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BS 2A 59:1962

Current
Current

The latest, up-to-date edition.

Specification for cadmium-plated steel hexagonal-headed bolts (B.A. and B.S.F. threads) with close tolerance shanks for aircraft
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

05-17-1962

Publisher

British Standards Institution

NO CONTENTS SECTION

Gives materials, dimensions, finish and inspection requirements for steel hexagonal headed bolts with B.A. and B.S.F. threads and with close tolerance shanks cadmium plated to be suitable for insertion in aluminium alloy materials, for aircraft.

1. This British Standard specifies the materials, dimensions, finish and inspection requirements for steel hexagonal-headed bolts with B.A. and B.S.F. threads, and with close tolerance shanks cadmium plated to be suitable for insertion in aluminium alloy materials, for aircraft.

Committee
ACE/12
DevelopmentNote
Supersedes BS A59(1954). (07/2005) Earlier was withdrawn in error by the publisher and now has been reinstated. (01/2013) Reviewed and confirmed by BSI, March 2013. (03/2013)
DocumentType
Standard
Pages
18
PublisherName
British Standards Institution
Status
Current

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 2S 116:1964 Specification for aircraft material. \'40\' carbon steel bright bars for machining (55-65 tonf/sq in: limiting ruling section ¾ inch) (primarily intended for the manufacture of machined bolts)
BS 2S 149:1976 Specification for 1.75% nickel-chromium-molybdenum steel bars for the manufacture of forged bolts and forged nuts
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 S148(1969) : 1969 SPECIFICATION FOR LOW NICKEL-CHROMIUM STEEL (BAR FOR THE MANUFACTURE OF FORGED BOLTS ONLY)
BS 3S102(1969) : 1969 SPECIFICATION FOR CARBON-MOLYBDENUM STEEL (BAR FOR THE MANUFACTURE OF FORGED BOLTS ONLY)
BS 2A 30:1962 Specification for steel hexagonal-headed bolts (B.A. and B.S.F threads) with close tolerance shanks for aircraft
BS 3S105(1969) : 1969 SPECIFICATION FOR CARBON STEEL - (BAR FOR THE MANUFACTURE OF FORGED BOLTS ONLY)
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)
BS S 158:1977 Specification for 1% chromium-molybdenum steel bars for the manufacture of forged bolts and forged nuts
BS 2S 147:1976 Specification for 0.5% nickel-chromium-molybdenum steel bars for the manufacture of forged bolts and forged nuts
BS 2S103(1964) : LATEST LOW NICKEL CHROMIUM STEEL (WIRE ONLY FOR THE MANUFACTURE OF BOLTS)

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