PREN 3859 : 200P1
Current
The latest, up-to-date edition.
AEROSPACE SERIES - TITANIUM ALLOY TI-P19001 - ANNEALED - SHEET AND STRIP, HOT ROLLED - A <= 6 MM
Hardcopy , PDF
English
24-06-1993
0 Introduction
1 Scope and field of application
2 References
Specifies the requirements relating to sheet and strip, hot rolled, a <= 6 mm, annealed, in titanium alloy TI-P19001 for aerospace applications.
| Committee |
C5
|
| DevelopmentNote |
Supersedes PREN 2528, PREN 3500. (10/2002)
|
| DocumentType |
Draft
|
| Pages |
5
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| DIN EN 3859:1992-12 (Draft) | Identical |
| 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 |
| 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 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 |
| PREN 4632-006 : DRAFT 2008 | WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - WELDABILITY AND BRAZEABILITY OF MATERIALS - PART 006: HOMOGENEOUS ASSEMBLIES TITANIUM ALLOYS |
| PREN 2500/4 : 200P3 | AEROSPACE SERIES - INSTRUCTIONS FOR THE DRAFTING AND USE OF METALLIC MATERIAL STANDARDS - PART 4: SPECIFIC REQUIREMENTS FOR TITANIUM AND TITANIUM ALLOYS |
| PREN 2600 : 200P1 | AEROSPACE SERIES - DESIGNATION OF METALLIC SEMI-FINISHED PRODUCTS - RULES |
| PREN 3544-2 : 200P1 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 2: PLATE, SHEET AND STRIP |
| PREN 3544-1 : 200P1 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 1: GENERAL REQUIREMENTS |
| EN 2338:2001 | Aerospace series - Sheets, hot rolled in titanium and titanium alloys - Thickness 0,8 mm < = a < = 6 mm - Dimensions |
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