BS 2A 58:1962
Withdrawn
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
Specification for steel hexagonal nuts (B.S.F. threads) for shear bolts for aircraft
Available format(s)
Hardcopy , PDF
Language(s)
English
Published date
17-05-1962
Publisher
Withdrawn date
24-09-2012
€93.10
Excluding VAT
NO CONTENTS SECTION
Gives the materials, dimensions, finish and inspection requirements for steel hexagonal slotted and thin nuts with B.S.F. threads for use with shear bolts for aircraft.
| Committee |
ACE/12
|
| DevelopmentNote |
Supersedes BS A57(1952) and BS A58(1952). (07/2005) Inactive for the new design. (12/2007)
|
| DocumentType |
Standard
|
| Pages |
12
|
| PublisherName |
British Standards Institution
|
| Status |
Withdrawn
|
| BS 2A 60:1962 | Specification for cadmium-plated steel hexagonal-headed shear bolts (B.S.F. threads) for aircraft |
| BS 2A 57:1962 | Specification for steel hexagonal-headed shear bolts (B.S.F. threads) for aircraft |
| BS 2S96(1964) : LATEST | 2.5% NICKEL-CHROMIUM-MOLYBDENUM STEEL (55/65 TONF/SQ IN: LIMITING RULING SECTION 6 IN.) |
| 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 2A 100:1968 | Specification for general requirements for bolts and nuts of tensile strength not exceeding 180000 lbf/in<sup>2</sup> (125 hbar) |
| BS S 154:1976 | Specification. 2½% nickel-chromium-molybdenum steel billets, bars, forgings and parts (880-1080 MPa: limiting ruling section 150 mm) |
| BS 2S 142:1977 | Specification for 1% chromium-molybdenum steel billets, bars, forgings and parts (900-1100 MPa: limiting ruling section 40 mm) |
| BS 350:2004 | Conversion factors for units |
| 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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