PREN 3464 : 200P3
Withdrawn
View Superseded by
AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - PLATE - 6 MM < A <= 100 MM
Hardcopy , PDF
English
12-13-2023
0 Introduction
1 Scope
2 Normative references
Describes the requirements relating to: Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Plate - 6 mm < a <= 100 mm, for aerospace applications.
| DevelopmentNote |
Supersedes PREN 2517. (10/2002)
|
| DocumentType |
Draft
|
| Pages |
5
|
| ProductNote |
Superseded by EN 3464:2012
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Withdrawn
|
| SupersededBy | |
| Supersedes |
| Standards | Relationship |
| 09/30210353 DC : 0 | Identical |
| DIN EN 3464:2012-11 | Identical |
| I.S. EN 4632-006:2013 | AEROSPACE SERIES - WELDABILITY AND BRAZEABILITY OF MATERIALS IN AEROSPACE CONSTRUCTIONS - PART 006: HOMOGENEOUS ASSEMBLIES OF TITANIUM ALLOYS |
| BS EN 2243-1:2005 | Aerospace series. Non-metallic materials. Structural adhesives. Test method Single lap shear |
| I.S. EN 2243-4:2005 | AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVES - TEST METHOD - PART 4: METAL-HONEYCOMB CORE FLATWISE TENSILE TEST |
| PREN 2243-4 : 200P1 | AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVES - TEST METHOD - PART 4: METAL-HONEYCOMB CORE FLATWISE TENSILE TEST |
| 09/30199811 DC : 0 | BS EN 4632-006 - AEROSPACE SERIES - WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - WELDABILITY AND BRAZEABILITY OF MATERIALS - PART 6: HOMOGENEOUS ASSEMBLIES TITANIUM ALLOYS |
| BS EN 2243-4:2005 | Aerospace series. Non-metallic materials. Structural adhesives. Test method Metal-honeycomb core flatwise tensile test |
| BS EN 4632-006:2013 | Aerospace series. Weldability and brazeability of materials in aerospace constructions Homogeneous assemblies of titanium alloys |
| EN 4632-006:2013 | Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 006: Homogeneous assemblies of titanium alloys |
| EN 2243-4:2005 | Aerospace series - Non-metallic materials - Structural adhesives - Test method - Part 4: Metal-honeycomb core flatwise tensile test |
| EN 2243-1:2005 | Aerospace series - Non-metallic materials - Structural adhesives - Test method - Part 1: Single lap shear |
| PREN 4632-006 : DRAFT 2008 | WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - WELDABILITY AND BRAZEABILITY OF MATERIALS - PART 006: HOMOGENEOUS ASSEMBLIES TITANIUM ALLOYS |
| 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 |
| PREN 2002-08 : 200P2 | AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - PART 8: MICROGRAPHIC DETERMINATION OF GRAIN SIZE |
| PREN 4800-001 : 200P2 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 1: PLATE, SHEET AND STRIP |
| EN 4258:1998 | Aerospace series - Metallic materials - General organization of standardization - Links between types of EN standards and their use |
| EN 3114-003:2006 | Aerospace series - Test method - Microstructure of (α + β) titanium alloy wrought products - Part 003: Microstructure of plate |
| 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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