EN 4800-002:2010
Current
Current
The latest, up-to-date edition.
Aerospace series - Titanium and titanium alloys - Technical specification - Part 002: Bar and section
Published date
03-11-2010
Publisher
Foreword
Introduction
1 Scope
2 Normative references
3 Terms and definitions
4 Wording of order
5 Health and safety
6 Technical requirements
This standard defines the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy bar and section. It shall be applied when referred to and in conjunction with the EN material standard unless otherwise specified on the drawing, order or inspection schedule.
| Committee |
ASD-STAN
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Current
|
| Standards | Relationship |
| NF EN 4800-002 : 2012 | Identical |
| NBN EN 4800-002 : 2010 | Identical |
| NEN EN 4800-002 : 2010 | Identical |
| NS EN 4800-002 : 2010 | Identical |
| I.S. EN 4800-002:2010 | Identical |
| PN EN 4800-002 : 2011 | Identical |
| SN EN 4800-002:2011 | Identical |
| UNI EN 4800-002 : 2011 | Identical |
| UNE-EN 4800-002:2010 | Identical |
| BS EN 4800-002:2010 | Identical |
| DIN EN 4800-002:2011-06 | Identical |
| BS EN 3813:2013 | Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Bar and wire for forged fasteners. D<sub>e</sub> ≤ 50 mm |
| UNI EN 4685 : 2011 | AEROSPACE SERIES - TITANIUM TI10V2FE3AL - BARS - D < 110 MM - R[M] >= 1240 MPA |
| NF EN 4685 : 2012 | AEROSPACE SERIES - TITANIUM TI10V2FE3AL - BARS - D < 110 MM - R[M] > OR = 1240 MPA |
| I.S. EN 3355:2012 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - EXTRUDED SECTION - D[E] <= 150 MM - 900 MPA <= R[M] <= 1160 MPA |
| UNI EN 3355 : 2013 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - EXTRUDED SECTION - D[E] <= 150 MM - 900 MPA <= R[M] <= 1160 MPA |
| 11/30254398 DC : 0 | BS EN 4685 - AEROSPACE SERIES - TITANIUM TI10V2FE3AL - BARS - D < 110 MM - R[M] >= 1240 MPA |
| UNI EN 4500-004 : 2014 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 004: SPECIFIC RULES FOR TITANIUM AND TITANIUM ALLOYS |
| UNI EN 3813 : 2013 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - BAR AND WIRE FOR FORGED FASTENERS - DE <= 50 MM |
| I.S. EN 4500-004:2012 | AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 004: SPECIFIC RULES FOR TITANIUM AND TITANIUM ALLOYS |
| BS EN 4500-004:2012 | Aerospace series. Metallic materials. Rules for drafting and presentation of material standards Specific rules for titanium and titanium alloys |
| BS EN 3355:2012 | Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Extruded section. De ≤ 150 mm. 900 MPa ≤ Rm ≤ 1 160 MPa |
| NF EN 4675 : 2012 | AEROSPACE SERIES - TITANIUM TI-P63002 (TI5AL5MO5V3CR0,4FE) - R[M] > OU = TO 1300 MPA - BARS - D[E] < 110 MM |
| EN 3355 : 2012 | Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Extruded section - De ≤ 150 mm - 900 MPa ≤ Rm ≤ 1 160 MPa |
| EN 4500-004:2012 | Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 004: Specific rules for titanium and titanium alloys |
| EN 3813:2013 | Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bar and wire for forged fasteners - De ≤ 50 mm |
| I.S. EN 3813:2013 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - BAR AND WIRE FOR FORGED FASTENERS - D[E] <= 50 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 |
| 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 ISO 6892-1:2016 | Metallic materials - Tensile testing - Part 1: Method of test at room temperature (ISO 6892-1:2016) |
| EN ISO 4288 : 1997 | GEOMETRICAL PRODUCT SPECIFICATIONS (GPS) - SURFACE TEXTURE: PROFILE METHOD - RULES AND PROCEDURES FOR THE ASSESSMENT OF SURFACE TEXTURE |
| 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 ISO 643:2012 | Steels - Micrographic determination of the apparent grain size (ISO 643:2012) |
| ISO 6892-1:2016 | Metallic materials Tensile testing Part 1: Method of test at room temperature |
| EN 3987:2009 | Aerospace series - Test methods for metallic materials - Constant amplitude force-controlled high cycle fatigue testing |
| 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 |
| ISO 643:2012 | Steels Micrographic determination of the apparent grain size |
| 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 2954-002:2010 | Aerospace series - Macrostructure of titanium and titanium alloy wrought products - Part 002: Macrostructure of bar, section, forging stock and forgings |
| 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 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 3238 : 2010 | AEROSPACE SERIES - METALLIC MATERIALS - TEST METHOD - SHEAR TEST FOR WIRES AND RIVETS |
| 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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