BS 2A 100:1968
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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 general requirements for bolts and nuts of tensile strength not exceeding 180000 lbf/in2 (125 hbar)
Available format(s)
Hardcopy , PDF
Superseded date
31-12-1991
Superseded by
Language(s)
English
Published date
29-07-1983
Publisher
Important note : All end users must be registered with an Account prior to user licenses being assigned.| Committee |
ACE/12
|
| DocumentType |
Standard
|
| Pages |
24
|
| PublisherName |
British Standards Institution
|
| Status |
Superseded
|
| SupersededBy |
| BS 2A 61:1962 | Specification for aluminium alloy hexagonal headed bolts (B.A. and B.S.F. threads) for aircraft |
| BS 4A112(1992) : 1992 | SPECIFICATION FOR CADMIUM PLATED STEEL SHEAR BOLTS (UNIFIED HEXAGONS AND UNIFIED THREADS) |
| BS 3A 109:1985 | Specification for steel shear bolts (Unified hexagons and Unified threads) |
| BS 3A 103:1962 | Specification for steel nuts (Unified hexagons and Unified threads) (ordinary, thin, slotted and castle) for aircraft |
| BS 2A 60:1962 | Specification for cadmium-plated steel hexagonal-headed shear bolts (B.S.F. threads) for aircraft |
| BS 2A 174:1962 | Specification for 100° countersunk head corrosion-resisting steel bolts (Unified threads) 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 2A 230:1974 | Specification for 100° countersunk head steel bolts [1100 MPa with Hi-torque speed drive recesses] |
| BS 2A 30:1962 | Specification for steel hexagonal-headed bolts (B.A. and B.S.F threads) with close tolerance shanks for aircraft |
| BS 3A 171:1962 | Specification for aluminium alloy pan head bolts (Unified threads) for aircraft |
| BS 2A 26:1962 | Specification for corrosion-resisting steel hexagonal-headed bolts (B.A and B.S.F. threads) for aircraft |
| BS A 226:1965 | Specification for steel hexagon head bolts (short thread: Class 3A) |
| BS 2A 58:1962 | Specification for steel hexagonal nuts (B.S.F. threads) for shear bolts for aircraft |
| BS 2A 210:1962 | Specification for brass nuts (Unified hexagons and Unified threads) for aircraft |
| BS 6S 100:2010 | Aerospace series. Procedure for inspection, testing and acceptance of wrought steels (other than plate, sheet, strip and tube) |
| BS 2A 229:1972 | Specification for hexagonal head steel bolts 160000 lbf/in<sup>2</sup> (1100/MPa) |
| BS 3A 116:1962 | Specification for steel pan head bolts (Unified threads) for aircraft |
| BS 2A 29:1962 | Specification for aluminium alloy hexagonal nuts (B.A and B.S.F. threads) (ordinary and slotted) for aircraft |
| BS A 237-240:1971 | Specification for plain hexagonal nut (of Class 3B UNJ thread) |
| BS A260,A261,A262,A263,A264,A265(1976) : 1976 AMD 4065 | SPECIFICATION FOR METRIC SCREWS |
| BS A 233-236:1971 | Specification for plain hexagonal thin nut (of Class 3B UNJ thread) |
| BS 2A 24:1962 | Specification for corrosion-resisting steel hexagonal nuts (B.A and B.S.F. threads) (ordinary, thin, slotted and castle) for aircraft |
| BS 2A 25:1962 | Specification for steel hexagonal-headed bolts (B.A. and B.S.F. 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 |
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