SAE AMS4897D : 2016
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
TITANIUM ALLOY, SHEET AND STRIP, 15MO - 3.0AL - 2.8CB - 0.20SI
Hardcopy , PDF
12-29-2020
English
09-13-2016
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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.
| Committee |
AMS G
|
| DocumentType |
Revision
|
| Pages |
8
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy |
| 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 AMS 2368 : 2017 | 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 AMS 2750 : 2012 | 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 AMS 2642 : 2016 | STRUCTURAL EXAMINATION OF TITANIUM ALLOYS ETCH-ANODIZE INSPECTION PROCEDURE |
| SAE AS 6279 : 2016 | STANDARD PRACTICE FOR PRODUCTION, DISTRIBUTION, AND PROCUREMENT OF METAL STOCK |
| SAE AMS 2249 : 2013 | CHEMICAL CHECK ANALYSIS LIMITS, TITANIUM AND TITANIUM ALLOYS |
| SAE AS 4194 : 2012 | 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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