC : MAR 91

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BS 3S144(1995) : 1995	SPECIFICATION FOR CHROMIUM-NICKEL-COPPER-MOLYBDENUM CORROSION RESISTING STEEL (PRECIPITATION HARDENING) BILLETS, BARS, FORGINGS AND PARTS (1130 MPA TO 1330 MPA)
BS 4A114(1999) : 1999	SPECIFICATION FOR CORROSION-RESISTING STEEL, MUSHROOM-HEADED, SLOTTED-DRIVE, BOLTS, STRENGTH CLASS 880 MPA
BS 3S145(1996) : 1996	SPECIFICATION FOR CHROMIUM-NICKEL-COPPER-MOLYBDENUM CORROSION RESISTING STEEL (PRECIPITATION HARDENING) BILLETS, BARS, FORGINGS AND PARTS (1270 MPA TO 1470 MPA)
14/30311855 DC : 0	BS 3S 144:1995+A2 - SPECIFICATION FOR CHROMIUM-NICKEL-COPPER-MOLYBDENUM CORROSION RESISTING STEEL (PRECIPITATION HARDENING) BILLETS, BARS, FORGINGS AND PARTS (1130-1330 MPA)
BS 4A104(2002) : 2002	AEROSPACE SERIES - SPECIFICATION FOR CORROSION-RESISTING STEEL BOLTS (UNIFIED HEXAGONS AND UNIFIED THREADS), STRENGTH CLASS 880 MPA, FOR AIRCRAFT