PREN 4800-002 : 200P2
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
Hardcopy , PDF
21-12-2023
English
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Superseded by EN 4800-002:2010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 |
Withdrawn
|
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 |
UNI EN 4675 : 2012 | AEROSPACE SERIES - TITANIUM TI-P63002 (TI5AL5MO5V3CR0.4FE) - R[M] >= 1300 MPA - BARS - D[E] < 110 MM |
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 - 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 2955:1993/AC:1995 | AEROSPACE SERIES - RECYCLING OF TITANIUM AND TITANIUM ALLOY SCRAP |
EN 3683 : 2007 | AEROSPACE SERIES - TEST METHODS - TITANIUM ALLOY WROUGHT PRODUCTS - DETERMINATION OF PRIMARY ALPHA CONTENT - POINT COUNT METHOD AND LINE INTERCEPT METHOD |
SAE AMS 2750 : 2012 | 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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