PREN 3813 : 200P2
Withdrawn
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
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AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AI-4V) - ANNEALED - BAR AND WIRE FOR FORGED FASTENERS - D[E] <= 50 MM
Available format(s)
Hardcopy , PDF
Withdrawn date
15-12-2023
Superseded by
Language(s)
English
Important note : Users cannot be edited or removed once added to your Multi user PDF.
Introduction
1 Scope
2 Normative references
Describes the requirements relating to: Titanium alloy TI-P64001 (Ti-6AI-4V) - Annealed - Bar and wire for forged fasteners - D[e] <= 50 mm for aerospace applications.
| DevelopmentNote |
Supersedes PREN 3353, PREN 3457, PREN 3458. (10/2002)
|
| DocumentType |
Draft
|
| Pages |
6
|
| ProductNote |
Superseded by EN 3813:2013
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Withdrawn
|
| SupersededBy | |
| Supersedes |
| Standards | Relationship |
| NF EN 3813 : 2013 | Identical |
| 09/30209898 DC : DRAFT SEP 2009 | Identical |
| DIN EN 3813:2013-04 | 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) |
| NF EN 4035 : 2006 | AEROSPACE SERIES - ROD ENDS, ADJUSTABLE WITH SELF-ALIGNING DOUBLE ROW BALL BEARING IN CORROSION RESISTING STEEL, REDUCED INTERNAL RADIAL CLEARANCE AND THREADED SHANK IN TITANIUM ALLOY - DIMENSIONS AND LOADS |
| BS EN 4636:2009 | Aerospace series. Screws, 100° countersunk head, six lobe recess, short thread, in titanium alloy TI-P64001, with aluminium pigmented coating. Classification: 1100 MPa (at ambient temperature) / 315°C |
| I.S. EN 4035:2006 | AEROSPACE SERIES - ROD ENDS, ADJUSTABLE WITH SELF-ALIGNING DOUBLE ROW BALL BEARING IN CORROSION RESISTING STEEL, REDUCED INTERNAL RADIAL CLEARANCE AND THREADED SHANK IN TITANIUM ALLOY - DIMENSIONS AND LOADS |
| PREN 4322 : 200P1 | AEROSPACE SERIES - BOLTS, DOUBLE HEXAGON HEAD WITH LOCKWIRE HOLES, RELIEVED SHANK, LONG THREAD, IN TITANIUM ALLOY TI-P63, ANODIZED, MOS[2] 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) |
| EN 4035:2006 | Aerospace series - Rod ends, adjustable with self-aligning double row ball bearing in corrosion resisting steel, reduced internal radial clearance and threaded shank in titanium alloy - Dimensions and loads |
| 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 4636:2009 | AEROSPACE SERIES - SCREWS, 100 DEGREE COUNTERSUNK HEAD, SIX LOBE RECESS, SHORT THREAD, IN TITANIUM ALLOY TI-P64001, WITH ALUMINIUM PIGMENTED COATING - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE)/315 DEGREE C |
| ONORM EN 4035 : 2006 | AEROSPACE SERIES - ROD ENDS, ADJUSTABLE WITH SELF-ALIGNING DOUBLE ROW BALL BEARING IN CORROSION RESISTING STEEL, REDUCED INTERNAL RADIAL CLEARANCE AND THREADED SHANK IN TITANIUM ALLOY - DIMENSIONS AND LOADS |
| 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) |
| 17/30369678 DC : 0 | PREN 7010 - AEROSPACE SERIES - USER GUIDE FOR CREATION AND DESIGNATION OF BOLTS |
| BS EN 4035:2006 | Aerospace series. Rod ends, adjustable with self-aligning double row ball bearing in corrosion resisting steel, reduced internal radial clearance and threaded shank in titanium alloy. Dimensions and loads |
| BS EN 4424:2006 | Aerospace series. Rod-ends, adjustable single fork and threaded shank with engagement: 1,5 x thread diameter in titanium alloys. Dimensions and loads |
| 07/30165636 DC : 0 | BS EN 4636 - AEROSPACE SERIES - SCREWS, 100 DEGREES COUNTERSUNK HEAD, SIX LOBES RECESS, SHORT THREAD, IN TITANIUM ALLOY TI-P64001, WITH ALUMINIUM PIGMENTED COATING - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE)/315 DEGREES 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 4636:2009 | Aerospace series - Screws, 100° countersunk head, six lobe recess, short thread, in titanium alloy TI-P64001, with aluminium pigmented coating - Classification: 1 100 MPa (at ambient temperature) / 315 °C |
| EN 4424:2006 | Aerospace series - Rod-ends, adjustable, single fork and threaded shank with engagement: 1,5 × thread diameter in titanium alloys - Dimensions and loads |
| 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) |
| PREN 4636 : 200P1 | AEROSPACE SERIES - SCREWS, 100 DEGREE COUNTERSUNK HEAD, SIX LOBE RECESS, SHORT THREAD, IN TITANIUM ALLOY TI-P64001, WITH ALUMINIUM PIGMENTED COATING - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE)/315 DEGREE C |
| PREN 3907 : 200P1 | AEROSPACE SERIES - BOLTS, DOUBLE HEXAGON HEAD, NORMAL SHANK, LONG THREAD, IN TITANIUM ALLOY TI-P63, MOS[2] COATED - CLASSIFICATION: 1 100 MPA (AT AMBIENT TEMPERATURE)/350 DEGREES C |
| TR 4661 : 2009 | AEROSPACE SERIES - HINGES, FLIGHT CONTROLS MATERIALS AND SURFACE TREATMENTS |
| PREN 4800-004 : 200P2 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 4: WIRE |
| PREN 4500-004 : 200P2 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 004: SPECIFIC RULES FOR TITANIUM AND TITANIUM ALLOYS |
| EN 2032-2:1994 | Aerospace series - Metallic materials - Part 2: Coding of metallurgical condition in delivery condition |
| 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 |
| PREN 4050-4 : 200P1 | AEROSPACE SERIES - TEST METHOD FOR METALLIC MATERIALS - ULTRASONIC INSPECTION OF BARS, PLATES, FORGING STOCK AND FORGINGS - ACCEPTANCE CRITERIA |
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