BS 3S95(1967) : 1967
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
SPECIFICATION FOR 1[1/2] PER CENT NICKEL-CHROMIUM-MOLYBDENUM STEEL - (880/1080 MPA: LIMITING RULING SECTION 150 MM)
Available format(s)
Hardcopy , PDF
Superseded date
01-09-2015
Superseded by
Language(s)
English
Published date
01-01-1967
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1 Inspection and testing procedure
2 Process of manufacture
3 Chemical composition
4 Surface dressing
5 Condition
6 Final heat treatment
7 Mechanical properties
| Committee |
ACE/61
|
| DevelopmentNote |
Supersedes 67/2360 DC and BS 2S95(1964). (07/2005) Earlier was withdrawn in error by the publisher, now has been reinstated. (04/2014) 1967 Edition Re-Issued in September 2015 & incorporates AMD 1 2015. Supersedes 15/30313994 DC. (10/2015)
|
| DocumentType |
Standard
|
| Pages |
8
|
| PublisherName |
British Standards Institution
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| BS 2A 57:1962 | Specification for steel hexagonal-headed shear bolts (B.S.F. threads) for aircraft |
| BS 2A173(1962) : 1962 | SPECIFICATION FOR 100 DEGREES COUNTERSUNK HEAD STEEL BOLTS (UNIFIED THREADS), CADMIUM PLATED, FOR AIRCRAFT |
| BS 3A 103:1962 | Specification for steel nuts (Unified hexagons and Unified threads) (ordinary, thin, slotted and castle) for aircraft |
| BS A 227:1965 | Specification for steel pan head bolts (short thread: Class 3A) |
| 13/30275815 DC : 0 | BS 2A 110+A1 - SPECIFICATION FOR STEEL NUTS (UNIFIED HEXAGONS AND UNIFIED THREADS) FOR SHEAR BOLTS FOR AIRCRAFT |
| 11/30252412 DC : 0 | BS 4A 116 - STEEL PAN HEAD BOLTS (UNIFIED THREADS) (CADMIUM PLATED) FOR AIRCRAFT |
| BS 2A 27:1962 | Specification for steel hexagonal nuts (B.A. and B.S.F threads) (ordinary, thin, slotted and castle) for aircraft |
| BS 3A 108:1962 | Specification for steel bolts (Unified hexagons and Unified threads) with close tolerance shanks for aircraft |
| BS SP33-39(1951) : 1951 | SPECIFICATIONS FOR TURNBARRELS, TENSION RODS AND SWAGED CABLE-END CONNECTIONS FOR AIRCRAFT |
| BS 2A 60:1962 | Specification for cadmium-plated steel hexagonal-headed shear bolts (B.S.F. threads) for aircraft |
| BS 4A 111:1993 | Specification for cadmium-plated steel bolts (Unified hexagons and Unified threads) with close tolerance shanks |
| BS 4A 116:2012 | Steel pan head bolts (Unified threads), cadmium plated, for aircraft |
| BS 2A 58:1962 | Specification for steel hexagonal nuts (B.S.F. threads) for shear bolts for aircraft |
| BS 2A 122; 2A 123; 2A 124:1981 | Specification for clinch nuts (Unified threads) for aircraft |
| BS 3A 116:1962 | Specification for steel pan head bolts (Unified threads) for aircraft |
| BS 2A110(1962) : 1962 | SPECIFICATION FOR STEEL NUTS (UNIFIED HEXAGONS AND UNIFIED THREADS) FOR SHEAR BOLTS FOR AIRCRAFT |
| BS A 226:1965 | Specification for steel hexagon head bolts (short thread: Class 3A) |
| BS 3A125 TO 3A[...](1981) : 1981 | AEROSPACE SERIES - SPECIFICATION FOR STIFFNUTS (UNIFIED THREADS) FOR AIRCRAFT |
| BS 2A 59:1962 | Specification for cadmium-plated steel hexagonal-headed bolts (B.A. and B.S.F. threads) with close tolerance shanks for aircraft |
| BS 2SP 93:1974 | Specification for elastomeric grommets (acrylonitrile-butadiene) for aerospace use |
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