BS SP119 & SP120(1957) : 1957
Current
The latest, up-to-date edition.
HIGH TENSILE STEEL FORK JOINTS (UNIFIED THREADS) - FOR AIRCRAFT
Hardcopy , PDF
English
01-01-1957
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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 |
| 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) |
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