PREN 4800-002 : 200P2
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 2: BAR AND SECTION
Available format(s)
Hardcopy , PDF
Language(s)
English
Superseded date
14-06-2024
Superseded by
€190.93
Excluding VAT
Foreword
Introduction
1 Scope
2 Normative references
3 Terms and definitions
4 Wording of order
5 Health and safety
6 Technical requirements
Describes the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy bar and section.
| DevelopmentNote |
Supersedes PREN 3544-1 and PREN 3544-3. (01/2003)
|
| DocumentType |
Draft
|
| Pages |
25
|
| ProductNote |
Superseded by EN 4800-002:2010
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| Standards | Relationship |
| DIN EN 4800-002:2011-06 | Identical |
| BS EN 3311:2009 | Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Bar for machining. D < 110 mm |
| I.S. EN 4685:2011 | AEROSPACE SERIES - TITANIUM TI10V2FE3AL - BARS - D < 110 MM - R[M] >= 1240 MPA |
| 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 |
| PREN 4685 : 200P1 | AEROSPACE SERIES - TITANIUM TI10V2FE3AL - BARS - D < 110 MM - R[M] >= 1240 MPA |
| BS EN 4675:2011 | Aerospace series. Titanium Ti-P63002 (Ti5Al5Mo5V3Cr0.4Fe). Rm ≥ 1 300 MPa. Bars. De < 110 mm |
| I.S. EN 3311:2009 | AEROSPACE SERIES - TITANIUM ALLOY TIP64001 (TI-6AL-4V) - ANNEALED - BAR FOR MACHINING - D < 110 MM |
| I.S. EN 4675:2011 | AEROSPACE SERIES - TITANIUM TI-P63002 (TI5AL5MO5V3CR0.4FE) - R[M] >= 1300 MPA - BARS - D[E] < 110 MM |
| PREN 3355 : 200P3 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AI-4V) - ANNEALED - EXTRUDED SECTION - D[E] <= 150 MM - 900 MPA <= R[M] <= 1160 MM MPA |
| 09/30201382 DC : 0 | BS EN 4685 - AEROSPACE SERIES - TITANIUM TI10V2FE3AL - BARS - D < 110 MM - R[M] >= 1240 MPA |
| BS EN 4685:2011 | Aerospace series. Titanium Ti10V2Fe3Al. Bars. D < 110 mm. Rm ≥ 1240 MPa |
| EN 3311:2009 | Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bar for machining - D < 110 mm |
| EN 4685:2011 | Aerospace series - Titanium Ti10V2Fe3Al - Bars - D < 110 mm - Rm ≥ 1 240 MPa |
| PREN 4675 : 200P1 | AEROSPACE SERIES - TITANIUM TI-P63002 (TI5AL5MO5V3CR0,4FE) - R[M] >= 1300 MPA - BARS - D[E] <= 100 MM |
| EN 9100:2009 | Quality Management Systems - Requirements for Aviation, Space and Defense Organizations |
| PREN 2002-16 : 200P1 | AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - PART 16: NON-DESTRUCTIVE TESTING - PENETRANT TESTING |
| EN 2003-009:2007 | Aerospace series - Test methods - Titanium and titanium alloys - Part 009: Determination of surface contamination |
| PREN 4050-1 : 200P1 | AEROSPACE SERIES - TEST METHOD FOR METALLIC MATERIALS - ULTRASONIC INSPECTION BARS, PLATES, FORGING STOCK AND FORGINGS - GENERAL INFORMATION |
| TR 2410 : 2 | AEROSPACE SERIES - METALLIC MATERIALS - RELATIONSHIP BETWEEN DIMENSIONAL STANDARDS AND MATERIAL STANDARDS |
| 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 3683:2007 | Aerospace series - Test methods - Titanium alloy wrought products - Determination of primary α content - Point count method and line intercept method |
| SAE AMS2750E | Pyrometry |
| EN 3684:2007 | Aerospace series - Test methods - Titanium alloy wrought products - Determination of β transus temperature - Metallographic method |
| PREN 3874 : 200P1 | AEROSPACE SERIES - TEST METHODS FOR METALLIC MATERIALS - CONSTANT AMPLITUDE FORCE-CONTROLLED LOW CYCLE FATIGUE TESTING |
| EN 2032-1:2001 | Aerospace series - Metallic materials - Part 1: Conventional designation |
| PREN 3987 : 200P1 | AEROSPACE SERIES - TEST METHODS FOR METALLIC MATERIALS - CONSTANT AMPLITUDE FORCE-CONTROLLED HIGH CYCLE FATIGUE TESTING |
| PREN 2954-002 : 200P1 | AEROSPACE SERIES - MACROSTRUCTURE OF TITANIUM AND TITANIUM ALLOY WROUGHT PRODUCTS - PART 002: MACROSTRUCTURE OF BAR, SECTION, FORGING STOCK AND FORGINGS |
| PREN 4259 : 200P1 | AEROSPACE SERIES - METALLIC MATERIALS - DEFINITION OF GENERAL TERMS |
| EN 2002-002:2005 | Aerospace series - Metallic materials - Test methods - Part 2: Tensile testing at elevated temperature |
| EN 3976:2006 | Aerospace series - Titanium and titanium alloys - Test method - Chemical analysis for the determination of hydrogen content |
| EN 2002-005:2007 | Aerospace series - Test methods for metallic materials - Part 005: Uninterrupted creep and stress-rupture testing |
| EN 4258:1998 | Aerospace series - Metallic materials - General organization of standardization - Links between types of EN standards and their use |
| EN 2002-001:2005 | Aerospace series - Metallic materials - Test methods - Part 1: Tensile testing at ambient temperature |
| PREN 3238 : 200P1 | AEROSPACE SERIES - METALLIC MATERIALS - TEST METHOD - SHEAR TEST FOR WIRES AND RIVETS |
| PREN 3988 : 200P1 | AEROSPACE SERIES - TEST METHODS FOR METALLIC MATERIALS - CONSTANT AMPLITUDE STRAIN-CONTROLLED LOW CYCLE FATIGUE TESTING |
| EN 3114-001:2006 | Aerospace series - Test method - Microstructure of (α + β) titanium alloy wrought products - Part 001: General requirements |
| PREN 4050-4 : 200P1 | AEROSPACE SERIES - TEST METHOD FOR METALLIC MATERIALS - ULTRASONIC INSPECTION OF BARS, PLATES, FORGING STOCK AND FORGINGS - ACCEPTANCE CRITERIA |
| EN 2078:2001 | Aerospace series - Metallic materials - Manufacturing schedule, inspection schedule, inspection and test report - Definition, general principles, preparation and approval |
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