EN 4322:2004
Current
The latest, up-to-date edition.
Aerospace series - Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in titanium alloy TI-P64001, anodized, MoS2 coated - Strength class: 1 100 MPa (at ambient temperature)
10-11-2004
Foreword
1 Scope
2 Normative references
3 Required characteristics
4 Designation
5 Marking
6 Technical specification
This standard specifies the characteristics of double hexagon headed bolts with lockwire holes, relieved shank and long thread, in TI-P64001, anodized, MoS2 coated, for aerospace applications.Strength class: 1 100 MPa )
| Committee |
ASD-STAN
|
| DevelopmentNote |
Supersedes PREN 4322 (12/2003)
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| NBN EN 4322 : 2005 | Identical |
| NEN EN 4322 : 2006 | Identical |
| NS EN 4322 : 2ED 2005 | Identical |
| I.S. EN 4322:2005 | Identical |
| PN EN 4322 : 2005 | Identical |
| SN EN 4322 : 2003 | Identical |
| UNI EN 4322 : 2005 | Identical |
| UNE-EN 4322:2004 | Identical |
| BS EN 4322:2004 | Identical |
| NF EN 4322 : 2005 | Identical |
| DIN EN 4322:2006-03 | Identical |
| ISO 5855-2:1999 | Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts |
| EN 2491:2011 | Aerospace series - Molybdenum disulphide dry lubricants - Coating methods |
| ISO 4095:1998 | Aerospace — Bihexagonal drives — Wrenching configuration — Metric series |
| ISO 3353:1992 | Aerospace — Rolled threads for bolts — Lead and runout requirements |
| EN 2424:2008 | Aerospace series - Marking of aerospace products |
| EN 3813:2013 | Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bar and wire for forged fasteners - De ≤ 50 mm |
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