EN 3813:2013
Current
Current
The latest, up-to-date edition.
Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bar and wire for forged fasteners - De ≤ 50 mm
Published date
16-01-2013
Publisher
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Foreword
Introduction
1 Scope
2 Normative references
This standard specifies the requirements relating to:Titanium alloy Ti-6Al-4VAnnealedBar and wire for forged fastenersDe £ 50 mmfor aerospace applications.
| Committee |
ASD-STAN
|
| DevelopmentNote |
Supersedes PREN 3813. (01/2013)
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| NF EN 3813 : 2013 | Identical |
| NBN EN 3813 : 2013 | Identical |
| DIN EN 3813:2013-04 | Identical |
| BS EN 3813:2013 | Identical |
| I.S. EN 3813:2013 | Identical |
| PN EN 3813 : 2013 | Identical |
| NS EN 3813 : 2013 | Identical |
| NEN EN 3813 : 2013 | Identical |
| UNE-EN 3813:2013 | Identical |
| XP PREN 3907 : 1995 XP | AEROSPACE SERIES - BOLTS, DOUBLE HEXAGON HEAD, NORMAL SHANK, LONG THREAD, IN TITANIUM ALLOY TI-P63, MOS[2] COATED - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE)/350 DEGRES C |
| PREN 3725 : 200P1 | AEROSPACE SERIES - BOLTS, PAN HEAD, SIX LOBE RECESS, NORMAL SHANK, LONG THREAD, IN TITANIUM ALLOY TI-P63, MOS[2] COATED - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE) |
| BS EN 3725:2004 | Aerospace series. Screws, pan head, six lobe recess, normal shank, long thread, in titanium alloy TI-P64001, anodized, MoS<sub>2</sub> coated. Strength class: 1100 MPa (at ambient temperature) |
| I.S. EN 4322:2005 | AEROSPACE SERIES - BOLTS, DOUBLE HEXAGON HEAD WITH LOCKWIRE HOLES, RELIEVED SHANK, LONG THREAD, IN TITANIUM ALLOY TI-P64001, ANODIZED, MOS[2] COATED - STRENGTH CLASS: 1100 MPA (AT AMBIENT TEMPERATURE) |
| I.S. EN 4323:2005 | AEROSPACE SERIES - SCREWS, 100 DEGREE COUNTERSUNK HEAD, SIX LOBE RECESS, THREADED TO HEAD, IN TITANIUM ALLOY TI-P64001, ANODIZED, MOS[2] COATED - CLASSIFICATION: 900 MPA (AT AMBIENT TEMPERATURE)/350 DEGREE C |
| BS EN 4322:2004 | Aerospace series. Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in titanium alloy TI-P64001, anodized, MoS<sub>2</sub> coated. Strength class: 1100 MPa (at ambient temperature) |
| XP PREN 3725 : 1997 XP | AEROSPACE SERIES - BOLTS, PAN HEAD, SIX LOBE RECESS, NORMAL SHANK, LONG THREAD, IN TITANIUM ALLOY TI-P63, MOS2 COATED - STRENGTH CLASS: 1100 MPA (AT AMBIENT TEMPERATURE) |
| BS EN 3724:2004 | Bolts, double hexagon head, relieved shank, long thread, in titanium alloy TI-P64001, MoS<sub>2</sub> coated. Strength class: 1100 MPa (at ambient temperature) |
| BS EN 3907:2004 | Aerospace series. Bolts, double hexagon head, normal shank, long thread, in titanium alloy TI-P64001, MoS<sub>2</sub> coated. Classification: 1100MPa (at ambient temperature)/350°C |
| EN 4322:2004 | 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) |
| EN 4323:2004 | Aerospace series - Screws, 100° countersunk head, six lobe recess, threaded to head, in titanium alloy TI-P64001, anodized, MoS2 coated - Classification: 900 MPa (at ambient temperature) / 350 °C |
| 06/30145496 DC : 0 | EN 4636 - AEROSPACE SERIES - SCREWS, 100 DEGREE COUNTERSUNK HEAD, SIX LOBES RECESS, SHORT THREAD, IN TITANIUM ALLOY TI-P64001, MOS[2] COATED - CLASSIFICATION - 100 MPA (AT AMBIENT TEMPERATURE)/315 DEGREE C |
| BS EN 4323:2004 | Aerospace series. Screws, 100° countersunk head, six lobe recess, threaded to head, in titanium alloy TI-P64001, anodized, MoS<sub>2</sub> coated. Classification. 900 MPa (at ambient temperature) / 350°C |
| EN 2032-2:1994 | Aerospace series - Metallic materials - Part 2: Coding of metallurgical condition in delivery condition |
| EN 4500-004:2012 | Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 004: Specific rules for titanium and titanium alloys |
| EN 3114-002:2007 | Aerospace series - Test method - Microstructure of (α + β) titanium alloy wrought products - Part 002: Microstructure of bars, sections, forging stock and forgings |
| EN 4258:1998 | Aerospace series - Metallic materials - General organization of standardization - Links between types of EN standards and their use |
| EN 4800-002:2010 | Aerospace series - Titanium and titanium alloys - Technical specification - Part 002: Bar and section |
| EN 4800-004:2010 | Aerospace series - Titanium and titanium alloys - Technical specification - Part 004: Wire |
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