EN 4800-001:2010
Current
Current
The latest, up-to-date edition.
Aerospace series - Titanium and titanium alloys - Technical specification - Part 001: Plate, sheet and strip
Published date
03-11-2010
Publisher
Sorry this product is not available in your region.
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 plate, sheet and strip. 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
|
| DevelopmentNote |
Supersedes PREN 4800-001. (04/2011)
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| NEN EN 4800-001 : 2010 | Identical |
| SN EN 4800-001:2011 | Identical |
| UNI EN 4800-001 : 2011 | Identical |
| DIN EN 4800-001:2011-06 | Identical |
| NF EN 4800-001 : 2012 | Identical |
| NS EN 4800-001 : 2010 | Identical |
| I.S. EN 4800-001:2010 | Identical |
| NBN EN 4800-001 : 2010 | Identical |
| UNE-EN 4800-001:2010 | Identical |
| PN EN 4800-001 : 2011 | Identical |
| BS EN 4800-001:2010 | Identical |
| I.S. EN 3354:2013 | AEROSPACE SERIES - TITANIUM ALLOY TI-6AL-4V - ANNEALED - SHEET FOR SUPERPLASTIC FORMING - A <= 6 MM |
| BS EN 3464:2012 | Aerospace series. Titanium alloy (Ti-6Al-4V). Annealed. Plate. 6 mm < a ≤ 100 mm |
| I.S. EN 3464:2012 | AEROSPACE SERIES - TITANIUM ALLOY TI-6AL-4V - ANNEALED - PLATE - 6 MM < A <= 100 MM |
| UNI EN 3456 : 2013 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - SHEET AND STRIP, HOT ROLLED - A <= 6 MM |
| BS EN 3456:2012 | Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Sheet and strip, hot rolled. a ≤ 6 mm |
| 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 |
| 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 |
| UNI EN 3464 : 2013 | AEROSPACE SERIES - TITANIUM ALLOY TI-6AL-4V - ANNEALED - PLATE - 6 MM < A <= 100 MM |
| EN 3456:2012 | Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Sheet and strip, hot rolled — a ≤ 6 mm |
| EN 3464:2012 | Aerospace series - Titanium alloy Ti-6Al-4V - Annealed - Plate - 6 mm < a ≤ 100 mm |
| 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 3354:2013 | Aerospace series - Titanium alloy Ti-6Al-4V - Annealed - Sheet for superplastic forming - a ≤ 6 mm |
| UNI EN 3459 : 2011 | AEROSPACE SERIES - TITANIUM ALLOY TI-P63001 (TI-4AL-4MO-2SN) - SOLUTION TREATED AND AGED - PLATE - 6 MM < A <= 50 MM |
| BS EN 3354:2013 | Aerospace series. Titanium alloy Ti-6Al-4V. Annealed. Sheet for superplastic forming. a ≤ 6 mm |
| I.S. EN 3456:2012 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - SHEET AND STRIP, HOT ROLLED - A <= 6 MM |
| EN 9100:2009 | Quality Management Systems - Requirements for Aviation, Space and Defense Organizations |
| EN ISO 12737:2010 | Metallic materials - Determination of plane-strain fracture toughness (ISO 12737:2010) |
| 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 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 (ISO 4288:1996) |
| 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 3873:2010 | Aerospace series - Test methods for metallic materials - Determination of fatigue crack growth rates using Corner-Cracked (CC) test pieces |
| EN 3987:2009 | Aerospace series - Test methods for metallic materials - Constant amplitude force-controlled high cycle fatigue testing |
| ISO 12737:2010 | Metallic materials Determination of plane-strain fracture toughness |
| PREN 2002-06 : 200P2 | AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - PART 6: BEND TESTING |
| 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 |
| 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 3114-004:2006 | Aerospace series - Test method - Microstructure of (α + β) titanium alloy wrought products - Part 004: Microstructure of sheet for superplastic forming |
| 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 |
| EN 3114-003:2006 | Aerospace series - Test method - Microstructure of (α + β) titanium alloy wrought products - Part 003: Microstructure of plate |
| 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 |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.