BS SP33-39(1951) : 1951
Current
The latest, up-to-date edition.
SPECIFICATIONS FOR TURNBARRELS, TENSION RODS AND SWAGED CABLE-END CONNECTIONS FOR AIRCRAFT
Hardcopy , PDF
English
01-01-1951
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Foreword
BS SP 33:1951+A5 2015 Turnbarrels
1 Material
2 Protective finish
3 Dimensions
4 Screw threads
5 Identification and marking
BS SP 34:1951+A5:2015 Screwed ends
1 Material
2 Protective finish
3 Dimensions
4 Screw threads
5 Identification and marking
BS SP 35:1951+A5:2015 Tension rods
1 Material
2 Protective finish
3 Dimensions
4 Screw threads
5 Identification and marking
BS SP 36:1951+A5:2015 Tapped ends
1 Material
2 Protective finish
3 Dimensions
4 Screw threads
5 Identification and marking
BS SP 37:1951+A5:2015 Eye ends
1 Material
2 Protective finish
3 Dimensions
4 Identification and marking
BS SP 38:1951+A5:2015 Fork ends
1 Material
2 Protective finish
3 Dimensions
4 Identification and marking
BS SP 39:1951+A5:2015 Eye ends for chains
1 Material
2 Protective finish
3 Dimensions
4 Identification and marking
Appendix
Gives a tensioning device for aircraft control cables and a variable range of cable-end fittings as a safeguard against the crossing of controls.
| Committee |
ACE/12
|
| DevelopmentNote |
Supersedes 12/30254195 DC. (08/2012) 1951 Edition Re-Issued in October 2015 & incorporates AMD 5 2015. Supersedes 15/30321773 DC. (10/2015)
|
| DocumentType |
Standard
|
| Pages |
26
|
| PublisherName |
British Standards Institution
|
| Status |
Current
|
| Supersedes |
| BS SP 53:1953 | Specification for swaged cable-end assemblies (B.A. and B.S.F. threads) for preformed steel wire rope for aircraft (suitable for use with British Standard W.9 wire rope) |
| BS 2SP 106:1955 | Specification for swaged cable-end assemblies (Unified threads) for preformed non-corrodible steel wire rope (W.11) for aircraft |
| BS 2SP 105:1955 | Specification for swaged cable-end assemblies (Unified threads) for preformed steel wire rope (W.9) for aircraft |
| BS SP 54:1953 | Specification for swaged cable-end assemblies (B.A. and B.S.F. threads) for preformed non-corrodible steel wire rope for aircraft (suitable for use with British Standard W.11 wire rope) |
| BS 2S96(1964) : LATEST | 2.5% NICKEL-CHROMIUM-MOLYBDENUM STEEL (55/65 TONF/SQ IN: LIMITING RULING SECTION 6 IN.) |
| BS 2SP101-104(1956) : 1956 | SPECIFICATIONS FOR TURNBARRELS, TENSION RODS AND SWAGED CABLE-END CONNECTIONS (UNIFIED THREADS), CADMIUM PLATED, FOR AIRCRAFT |
| BS 3S95(1967) : 1967 | SPECIFICATION FOR 1[1/2] PER CENT NICKEL-CHROMIUM-MOLYBDENUM STEEL - (880/1080 MPA: LIMITING RULING SECTION 150 MM) |
| 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 3T35(1948) : LATEST | 35-TON STEEL TUBES (SUITABLE FOR WELDING) |
| BS 7S1(1964) : 1964 | SPECIFICATION FOR CARBON STEEL BRIGHT BARS FOR MACHINING - (540 MPA; MAXIMUM SIZE, 101 MM DIAMETER OR MINOR SECTIONAL DIMENSION |
| BS 228:1994 | Specification for short-pitch transmission precision roller chains and chain wheels |
| BS 2S 117:1964 | Specification for aircraft material. 1 per cent chromium steel (55/65 tonf/sq in: limiting ruling section 1⅛ inch) |
| BS 4T45(1972) : 1972 | SPECIFICATION FOR CARBON-MANGANESE STEEL TUBE (700 MPA) (TUBE 12.5 MM OUTSIDE DIAMETER AND GREATER) (WELDABLE) |
| BS 84:2007 | Parallel screw threads of Whitworth form. Requirements |
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