SAE AMS4897D
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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Titanium Alloy, Sheet and Strip 15Mo - 3.0AI - 2.8Cb - 0.20Si
Hardcopy , PDF
29-12-2020
English
13-09-2016
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. ACKNOWLEDGEMENT
7. REJECTIONS
8. NOTES
Specifies a titanium alloy in the form of sheet and strip 0.125 inch (3.18 mm) and under in nominal thickness.
| DocumentType |
Standard
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| Pages |
8
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| PublisherName |
SAE International
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| Status |
Superseded
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| SupersededBy | |
| Supersedes |
This specification covers a titanium alloy in the form of sheet and strip 0.125 inch (3.18 mm) and under in nominal thickness.
| 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 |
| NFL 06 380-24 : 2008 | AEROSPACE SERIES - WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - WELDABILITY AND BRAZEABILITY OF MATERIALS - PART 24: HOMOGENEOUS ASSEMBLIES 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 |
| UNI EN 4632-006 : 2014 | AEROSPACE SERIES - WELDABILITY AND BRAZEABILITY OF MATERIALS IN AEROSPACE CONSTRUCTIONS - PART 006: HOMOGENEOUS ASSEMBLIES OF TITANIUM ALLOYS |
| ASTM E 2371 : 2013 | Standard Test Method for Analysis of Titanium and Titanium Alloys by Direct Current Plasma and Inductively Coupled Plasma Atomic Emission Spectrometry (Performance-Based Test Methodology) |
| SAE AMS2368D | Sampling and Testing of Wrought Titanium Raw Material Except Forgings and Forging Stock |
| ASTM A 480/A480M : 2017-11 | SPECIFICATION FOR GENERAL REQUIREMENTS FOR FLAT-ROLLED STAINLESS AND HEAT-RESISTING STEEL PLATE, SHEET, AND STRIP |
| SAE AMS 2809 : 2007(R2011) | IDENTIFICATION, TITANIUM AND TITANIUM ALLOY WROUGHT PRODUCTS |
| SAE AMS2750E | Pyrometry |
| ASTM E 1409 : 2013 : REDLINE | Standard Test Method for Determination of Oxygen and Nitrogen in Titanium and Titanium Alloys by Inert Gas Fusion |
| SAE ARP 1917 : 2002 | CLARIFICATION OF TERMS USED IN AEROSPACE METALS SPECIFICATIONS |
| SAE AMS2642E | Structural Examination of Titanium Alloys Etch-Anodize Inspection Procedure |
| SAE AS6279A | Standard Practice for Production, Distribution, and Procurement of Metal Stock |
| SAE AMS2249G | Chemical Check Analysis Limits Titanium and Titanium Alloys |
| SAE AS4194A | Sheet and Strip Surface Finish Nomenclature |
| SAE AMS 2242 : 2014 | TOLERANCES, CORROSION AND HEAT RESISTANT STEEL, IRON ALLOY, TITANIUM, AND TITANIUM ALLOY SHEET, STRIP, AND PLATE |
| ASTM E 290 : 2014 : REDLINE | Standard Test Methods for Bend Testing of Material for Ductility |
| ASTM E 8/E8M : 2016-09 | TEST METHODS FOR TENSION TESTING OF METALLIC MATERIALS |
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