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BS 3A 171:1962

Current

Current

The latest, up-to-date edition.

Specification for aluminium alloy pan head bolts (Unified threads) for aircraft

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

11-08-1962

US$156.28
Excluding Tax where applicable

NO CONTENTS SECTION

Gives materials, dimensions and inspection requirements for aluminium alloy pan head bolts with Unified threads for aircraft.

Committee
ACE/12
DevelopmentNote
Supersedes BS 2A171(1956) (07/2005) Earlier was withdrawn in error by the publisher and now has been reinstated.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
7
PublisherName
British Standards Institution
Status
Current

1. This British Standard specifies the materials, dimensions and inspection requirements for aluminium alloy pan head bolts with Unified threads for aircraft.

Standards Relationship
UNE-EN IEC 60601-2-54:2024 Identical

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 350:2004 Conversion factors for units
BS L 168:1978 Specification for bars and extruded sections of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and artificially aged) (not exceeding 200 mm diameter or minor sectional dimension) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8)

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