EN 3818:2004
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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Aerospace series - Bolts, MJ threads, in titanium alloy TI-P64001 - Strength class: 1 100 MPa (at ambient temperature) - Technical specification
Published date
10-11-2004
Publisher
Superseded date
15-05-2019
Superseded by
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Foreword
1 Scope
2 Normative references
3 Terms and definitions
4 Quality assurance
4.1 Qualification
4.2 Acceptance
5 Requirements
This standard specifies the characteristics, qualification and acceptance requirements for bolts with MJ threads in TI-P64001.Strength class: 1 100 MPaIt is applicable whenever referenced.
| Committee |
ASD-STAN
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Superseded
|
| SupersededBy |
| Standards | Relationship |
| DIN EN 3818:2018-12 (Draft) | Identical |
| I.S. EN 3818:2019 | Identical |
| NF EN 3818 : 2005 | Identical |
| I.S. EN 3818:2005 | Identical |
| DIN EN 3818:2005-09 | Identical |
| BS EN 3818:2019 | Identical |
| NEN EN 3818 : 2006 | Identical |
| NS EN 3818 : 2ED 2005 | Identical |
| PN EN 3818 : 2006 | Identical |
| BS EN 3818:2004 | Identical |
| NBN EN 3818 : 2005 | Identical |
| NEN-EN 3818:2019 | Identical |
| DS EN 3818 : 2005 | Identical |
| UNE-EN 3818:2004 | Identical |
| PREN 3724 : 200P1 | AEROSPACE SERIES - BOLTS, DOUBLE HEXAGON HEAD, RELIEVED 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 3725:2005 | AEROSPACE SERIES - SCREWS, PAN HEAD, SIX LOBE RECESS, NORMAL SHANK, LONG THREAD, IN TITANIUM ALLOY TI-P64001, ANODIZED, MOS[2] 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 3907:2005 | AEROSPACE SERIES - BOLTS, DOUBLE HEXAGON HEAD, NORMAL SHANK, LONG THREAD, IN TITANIUM ALLOY TI-P64001, MOS[2] COATED - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE)/350 DEGREE C |
| 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 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) |
| I.S. EN 3724:2005 | AEROSPACE SERIES - BOLTS, DOUBLE HEXAGON HEAD, RELIEVED SHANK, LONG THREAD, IN TITANIUM ALLOY TI-P64001, MOS[2] 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 3725:2004 | Aerospace series - Screws, pan head, six lobe recess, normal shank, long thread, in titanium alloy TI-P64001, anodized, MoS2 coated - Strength class: 1 100 MPa (at ambient temperature) |
| EN 3907:2004 | Aerospace series - Bolts, double hexagon head, normal shank, long thread, in titanium alloy TI-P64001, MoS2 coated - Classification: 1 100 MPa (at ambient temperature) / 350 °C |
| 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 |
| EN 3724:2004 | Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in titanium alloy TI-P64001, MoS2 coated - Strength Class: 1 100 MPa (at ambient temperature) |
| 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 |
| ISO 5855-2:1999 | Aerospace — MJ threads — Part 2: Limit dimensions for bolts and nuts |
| ISO 6892:1998 | Metallic materials — Tensile testing at ambient temperature |
| ISO 3452:1984 | Non-destructive testing — Penetrant inspection — General principles |
| ISO 7961:1994 | Aerospace — Bolts — Test methods |
| PREN 9133 : 200P1 | AEROSPACE SERIES - QUALITY MANAGEMENT SYSTEMS - QUALIFICATION PROCEDURE FOR AEROSPACE STANDARD PRODUCTS |
Summarise
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