BS 2SP101-104(1956) : 1956
Current
The latest, up-to-date edition.
SPECIFICATIONS FOR TURNBARRELS, TENSION RODS AND SWAGED CABLE-END CONNECTIONS (UNIFIED THREADS), CADMIUM PLATED, FOR AIRCRAFT
Hardcopy , PDF
English
01-01-1956
Foreword
BS 2SP 101:1956 + A3:2015 Turnbarrels (unified threads)
1 Material
2 Protective finish
3 Dimensions
4 Screw threads
5 Identification and marking
BS 2SP 102:1956 + A3:2015 Screwed ends (unified threads)
1 Material
2 Protective finish
3 Dimensions
4 Screw Threads
5 Identification and marking
BS 2SP 103:1956 + A3:2015 Tension rods (unified threads)
1 Material
2 Protective finish
3 Dimensions
4 Screw threads
5 Identification and marking
BS 2SP 104:1956 + A3:2015 Tapped ends (unified threads)
1 Material
2 Protective finish
3 Dimensions
4 Screw Threads
5 Identification and marking
Appendix
| Committee |
ACE/14
|
| DevelopmentNote |
Supersedes BS SP101-104(1953) (07/2005) Supersedes 11/30254201 DC. (03/2012) 1956 Edition Re-Issued in July 2015 & incorporates AMD 3 2015. Supersedes 15/30317040 DC. (07/2015)
|
| DocumentType |
Standard
|
| Pages |
20
|
| PublisherName |
British Standards Institution
|
| Status |
Current
|
| Supersedes |
| BS 2SP 106:1955 | Specification for swaged cable-end assemblies (Unified threads) for preformed non-corrodible steel wire rope (W.11) for aircraft |
| BS SP33-39(1951) : 1951 | SPECIFICATIONS FOR TURNBARRELS, TENSION RODS AND SWAGED CABLE-END CONNECTIONS FOR AIRCRAFT |
| BS 2SP 105:1955 | Specification for swaged cable-end assemblies (Unified threads) for preformed steel wire rope (W.9) for aircraft |
| BS 2S 114:1964 | Specification for aircraft material. Manganese-molybdenum steel (55/65 tonf/sq in: limiting ruling section 2½ inches) |
| BS S 154:1976 | Specification. 2½% nickel-chromium-molybdenum steel billets, bars, forgings and parts (880-1080 MPa: limiting ruling section 150 mm) |
| BS 3S105(1969) : 1969 | SPECIFICATION FOR CARBON STEEL - (BAR FOR THE MANUFACTURE OF FORGED BOLTS ONLY) |
| BS T 64:1972 | Specification for carbon-manganese steel tube (550 N/mm<sup>2</sup>) (tube less than 12.5 mm outside diameter) (weldable) |
| 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) |
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