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BS 2A 60:1962

Current
Current

The latest, up-to-date edition.

Specification for cadmium-plated steel hexagonal-headed shear bolts (B.S.F. threads) for aircraft
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

17-05-1962

Publisher

British Standards Institution

NO CONTENTS SECTION

Gives materials, dimensions, finish and inspection requirements for steel hexagonal headed shear bolts with B.S.F. threads, and with close tolerance shanks cadmium plated 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 shear bolts with 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 A60(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 (07/2005) Earlier was withdrawn in error by the publisher and now has been reinstated.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 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 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 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 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 143:1976 Specification for chromium-nickel-copper-molybdenum corrosion-resisting steel (precipitation hardening) billets, bars, forgings and parts (930-1080 MPa)
BS 2S 117:1964 Specification for aircraft material. 1 per cent chromium steel (55/65 tonf/sq in: limiting ruling section 1⅛ inch)
BS 2A 57:1962 Specification for steel hexagonal-headed shear bolts (B.S.F. threads) for aircraft
BS 2A 58:1962 Specification for steel hexagonal nuts (B.S.F. threads) for shear bolts for aircraft

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