Specification for aircraft material. Fork joints (low tensile type) (for sizes No. 4 B.A. to ½ inch B.S.F. inclusive)

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

02-19-1943

Publisher

British Standards Institution

NO CONTENTS SECTION

Refers to the manufacture, testing, material and marking of fork joints for aerospace use.

Committee	ACE/12
DevelopmentNote	Supersedes BS 2SP3(1929) (07/2005) Inactive for the new design. (12/2011)
DocumentType	Standard
Pages	12
PublisherName	British Standards Institution
Status	Current

BS SP8(1939) : 1939

SPECIFICATION FOR TURNBUCKLES (TENSION ROD TYPE) FOR AIRCRAFT PURPOSES

BS 2S96(1964) : LATEST	2.5% NICKEL-CHROMIUM-MOLYBDENUM STEEL (55/65 TONF/SQ IN: LIMITING RULING SECTION 6 IN.)
DTD 904C : MAY 63	CADMIUM PLATING
BS 3S80(1964) : LATEST
BS 93:1951	Specification for British Association (B.A.) screw threads with tolerances for sizes 0 B.A. to 16 B.A.
BS 7S1(1964) : 1964	SPECIFICATION FOR CARBON STEEL BRIGHT BARS FOR MACHINING - (540 MPA; MAXIMUM SIZE, 101 MM DIAMETER OR MINOR SECTIONAL DIMENSION
BS 3S 62:1964	Specification for aircraft material. 12 per cent chromium corrosion-resisting steel (45/55 tonf/sq in: limiting ruling section 6 in)
BS 970:1955	Wrought steels (bars billets and forgings
BS 3S 61:1964	Specification for aircraft material. 12 per cent chromium corrosion-resisting steel (35/45 tonf/sq in: limiting ruling section 6 in)
BS 84:1956	Specification for parallel screw threads of Whitworth form

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BS 3SP 3:1943