SPECIFICATION FOR TURNBUCKLES (TENSION ROD TYPE) FOR AIRCRAFT PURPOSES

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Hardcopy , PDF

Language(s)

English

Published date

01-01-1939

Publisher

British Standards Institution

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Foreword
1 General
2 Fork Joints
3 Pins
4 Lock Nuts
5 Tension Rods and Rollers

Refers to the material, manufacture, dimensions and finish of turnbuckles for aerospace purposes.

Committee	ACE/12
DevelopmentNote	1939 Edition Re-Issued in November 2012 & incorporates AMD 7 2012. Supersedes 12/30254233 DC. (11/2012)
DocumentType	Standard
Pages	10
PublisherName	British Standards Institution
Status	Current
Supersedes	12/30254233 DC : 0

BS 2S96(1964) : LATEST	2.5% NICKEL-CHROMIUM-MOLYBDENUM STEEL (55/65 TONF/SQ IN: LIMITING RULING SECTION 6 IN.)
BS 2S 114:1964	Specification for aircraft material. Manganese-molybdenum steel (55/65 tonf/sq in: limiting ruling section 2½ inches)
BS 3SP 3:1943	Specification for aircraft material. Fork joints (low tensile type) (for sizes No. 4 B.A. to ½ inch B.S.F. inclusive)
BS 2S94(1955) : LATEST	55-TON LOW ALLOY STEEL
BS 3S80(1964) : LATEST
BS A16(1939) : LATEST	HEXAGONAL STEEL NUTS (ORDINARY, THIN, SLOTTED AND CASTLE)
BS 7S1(1964) : 1964	SPECIFICATION FOR CARBON STEEL BRIGHT BARS FOR MACHINING - (540 MPA; MAXIMUM SIZE, 101 MM DIAMETER OR MINOR SECTIONAL DIMENSION
BS 5SP 4:1944	Specification for aircraft material. Steel pins
BS 84:1956	Specification for parallel screw threads of Whitworth form
BS 2S 117:1964	Specification for aircraft material. 1 per cent chromium steel (55/65 tonf/sq in: limiting ruling section 1⅛ inch)

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Features

BS SP8(1939) : 1939