BS 3A 171:1962
Current
The latest, up-to-date edition.
Specification for aluminium alloy pan head bolts (Unified threads) for aircraft
Hardcopy , PDF
English
08-11-1962
Important note : Users cannot be edited or removed once added to your Multi user PDF.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Supersedes BS 2A171(1956) (07/2005) Earlier was withdrawn in error by the publisher and now has been reinstated.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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