HIGH TENSILE STEEL FORK JOINTS (UNIFIED THREADS) - FOR AIRCRAFT

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-1957

Publisher

British Standards Institution

Foreword
1 Scope
2 Material
3 Dimensions
4 Screw threads
5 Protective finish
6 Freedom from defects
7 Identification and marking

Describes the materials, dimensions and finish of high tensile steel fork joints with Unified threads for aircraft.

Committee	ACE/14
DevelopmentNote	1957 Edition Re-Issued in August 2012 & incorporates AMD 2 2012. Supersedes 12/30254191 DC. (08/2012)
DocumentType	Standard
Pages	8
PublisherName	British Standards Institution
Status	Current
Supersedes	12/30254191 DC : 0

BS 7S 80:2002	High chromium-nickel corrosion resisting steel forging stock, bars, forgings and parts (880 to 1080 MPa: limiting ruling section 100 mm)
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 2S94(1955) : LATEST	55-TON LOW ALLOY STEEL
DTD 904C : MAY 63	CADMIUM PLATING
BS 2S 117:1964	Specification for aircraft material. 1 per cent chromium steel (55/65 tonf/sq in: limiting ruling section 1⅛ inch)