BS 4A 169:2002
Withdrawn
Specification for aluminium alloy bolts (Unified hexagons and Unified threads) for aircraft
Hardcopy , PDF
English
06-30-2006
02-25-2019
Committees responsible
Foreword
1 Scope
2 Normative references
3 General requirements
4 Materials and manufacture
5 Dimensions and tolerances
7 Anti-corrosion treatment
8 Hardness values
9 Identification and marking
10 Quality assurance procedure
Bibliography
Defines materials and manufacture, dimensions, protective treatment and quality assurance requirements for aluminium-alloy hexagon-head bolts with unified threads.
| Committee |
ACE/12
|
| DevelopmentNote |
Supersedes BS 3A169(1962) and 00/704899 DC. (02/2002) Reviewed and confirmed by BSI, November 2012. (10/2012)
|
| DocumentType |
Standard
|
| Pages |
20
|
| PublisherName |
British Standards Institution
|
| Status |
Withdrawn
|
| Supersedes |
| BS 2853:1957 | Specification for the design and testing of steel overhead runway beams |
| BS 3A125 TO 3A[...](1981) : 1981 | AEROSPACE SERIES - SPECIFICATION FOR STIFFNUTS (UNIFIED THREADS) FOR AIRCRAFT |
| BS 3A 100:1991 | Specification for general requirements for bolts and free running nuts of tensile strength not exceeding 1249 MPa |
| 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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