Specification for aircraft material. Carbon-manganese steel (suitable for welding) (40/55 tonf/sq in: limiting ruling section 4 in)

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

31-01-1964

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 carbon manganese steel.

Committee	ACE/61/-/15
DevelopmentNote	Supersedes BS S92(1949). (07/2005) To be read in conjunction with BS 4S100(1975). (06/2013) Earlier it was withdrawn in error by publisher, now has been reinstated. (07/2013) Reviewed and confirmed by BSI, January 2014. (12/2013)
DocumentType	Standard
Pages	8
PublisherName	British Standards Institution
Status	Current

BS 3A 103:1962	Specification for steel nuts (Unified hexagons and Unified threads) (ordinary, thin, slotted and castle) for aircraft
BS 2SP151-153(1979) : 1979	SPECIFICATION FOR UNIFIED ALLOY STEEL WASHERS
BS 3A125 TO 3A[...](1981) : 1981	AEROSPACE SERIES - SPECIFICATION FOR STIFFNUTS (UNIFIED THREADS) FOR AIRCRAFT

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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BS 2S 92:1964

Specification for aircraft material. Carbon-manganese steel (suitable for welding) (40/55 tonf/sq in: limiting ruling section 4 in)

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